142
'POSTED :3 ~p87 ~ (USAF) T.O.2R-R2000-24 Ie i l TECHNICAL MANUAL ILLUSTRATED PARTS BREAKDOWN AIRCRAFT ENGINES USAF MODELS R-2000-4 R2000-7M2 (PRATT & WHITNEY AIRCRAFT) (DIVISION OF UNITED AIRCRAFT CORPORATION) NOw 66-0294-k F41608-81-D-A062 .~- .... -* ~- "DISTRIBUTION STATEMENT -Tf-jIS PUBLICATION IS REQUI RED FOR OFFICIAL USE OR FOR ADMINISTRATIVE OR OPERATIONAL PURPOSES O'NL.:Y. DISTRIBUTION IS LIMITED TO U.S. GOVERNMENT AGENCIES. OTHER REQUESTS FOR THIS DOCUMENT MUST BE REFERRED TO SAN ANTONIO ALCjMMEDT. KELLY AFB, TEXAS 78241." PUBLISHED UNDEB AUTHOBITY OF THE SECRETABY OF THE AlB FORCE 15 APRIL 1980 CHANGE 1- 15 DECEMBER 1981

AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

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Page 1: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

'POSTED:3 ~p87

~

(USAF) T.O.2R-R2000-24

Ie

i

l

TECHNICAL MANUAL

ILLUSTRATED PARTS BREAKDOWN

AIRCRAFT ENGINES

USAF MODELSR-2000-4R2000-7M2

(PRATT & WHITNEY AIRCRAFT)

(DIVISION OF UNITED AIRCRAFT CORPORATION)

NOw 66-0294-k

F41608-81-D-A062

.~-....-* ~-"DISTRIBUTION STATEMENT -Tf-jIS PUBLICATION IS REQUI RED FOR OFFICIAL USE OR FOR ADMINISTRATIVEOR OPERATIONAL PURPOSES O'NL.:Y. DISTRIBUTION IS LIMITED TO U.S. GOVERNMENT AGENCIES. OTHERREQUESTS FOR THIS DOCUMENT MUST BE REFERRED TO SAN ANTONIO ALCjMMEDT. KELLY AFB, TEXAS

78241."

PUBLISHED UNDEB AUTHOBITY OF THE SECRETABY OF THE AlB FORCE

15 APRIL 1980CHANGE 1 - 15 DECEMBER 1981

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T.O.2R-R2000-24INSERT lATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

LIST OFHFECTIVE PAliESNOTE: The portion of the text affected by the changes is indicated by a

vertical line in the outer margins of the page. Changes to illustr?-tions are indicated by miniature pointing hands. Changes to wir-ing diagrams are indicated by shaded areas.

Dates of issue for originai and changed pages are:

Or~iilal.... .0 .. 15 Apr 80

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 140 CONSISTING OF THE FOllOWING:

PageNo.

TitleAi.ii Blank.1-1 -1-51-6 Blank.2-1 - 2-96.3-1 - 3-33.3-34 Blank.

'ChangeNo.

.0

.0

.0

.0.0

. .. 0.0

... 0.0

PageNo.

• ChangeNo.

PageNo.

'ChangeNo. •

A

* Zero in thi, column indicatc, an ori~nal pagc.

USAF

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(USAF) T.O. 2R-R2000-24

TECHNICAL MANUAL

ILLUSTRATED PARTS BREAKDOWN

AIRCRAFT ENGINES

USAF MODELS

R-2000-4R2000-7M2

(PRATT & WHITNEY AIRCRAFT)

(DIVISION OF UNITED AIRCRAFT CORPORATION)

NOw 66-0294-k

F41608-78-D-A005

THIS PUBLICATION REPLACES T.O. 2R-R2000-24 DATED 15 DECEMBER 1964.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE

" .....•... 4~'~ ....•.~ ~:.~;

,,

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T;O. 2R-R2000-24INSERT LATEST CHANGED PAGES, DESTf.WV SUPERSEDED PAGES.

LIST OF EFFECTIVE PAGESNOTE: The portion of the text affected by the changes is indicated by a

vertical line inthe outer margins of the page. Changes to illustr~.tions are indicated by miniature pointing hands. Changes to wir.ing diagrams are indicated by shaded areas.

Oates of issue for original and changed pages are:

Original. .. .0 .. 15 Apr 80 _. .Change 1 15 Dec81 •

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 140 CONSISTING OF THE FOLLOWING:

PageNo.

.ChangeNo.

PageNo.

• ChangeNo.

PageNo.

.ChangeNo.

A

Title 1A .. - .. . •. 1i. . . . . . .. .. . .... 0ii Blank. . . . .. .. ...01.1 .1-5 .. ..01-6 Blank 02.1 - 2.10. .02.11. . . . .12.12 . 2.78. .. . .. 02.79. . . .12-80 . 2-85. . . . . . 02.86. . . . .. 12-87 .2.96. . .. 03.1 .. 13.2 . 3-4 . . . . . . 03.5 13-6 - 3.33. . . . . . . 03-34 Blank. .. 0

l

r

* I.no in this column indicates an original page.

Change 1 USAF

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T.b. 2R-R2000-24

TABLE OF CONTENTS

Creeper Desludging Clutches. 2-71

Reduction Gear Housing-(Continued). 2-12

Crankshaft and Connecting Rods. 2-25

Section

I

II

INTRODUCTION.

GROUP ASSEMBLY PARTS LIST••

Reduction Gear Housing and MagnetoDrive.

Front Oil Pump and Pipes.

Propeller Shaft and ReductionGearing

Reduction Gearing CouplingBearing Support

Main Crankcase. '

Main Crankcase-(Continued).

Cylinders, Pistons, and Piston-rings

Cylinder Pushrods, Intake Pipes,and Rockerbox Covers.

Deflectors.

Deflectors (-7M2 Engines)

Main Oil Sump

Collector Case.

Intermediate Rear Case.

PageNumber

1-1

2-1

2-32-5

2-7

2-14

2-17

2-22

2-31

2-37

2-40

2-49

2-54

2-56

2-59

Section

Fuel Feed Valve, Clutch SelectorValve, and Accelerating Pump.

Impeller Shaft, Accessory DriveShaft, and Starter Jaw.

Impeller Intermediate Drive GearAssembly (-7M2 Only)

Rear Case.

Hydraulic Pump Drive

Side Accessory Drives.

Tachometer, Fuel, and Oil Pump'Drives

Generator Drive.

Lower Vacuum Pump Drive.

Rear Oil Pump.

Main Oil Screen, Rear Breather, andOil Pressure Relief Valve.

Ignition System.

Magneto Vent System

Magneto to Distributor BlockAttaching Parts.

Carburetor Attaching Parts-(For -4,and -7M2 Engines Only)

PageNumber

2-65

2-73

2-75

2-79

2-80

2-82

2-84

2-86

2-87

2-90

2-92

2-93

2-94

2-96

Intermediate Rear Case-(Corttinued). 2-62

III NUMERICAL INDEX. 3-1

i/ii

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l__.<

..~ I

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T.O. 2R-R2000-24

SECTION 1

INTRODUCTION

1. PURPOSE. This manual lists and describes the partsfor the Model R2000-4 Engines manufactured by Prattand Whitney Aircraft, Division of United Aircraft Cor-poration, East Hartford, Connecticut 06108 USA and USGovernment configured R2000-7M2 engines. Unless speci-fied otherwise parts applicable to the R2000-7M2 en-gines are the same as those specified in this publi-cation for R2000-4 engines.

2. TABLE OF CONTENTS. The Table of Contents at thefront of the manual outlines the three sections andshows the method of grouping the parts and the seq-uence of the groups.

J. GROUP ASSEMBLY PARTS LIST. The Group AssemblyParts List (Section II) consists of the complete eng-ine divided into J6 main groups as shown in the Tableof Contents. Each assembly listed has its componentparts indented, thereunder, to show their relation-ship to the assembly. Component parts of the completeengine, which are not included any assembly, butwhich are used in conjunction with, attach, or attachto a certain assembly, are listed either precedingthe first detail or following the last detail of thatassembly, and in line with the major assembly.

4. UNITS PER ASSEMBLY. The quantites listed in the"Units per Assy." column of the Group Assembly PartsList are, in the case of assemblies, the total quan-tity used per engine at the location indicated, whilethe component parts indented under the asssembliesare the quantity used per assembly. For total quan-tities used per engine, Air Force personnel shall re-fer to the Numerical Index (Section III) for the to-tal quantities used per engine.

5. INDEX NUMBERS. The index numbers appearing on theillustrations are numerically arranged by figure num-bers in the Group Assembly Parts List and are usedmainly to assist in locating a part in the GroupAssembly Parts List after it has been found on anillustration. The illustrations in this catalog areintended only to facilitate the identification ofparts. These illustrations shall not be used as aparts assembly guide. A break in the continuity ofthe numerical sequence of the index numbers indicatesthat the item deleted has either been relocated, oris no longer applicable to the engine covered by thiscatalog.

6. NUMERICAL INDEX. The Numerical Index (SectionIII) is compiled in accordance with the numericalpart number filing system described below:

a. The filing principle of the system is basicallythe same as the surname arrangement found in the citytelephone directories and dictionaries, except thatnumbers and dashes are added.

b. Part number numerical arrangement starts on theleft-hand column and continues from left to right,one column at a time, until part number numerical ar-rangement is determined.

c. The order of precedence in part number numericalarranging is as follows:

(1) Space (blank column).

(2) Dash (-).

(J) Letters A through Z.

(4) Numerals 0 through 9.

EXAMPLES

A-22707 10-27625-4

ANlOOOJ9 104228

ASlOOOOl 11477

C4PlO11-Jl 27549

MS122l22 JJJ74

NAS565-2l 77909

P8J20 80Jd. A part number appearing in this section in paren-thesis indicates that the part has been (1) supersed-ed, (2) replaced, (J) is a part listed under the op-tional procurement number, or (4) the Pratt & Whitneyequivalent part number for a vendor item.

7. NONPROCURABLE PARTS. In the Numerical Index (Sec-tion III) nonprocurable parts (part numbers precededby an *) are given the figure and index number of thepreceding illustrated part in the Group AssemblyParts List (Section II) in order to facilitate thelocation of the nonprocurable part in the text of theGroup Assembly Parts List. Assemblies that are notassigned an index number although all their detailparts have been indexed, are given the figure number(s) in which the assembly is illustrated, for refer-ence purposes in the Numerical Index (Section III).

1-1

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T.O.2R-R2000-24

8. SUPERSEDES AND REPLACES. "Supersedes" indicatesthat the old and the new parts are interchangeable."Replaces" indicates that the old and the new partsare not interchangeable; however, in some instancesreplaced parts can be reworked to the new part con-figuration. The disposition of parts subject to theterms "Supersedes" and "Replaces'! as identified inthis catalog shall be governed by applicable specificGovernment Instructions, such as Time ComplianceTechnical Orders and Engine Overhaul TechnicalManuals.

9. VENDOR PART NUMBERS. Various items of equipmentsuch as carburetors, sparkplugs, magnetos, etc., arelisted under the vendor's part number with the Pratt& Whitney Aircraft part number following the descrip-tion in the Group Assembly Parts List (Section II).

10. REPLACEMENT STUDS. Where "oversize studs (e.g., o.004 in. oversize) are listed in the Group AssemblyParts List (Section II), they are used as the firstreplacement of the standard size studs originally in-stalleu in the engine.

11. DIRECTIONAL REFERENCES. Right and left, clockwiseand counterclockwise, top and bottom, and similar di-rectional references apply to the engine as viewedfrom the rear" (anti-propeller end) with the engine ina horizontal position.

12. CYLINDER NUMBERS. Viewing the engine from therear, cylinders are numbered consecutively in a clock-wise direction around the engine starting with thenumber one cylinder, which is the top cylinder of therear row, and continuing with number two cylinder,which is located in the front row immediately to theright of the vertical center line. By this designa-tion, all odd numbered cylinders are located in therear row and all even numbered cylinders are locatedin the front row.

13. REFERENCE liANDBOOKS. Organizational maintenanceinstructions are covered by the applicable aircrafttechnical manual. Overhaul instructions are coveredby T.O. 2R-R2000-23.14. ABBREVIATIONS.

DEG

DIAFT.

ID

IN.

LB.

LHM

N

NC

NEF

NFNO.NP

NPT

NS

OD

OZ,

P

PD

PRo

PW

R

Degree

DiameterFeet

Inside Diameter

Inch( es)

Pound

Left Hand

Undersize for standard part

National Form (thread)

National Coarse (thread)"

National Extra Fine (thread)

National Fine (thread)

Number( s)

Indicates parts or assemblies thatare not procurable

National Taper Pipe Thread

National Special Thread

Outside Diameter

Ounce(s)

Oversize for standard part

Pitch Diameter

Pair

Pratt & Whitney Aircraft Divisionof United Aircraft Corporation, EastHartford, Connecticut 06108, U.S.A.

Combination oversize and undersizepart'

Abbreviation

ANPT

AR

CL

CRES

CSK

Full Name

Aeronautical National Pipe Thread

Indicates units for oversizes and/or undersizes "as required"

Class

Corrosion Resistant Steel

Countersunk

RH

SP

THD

UACL

UNC

UNF

UPA

Right Hand

Special

Thread

United Aircraft of Canada Limited,P.O. Box 10, Longueuil, Quebec,Canada

Unified National Coarse (thread)

Unified National Fine (thread)

Units per Assembly

1-2

15. SYMBOLS. The symbols used throughout this manualand their explanations are as follows:

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T.O; 2R-R2000-24

*-Indicates parts or assemblies that are not pro-curable.

t-Indicates a classified part or a part availablein oversize and/or undersize.

U -Part numbers or figure and index numbers preced-ed by this symbol ( ) in the Numerical Index (SectionIII) are parts not illustrated. To facilitate loca-tion in the Group Assembly Parts List (Section II)such parts are provided with the same figure and in-dex number as a related illustrated part.

16. CROSS REFERENCES. Cross references to manufact-urer's code symbols. Federal supply code for manu-facturers cataloging handbook H-4-1.

17. LIST OF MAJOR SUB-CONTRACTOR VENDOR EQUIPMENT:

06848

77820

78570

Energy Controls DivisionBendix Corporation717 North Bendix DriveSouth Bend, Indiana 46620

Scintilla DivisionBendix CorporationSidney, New York 13838

Titeflex, IncorporatedHendee StreetSpringfield, Massachusetts 01100

Vendors Part No Nomenclature Publication No••

10-27625-4 or Magneto 8E2:-5-5-44

10-81725-1 Magneto 8E2-5-5-44

various Spark Plugs 8E2-6-1-37

30n8 Ignition ,Harness Assembly 8E2-4-3-94

442390 Ignition Harness Assembly SE2-4-J-94

390926 Carburetor 6RI- 3-Y.4

8627 Container - Engine 35E20-3-19-4

18. SPARE PARTS SOURCES. Sole sourc~ spare parts aremanufactured by United Aircraft of Canada Limited,P.O. Box 10, Longueuil. Quebec, Canada. Sources ofall other spare parts are controlled by Dir Mat Mgt.Service Engineering (MMPRR) Kelly Air Force Base,Texas.

19. LOCKWIRE. Lockwire Military Standard MS20995C32,NSN .9505-00-293-4208 or MS20995CC41, NSN 9505-00-603-4120, shall be used at those locations whereMS20995 is.specified except Figure and Index 9-62where MS20995N51, NSN 9525c-00-6L8~5462 shall beused.

1-3

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T.O. 2R.R2000.24

HOWTO USE THE ILLUSTRATED PARTS BREAKDOWN

T, O. 2R-R2000-24

Hydraulic Pump Drive •

DesludgingClutchea-(For-9AEngines Only) •

ImpellerShaft, AcceuoryDriveShalt, <LndSlarterJaw .

SldeAccenoryDrlves.

Creeper DedudglngClulch.es ..

Po ••NumlM:!r

RPdllcl\on~aringCollpling"BearlngSllpport.

RedllClionGe:arHollsing-(Con-Unued) •

FcontOllPumpandPipell

PTopelierShaftanl!Re;iuclionGearing.

TABU Of COIInJII'S

I INTRODUCTION.

Main Crankcase,

MalnCrlLllkcue-(Conlln"",d) • Lower Vacuum Pump Drive,

Cranli:sll2Jland ConneclingRods , R••••rOl! Pl.tmp •

Cylindeu, Pistons, andPlslon-ring ••.•

MalnOUScrf!'l:'n, Rear Breath.er,and Oil Pressllre Relief Valve.

Cylinder P\L8hroda, lntakePipes,and RockerboxC""ers 19nit.lon:lJldM"gn~loVentS).",lem .

neJlectors .'

RoekcrSump - (For -9" EnginesOnly) .•

MalJ'lOIlSump.

Interlll~laleRearCaJle ..

Intermediate Rear C~8e - (Con-

Ignition SYlItl"m •

MagnetoVl"nl SYlll~m. (USAFEnginn).

Cylinder PrlmingSYlIll"m-(ForAir Forcl"EnglneeOnly).

Carb1J.rl"torAllachlngParlll.(For-4, .4)" -6. and -6A EngIne... Only).

CarburelorAttachingParts-(For-9AEngin"lIOnly).

WHEN THE PART NUMBER IS NOT KNOWN

(1) Determine the function and application of the partrequired. Turn to the Table of Contents and selectthe most appropriate title. Note the illustration pagenumber.

(2) Turn to the page indicated and locate the desiredpart on the illustration.

(3) From the illustration, obtain the index number as-signed to the part desired. Refer to the accompanyingdescription for specific information regarding the part.

Page 11: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

HOWTO USE THE ILLUSTRATED PARTS BREAKDOWN

....,,

I~H0I)P20

••mJO~18'IOPW

"-m~J

BlIoaIN9}212

.19""'9

19(,1o\1p.19f"\lrB-~mlll~

IIb2j

.~ l~J79':J

I11J116

!Y<!~3~

I~5H

7)IJ7

92ll'n

"."

b-17b-I~

6-3~

6-37

~.- -,-=-=r=~-.,., ---

I ~fJ)Ur. ~ ~.q!w:: ~rAII",tll: ~~A~rfr. -UrM"'l'

., II '1~11;~"'3 I ::::~'~~;~J~;r~~':F~~~;~:~~l:::"I 1l>1'f)1'~ I 1"'~"I"lO; ".~ •• ~'-l)') ',',1-, ,,-v.' In. ~v•.••"~_,,

I2~1':I')rl~ ••••~"\,,' •• ",.. '" 2( I)} ~"!1 .1.>1<:In, •••••r'l ••

•~~]'ZII'JU Ii INc."i C-l' ",,',,", ,., 2(.')) 'nil .','j(; In. "'.r,,',e. - ., ..•../f "' n _ : 'r.,\".'~ . 12': ., In' • J' ~ I". I >'''' I f •••••nt u 11

VU"'" IN.r",ot>t. eH" ' .•••":"", , ....'3(.o~~ 1"'~'.]"f,;,.;~.~;;"r~~:~:,~,~r',:~~~t'."O.'~.~5~c.'-'nJIJ'.0<>lll'o """.le .•• "0'" •• JLOii~ .•oly .~0', I"" ".or,'... .

, ••••cr.!'". ~"~I.,~ ' .•••.r~ u~ r_o,•• II.o ,;•••. Ir,,. -9> "'.I"Jh,,){,I'~ ~"""l"r •••••.," 4.U~f ~,.ls ,:'OJ In. ~v.r:,".

'1~4(fJ1.'IL ~~~":~,~:?';",~',~~~td~~.l: :~~ :~: ;.~~O)~:"'~t r.I~',.•.1"o'Lon ~ou 1,~••,l"l!J, ..:~~~:::~;~~~:~:~ :~:~::;~:~:

rln •••••••• l~ or.l~ .0)0 '". o.or"" . . . . .6U,"LfIl! .Ihl~ Ill, .?IO."u •. j'. •. In. lo.>n~!_r,noto

dr'" L~lor•••dl.,U r,•• r,. ,!OJ..nln, ••••••• 41A7ltO~l:l .'.It' ,~, '''~r"I... . . .rlr _ <tr",nt ,I"J 010 • J.':>/, :~. In"" h ••."",tc d., ••

Lnter_dLAto ,u. ~~.nl,,,,,I. , , .."r . StUI"", ,I{~ dLa • ,~:)O I~, I<>~ (dr'Lho ,.,10 I~

S""f,,~:n~~~~r:";:~~~~~~r~,;lr::..:~.~~I~I..I\olt -1~{;~':':~l:~Ot~.~t~o~{'~ ,~, ~~t~ '~'r<>~,~Il •.~~

••••r .500 "UII\C~ nun •. )12,-2" \1' •. 21~ I~,

U,I~" (fro"t oLl """" I~hr""dl.h c.".n' ..••r bdt'.COUorpln _ Corr""on r.Ol.Unt .Cbf,.,:no O,~ •. 7~(. In,

lo"f: (r""nt ,,11 pu~ Inhp_d,u ••••• r\l"eor '~I' •.••'Our _ rro~t •••• re""cUnn ~ppor • lower . . . . , ,

;::: ~~~I~~~a~7~~~ ~~~.;£~.~~I:'I~:~r.f~~~Lfl:~:r_~rlll'O Itnrudad '0<>\0 In roo. r~.oM .~<> •• ' •• , ,""., ,-.,.-9> only) .. , .•. , ..

PLIIC ••••••• \91',_9 only ,0(>1< \~, o"or, I ••n~ ••• _ a" 191'..••9 only .uoa In. " •• r"I~.

~~;e~ ~~:-:;'.;r<:;,:~~.,..r.~~":'~~f,~or.. , .Woo""r _ Cha.c •••• d . )')1 III •. B'I~ Oil •. O\l'< I, .. t'.'ok

(front CO"reO~ttLon •.••rl, . . . . . . , ,

1M r~;~~r.;.~~:~~.~:~~t;~.;.~1~~~r::~.:~~~.~.;..~"or Ih:.~N 15004l~1 . . . . , , , . . . . , ' ,

rOU.rpln _ Cor""oLnnr." "ont .0lil',•.•••')~ ~10 •. 1i2~I rOo

~I~A-1~2i1(;~:~r.~:o:e~~~g~~~~e=~~~~;).57~' Ir.: ';'n,'(""wort plot_ tvp OIl ~,'•• ~vro ta~), . . . .

C""Pll'l,._e:~r~t~ :t:6:'~~I;J~ed~tt~<>n.,.~ ~.I~. :ro~

"o~Pll~;~~~)~t1~n ~oo~O~'¥~ (:rr._~: _~~',_~: •. ,

RI¥.1~••~~,.~~:~p;.p~{~7'r~~,,!.~~gi~lJ,:.~:'i"~~IY)lloa,"L1r~d~~m)~~I:~5~~~c~~p~~~~~~~n~~;~:1~,:6,nn - Strotgnl .1661~ ~Io •. ~50 In. I~'l!l ('"*"""t~~n

!~ ••••~~r~7:J~;1~6ri~~~:~..;~~~~~::~~~:::.t'Ire1t~.\lon Orl'1n ."vpll •••.o~"""rt b_rl'~~ .

LOc_p.n- .11) ~lo • ,1i2~In. lo,,!! Ir.""Hton d.lventP~~II•••.o""""rl h","LtIt opo""""""'l.

WHEN THE PART NUMBER IS KNOWN

(1) When the part number is known, refer to SectionITINumerical Index. Locate the part number and notethe figure and index number assigned to the part num-ber.

(2) Turn to the Figure Number indicated and locate theIndex Number Referenced in the Numerical Index.

(3) If a pictorial representation of the part, or its loca-tion is desired, refer to the same index number on theaccompanying illustration.

1-5/(1.6 blank)

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. (

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SECTION II

GROUP ASSEMBLY PARTS LISTI

T.O.2R-R2000-24

INDEX NO. DESCRIPTION

1 NOSE SECTION ....................•....•

2 POWER SECTION •....•.•...•.•......•..•

3 COLLECTOR SECTION .........•......•....

4 INTERMEDLATE REAR SECTION .•...........•

5 REAR SECTION ..•..•...•....•......••.••

FIGURE 1 - VIEW OF COMPLETE ENGINE

FIGURE NO.

2 THRU 5

6 THRU 14

15

16 THRU 21

22 THRU 35

2-1

Page 14: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

REDUCTION GEAR HOUSING AND MAGNETO DRIVE

2-2

2-1

2

2-2

2-3

2-4

2-5

2-6

2-7

2

2-8

2-9

2-10

2-11

2-12

2-13

2

2-14

109286

446868

114181

AN122583

MS21044N5

149533

249280

AN123859

*109285

34770P6234770P534770P10t31157P4

31157P831157P12t20543P4

20543P820543P1231153

20731

t46575

46575P546575P10t9252P4

9252P89252P12t120:;4P4

12054P812054P12

Case & Stud Assy-Reduction gear (for use with engines havingnon-flooded systems and using PIN's 150246, 156075, or 16448crankcase assemblies, for -4 and -7M2) .Case assembly-reduction gear (replaces PIN 109286 which canbe rewprked to 446868 for engines having flooded rockerboxsystem and using PIN 460992 crankcase assembly) .Case & Prop Shaft Assy Complete -4 and -7M2 Engines (In ser-vice fix for engines with half engine life or less. Furnished onreq uest . . . . . . . . ; . . . . . . . . . . . . . . . . . . . . . . . .

ATTACHING PARTS

Washer - Plain .328 ID x .625 OD x .0625 in. thick (reductiongear case to main crankcase; supersedes No. 172 and 12734;use (20) units for -4 and -7M2) .Locknut - Nonmetalic lock .500 Hexagon head x .3125-24thd x .344 in. thick (Reduction gear case to main crankcase;supersedes 33415; use (20) units for -4 and -7M2) .Washer - Plain .3625 ID x .625 OD x .062 in. thick (reduction

gear case to main crankcase bolt) .Bolt - Drilled hexagon head .3125-18 thd x 4.540'in. long (re-

duction gear case to main crankcase at oil pump; useNo. MS20995 wire; replaces No. 143991; replaces No.31542) .

Seal- "0" Ring oil resistant .203-.213 ID x .344 OD x .067-.073 in. thick (reduction gear case to main crankcaseat oil pump bolt; for use with Part No. 249280 bolt) .

- - - - * - - --Case Machining Assembly - Reduction gear. (for use with

Part No. 109286; for -4 and -7M2) .Liner same as 34770 only .062 in. oversize .Liner same as 34770 only .005 in. oversize .Liner same as 34770 only .010 in. oversize .Stud - Drilled .375-16-24 thd x 1.656 in. long (reduc-

tion fixed gear support; for -4 and -7M2 .004 in.oversize)(usewith support PIN 70464) .

Stud same as 31157 only .008 in. oversize .Studsameas311570nly.012 in. oversize .Stud - Drilled .375-16-24 thej x 1.750 in long (fixed

gear; .004 in. oversize) (use with support PIN36061) .

Stud same as 20543 only .008 in. oversize .Stud same as 20543 only .012 in. oversize .Stud - Knurled .375-24 NF thd x 3.656 in. long (prop-

eller thrust bearing cover; for -4 and -7M2)(usewith support PIN 70464) .

Stud - Knurled .375-24 NF thd x 3.750 in. long (prop-eller thrust bearing cover; use with anchor PIN36061) .

Bushing - Flanged .865 ID x 1.065 OD x 1.657 in. long(governor driven gear) .

Bushing same as 46575 only .005 in. oversize .Bushing same as 46575 only .010 in. oversize .Stud - Plain .3125-18-24 thd x 2.094 in. long (cylinder

sump suction & vent pipe; for use with engineshaving Part No. 150246, 156075, or 164448 crank-case assembly) .004 in. 'oversize .

Stud same as 9252 only .008 in. oversize .Stud same as 9252 only .012 in. oversize .Stud - Plain .3125-18-24 thd x 1.250 in. long (cover,

front oil pump inlet pad; for engines having PartNo. 460992 crankcase assembly) .004 in. oversize .

Stud same as 12054 only .008 in. oversize .Stud same as 12054 only .012 in. oversize .

AR

20

20

2

2

2

NPARARAR

8ARAR

8ARAR

10

10

1ARAR

2ARAR

ARARAR

..

.'

Page 15: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

[40

41

33

I

I1-14

I

I14-1

Ar:." 0-3523~do;--24 ~ "'--34

",/ ~~32, " : 26 30 ~

37--, J -a..d>-~ ~-- 3136 ~-- 25 . "" 0-27 7

~ I r.L1 '"'" ('/'- 28 113-+1 i

21 @___"",-@«.,19 I' ~_::J /'~------ "~ \, .--O~.~- 2 2 ----"I.~'

8 ~ 'V\ ..• \ 11

"',I\~2_~ )@-@) .~~\

. ~~/""~

I I3938

6

~.--I_~-0-7

15~17_~ ~

-.ib .,~~- 1618 ~ .,

Figure 2. Reduction Gear Housing and Magneto Drive

REDUCTION GEAR HOUSING AND MAGNETO DRIVE

2-15 156011

2-16 156010

2-17 215

2-18 1344482-19 t84692P4

84692P884692P12

2-20 t 110011P4

110011P8e 2-21 AN932D2

2-22 t44588P4

44588P844588P12

2-23 t34119P4

34119P8

Disk - Name plate mounting (for use with Part No.156010 spacer; supersedes No. 139275; super-sedes No. 84477). . . . . . . . . . . . . . . . . . . . . . . . . .. 1

Spacer - Name plate mounting disk (for use with PartNo. 156011 disk) .

Screw - Countersunk 8-32 x .3125 in. long (name platemounting disk; supersedes No. 84478). . . . . . . . . . . .. . 4

Plate - Company name (supersedes No. 84560) . . . . . . . . . . . . 1Stud - Plain .3125-18-24 thd x 2.281 in. long (prop-

eller governor pad) .004 in. oversize. . . . . . . . . . . . . . . 3Stud same as 84692 only .008 in. oversize. . . . . . . . . . . . . . . ARStud same as 84692 only .012 in. oversize. . . . . . . . . . . . . . . ARStud - Plain .3125-18-24 thd x 2.156 in. long (prop-

eller governor pad right rear; for -4 and -7M 1). . . . . . . . . 1Stud same as 110011 only .008 in. oversize. . . . . . . . . . . . . . ARPlug - Hexagon socket .125 in. ANPT (governor oil feed

hole) .Stud - Plain .375-16-24 thd x 2.094 in. long (left & right

hand magneto pads) .004 in. oversize . . . . . . . . . . . . . . 8Stud same as 44588 only .008 in. oversize. . . . . . . . . . . . . . . ARStud ~ame as 44588 only .012 in. oversize. . . . . . . . . . . . . . . ARBushing - Screw .190-32 x .312-24 x .375 in. long

(magneto driven gear adjusting plate holdingscrew; supersedes No. 36627) .004 in. oversize. . . . . . . . 6

Bushing same as 34119 only .008 in. oversize. . . . . . . . . . . . . AR

2-3

Page 16: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & -/'UNITSINDEX DESCRIPTION

" PER ASSYNUMBER PART NUMBER 1 2 345 6 7

REDUCTION GEAR HOUSING AND MAGNETO DRIVE

2.24

2

2-2522-26

2-27

2-28

2-29

2-30

2

2-312-322-33

2-34

2-35

2-362-37

2-38

,2-39

2-402-412-42

2-43

2-44

3-1

3-2

2-4

28151

t145899

145899PI046050*46040tAN122696

MS9164-009MS9164-02917187

337475

332544

288936

126419

362525460936115

AN960-416

AN121552

774607359

MS35769-26

32971

7046436061AN121554

10109

MS24665-300

152819

109273

Pin - Straight .072 dia x .250 in. long (magneto drivengear adjusting plate holding screw bushing) .

Spacer - Plain 9.090 10 x 9.500 00 x .056 in. thick (prop-eller shaft thrust bearing liner; for service procurement) .

Spacer same as 145899 only .010 in. oversize .Gear & Pin Assembly - Propeller governor driven .

Gear - Propeller governor driven .Pin - Straight, headless .125 in. dia x .875 in. long (prop-

eller governor driven gear; supersedes Part No.37) .

Pin same as AN122696 only .002 in. oversize .Pin same as AN122696 only .005 in. oversize .

Snapring - 1,00000 x .092 in. thick (propeller governordriven gear) .

Seal - Oil .375 lOx. 754 OD x .250 in. thick (propellershaft oil pressure pipe: supersedes No. 53032,supersedes No. 70230) .

Seal - Oil propeller shaft oil transfer tube (Use with Part No.410874) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Bearing Option - Magneto driven gear (procurement numberconsists of:Part No. 122 Bearing - Ball 1.1807-1.1811 10 x 2.4404-2.440900 x .3887-.3937 in. long (optional to PartNo. 288904 or 359233)Part No. 288904 Bearing. Ball 1.1811 ID x 2.4409 00x .3937 in. Wide (optional to Part No. 122 or 359233)Part No. 359233 Bearing - Ball 1.1811 10 x 2.440900x .3937 in. Wide (optional to Part No. 122 or 288904) .....

Liner - Front case magneto driven gear bearing (for serviceprocurement) .

Gear - Magneto driven , , .Support - Magneto driven gear bearing .Screw. Flat fillister head, drilled shank .250-28 NF thd x

1.547 in. long (magneto driven gear bearing support) .Washer-Plain .266 10 X .500 00 x .062 in. thick (Magneto

driven gear bearing support: Supersedes 171) .Nut-Castle .250-28 thd x .282 in. thick (magneto driven

gear bearing support: supersedes No. 502; use No.MS20995 wire) .

Insert-Magneto driven gear adjusting (supersedes No. 45476) .Screw-Flat head .190-32 thd x .500 in. long (magneto

driven gear adjusting plate; supersedes No. 45477) .Gasket-1.1325 ID x .125 Wall x .094 in. thick (timing hole

plug) (supersedes No. AN900-18) .Plug-1.000 Hexagon head x 1.125-12 NF-3thd x .938 in.

long (timing hole; use No. MS20995 wire) .Support-Reduction fixed gear (for .4 and -7M2) .Anchor-Fixed gear (for AF converted -4 and -7M2) ,Nut-Castle .375-24 thd x .406 in. thick (reduction fixed

gear support: supersedes No. 521; use No. MS20995wire on (16) units) .

Nut-casted .375-24 thd x .456 in. thick MFG code 66640.(Use 18 units with support 70464 and long stud20543 and 20731 combination) .

Cotterpin-corrosion resistant .086 - .096 dia. x .750 in. long(reduction drive fixed gear support nut; supersedesAS123791) .

FRONT OIL PUMP AND PIPES

Pump Assembly-Front oil (supersedes No. 109273; for-4and -7M2) .

Pump Assembly Complete-Front oil (replaces No. 81885) .

6

1AR1NP

1ARAR1

1

1

4

122

8

8

82

6

111

18

AR

2

Page 17: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000.24

9 20

8 18 "II I~:g:::(j

jd-;2I

27

Figure 3. Front Oil Pump and Pipes

FRONT OIL PUMP AND PIPES

ATTACHING PARTS

3-3 109281 Screw-Oval fillister head drilled .250-20 NC thd x 3.000 in.long (front oil pump: use No. MS20995 wire; replacesNo. 16330) .

- - - - * - - --2

3-4 152818

3-5 109287

3 *1092703-6 t45078

45078P1045078P20

3-7 t45173

45173P545173P10

3-8 152816

3-9 152822

3-10 152821

3-11 109271

3-12 152824

Body Assembly - Front oil pump rear (for use with PartNo. 152819 pump assembly; spline type) .

Body Assembly - Front oil pump rear (for use with PartNo. 109273 pump assembly: key type; replacesNo. 45094 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

Body - Front oil pump rear (replaces No. 46557). .. . . . . . . NPSleeve - 1.2495 10 x 1.38600 x .375 in. long (front

oil pump body) '. . . . . . . . . . . . . . . 1Sleeve same as 45078 only .010 in. oversize. . . . . . . . . . . . ARSleeve same as 45078 only .020 in. oversize. . . . . . . . . . . . ARPin - Straight .095 dia x 1/4 in. long (front oil pump

body sleeve). . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Pin same as 45173 only .005 in. oversize. . . . . . . . . . . . . . ARPin same as 45173 only .010in. oversize. . • . . . . . . . . . . . ARShaft - Oil pump idler gear (for use with Part No.

152818 body assembly) .Pin - Straight .12625 dia x .720 in. long (oil pump

idler gear shaft; for use with Part No. 152818body assembly). . . . . . . . . . . . . . . . . . . . . . . . . . . 1

Body - Front oil pump front (for use with Part No.152819 pump assembly) .

Body - Front oil pump front (for use with Part No.109273 pump assembly; replaces No. 25850) .

Plate - Front oil pump center section (for use with PartNo. 152819 pump assembly). . . . . . . . . . . . . . . . . . . . 1

2.5

Page 18: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & -UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

FRONT 01L PUMP AND PI PES

2-6

3-13

3-14

3-15

3-16

3-17

3-183-19

3-20

3-21

3-22

3-23

3-24

3-25

3-26

3-27

3-28

3

3-29

3

3-30

3

3-313-323-333-34

3-35

3

109272

109298

109280

152848

109284

1092761124

AN122696

MS9164-009MS9164-029152820

154965

157741

49107

11624

AS123788

t224886

224886P2224886P5224886P10224886P20224886P20S224886P30224886P30S224886P40S224886P50S224886P60S152814

109274

152815

92661

152817

1122

109278109283109282AN122583

MS21044N5

446867

Plate - Front oil pump center section (for use with PartNo. 109273 pump assembly: replaces No. 25850) ..

Screw - Oval fillister head drilled .250-20 NC thd x2.500 in. long (front oil pump: use No. MS 20995wire) .

Screw - Oval fillister head drilled .250-20 NC thd x2.500 in. long (front oil pump: use No. MS20995wire)." .

Gear - Oil pressure pump idler (for use with Part No.152819 pump assembly) .

Gear & Shaft Assembly - Front oil pump idler (for usewith Part No. 102973 pump assembly) .

Shaft - Front oil pump idler .Gear - Drilled hole .561 dia x .5605 in. long (front oil

pump) .Pin - Straight, headless .125 dia x .875 in. long (front

oil pump idler gear; supersedes No. 37) .Pin same as AN122696 only .002 in. oversize .Pin same as AN 122696 only .005 in. oversize .

Shaftgear - Front oil pump drive (for use with Part No.152819 pump assembly) .

Shaftgear - Front oil pump drive (for use with PartNo. 109273 pump assembly) , .

Gear - Front oil pump drive driven (replaces No. 81441or 109275) .

Washer - .328 ID x .750 OD x .063 in. thick (front oilpump drive gear) " .

Nut - Shear .500 Hexagon head x .3125-24 thd x .218in. thick (front oil pump drive gear) .

Cotterpin - Corrosion resistant .086 - .090 dia x .500 in.long (front oil pump drive gear nut) .

Key - Flat .438 x .091 x .1275 in. (front oil pump gear:for use with Part No. 109273 pump assembly;supersedes No. 32507) .

Key - Flat same as 224886 only .002 in. oversize .Key - Flat same as 224886 only .005 in. oversize .Key - Flat same as 224886 only .0lD in. oversize .Key - Flat same as 224886 only .020 in. oversize .Key - Stepped same as 224886 only .020 in. oversize .Key - Flat same as 224886 only .030 in. oversize .Key - Stepped same as 224886 only .030 in. oversize .Key - Stepped same as 224886 only .040 in. oversize .Key - Stepped same as 224886 only .050 in. oversize .Key - Stepped same as 224886 only .060 in. oversize .Gear - Front oil pump drive (for use with Part No.

152819 pump assembly) - .Gear-Keyed .561 dia x 1.5570 in. long (front oil pump;

for use with Part No. 109273 pump assembly) .Gear-Oil pump idler (for use with Part No. 152819

pump assembly) .Gear-Drilled hole .561 dia x 1.5570 in. long (front oil

pump; for use with Part No. 109273 pump assembly) ....Gear-Front oil pump drive (for use with Part No. 152819

pump assembly; spline type) .Gear-Keyed .561 dia x .5605 in. long (front oil pump: for

use with Part No. 109273 pump assembly; key type) .Gasket-Cylinder sump suction .Tube & Flange Assembly Cylinder sump suction .Flange-Cylinder sump suction & vent tube long .Washer-Plain .328 ID x .562 OD x .062 in. thick (cylinder

sump suction & vent tube flange nut supersedesNo. 172) .

Locknut-Fibre .500 Hexagon head x .3125-24 thd x .344in. thick (cylinder sump suction & vent tube flange)(Supersedes No. 33415) .

Cover-Front oil inlet pad (for engines having part No. 460992crankcase assembly) .

2

2

11

1ARAR

1

3ARARARARARARARARARAR1

1

1211

2

2

Page 19: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000.24

18

Ii~-19

~----~25@-l

30~f/ 26L@"3124-~-C 21l--j

23I

i I,@-32 27 ~

~-33 2~~-29

~-34 a -22

35-@

I

---~

17-~

~-1615-~

/

5-~

-8

14_!13-12-011-0

Figure 4. Propeller Shaft and Reduction Gearing

..m

Page 20: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &INDEX DESCRIPTION UNITS

NUMBER PART NUMBER 1 2 3 4 5 6 7PER ASSY

PROPELLER SHAFT AND REDUCTION GEARING

II

260899

4-2

4-34-44-5

4-6

4-7

4-8

4-9

,4-104-11

4-12

4-13

4-14

4-15

4-16

4-17

4-18

44

4-19

4-20

4.21

4-2'2

2-8

*260877

4229

AN5012.50MS27423-442117

36103

29615

302561

97946

2961424306

24305

11618

AN115805

50195

36106P5134869

42051

214091

*90962*213527

t75024

, 75024P275024P575024P10t2036320363P220363R1

tl75993

175993Pl

I75993P5

175993P6.5

178027

Shaft Assembly-Propeller (supersedes No. 172254; for -4and -7M2) .

Shaft-Propeller (supersedes No. 92527 or 135011; for -4and -7M2) .

Pin-Straight .1285 dia x .281 in. long (front oil transferpipe support to propeller shaft; for -4 and -7M2) .

Protector-Propeller shaft thread (for -4 and -7M2) .Protector-Propeller Shaft splines .Plug-Propeller shaft front oil feed pipe rear (for -4 and

-7M2) .Screw-7/16-14 NC thd xl 3/16 in. long (propeller shaft

front oil feed pipe rear plug; for -4 and -7M2) .Gasket -2.56210 x 2.79 00 x .063 in. thick (front propel-

ler shaft oil feed pipe plug) .Pipe Assembly-Front propeller shaft oil feed (supersedes

No.36113) .Gasket - 1.500 lOx 2.800 00 x .031 in. thick (propeller

shaft plug nut cover to propeller shaft oil trans-fer support) .

Cover-Propeller shaft tube .Nut-2.875 Hexagon head x 2 7/8-16 N thd x 3/4 in. thick

(front propeller shaft plug) .Lockwasher-2 1/810 x 3 1/3200 x 1/32 in. thick (pro-

peller shaft pi ug) .Washer-Plain .203 10 x .375 OD x .0315 in. thick (front pro-

peller shaft plug lockwasher screw) .Screw-Flat fillister, drilled head .190 (No. 10)-32NF-3A

thd x .250 in. long (front propeller shaft plug lock-washer: supersedes No. 24304; use No. AS100029wire) '.'

Seal - Oil .625 10 x 1.12500 x .375 in. thick (crankshaftto propeller shaft oil transfer pipe) .

Plug same as 36106 only .005 in. oversize .Support - Crankshaft to propeller shaft oil transfer pipe (for

-4 and -7M2) .Snapring - 2.688 00 x .062 in. thick (crankshaft to pro-

peller shaft oil transfer pipe support retaining) .Gears Assembly - Reduction drive 2:1 (replaces Nos. 90963

or 214092 which can be reworked to No. 202215 inaccordance with T.O. 2R-R2000-23 and then used asa suitable substitute for No. 214091) .

Gear - Red uction .Pinton - Reduction drive (supersedes No. 52144, 59812

or 213528) .Bearing - Flanged 1.259610 x 1.4702 OD x 1.818 in.

long (reduction drive pinion; supersedes No.54430 for -4 and -7M2) .

Bearing same as 75024 only .002 in. overSize .Bearing same as 75024 only .005 in. oversize .Bearing same as 75024 only .010 in. oversize .Liner - Propeller shaft bearing .Liner same as 20363 only .002 in. oversize .Liner same as 20363 only .002 in. oversize on 00 &

minus .020 in. depth to 10 flange inner side .Shaft - Reduction gear pinion (for use with Part No.

204506 bearing assembly plain) .Shaft same as 175993 only .001 in. oversize on small

inner end only .Shaft same as 175993 only .005 in. oversize on small

inner end only .Shaft same as 175993 only .0065 in. oversize on small

inner end only .Plug - Reduction gear pinion transfer shaft oil (for use with

Part No. 204506 bearing assembly plain) .

1

NP

211

1

2

1

1

11

1

3

3

1AR1

1

1NPNP

6ARARAR2ARAR6

ARARAR6

Page 21: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE &INDEX DESCRIPTION UNITS

NUMBER PART NUMBER 1 2 3 4 5 6 7 PER ASSY

PROPELLER SHAFT AND REDUCTION GEARING

4-23

4-24

4-25

4-26

4-27

4-28

4-29

4-30

44-31

4-32

4-33

4-34

4-35

t125072

125072P1

120572P5

120572P7

20362

125392

125392M5W125392M7W125392M9W125392MllW125392M13W125392M15W125392M17W125392M19W125392M21W125392M23W125392P15Wt31707

31707M13W31707M15W31707M17W31707M19W31707M21 W31707M23W31707 P15W

t204506204506P15W

204506P30W

144722

t160637

160637P15Wl,60637P30W158403

*135705125391

157247

t41624

41624P30W25858

22157

Shaft - Reduction pinion (for usewith Part No. 157247ball bearing: supersedesNo ..52791) .

Shaft sameas 125072 only .001 in. oversize on flangethickness .

Shaft same as 125072 only .005 in. oversize on flangethickness " .

Shaft sameas 125072 only .007 in. oversize on flangethickness .

Pin - Straight .3105 dia x 2.031 in. long (reduction drivepinion shaft locking) .. . .

Washer - Reduction drive pinion bearing (for usewith PartNo. 204506 bearing assembly plain type) .

Washer sameas 125392 only .005 in. undersize on width .Washer sameas 125392 only .007 in. undersize on width .Washer sameas 125392 only .009 in. undersize on width .Washer sameas 125392 only .011 in. undersize on width .Washer sameas 125392 only .013 in. undersize on width .Washer sameas 125392 only .015in. undersize on width .Washer sameas 125392 only .017 in. undersize on width .Washer sameas 125392 only .019 in. undersize on width .Washer sameas 125392 only .021 in. undersize on width .Washersameas 125392 only .023 in. undersize on width .Washer sameas 125392 only .015 in. oversize on width .Washer - 1.474 10 x 2.25000 x .063 in. thick (reduction

drive pinion bearing inner: for usewith Part No.157247 ball bearing) ',' .

Washer sameas 31707 only .013 in. undersize on width .Washer sameas 31707 only .015 in. undersize on width .Washer sameas 31707 only .017 in. undersize on width .Washer sameas 31707 only .019 in. undersize on width .Washer sameas 31707 only .021 in. undersize on width ,.Washer sameas 31707 only .023 in. undersize 0t;! width .Washer sameas 31707 only .015 in .oversize on width .

Bearing Assembly - Plain type, reduction drive pinion thrust .....Bearing Assembly sameas 204506 only .015in. oversize on

width .Bearing Assembly sameas 204506 only .030 in. oversize on

width " .Bearing - Reduction drive pinion thrust (for usewith Part

No. 204506 bearing assembly). . . . . . .. . .Seat - Reduction drive pinion thrust bearing (for usewith

Part No. 204506 bearing assembly) .Seat sameas 160637 only .015 in. oversize on width .Seat sameas 160637 only .030 in. oversize on width .

Spacer Assembly - Reduction.drive pinion thrust (for usePart No. 204506 bearing assembly) .

Spacer- Reduction drive pinion thrust bearing.. . .Pin - Stepped .19125 dia x .3751n. long (reduction drive

pinion thrust spacer) . . . .. . .Bearing - Ball 1.2987-1.299210 x .2.4405.2.440900 x .5906

in. long (reduction drive pinion thrust: supersedesNo. 31706) .. . . . . . . . . . . . . . .. . . . . . . . . .. . ...

Washer- 1.26510 x 1.75000 x .032 in. thick Special (re-duction drive pinion bearing outer: for 'usewith PartNo. 157247 ball bearing; for Air Force engines only) .

Washer sameas41624 only .030 in. oversize .on width .RetalnerAssembly - 'Reduction drive pinion shaft (for use

with Part No. 157247 ball bearing) ...•.............Snapring- LOOO 00 x:062 in. thick (reduction drive

pinion retainer retaining) ............•..........

6

ARARAR

6

6ARARARARA'RARARARARARAR

6ARARARARARARAR6

AR

AR1

1ARA'R

6NP4

6

-6AR6

6

2-9

Page 22: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000.24

FIGURE & UNITS.INDEX DESCRIPTION

NUMBER PART NUMBER 1 2 345 6 7PER ASSY

PROPELLER SHAFT AND REDUCTION GEARING

-~1

4-37 94034

4-38 94033

4-39 361304-40 117130

4-41 117131

4-42 361324 *447314.43 337475

4-44 366404-45 332541

4-46 332547

4-47 332546

4-48 332548

4-49 1635404-50 341944-51 288952

4.36

4-52

4-53

4-54

4-55

44-564-57

4-58

2-10

352143

36445

26689

AN122584

D52EE064TF

*364442719127144

tl6268

Bearing Option - Ball front & rear reduction gears (procure-ment number consists of:Part No. 352144 Bearing - Ball 3.9750 10 x 5.708700 x .7087 in. Wide (optional to Part No. 204529 or452243)Part No. 204529 Bearing - Ball 3.9570 ID x 5.7087 00x .7087 in. Wide (supersedes No. 20218; optional toPart No. 352144 or 452243)Part No. 452243 Bearing - Ball, annular 3.9570 ID x5.708700 x .7087 in. Wide (optional to Part No.204529 or 352144) .

Spannernut - 3.9375-12 thd x .420 in. thick (rear propellershaftbearing;for-4and-7M2) .

Screw - Knurled No. 10-32 thd x .620 in. long (rear propel-ler shaft bearing nut; for -4 and -7M2) .

Spacer - Propeller thrust bearing .Spacer - Front propeller shaft rear bearing (for use with

converted R-2000-4 & -7M2) .Spacer - Chamfered 3.15210 x 3.75000 x .286 in. thick

(rear propeller shaft rear bearing; for use with con-verted R-2000-4 & -7M2) .

Bearing Assembly-Propeller shaft oil transfer .Bearing-Propeller shaft oil transfer .Seal-Oil .375 10 x .75400 x .250 in. thick (propeller

shaft oil pressure pipe; supersedes No. 53032 or70230) .

Retainer-Oil seal, propeller shaft oil pressure pipe .Bearing-Propeller Shaft oil transfer (Use with Part No.

410874) .Washer-Spring propeller shaft oil transfer bearing (Use with

Part No. 410874) .Seal-Propeller Shaft oil transfer tube (Use with Part No.

410874) ; .Nut-Propeller shaft oil transfer tube seal(Use MS20995 wire;

Use with with Part No. 410874) .Slinger-Propeller thrust bearing oil (supersedes No. 27190) - .Ring-Propeller thrust bearing spacer .Bearing Option-Propeller thrust (procurement number

consists of: Part No. 41017 Bearing-Ball 3.9360-3.937010 x 7.0856-7.086600 x 1.1230-1.1250in. long (optional to Part No. 288922 or 457059)Part No. 288922 Bearing-Ball 3.9370 10 x 7.086600 x 1.1250 in. Wide (optional to Part No. 41017or 457059) Part No. 457059 Bearing-Ball, annular3.937010 x 7.0866 OD x 1.1250 in. Wide (optionalto Part No. 41017 or 288922) .

Cover Assembly-Propeller thrust bearing .

ATTACHING PARTS

Spacer-Plain .391 10 x .688 00 x .375 in. thick (propellerthrust bearing cover) .

Washer-Plain .391 lOx .68800 x .062 in. thick (propellerthrust bearing cover; supersedes 173) .

Nut-non-metalic lock .562 Hexagon head x .375-24 thd x.453 in. thick (propeller thrust bearing cover; Mfgcode 72962; supersedes P & W 26432) .

- - - - * - - --Cover-Propeller thrust bearing .Liner-Propeller thrust bearing cover .Plug-Hexagon socket .0625 ANPT x .312 in. long Special

(propeller thrust bearing slushing oil) .Ring-Oil seal 5.12500 x .1235 in. thick (propeller thrust

bearing nut) - .

2

1

11

1

1

1NP

1

111

11

10

10

10

NP1

2

Page 23: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

PROPELLER SHAFT AND REDUCTION GEARING

UNITSPER ASSY

.,

4-59

16268P516268P5P10W

16268P5P20W

16268P1016268P10W16268P10P10W

16268P10P20W

16268P20W152224

Ring sameas 16268 only .005 in. oversize .Ring sameas 16268 only .005 in. oversize on 00 & .010

in. oversize on width .Ring sameas 16268 only .005 in. oversize on 00 & .020

in. oversize on width .Ring sameas 16268 only .010 in. oversize .Ring sameas 16268 only .010 in. oversize on width .Ring sameas 16268 only .010 in. oversize on 00 & .010

in. oversize on width .Ring sameas 16268 only .020 in. oversize on 00 & .020

in. oversize on width .Ring sameas 16268 only .020 in. oversize on width .Nut-3.9375-12 N thd X 1.098 in. long (propeller thrust

bearing) .

REDUCTION GEAR HOUSING

ARARARARARARARAR

5-15-2

5-3

5.4

5-5

5.65-7

5-8

5-9

5-10

5-11

5-12

5-13

5-14555-15

5-16

5.17

5-18e 5-19

5-20

59837332542

MS35769-18

77094

54140

54141MS9144.01

108733

AN122583

MS21044N5

MS21083N5

MS20913-6S

MS3397-13

998891235541210499876

D52EE064TF

6558

827

108203

25855

Pipe Assembly-Propeller shaft oil transfer bearing .Tube Assembly propeller shaft oil transfer (Use with Part

No. 410874) .Gasket..882510 x .125 Wall x .094 in. thick (propeller

shaft oil transfer pipe hole plug; supersedesNo.AN900-14) .

Plug - .875 Hexagon head x .875-14 NF-3 thd x .781 in. long(propeller shaft oil transfer hole: useNo. MS20995wire; supersedesNo. 17490) .

Gasket.J.12 ID x 3.64 00 x .021 in. thick (propeller gov.enor adapter) .

Adapter-Propeller governor .Gasket-Propeller governor pad (flight and shipping; super-

sedesNo. 97282,128290,201991 or 230625) .Cover-Propeller governor pad (for usewith Part No. 109342

plug in shipping; supersedesNo. 115590) .Washer-Plain .328 10 x .562 00 x .062 in. thick (governor

drive cover nut; supersedes172) .Locknut-non.metalic lock, .500 hexagon head x .3125-24

thd x .344 in. thick (governor drive cover; supersedes33415) .

Locknut-nsm-metalic lock .500 hexagon head x .3125-24 thdx .250 in. thick (governor drive cover; for usewithPN 110011 stud; supersedes49624) .

Plug-Governor pad cover supersedesNo. 109342 (Use No.MS20995 wire) .

Plug-Governor pad dehydrator (for useon -4 and -7M2engines; supersedesAN4061-3) .

Gasket-Magneto pad .Adapte(-Magneto .Ventilator-Magneto (use No. MS20995 wire; for Navy engines) .Washer-Chamfered .391 ID x .75000 x .094 in. thick

(magneto) .Nut-non-metalic lock, .562 Hexagon head x .375-24 thd x

.453 in. thick; mfg code 72962 (Magneto; supersedesP& W 26432) .

Gasket-.531 10 Pipe flanged x .031 in. thick (blower oilsuction tube to reduction housing) .

Gasket-.688 10 Pipe Flanged x .031 in. thick (blower oilsuction tube to blower) .

Tube Assembly-Reduction gear housing to blower oilreturn ( for -4 and -7M2) .

ATTACHING PARTS

Bolt-Drilled .500 Hexagon head x .3125-18 NC thd x 1.688in. long (blower oil suction tube to reduction housing;useNo. MS20995 wire) .

1

11

1

1

4

3

1248

8

8

1

1

2

Change 1 2-11

Page 24: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24.

38

I

38

~4'S-3

/-'34

"~2122

23-~"- ~-1826_ ••.~..•-25

I24

Figure 5. Reduction Gear Housing (Continued)

REDUCTION GEAR HOUSING

5-21

5-22

5-235-24

5-25

5-26

5-275-285-295-305-31

2-12

MS21044N5

25870

25869107718

MS21044N7

MS9122-04

850399773833976413624979747

Locknut-Non-metalic lock .500 Hexagon head x .3125-24thd x .344 in. thick (blower oil suction tube to blower;supersedes 33415) .

- - - - * - - --Grommet-.500 lOx. 75000 x .750 in. long (oil return tube

clip) .Clip-5/8 in. 00 (oil return tube) .Bracket Assembly-Reduction gear housing to blower oil

return tube (for .4 and -7M2) .

ATTACHING PARTS

Nut-non-metalic lock .750 Hexagon head x .4375-20 thdx .450 in. thick (reduction gear housing to bloweroil return tube bracket; supersedes 43781; for -4 and-7M2) .

Screw-.375 Slotted hexagon head x .190-32NF thd x .562in. long (supersedes 92938; reduction gear housingto blower oil return tube bracket to clip; for -4 and-7M2) .

_. - - * - - _.Chromseal Sheet-Engine data plate .Plate-Engine. data .Plate-Indent data (-7M2) .Spring-PIS oil trans pipe .Tabwasher-.203 lOx .57900 x .028 in. thick (engine data

plate bolt) .

2

1

1111

4

Page 25: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000.24

FIGURE & UNITSINDEX DESCRIPTION PER ASSYNUMBER PART NUMBER 1 2 3 4 5 6 7

REDUCTION GEAR HOUSING

5.32

5-33

5-345-35

5.36

5-375.38

6.1

6.2

6.3

106319

38606

126440107794

94931

9493085594

93714

135984

31537

Bolt-Plain .375 Hexagon head x .190-24 NC thd x .350 in.long (engine data plate) .

Seal.16.625 10 x .125 in. dia Round (reduction gear housingshim) .

Shim-Reduction gear housing (for -4 and -7M2) .Tube-Crankcase to propeller shaft oil transfer (for -4 and

-7M2) .Pipe Assembly Complete-Cylinder drain oil suction (for use

with engineshaving Part No. 150246, 156075 or 164448crankcaseassembly) .

PipeAssembly-Cylinder drain oil suction .Seal-.500 in. 00 Tube (cylinder sump suction Pipe) .

REDUCTION GEARING COUPLING BEARING SUPPORT

Elbow-.125 in. pipe thd _350 (Support plate tap oil pressuretap; applicable to -4 and -7M2; for Field useonly; useshipping plug MS20913-1S on enginesat overhaul) .

Support Assembly.Reduction drive (for -4 and .7M2) .

ATTACHING PARTS

Screw.Flat head .250-20 NC thd x 1.344 in. long (front mainbearing support to main crankcase) .

*

4

21

112

11

3

666.4

6.5

6-6

6-7

6-8

6-9

6.10

6.11

6-12

6-136-14

6-15

135983*135982t3421234212P534212P1034212P62t27

27P627P11t26199

26199P326199P526199P1026199P3043568

t36088

36088P5t44096

44096P544096P10t15

15P1015P2015P30t41870

41870P1056

15103726198

11624

Support Assembly-Reduction drive. . . . . . . . . . . . . . . . . . . . 1Support-Reduction drive. . . . . . . . . . . . . . . . . . . . . . . . . NPLiner-Reduction driven coupling bearing support. . . . . . . . . 1Liner sameas34212 only .005 in. oversize. . . . . . . . . . . . . ARLiner sameas 34212 only .010 in. oversize. . . . . . . . . . . . . ARLiner sameas 34212 only .062 in. oversize. . . . . . . . . . . . . ARPin-Straight .1885-.1890 dia x .500 in. long (reduction

driven coupling bearing support liner) . . . . . . . . . . . . 4Pin sameas27 only .006 in. oversize. . . . . . . . . . . . . . . . . ARPinsameas270nly.011 in. oversize. ARBl:Jshing.Flanged.802 lOx 1.00200 x 1.255 in. long

(front oil pump intermediate gear) . . . . . . . . . . . . . . 1Bushing sameas26199 only .003 in. oversize. . . . . . . . . . . ARBushing sameas26199 only .005 in. oversize. . . . . . . . . . . ARBushing sameas26199 only .010 in. oversize. . . . . . . . . . . ARBushing sameas26199 only .030 in. oversize. . . . . . . . . . . ARPin-Straight .1285 dia x .344 in. long (front oil pump

intermediate gear bushing) .Bushing-Flanged .740 10 x .939500 x 1.328 in. long

(front cam reduction gear) . . . . . . . . . . . . . . . . . . . 2Bushing same as36088 only .005 in oversize ARBushing.Front Cam reduction gear (For some Air Force

converted -4 and -7M2). . . . . . . . . . . . . . . . . . . . . . 2Bushing sameas44096 only .005 in. oversize .... ; . . . . . . ARBushing sameas44096 only .010 in. oversize. . . . . . . . . . . ARPin-Straight .1285 dia x .406 in. long (front cam

reduction gear bushing) . . . . . . . . . . . . . . . . . . . . . 2Pin sameas 15 only .010 in. oversize. . . . . . . . . . . . . . . . . ARPin sameas 15 only .020 in. oversize. . . . . . . . . . . . . . .. . ARPin sameas 15 only .030 in. oversize. . . . . . . . . . . . . . . . . ARBushing-.812510 x .97000 x .969 in. long (magneto

drive intermediate gear) . . . . . . . . . . . . . . . . . . . . . 2Bushing sameas41870 only .010 in. oversize. . . . . . . . . . . ARPin.Straight .163 dia x .656 in. long (magneto drive

intermediate gear bushing) . . . . . . . . . . . . . . . . . . . 2Shaftgear-I ntermediate front oil pump. . . . . . . . . . . . . . . . . . 1Bolt-5/16-24 NF thd x 1 59/64 in. long (front oil pump

intermediate shaftgear) .Nut.Shear .500 Hexagon head x .3125.24 thd x .218 in.

thick (front oil pump intermediate shaftgear bolt). . . . . . 1

2.13

Page 26: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

I.

T.O. 2R.R2000-24.

2-14

Figure 6 R. eduction Gear.mg Coupling Bearing Support

III_I

Page 27: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

. T.O. 2R-R2000-24

DESCRIPTIONPART NUMBER 1 2 3 4 5 6 7

REDUCTION GEARING COUPLING BEARING SUPPORT

FIGURE &INDEX

NUMBER

e 6-16

6-176-18

6-196-206-21

6-22

6-23

6-24

6-25

66-26

6

6-27

6-28

6-29

6-30

6-316-32

6-33

6-34

6-35

6-36

6-37

6-38

MS24665-300

83104AN932D2

730923420731156

11623

MS24665-300

MS20913-1S

92535

*9253373137

*92534

92893

92892

MS24665-370

93406

93407AN150432

MS24665-151

288949

45416

40500

514

MS24665-227

Cotterpin-corrosion resistant steel .093 dia x .750 in.long: (Supersedes AS123791; front oil pumpshaft-gear bolt nut) .

Gear-Front cam reduction upper & lower .Plug-Hexagon socket .125 in. ANPT (support plate drilled

oil passage; for -4 and -7M2) .Spacer-Front cam lower reduction gear .Gear-Governor drive .Washer-Chamfered .391 10 x .87500 x .094 in. thick

(front cam reduction gear) .Nut-Hexagon, shear, slotted .375-24 thd x .2656 in:

thick (front cam reduction gear; supersedes No.524 or AN150435) .

Cotterpin-corrosion resistant steel .093 dia x .750 in.long. Trim to .625 in. long before use. (Super-sedes AS123790; front cam reduction gear nut) .

Plug-.281 square head x .125-27 pipe x .578 in. long:(Supersedes 17346; support plate top oil pressuretap) .

Coupling & Bearing Assembly-Reduction gear drive (for-4 and -7M2) .

Coupling-Reduction gear drive (for -4 and -7M2) .Rivet - .122 dia x .203 in. long Special (reduction

gear drive coupling; for -4 and -7M2) .Bearing-3.1325 10 x 5.5190 00 x 2.280 in. long

(reduction drive gear coupling; for -4 and -7M2) .Pin-Straight .18875 dia x .250 in. long (reduction

drive gear coupling to coupling bearing; for -4 and-7M2), .

Spannernut-5.875-16 N LH thd x 6.750 x .372 in. thick(reduction driven coupling support bearing) .

Cotterpin-corrosion resistant 0.118-0.122 in. dia x 1.000 in.long (reduction driven coupling support bearing span-nernut; supersedes Part No. 59297 & AS123806) .Spacer-Plain .266 10 x .4375 00 x .281 in. thick (timing

indicator pin) .Pin-Timing indicator .Nut-Hexagon, shear, slotted .190 (No.10)-32 thd x .188

in. thick (timing indicator pin; supersedes No. 507) .Cotterpin-corrosion resistant steel .062 dia x .500 in.

long (Supersedes AS123773; timing indicator pin nut) .....Bearing Option-Reduction driven coupling support (pro-

curement number consists of: Part No. 34218 Bearing-Roller 5.9045-5.9055 lOx 8.2665-8.2677 00 x L0974-1.1024 in. long (optional to Part No. 288917, 288918, or359239) .Part No. 288917 Bearing-Rol.ler 5.9055 lOx8.2677 00 x 1.1024 in. Wide (optional to Part No.34218,288918 or 359239) Part No. 288918 Bearing-Roller 5.9055 ID x 8.2677 00 x 1.1024 in. Wide (op-tional to Part No. 34218, 288917 or 359239) Part No.359239 Bearing-Roller 5.905510 x 8.2677 00 x 1.1024in. Wide (optional to Part No. 34218, 288917 or 288918).

Support Assembly-Magneto drive intermediate level .

ATTACHING PARTS

Washer.Plain .328 ID x .562 00 x .0315 in. thick(magneto drive intermediate gear supports to main bearingsupport) ...........•.......................

Nut-Shear .500 Hexagon head x .3125-24 NF thd x .266in. thick (magneto drive intermediate gear supports tomain beari ng support) : .

Cotterpin.078 dia x .500 in. long (supersedes 7916; magnetodrive intermediate gear supports to main bearing supportnut) .

- - - - * - ~- -

UNITSPER ASSY

12

211

2

2

2

2

1NP

NP

3

2

11

12

4

4

4

2-15

Page 28: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

'FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

REDUCTION GEARING COUPLING BEARING SUPPORT

l

66-39

6-40

6-41

6-42

6-436-44

6-45

6-466.47

7-1

7

7

77777-2

7-377-4

7-5

7-6

7-7

7-8

7-9

2-16

*4541545417

28151

t637P4

637P8637P124617

41862514

42745

41873MS24665-229

164448R1

164448

460992

*143993*145998*143992*127140t9664396643P596643P10402888*50034AN122583

733

145996

t127170

1271 70P106560

t9667596675M296675M596675M1096675P596675R1

96675R6

Support-Magneto drive intermediate gear .Bearing-Flanged .365 I D x .502 OD x .5005 in. long

(magneto drive intermediate gear support) .Pin-Straight .072 dia x .250 in. long (magneto drive

intermediate gear bushing) .Stud-Drilled .3125-18-24 thd x 1.562 in. long (magneto

drive intermediate gear supports to main bearingsupport) .004 in. oversize .

Stud same as 637 only .008 in. oversize .Stud same as 637 only .012 in. oversize .

Dowel-Straight .1875 dia x .438 in. long (magneto driveintermediate gear supports locating) .

Gear-Magneto drive driving .Nut-Shear .500 Hexagon head x .3125-24 NF thd x .266

in. thick (magneto drive driving gear shaft) .Gear-Magneto drive intermediate bevel (replaces No. 41861

or 41863 for -4 & -7M2 engines) .Shaft-Magneto drive .Cotterpin-.073 dia x .750 in. long; trim to .625 in. long

before use; (supersedes 22473; magneto drive gearshaft nut) .

MAIN CRANKCASE

Crankcase Assy of, main (For use on Air Force -4 and -7M2engines having non-flooded rockerbox system; sameas 164448 only less front and rear main bearings; sup-ersedes No. 150246 and 156075) (USAF configuration) ....

Crankcase Assy of, main (same as 164448R1 only hasJront& rear main bearings installed) (USAF configuration) .

Crankcase Assy of, main (For use on engines having floodedrockerbox system; supersedes No. 150246, 156075and 164448) (When flooded rocke,rbox configurationis used) .Crankcase Assy-Main (supersedes No. 146035) .Crankcase-Center main (supersedes No. 127139) .Crankcase-Front main (supersedes No. 127247) .Crankcase-Rear Main .Liner-Center main crankcase .Liner same as 96643 only .005 in. oversize .Liner same as 96643 only .010 in. oversize .

Support Assembly-Main oil sump .Support-Main oil'sump .

Washer-plain .328 ID x .625 OD x .0625 in. thick (Mainoil sump support screw; supersedes No. 171 and 118065) ...

Screw-Drilled .500 Hexagon head x .3125-18NC thd x1.094 in. long (main oil sump support: use No.MS20995 wire; supersedes No. 18185) .

Seal-Crankcase oil (for use in grooves in mating faces ofcenter section; replaces No. 145977 and 175599) .

Dowel-.4360-.4365 dia x 1.000 in. long (main crankcasealigning; for -4 and -7M2) .

Dowel same as 127170 only .010 in oversize .Plug-.188 Hexagon head x .4375-20 NF-3 thd x .312 in.

long (magneto vent tube retaining stud hole) .Bearing-Front & rear main crankcase " .Bearing same as 96675 only .002 in. undersize .Bearing same as 96675 only .005 in. undersize .Bearing same as 96675 only .010 in. undersize .Bearing same as 96675 only .005 in. oversize .Bearing same as 96675 only .005 in. oversize on OD & .002

in. undersize on I D .Bearing same as 96675 only .005 in. oversize on OD &

.002 in. undersize on ID & .020 in. oversize on flangethickness .

NP1

4ARAR42

2

22

2

1

AR

1NPNPNPNP1ARAR1NP2

2

14

4AR22ARARARARAR

AR

Page 29: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

/I 40

JAs ).'I I /, \I; \

Ii "'"'0,*==""""/' I.

42

~-506-51<6-52

I

59-V

~:c~~I61"~62

-33

~

I49

Figure 7. Main Crankcase

2-17

Page 30: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

'1

FIGURE &INDEX

NUMBER PART NUMBER 1 2 3 4 5 6 7DESCRIPTION UNITS

PER ASSY

7-10

7-11

7-12

7-13

7.14

7-15

7-16

7-17

7-18

7-19

7.20

2.18

96675R2

96675R4

96675P1096675R 7

96675R3

96675R5

96675P2096675P3096675P30M5

96675P4096675P50MS122122

t31541P4

31541P1231541P8127145

127146

t115528

115528P10t126056

126056P10126056P20126056P30126056P40t22744P4

22744P822744P12t29981P4

29981P829981P12t9085P4

9085P89085P12t31416P4

31416P831416P12t64

64P464P864P1264P30

MAIN CRANKCASE

Bearing same as 96675 only .005 in. oversize on OD & .005in. undersize on ID .

Bearing same as 96675 only .005 in. oversize on OD & .020in. oversize on flange thickness .

Bearing same as 96675 only .010 in. oversize .Bearing same as 96675 only .010 in. oversize on OD &

.002 in. undersize on 10 .Bearing same as 96675 only .010 in. oversize on 00 &

.005 in. undersize on 10 .Bearing same as 96675 only .010 in. oversize on 00 &

.020 in. oversize on Flange thickness .Bearing same as 96675 only .020 in. oversize .Bearing same as 96675 only .030 in. oversize .Bearing same as 96675 only .030 in oversize on 00 &

.005 in. undersize on 10 .Bearing same as96675 only .040 in. oversize .Bearing same as 96675 only .050 in oversize .Insert-Corrosion resistant steel, helical-coil, coarse

thread .3125.18 x .469 in. long (crankcase to reductionhousing at oil pump bolt; supersedes No. 86573) .

Stud-Plain 5/16-18-24 thd x 2-5/8 in. long (front maincrankcase to reduction gear housing; supersedes No.54431 (12) units which supersedes No. 31540 (12)units) .004 in. oversize .

Stud same as 31541 only .008 in. oversize .Stud same as 31541 only .012 in. oversize .Stud - Rosan .375.24 & .4375-14 thd x 2.015 in. long

(cylinder flange; for -4 and -7M2) .Stud - Rosan .375-24 & .4375-14 thd x 2.110 in. long

(cylinder flange; for -4 and -7M2) .Bolt - .375-24 NF thd x 2.230 in. long (cylinder flange;

for -4 and -7M2) .Bolt same as 115528 only .010 in. oversize .Lockring - .381 ID x .555 00 x .148 in. thick (cylinder

flange stud; for -4 and. 7M2) .Lockring same as 126056 only .010 in. oversize .Lockring same as 126056 only .020 in. oversize .Lockring same as 126056 only .030 in. oversize .Lockring same as 126056 only .040 in. oversize .Stud. Plain .3125-18-24 thd x 2.468 in. long (main

crankcase to reduction housing at governor pad).004 in. oversize .

Stud same as 22744 only .008 in. oversize .Stud same as 22744 only .012 in. oversize .Stud - Plain .3125-18-24 thd x 1.3125 in. long (front

main crankcase oil inlet feed pipe elbow; for -4and -7M2) .004 in. oversize .

Stud same as 29981 only .008 in. oversize .Stud same as 29981 only .012 in. oversize .Stud - Plain .3125-18-24 x 1.375 in. long (front main

crankcase oil inlet feed pipe elbow) .004 in.oversize .

Stud same as 9085 only .008 in. oversize .Stud same as 9085 only .012 in. oversize .Stud - Drilled .250-20-28 thd x .953 in. long (main

crankcase to cam bearing; supersedes No. 38691).004 in. oversize .

Stud same as 31416 only .008 in. oversize .. Stud same as 31416 only .012 in. oversize .Pin - Straight, headless .312 dia x .625 in. long

(rear main crankcase to blower locating) .Pin same as 64 only .004 in. oversize ' .Pin same as 64 only .008 in. oversize .Pin same as 64 only .012 in. oversize .Pin same as 64 only .030 in. oversize .

AR

ARARARARARARARARARAR

2

18ARAR112

56

56AR168ARARARAR

2ARAR

2ARAR

2ARAR

16ARAR1ARARARAR

Page 31: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

FIGURE &. INDEXNUMBER

DESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

MAIN CRANKCASE

T.O.2R-R2000-24

UNITSPER ASSY

..7-24

S 7-25

7-26

7-27

7-28

7-29e 7-30

7-31

7-32

7-33

t.;~

7-21

7-22

7-23

7

7

7

7

t31538

31538P431538P826553

t24856

24856P324856P524856P10t24856

24856P324856P524856P1042

25

25070

t32336

32336P232336P432336P828151

43199

57959

28151

t106753

106753P10106753P15106753P40tl06750

106750P10106750P15106750P40tl56072

156072P10156072P15156072P40t156073

156073P10156073P15156073P40tl06754

106754P10106754P15106754P40

Dowel - Straight .312 dia x 1.312 in. long (front maincrankcase to reduction housing locating) .

Dowel same as 31538 only .004 in. oversize .Dowel same as 31538 only .008 in. oversize .Dowel - Stepped .252 dia x .344 in. long (rear main

crankcase to cam bearing locating) .Bushing - Flanged. 740 lOx .939500 x 1.078 in. long

(rear cam reduction gear) .Bushing same as 24856 only .003 in. oversize .Bushing same as 24856 only .005 in. oversize .Bushing same as 24856 only .010 in. oversize .Bushing - Flanged. 740 lOx .9395 00 x 1.078 in. long

(front cam reduction gear) .Bushing same as 24856 only .003 in. oversize .Bushing same as 24856 only .005 in. oversize .Bushing same as 24856 only .010 in. oversize .Pin - Straight .165 dia x .125 in. long (rear main

crankcase drilled oil hole) .Pin - Straight .165 dia x .500 in. long (rear main

crankcase drilled oil hole) .Pin - Straight .2525 dia x .375 in. long (front main

crankcase drilled oil hole) .Insert - .3125-24 NF 10 x .5625-18 N 00 x .750 in. long

(main oil sump support) .Insert same as 32336 only .002 in. oversize .Insert same as 32336 only .004 in. oversize .Insert same as 32336 only .008 in. oversize .Pin - Straight .072 dia x .250 in. long (main oil sump

support) .Insert - Flanged .5005 10 x .6265 00 x .672 in. long

(front lower main crankcase oil inlet pipe) .Insert - Plain .3125-1810 x .500-13 00 x .500 in. long

(front lower main crankcase cast manifold stud) .Pin - Straight .072 dia x .250 in. long (cast manifold

stud insert) .Guide - Intake valve tappet upper front (use (3) units

with Part No. 150246, 156075 or 164448 crank-case assembly) .

Guide same as 106753 only .010 in. oversize .Guide same as 106753 only .015 in. oversize .Guide same as 106753 only .040 in. oversize .Guide - Intake valve tappet upper rear (use (3) units with

Part No. 150246, 156075 or 164448 crankcaseassembly) .

Guide same as 106750 only .010 in. oversize .Guide same as 106750 only .015 in. oversize .Guide same as 106750 only .040 in. oversize .Guide - Exhaust valve tappet upper front (supersedes

No. 106755; use (3) units with Part No. 150246,156075 or 164448 crankcase assembly) .

Guide same as 156072 only .010 in. oversize .Guide same as 156072 only .015 in. oversize .Guide same as 156072 only .040 in. oversize .Guide - Exhaust valve tappet upper rear (supersedes

No. 106752; use (3) units with Part No. 150246,156075 or 164448 crankcase assembly) .

Guide same as 156073 only .010 in. oversize .Guide same as 156073 only .015 in. oversize .Guide same as 156073 only .040 in. oversize .Guide - I ntake valve tappet lower front (use (2) units

with Part No. 460992 crankcase) .Guide same as 106754 only .010 in. oversize .Guide same as 106754 only .015 in. oversize .Guide same as 106754 only .040 in. oversize .

1ARAR

2ARARAR

2ARARAR1

1

1

1ARARAR

2

2

5ARARAR

5ARARAR

5ARARAR

4ARARAR

4ARARAR

2-19

Page 32: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000.24

FIGURE &UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2 345 6 7 PER ASSY

7

7

7

7

7

7.34

7.35

].36

7.37

7.38

7-39

7.40

7.41

7-42

7.43

7.44

7-45

2.20

tl06749

106749P10106749P15106749P40t367350

367350P10367350P15367350P40t367351

367351P10367351P15367351P40t106756

106156P10106756P15106756P40tl06751

106751P10106751P15106751P40121337

121323

9401

AN121555

121319

t142642P4

142642P8142642P60142642P62AN123861

9400

t203170P4

203170P8203170P12203170P62t121336P4

121336P8121336P6272624

tl27097P4

127097P8127097P62

MAIN CRANKCASEGuide. Intake valve tappet lower rear (use (2) units with

Part No. 460992 crankcase) .Guide sameas 106749 only .010 in. oversize .Guide sameas 106749 only .015 in. oversize .Guide sameas 106749 only .040 in. oversize .Guide. Exhaust valve tappet, front (for usewith Part

No. 460992 crankcase assembly) .Guide sameas 367350 only .010 in. oversize .Guide sameas 367350 only .015 in. oversize .Guide sameas 367350 only .040 in. oversize .Guide. Exhaust valve tappet, front (for usewith Part

No. 460992 crankcase assembly) .Guide sameas 367351 only .010 in. oversize .Guide sameas 367351 only .015 in. oversize .Guide sameas 367351 only .040 in. oversize .Guide. Exhaust valve tappet lower front (for usewith Part

No. 150246, 156075 or 164448 crankcase assembly) .Guide sameas 106756 only .010 in. oversize .Guide sameas 106756 only;015 in. oversize .Guide sameas 106756 only .040 in. oversize .Guide . Exhaust valve tappet lower rear (for usewith Part

No. 150246, 156075, or 164448 crankcase assembly) .Guide sameas 106751 only .010 in. oversize .Guide sameas 106751 only .015 in. oversize .Guide sameas 106751 only .040 in. oversize .Spacer-1.1332 10 x 1.35000 x.345 in. thick (rear tappet

guide; for.4 and .7M2) .Nut - .618 slotted hexagon head x .4375-20 thd x .328 in.

thick (main crankcase stud front; for .4 and -7M2) .Washer.Chamfered .4531 lOx .80200 x .093 in. thick

(main crankcase studs; use (6) units for.4 & -7M2) .....Nut-Castle .4375-20 thd x .454 in. thick (main crankcase

studs rear: supersedesNo. 533; use (6) units for.4 & .7M2) .

Spacer.Chamfered .453 lOx. 79500 x .310 in. thick(front casethru stud upper: front & rear casethrustud lower; for -4 & .7M2) .

Stud ..4375-14.20 thd x 5.890 in. long (center & rearmain crankcase attaching; for -4 and -7M2) .004 in.oversize .

Stud sameas 142642 only .008 in. oversize .Stud sameas 142642 only .060 in. oversize .Stud sameas 142642 only .062 in. oversize .Seal."O" Ring oil resistant .296'.306 I0 x .438 00 x

.067-.073 in. thick (crankcase stud: supersedesNo. AN123860; for.4 and -7M2) .

Nut.Shear .625 Hexagon head x .4375.20 NF thd x .328in. thick (center & rear main crankcase stud lower& center to front main crankcase stud upper) .

Stud-Drilled .4375-14.20 thd x 8.260 in. long (maincrankcase front: supersedesNo. 142643; for -4 &.7M2) .004 in. oversize .

Stud sameas 203170 only .008 in. oversize .Stud sameas 203170 only .012 in. oversize .Stud sameas 203170 only .062 in. oversize .Stud-Drilled .4375.14.20 thd x 2.000 in. long (lifting

link; for -4 and .7M2) .004 in. oversize .Stud sameas 121336 only .008 in. oversize .Stud sameas 121336 only .062 in. oversize .Bolt.Shouldered .625 Hexagon head x .4375.20 NF

thd x 4.160 in. long (main crankcase liftinglinks; for .9A) .

Stud-Plain .4375-14-20 thd x 1.406 in. long (oil pipeclip; for .4 & -7M2) .004 in. oversize .

Stud sameas 127097 only .008 in. oversize .Stud sameas 127097 only .062 in. oversize .

4ARARAR2ARARAR3ARARAR4ARARAR4ARARAR

14

6

25

13

2

6ARARAR

18

2

6ARARAR3ARAR

3

1ARAR

Page 33: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

7-46

7-477-48

7.497.507-51

7-52

7-53

7-547-55

7-56

7-57

7-5877

7-59

7-60

7.61

7-62

7

7-63

777

7-64

7-65

7.667-677-68

7-69

7-70

7-717-72

7-73

t142641P4

142641P8142641P60142641P6243408AN121555

126874135822135903

84058

MS24665-300

125810224999

64406

38745

10675877546*106757

t162625162625P10t5613256132P10225637

225634

207888

69E35002-1

*111655*111656111654

27956

5213

32820106759AN960-416

AN121552

92555

106760AN960.416

AN121552

MAIN CRANKCASE

Stud •.4375-14-20 thd x 4.260 in. long (main crankcasefront section upper & rear section lower attaching;for -4 & -7M2) .004 in. oversize .

Stud same as 142641 only .008 in. oversize .Stud same as 142641 only .060 in. oversize .Stud same as 142641 only .062 in. oversize .Link-Engine lifting .Nut-Castle .4375-20 thd x .454 in. thick (lifting link studs;

supersedes No. 533) .Spacer-Reduction drive support rear (for .4 & -7M2) .

Plug-Upper thru stud nut hole front crankcase (for -4 & -7M2) .Snapring-1.562 00 x .063 in. thick (upper thru stud nut

hole plug; for -4 & -7M2) .Seal-1.l30 10 x .100 in dia Round (upper thru stud nut

hole plug; for -4 & -7M2) .Cotterpin-corrosion resistant .093 dia x .750 in. long. Trim

to .625 in. long before use. (main crankcase stud;for -4 & -7M2) .

Elbow-Front main crankcase oil drain tube (for -4 & -7M2) .Connector-.625 in. 00 Tube (front main crankcase oil drain

tube: supersedes No. 125809; for -4 & -7M2) .Gasket-.880 lOx 1.25000 x .032 in. thick (front crankcase

oil drain tube connector; for -4 & -7M2) .Seal-.500 10 x .125 in. thick (front crankcase oil drain tube

elbow; for -4 & -7M2) .Tappet Assembly-Valve .

Socket-Push rod ball .Tappet-Valve (for use with Part No. 106758 tappet assem-

bly) .Roller-Valve tappet (replaces No. 56131) .Roller same as 162625 only .010 in. oversize .Pin-Straight .37325 dia x .781 in. long (valve tappet roller) .Pin same as 56132 only .010 in. oversize .Bolt-Universal elbow .3125-24 thd x .713 in. long (tappet

guide: use No. MS20995 wire; supersedes No. 15670) ...Bolt-Drilled .500 Hexagon head x .3125-24 NF thd x .430

in. long (tappet guide; supersedes No. 16274) .Washer-Chamfered .4075 10 x .7075 00 x .145 in. thick

(cylinder flange bolt: spherical seat: for service:useasrequired;for-4&-7M2) .

Baffle Assy-Rear Main Crankcase for -4 & -7M2, fabricatedfrom Part No. 27843. (Replaces Part Nos. 27843,127942, and 127944) .

Tube-1.000 00 x .035 thick (rear main breather baffle) .Baffle-Rear main breather .Bracket-Rear main breather baffle .

ATTACHING PARTS

Stud-Drilled, shouldered .250-28 & .3125-24 NF thd x 1.285 in.long (breather baffle; use No. AS100029 wire) .

Nut-7/16 Slotted Hexagon head x 1/4-28 thd x 3/16 in. thick(breather baffle stud; use No. MS20995 wire) .

- - - - * - - --Bearing-7.129 10 x 77/800 xl 15/16 in. long (rear cam) .Cam-Rear, wide track, 'use for both wide and narrow trackWasher-plain .266 10 x .500 00 x .062 in. thick (rear cam

bearing nut; supersedes No. 171) .Nut-Castle .250-28 thd x .282 in. thick (front cam bearing

retaining: use No. MS20995wire;supersedes No. 502) .....Bearing-Flanged 7.129 10 x 7.42600 x 1.187 in. long (front

cam) .Cam-Front, wide track, use for both wide & narrow track .Washer-plain .266 10 x .500 00 x .062 in. thick (front cam

bearing nut; supersedes No. 171) .Nut-Castle .250-28 thd x .282 in. thick (front cam bearing

retaining: use No. MS 20995 wire; supersedes No. 502) .....

2ARARAR3

311

1

1

141

1

1281

NP28AR28AR6

12

AR

1NPNP7

7

7

11

8

8

11

8

8

2-21

Page 34: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

2R.R2000.24T.O.

36

I

14

.-iI 35L34 I

I [0"@{~~1822 I

i I ~ _ 23I I I

i:l~ ~.Jf.,L.. .--~1i-~~i-~ : (/I~

17 "" I19 I

1227-1

g;;-26

r--II

~I

24

(Continued)"Main CrankcaseFigure 8.

2-22

Page 35: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

8-18-2

8-3

8-4

8-5

8-6

8-788-8

8-9

8-10

8-11

8-12

8-13

8-14

8-15

8-16

8-17

8-18

8-19

8-208-21

8-22

8-23

8-248-25

8-26

96639t101116101116P4101116R1

94032

5121

AS123775

MS35769-21

149698*149697143519

MS35769-18

84237

51C9610.1

6558

18502

121325

111090

MS21044-N5

25870

25869

125310

99541134944

MS9122-04

134944

12520871547

225635

MAIN CRANKCASE

Retainer.Crankshaft center main bearing .Bearing Assembly.Crankshaft center .Bearing Assembly same as 101116 only .004 in. oversize .Bearing Assembly same as 101116 only .004 in. oversize

on 00 & .004 in undersize on 10 .Bolt.Drilled shank .500 hexagon head x .3125-24 NF thd x

1.656 in. long (crankshaft center main bearing retainer) ....Nut.Shear .500 Hexagon head x .3125-24 NF thd x .219 in.

thick (crankshaft center main bearing retainer bolt;supersedes No. 11624) .

Cotterpin.Corrosion resistant .058-.061 dia x .625 in. long(crankshaft center main bearing retainer bolt nut) .

Gasket-1.008 lOx 1.250 00 x .094 in. thick (rear main crank.case breather; supersedes AN900-18) .

Breather Assembly.Rear main crankcase (for -4 & -7M2) .Breather-Rear main crankcase .Screen Assembly.Rear main crankcase breather (supersedes

No. 11951) .Gasket-7/8 10 xl 1/8 in. 00 (rear main crankcase breather

pipe connection; supersedes No. 18502; 28822, orAN900-14) .

Pipe Assembly.Rear main crankcase breather (supersedes23964) .

Plug.sealing rear main crankcase breather pipe; (supersedes81401 and P-6792) .

Gasket'.531 10 Pipe flanged x .031 in. thick (blower oilpressure pipe elbow to main crankcase; for -4 & .7M2) .....

Gasket-.812 ID x 1.12500 x .031 in. thick (front maincrankcase oil pressure pipe to blower) .

Tube Assembly.Coliector case to front main crankcase oilpressure (for -4 & -7M2) .

Hose-for use on tube assembly No. 121325 .

ATTACHING PARTS

Nut.non.metalic lock .500 hexagon head x .3125-24 thd x.344 in. thick. (Collector oil pressure tube to frontmain crankcase, supersedes No. 33415) .

*Bushing-Collector to front main crankcase oil pressure tube

clip .Clip-5/8 in. 00 (collector to front main crankcase oil pres.

sure tube) .Bracket Assembly-Collector caseto front main crankcase oil

pressure tube.Bracket-Coil case to front main C/C oil pressure tube (-7M2) .....Bolt.Drilled 0.625 hex head x 9.4375 -20 NF thd x 0.360 in.

long oil pressure tube bracket to Fr. C/C (-7M2) .

ATTACHING PARTS

Screw-Machine slotted hex head x .190.32 NF thd x .562 in.long (collector to front main crankcase oil pressuretube bracket to clip; for -4 & .7M2; supersedes No. 92938) .

Bolt.Drilied .625 Hexagon head x .4375-20 N F thd x .630 in.long (oil pressure tube bracket to front crankcase; for-4 & -7M2) .

- - - - * - -.-Tube.Cam oil pressure (for -4 & -7M2) .Pipe Assembly.Front main crankcase to magneto advance

fitting .

ATTACHING PARTS

Bolt.Drilied .500 Hexagon head x .3125-24 NF thd x .475in. long (magneto advance fitting pipe clip to frontmain crankcase; supersedes No. 34020) .

21ARAR8

8

8

11NP

1

1NP

2

13

1

1

2

2-23

.. 1

d

Page 36: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

MAIN CRANKCASE

8-27

8-28

88-298-308-318-32

8-338-34

8-358.36

8

9-1

99-2

9-39.4

9-59-6

9-7

9-8

9-9

99-10

9-119-129-13

9-149-159

2-24

225636

138863

*1253531213324366231543MS35769-18

43661t6467

6467P30W8143938606

12584

374605

*10123416681

135180t15

15P1015P2015P3042042144542

6560

t126239

126239P2126239P5126239P10126239P2023407

*118858t121575121575P10121573121574MS24665-370

15093597257150932

Bolt-Universal elbow .3125-24 thd x .758 in. long (magnetoadvance fitting pipe clip to front main crankcase;supersedes No. 49482) .

- - - - * - - - -Manifold Assembly -Pressure junction (propeller governor oil;

for -4 & -7M2) .Connector-Cam oil feed .Tube-Pressure junction manifold .

Fitting-Oil feed .Pipe-Oil feed fitting .Gasket-.883 10 x 1.12500 x .094 in. thick (manifold gov-

ernor oil cap; supersedes No. AN900-14) .Cap-Manifold governor oil .Spacer-Chamfered .781 10 x 1.12500 x .093 in. thick (rear

cam reduction gear) .Spacer same as 6467 only .030 in. oversize on width .Gear-Rear cam reduction .Seal-16.625 10 x .125 in. dia Round (rear main crankcase

to blower case) .Seal-16.000 10 x .125 in. dia Round (support plate to front

main crankcase) .

CRANKSHAFT AND CONNECTING RODS

Crankshaft Assembly - (supersedes No. 96652,101236,119341,150936,151733,167464, or 384254) .

Crankshaft .Pin - Straight .1572-.1577 dia x .340 in. long (front

crankshaft) .Plug - Crankpin drilled oil passage .Pin - Straight .1285 dia x .406 in. long (crankpin

drilled oil passage plug) .Pin same as 15 only .010 in. oversize .Pin same as 15 only .020 in. oversize .Pin same as 15 only .030 in. oversize ' .Standpipe - Crankshaft rear crankpin .Standpipe - Crankshaft front & rear crankpin lubricat-

ing .Plug - .188 Hexagon head x .4375-20 NF-3 thd x .312 in.

long (crankshaft rear crankpin drilled oil passages) .Liner - Crankshaft flyweight (replaces No. 137233: for

use with Part No. 23407 flyweight: use Part No.137233 liner with Part No. 135413 flyweight) .

Liner same as 126239 only .002 in. oversize .Liner same as 126239 only .005 in. oversize .Liner same as 126239 only .010 in. oversize .Liner same as 126239 only .020 in. oversize .Flyweight - Crankshaft power impulse dampening (replaces

No. 135413 for Air Force engines: for use with PartNo. 126239 liner; use Part No. 135413 flyweightwith Part No. 137233 liner) .

Counterweight - Front & rear .Sleeve - Counterweight bolt. .Sleeve same as 121575 only .010 in. oversize .Bolt - .625-18 NF thd x 2.510 in. long (counterweight) .Nut - Counterweight bolt .

Cotterpin-corrosion resistant 0.118.0.122 in. dia x 1.000 in.long. (Counterweight bolt nut; supersedes Part No. 59297& AS123806) .Tube. Crankshaft .Jet - Crankshaft front. .Tube - Counterweight (lead coated; for use with Part

No. 161965 & 167464 crankshaft assembly) .

1

1NP111

2AR2

1NP11

1ARARAR2

4

2ARARARAR

2NP8AR88

811

1

Page 37: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

35 -

34..50

It \

0-48149

_I

27 28

--.-32

Crankshaft and Connecting RodsFigure 9.

2-25

...J

Page 38: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

1

IFIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

CRANKSHAFT AND CONNECTING RODS

UNITSPER ASSY

2-26

9

9

9-16

9-179-18

9-199-20

9-21

9

9

9-22

9

9-23

9-24

9-259-26

9-279-289

9-299

9

9

9-309-31

9-32999

Ii

L _

150933

105731

t4203942039P342039P642038tl50755150755P5150934t9254192541P20W92541P40W92541P75Wt374385

374385P2374385P5374385P8374385P11374385P14374385P17374385P25374385P27*374384

100536

t501782

501782P20t374391

374391P20t374390

374390P2050195

9725997258

966579665673137

13487043516

523

41764

19218826486

166582283110*36700*21779

Tube - Counterweight (lead coated; for use with PartNo. 161965 & 167464 crankshaft assembly) .

Plug - Steel .062-27 ANPT x .059 Jet (crankshaft front& rear counterweight: for use with crankshaftsnot incorporating counterweight stand pipes; sup-ersedes No. 27144) .

Plug - Crankpin .Plug same as 42039 only .003 in. oversize .Plug same as 42039 only .006 in. oversize .Snapring - 1.438 00 x .0625 in. thick (crankpin plugs) .Plug - Crankshaft oil (rear crankshaft cheek) .Plug same as 150755 only .005 in. oversize .Tube - Crankshaft .Plate - Crankshaft thrust .Plate same as 92541 only .020 in. oversize on width .Plate same as 92541 only .040 in. oversize on width .Plate same as 92541 only .075 in. oversize on width .Hub Assembly - Red uction gear drive (replaces No.

96725; for use with Part No. 374605 crankshaft) .Hub Assembly same as 374385 only .002 in. oversize .Hub Assembly same as 374385 only .005 in. oversize .Hub Assembly same as 374385 only .008 in. oversize .Hub Assembly same as 374385 only .011 in. oversize .Hub Assembly same as 374385 only .014 in. oversize .Hub Assembly same as 374385 only .017 in. oversize .Hub Assembly same as 374385 only .025 in. oversize .Hub Assembly same as 374385 only .027 in. oversize .

Hub - Reduction gear drive (replaces No. 96724; foruse with Part No. 374605 crankshaft) .

Pin - Straight .1260-.1265 dia x .280 in. long(reduction drive gear hub) .

Washer - Key 1.780 10 x 2.062 dia x .050 in. thick (reductiongear drive hub; replaces No. 96733 or 174576) .

Washer same as 501782 only .020 in. oversize .Retainer Assembly - Reduction drive hub (replaces No.

97255; for use with Part No. 374605 crankshaft) .Retainer Assembly same as 374391 only .020 in. oversize .

Retainer - Reduction drive hub (replaces No. 97254;for use with Part No. 374605) .

Retainer same as 374390 only .020 in. oversize .Seal - Oil .625 ID x 1.125 OD x .375 in. thick

(reduction drive hub retainer) .Support - Reduction drive hub retainer oil tranfer tube .Snapring - 1.250 OD x .078 in. thick (reduction drive

hub retainer) .Coupling Assembly - Reduction drive Intermediate .

Coupling - Reduction drive intermediate .Rivet - .122 dia x .203 in. long Special (reduction drive

intermediate coupling) .Support - Accessory drive shaft .Bolt - 9/16 Hexagon head drilled x 3/8-24 thd x 1 7/32 in.

long (center crankshaft main bearing liner) .Nut - Shear .562 Hexagonhead x .375-24 NF thd x .328 in.

thick (center crankshaft main bearing liner bolt) .Bolt - Shouldered .562 Hexagon head x .375-24 N F thd

x .688 in. long (center crankshaft main bearing liner;use No. MS20995 wire) .

Gear - Crankshaft rear (supersedes No. 100949) .Bolt - Shouldered .500 Hexagon head x .375-24 NF thd

x 1.224 in. long (crankshaft rear gear; use No.MS20995 wire) .

Masterod & Bolts Assembly - (supersedes No. 105264) .Masterod Assembly - (for spares procurement) .

Masterod .Cap - Masterod .

1

22ARAR21AR11ARARAR

1ARARARARARARARARNP1

1AR1AR1AR11

111

11

4

4

41

821NPNP

••

Page 39: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

FIGURE &INDEX DESCRIPTION

NUMBER PART NUMBER 1 2 3 4 5 6 7

CRANKSHAFT AND CONNECTING RODS

T.O.2R-R2000-24

UNITSPER ASSY

9-33

9-34

9-35

9-369-379-38

9

99-399-40

t7160171601P171601P271601P371601P471601P5t84251

84251P584251P1040606

4365943978t73341CL A

73341CL B73341CL C73341PlD73341P1E73341P1F73341P5A73341P5B73341P5C73341P6D73341P6E73341P6F73341P10A73341PlOB73341P10C73341PllD73341P11E73341PllF73341P15A73341P15B73341P15C73341P16D73341P16E73341P16F*7315426448t73342CL A

73342CL B73342CL C73342P1D73342P1E73342P1F73342P5A73342P5B73342P5C73342P6D73342P6E73342P6F73342P10A73342P10B73342P10C73342P1lD73342PllE73342P11F73342P15A73342P15B73342P15C73342P16D

Shim - Masterod & cap .Shim same as 71601 only .001 in. oversize .Shim same as 71601 only .002 in. oversize .Shim same as 71601 only .003 in. oversize .Shim same as 71601 only .004 in. oversize .Shim same as 71601 only .005 in. oversize .Bushing - 1.375 10 x 1.534800 x 1.750 in. long

(masterod piston pin) .Bushing same as 84251 only .005 in. oversize .Bushing same as 84251 only .010 in. oversize .Pin - Straight .163 dia x .328 in. long (masterod

piston pin bushing) .Bolt - .625-14 Aero thd x 6.7031 in. long (mastered) .Nut - .625-14 Circle thd x .781 in. thick (masterod bolts) .

Linkpin Assembly - Double shouldered (for use with PartNo. 106965) - 1.0594-1.0597 in. 00 .

Linkpin Assembly - 1.0597-1.0600 in. 00 .Linkpin Assembly - 1.0600-1.0603 in. 00 .Linkpin Assembly - 1.0603-1.0606 in. 00 .Linkpin Assembly - 1.0606-1.0609 in. 00 .Lirikpiri Assembly - 1.0609.1.0612 in. 00 .Linkpin Assembly - 1.0644-1.0647 in. 00 .Linkpin Assembly - 1.0647-1.0650 in. 00 .Linkpin Assembly - 1.0650-1.0653 in. 00 .Linkpin Assembly - 1.0653-1.0656 in. 00 .Linkpin Assembly - 1.0656-1.0659 in. 00 .Linkpin Assembly - 1.0659-1.0662 in. 00 .Linkpin Assembly - 1.0694-1.0697 in. 00 .Linkpin Assembly - 1.0697-1.0700 in. 00 .Linkpin Assembly - 1.0700-1.0703 in. 00 : .Linkpin Assembly - 1.0703-1.0706 in. 00 .Linkpin Assembly - 1.0706-1.0709 in. 00 .Linkpin Assembly - 1.0709-1.0712 in. 00 .Linkpin Assembly - 1.0744-1.0747 in. 00 .Linkpin Assembly - 1.0747-1.0750 in. 00 .Linkpin Assembly - 1.0750-1.0753 in. 00 .Linkpin Assembly - 1.0754-1.0757 in. 00 .Linkpin Assembly - 1.0757-1.0760 in. 00 .Linkpin Assembly - 1.0760-1.0763 in. 00 .

Linkpin - Double shouldered .. Screw - .625-18 NF thd x .375 in. long (Iinkpin) .Linkpin Assembly - Partially intersected (for use with Part

No. 106965) - 1.0595-1.0598 in. 00 .Linkpin Assembly - 1.0598-1.0601 in. 00 .Linkpin Assembly - 1.0601-1.0604 in. 00 .Linkpin Assembly - 1.0604-1.0607 in; 00 .Linkpin Assembly - 1.0607-1.0610 in. 00 .Linkpin Assembly - 1.0610-1.0613 in. 00 .Linkpin Assembly - 1.0645-1.0648 in. 00 .Linkpin Assembly - 1.0648 -1.0651 in. 00 .Linkpin Assembly - 1.0651-1.0654 in. 00 .Linkpin Assembly - 1.0654-1.0657 in. 00 .Linkpin Assembly - 1.0657-1.0660 in. 00 .Linkpin Assembly - 1.0660-1.0663 in. 00 .Linkpin Assembly - 1.0695-1.0698 in. 00 .Linkpin Assembly - 1.0698-1.0701 in. 00 .Linkpin Assembly - 1.0701-1.0704 in. 00 .Linkpin Assembly - 1.0704-1.0707 in. 00 .Linkpin Assembly - 1.0707-1.0710 in. 00 .Linkpin Assembly - 1.0710-1.0713 in. 00 .Linkpin Assembly - 1.0745-1.0748 in. 00 .Linkpin Assembly - 1.0748-1.0751 in. 00 ~ .Linkpin Assembly - 1.0751-1.0754 in. 00 .Linkpin Assembly - 1.0755-1.0758 in. 00 .

2ARARARARAR

1ARAR144

4ARARARARARARARARARARARARARARARARARARARARARARARNP1

4ARARARARARARARARARARARARARARARARARARARARAR

2-27

Page 40: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &INDEX DESCRIPTIONNUMBER PART NUMBER 1 2 3 4 5 6 7

UNITSPER ASSY

1I

73342P16E73342P16F

9 *731559-41 26240

9-42 t73340CL A

73340CL B73340CL C73340PlD73340P1E73340P1F73340P5A73340P5B73340P5C73340P6D73340P6E13340P6F73340P10A73340P10B73340P10C73340P1lD73340P11E73340P11F73340P15A73340P15B73340P15C73340P16D73340P16E73340P16F

9 *731539 t24919CL A

24919CL B24919CL C24919PlD24919P1E24919P1F

9 24919P5A24919P5B24919P5C24919P6D24919P6E24919P6F24919P10A24919P10B24919P10C24919PllD

,.' 24919P11E24919P11F24919P15A24919P15B24919P15C24919P16D24919P16E24919P16F

9 *249209 264489 t51894CL A

51894CL B51894CL C51894PlD

Linkpin Assembly - 1.0758-1.0761 in. 00 .Linkpin Assembly. 1.0761-1.0764 in. 00 .

Linkpin - Partially intersected .. Screw. Headlesssocket .500-20 NS thd x .250 in. long

(linkpin) .Linkpin Assembly - Fully intersected (for usewith Part

No. 106965) . 1.0595-1.0598 in. 00 .Linkpin Assembly - 1.0598-1.0601 in. 00 .Linkpin Assembly - 1.0601-1.0604 in. 00 .Linkpin Assembly -1.0604~l.0607 in. 00 .Linkpin Assembly - 1.0607-1.0610 in. 00 .Linkpin Assembly. 1.0610-1.0613 in. 00 .Linkpin Assembly - 1.0645-1.0648 in. 00 .Linkpin Assembly - 1.0648-1.0651 in. 00 .Linkpin Assembly - 1.0651-1.0654 in. 00 .Linkpin Assembly - 1.0654-1.0657 in. 00 .Linkpin Assembly - 1.0657-1.0660 in. 00 .Linkpin Assembly - 1.0660-1.0663 in. 00 .Linkpin Assembly - 1.0695-1.0698 in. 00 .Linkpin Assembly - 1.0698-1.0701 in. 00 .Linkpin Assembly. 1.0701-1.0704 in. 00 .Linkpin Assembly - 1.0704-1.0707 in. 00 .Linkpin Assembly - 1.0707.1.0710 in. 00 .Linkpin Assembly - 1.0710-1.0713 in. 00 .Linkpin Assembly - 1.0745-1.0748 in. 00 .Linkpin Assembly. 1.0748-1.0751 in. 00 .Linkpin Assembly - 1.0751-1.0754 in. 00 .Linkpin Assembly - 1.0755-1.0758 in. 00 .Linkpin Assembly - 1.0758-1.0761 in. 00 .Linkpin Assembly - 1.0761.1.0764 in. 00 ; .

Linkpin - Fully intersected .Linkpin Assembly - (for usewith Part No. 43924 linkrod

assembly) - 1.0594-1.0597 in. 00 (not applicableto AF engines) .

Linkpin Assembly - 1.0597.1.0600 in. 00 .Linkpin Assembly - 1.0600-1.0603 in. 00 .Linkpin Assembly - 1.0603-1.0606 in. 00 .Linkpin Assembly - 1.0606.1.0609 in. 00 .Linkpin Assembly. 1.0609-1.0612 in. 00 .Linkpin Assembly. 1.0644.1.0647 in. 00 .Linkpin Assembly - 1.0647-1.0650 in. 00 .Linkpin Assembly. 1.0650.1.0653 in. 00 .Linkpin Assembly - 1.0653-1.0656 in. 00 .Linkpin Assembly. 1.0656.1.0659 in. 00 .Linkpin Assembly - 1.0659-1.0662 in. 00 .Linkpin Assembly - 1.0694-1.0697 in. 00 .Linkpin Assembly - 1.0697-1.0700 in. 00 .Linkpin Assembly - 1.0700-1.0703 in. 00 .Linkpin Assembly - 1.0703-1.0706 in. 00 .Linkpin Assembly - 1.0706-1.0709 in. 00 .Linkpin Assembly - 1.0709-1.0712 in. 00 .Linkpin Assembly - 1.0744-1.0747 in. 00 .Linkpin Assembly - 1.0747-1.0750 in. 00 .Linkpin Assembly - 1.0750-1.0753 in. 00 .Linkpin Assembly. 1.0754-1.0757 in. 00 .Linkpin Assembly - 1.0757-1.0760 in. 00 .Linkpin Assembly - 1.0760-1.0763 in. 00 .

Linkpin (Not applicable to AF engines) .. Screw - .625-18 thd x .375 in. long (Iinkpin) .Linkpin Assembly. Intersected (for usewith Part No. 43924

linkrod assembly) - 1.0595.1.0598 in. 00 (notapplicable to AF engines) ' .

Linkpin Assembly - 1.0598-1.0601 in. 00 .Linkpin Assembly - 1.0601-1.0604 in. 00 .Linkpin Assembly - 1.0604-1.0607 in. 00 .

ARARNP1

4ARARARARARARARARARARARARARARARARARARARARARARARNP

4ARARARARARARARARARARARARARARARARARARARARARARARNP1

4ARARAR

2-28

Page 41: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

CRANKSHAFT AND CONNECTING RODS

.;

99

9

9

99

9-43

9-449-45

9-46

99-47

9

51894PIE51894PIF51894P5A51894P5B51894P5C51894P6D51894P6E51894P6F51894PI0A51894PI0B51894PI0C51894PllD51894PllE51894PllF51894P15A51894P15B51894P15C51894P16D51894P16E51894P16F*5177826240

t32818CL A

32818CL B32818CL C32818PlD32818PIE32818PIF

. 32818P5A32818P5B32818P5C32818P6D32818P6E32818P6F32818PI0A32818PI0B32818PI0C32818PllD32818PllE32818Pll F32818P15A32818P15B32818P15C32818P16D32818P16E32818P16F*3177626240

26240

166131ANI03907

106965

*106957t43924

43924Rl*43658

Linkpin Assembly - 1.0607-1.0610 in. 00 .Linkpin Assembly - 1.0610-1.0613 in. 00 .Linkpin Assembly - 1.0645-1.0648 in. 00 .Linkpin Assembly - 1.0648-1.0651 in. 00 .Linkpin Assembly - 1.0651-1.0654 in. 00 .Linkpin Assembly - 1.0654-1.0657 in. 00 .Linkpin Assembly - 1.0657-1.0660 in. 00 .Linkpin Assembly - 1.0660-1.0663 in. 00 .Linkpin Assembly - 1.0695-1.0698 in. 00 .Linkpin Assembly - 1.0698-1.0701 in. 00 .Linkpin Assembly - 1.0701-1.0704 in. 00 .Linkpin Assembly - 1.0704-1.0707 in. 00 .Linkpin Assembly - 1.0707-1.0710 in. 00 .Linkpin Assembly - 1.0710-1.0713 in. 00 .Linkpin Assembly - 1.0745-1.0748 in. 00 .Linkpin Assembly - 1.0748-1.0751 in. 00 .Linkpin Assembly - 1.0751-1.0754 in. 00 .Linkpin Assembly - 1.0755-1.0758 in. 00 .Linkpin Assembly - 1.0758-1.0761 in. 00 .Linkpin Assembly - 1.0761-1.0764 in. 00 .

Linkpin. (Not Applicable to AF engines) .Screw - Headless socket .500-20 thd x .250 in. long

(Iinkpin) .Linkpin Assembly - (for use with Part No. 43924 linkrod

assembly) - 1.0595-1.0598 in. 00 (Not Applicableto AF engines) .

Linkpin Assembly - 1.0598-1.0601 in. 00 .Linkpin Assembly - 1.0601-1.0604 in. 00 .Linkpin Assembly - 1.0604-1.0607 in. 00 .Linkpin Assembly - 1.0607-1.0610 in. 00 .Linkpin Assembly - 1.0610-1.0613 in. 00 .Linkpin Assembly - 1.0645-1.0648 in. 00 .Linkpin Assembly - 1.0648-1.0651 in. 00 .Linkpin Assembly - 1.0651-1.0654 in. 00 .Linkpin Assembly - 1.0654-1.0657 in. 00 .Linkpin Assembly - 1.0657-1.0660 in. OD .Linkpin Assembly - 1.0660-1.0663 in. 00 .Linkpin Assembly - 1.0695-1.0698 in. 00 .Linkpin Assembly - 1.0698-1.0701 in. 00 .Linkpin Assembly - 1.0701-1.0704 in. 00 .Linkpin Assembly - 1.0704-1.0707 in. 00 .Linkpin Assembly - 1.0707-1.0710 in. 00 .Linkpin Assembly - 1.0710-1.0713 in. 00 .Linkpin Assembly - 1.0745-1.0748 in. 00 .Linkpin Assembly - 1.0748-1.0751 in. 00 .Linkpin Assembly - 1.0751-1.0754 in. 00 ; .Linkpin Assembly - 1.0755-1.0758 in. 00 .Linkpin Assembly - 1.0758-1.0761 in. 00 .Linkpin Assembly - 1.0761-1.0764 in. 00 .

Linkpin (Not applicable to AF engines) .Screw - Headless socket .500-20 thd x .250 in long

(linkpin) .Screw - Headless socket .500-20 NS thd x .250 in. long

(Iinkpin) .Lock - Linkpin lower (supersedes No. 119296) .Bolt - 0.3125-24 thd x 0.560 in. long (Iinkpin locks; super-

sedes No. 126375; use No. MS20995N51, composition304, condition A, dia 0.051 in., lockwire) .

Linkrod Assembly - (for use with Part No. 73340, 73341, &73342 linkpin assembly; supersedes No. 43924) .

Linkrod - (for use with Part No. 106965 linkrod assembly) .Linkrod Assembly - (for use with Part No. 24919, 32818 &

51894 linkpin assembly) .Linkrod Assembly same as 43924 only 1.049-1.053 in. undersize ..

Linkrod - (for use with Part No. 43924 linkrod assembly) .....

ARARARARARARARARARARARARARARARARARARARARNP

4ARARARARARARARARARARARARARARARARARARARARARARARNP

14

4

12NP12ARNP

2-29

Page 42: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

CRANKSHAFT AND CONNECTING RODS

UNITSPER ASSY

Cylinder Assembly Complete - Front (for -4 & -7M2). . . . . . . . . . 7Cylinder Assembly Complete - Rear (for -4 & -7M2). . . . . . . . . . . 7

9-48 t44689

44689P109-49 t84251

84251P584251P10

9-50 14634

9-51 t195860195860M1195860M2195860M4195860M6195860M8195860M10195860M12195860M14195860M16195860M 18195860M20195860P10195860R1

195860R2

.....> 195860R3

AS195860R4

9-52 MS24665-370

Bushing - 1.051 ID x 1.189 OD x 1.234 in. long (Iinkrodknuckle pin; for use with Part No. 43924 Iinkrodassembly) .

Bushing same as 44689 only .010 in. oversize .Bushing - 1.375 ID x 1.5348 OD x 1.750 in. long (Iinkrod

piston pin) .Bushing same as 84251 only .005 in. oversize .Bushing same as 84251 only .010 in. oversize .Dowel - Straight .163 dia x .234 in. long (Iinkrod

pistonpin bushing) .Bearing - Masterod (supersedes No. 83320 or 198220) .Bearing same as 195860 only .001 in. undersize .Bearing same as 195860 only .002 in. undersize .Bearing same as 195860 only .004 in. undersize .Bearing same as 195860 only .006 in. undersize .Bearing same as 195860 only.008 in. undersize .Bearing same as 195860 only .010 in. undersize .Bearing same as 195860 only .012 in. undersize .Bearing same as 195860 only .014 in. undersize .Bearing same as 195860 only .016 in undersize .Bearing same as 195860 only .018 in undersize .Bearing same as 195860 only .020 in undersize .Bearing same as 195860 only .010 in. oversize .Bearing same as 195860 only .010 in. oversize & .002 in.

undersize .Bearing same as 195860 only .010 in. oversize & .006 in.

undersize .Bearing same as 195860 only .010 in. oversize & .004 in .

undersize .Bearing same as 195860 only .010 in. oversize & .008 in.

undersize I.D .Cotterpin-corrosion resistant 0.118-0.112 in. dia x 1.000 in.

long. (Masterod bolts; supersedes Part No. 22118, 59297 &AS123806) .

CYLINDERS AND PISTONS

1AR1ARAR14ARARARARARARARARARARARARARARARAR

8

! .

ATTACHING PARTS

Washer - .406 ID x .5781 OD x .125 in. thick (cylinderFlange) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 224

Nut-Plain .562 Hexagon head x .375-24 NF thd x .375 in.thick (cylinder flange; for -4 & -7M2) . . . . . . . . . . . . . . . . 224

Palnut .562 hexagon x.375-24 PD (cylinder flange; for-4and -7M2; supersedes No. AAF356-624) . . . . . . . . . . . . . . 224

- - - - * - - - -Cylinder Assembly-Front (for -4 & -7M2) .Cylinder Assembly same as 153071 only includes .030

in. undersize exhaust valve guide . . . . . . . . . . . . . . . . . ARCylinder Assembly-Rear (for -4 & -7M2) . . . . . . . . . . . . . . . . 1Cylinder Assembly same as 153072 only includes .030

in. undersize exhaust valve guide . . . . . . . . . . . . . . . . . ARHead-Front cylinder (supersedes No. 91735 or 97283). . . . . NPHead-Rear cylinder (supersedes No. 91736 or 07284). . . . . . NPBarrel and Fin assembly front & rear cylinder for -4 &

-7M2 '. . . . . . . . . . . 1Barrel and Fin assembly same as 98874 only :020 in:

oversize. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A R

.2-30

Page 43: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

2-31

. ,"'.:r ...."..• ,'"

.!i;~:'

,_ ..... 15

I

~14

•-r-A' .•.-2016

13-~/

,

~@

I'ifl)I ....~

.2 3 I

. 4

Figure 10 .. Cylmders Pi t, sons ad', n Plstonrings

52 ~@

47 28--~51=t--@ ~~44-48

~~P~-[4546 50 49

17

~J

27

/

13-if

53~

Page 44: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

.',,", ~FIGURE &

UNITSINDEX DESCRIPTIONNUMBER PART NUMBER 1 2 3 4 5 6 7 PER ASSY

CYLINDERS AND PISTONS

10

10

10-6

10-7

10-8

10-9

10

10-10

10-11

2-32,

9887398873P209887298872P20t3254432544P332544P532544P10t113651113651P5113651P20113651P10144355144355P5144355P10144355P20144355P30144355P40144355P50t127422127422M30127422R1

127422R2

127422R3

127422R4

127422R5

127422R6

127422R7

127422R8

127422R9

127422P3127422P5127422P10127422P20127422P30127422P40127422P50127422P60t57580

57580P257580P2P15W

57580P557580P5P15W

57580P1057580P1557580P15Wt5758157581P257581P2P15W

57581P5

Barrel-cylinder (For use on -4 & -7M2) .Barrel-cylinder same as 98873 only .020 in. oversize .Fin-muff (For use on -4 & -7M2) .Fin-Muff same as 98872 only .020 in. oversize .Guide-Intake valve .Guide same as 32544 only .003 in. oversize .Guide same as 32544 only .005 in. oversize .Guide same as 32544 only .010 in. oversize .Seat.1 ntake valve (supersedes No. 27592 or 114184) .Seat same as 113651 only .005 in. oversize .Seat sameas 113651 only 0.020 in. oversize .Seat same as 113651 only 0.010 in. oversize .Seat-Exhaust valve (supersedes No. 17930 or 50279) .Seat same as 144355 only .005 in. oversize .Seat same as 144355 only .010 in. oversize .Seat same as 144355 only .020 in. oversize .Seat same as 144355 only .030 in. oversize .Seat same as 144355 only .040 in. oversize .Seat same as 144355 only .050 in. oversize .Guide Assembly-Exhaust valve .Guide Assembly same as 127422 only .030 in. undersize .Guide Assembly same as 127422 only .030 in. undersize

on 10 & .003 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .005 in. oversize on OD .Guide Assembly same as 127422 only.030 in. undersize

on ID & .010 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .020 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .030 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .040 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .050 in. oversize on OD .Guide Assembly same as 127422 only .030 in. undersize

on ID & .060 in. oversize on OD .Guide same as 127422 only .030 in. undersize on 10,

.100 in. oversize on OD and .075 in. oversize flangeth ickness .

Guide Assembly same (IS 127422 only .003 in. oversize .Guide Assembly same as 127422 only .005 in. oversize .Guide Assembly same as 127422 only .010 in. oversize .Guide Assembly same as 127422 only .020 in. oversize .Guide Assembly same as 127422 only .030 in. oversize .Guide Assembly same as 127422 only .040 in. oversize .Guide Assembly same as 127422 only .050 in. oversize .Guide Assembly same as 127422 only .060 in. oversize .Bearing-Sleeve .685 10 x .878 OD x .860 in. long (valve

rocker shaft short) .Bearing same as 57580 only .002 in. oversize .Bearing same as 57580 only .002 in. oversize on OD &

.015 in. oversize on width .Bearing same as 57580 only .005 in. oversize .Bearing same as 57580 only .005 in. oversize on OD &

.015 in. oversize on width .Bearing same as 57580 only .010 in. oversize .Bearing same as 57580 only .015 in. oversize .Bearing same as 57580 only .015 in. oversize on width .Bearing-Sleeve, valve rocker shaft long .Bearing same as 57581 only .002 in. oversize : .Bearing same as 57581 only .002 in. oversize on OD &

.015 in. oversize on width .Bearing same as 57581 only .005 in. oversize .

1AR1AR1ARARAR1ARARAR1ARARARARARAR1ARARARARARARARARAR

ARARARARARARARARAR2ARARAR

ARARARAR2ARARAR

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FIGURE &INDEXNUMBER

DESCRIPTIONPART NUMBER 1 2 3 4 5 6 7

CYLINDERS AND PISTONS

T.O. 2R-R2000-24

UNITSPER ASSY

59417P359417P559417P1559417P2059417P30

10-19 12669

10-20 34137

10-21 t22673P4

22673P8

e 22673P1210-22 t44046

44046P1044046P20

10-23 t4396443964P20

10-24 t12317P4

12317P812317P12

10-12

10-13

10-141010-15

10-16

10.17

10-18

10

57581P1057581P1557581P15Wtl361813618P413618P813618P1213618P3013618P62t332403332403P10332403P20332403P30332403P40332403P5044509*3366325336

33334

t13940P4

13940P813940P12tMS9018-01

MS9018-02MS9018-03MS9018-04MS9018-09MS9018-10t59417

Bearing sameas 57581 only .010 in. oversize .Bearing sameas 57581 only .015 in. oversize .Bearing sameas57581 only .015 in. oversize on width .Connector-Pushrod cover .Connector sameas 13618 only .004 in. oversize .Connector sameas 13618 only .008 in. oversize .Connector sameas 13618 only .012 in. oversize .Connector sameas 13618 only .030 in. oversize .Connector sameas 13618 only .062 in. oversize .Linear Flanged-Exhaust port (supersedesNo. 43905) .Linear sameas 332403 only 0.010 in. oversize .Linear sameas 332403 only 0.020 in. oversize .Linear sameas 332403 only 0.030 in. oversize .Linear sameas332403 only 0.040 in. oversize .Linear sameas 332403 only 0.050 in. oversize .Pipe Assembly-Cylinder head oil drain .

Pipe-Cylinder head oil drain .. Support-Sparkplug conduit at cylinder head oil

drain pipe .Fitting-Cylinder head oil drain pipe (use antiseize

compound specification MIL-A-907D on threadedfittings) .

Stud-Plain .250-20-28 thd x 1.062 in. long (deflectorfastening: use (4) units for rear cylinders: use (1)unit for intake pipe pn all front cylinders) .004 in.oversize .

Stud sameas 13940 only .008 in. oversize .Stud sameas 13940 only .012 in. oversize .Insert-Helical-coil corrosion resistant steel 18 M/M-

1.5 M/M x .0675 in: long (sparkplug: supersedesNo. 94715, 119589,464772; for usewith cyl-inder heads incorporating helical coil inserts) .

Insert sameas MS9018-01 only 0.003 in. oversize .Insert sameasMS9018-01 only 0.005 in. oversize .Insert sameasMS9018-01 only 0.010 in. oversize .Insert sameasMS9018-01 only 0.015 in. oversize .Insert sameasMS9018-01 only 0.010 in. oversize .Insert-Screw thread sparkplug (replaces No. 16715:

for usewith cylinder headsprior to Part No. 91735&91736)(Service fix for cylinder heads87511'&87512 when sparkplug hole requires helical-coil-insertover .015 in. oversize) .

Insert sameas59417 only .003 in. oversize .Insert sameas59417 only .005 in. oversize .Insert sameas59417 only .015 in. oversize .Insert sameas59417 only .020 in. oversize .Insert sameas59417 only .030 in. oversize. : .Insert-Flanged 1/4-2010 x 7/16-1400 x 7/16

in. long (cylinder head deflector: all rear cylinders) .....Stud-1/4-28 NF thd x 1 3/8 in. long (deflector fast-

ening at inter ear oil drC!inpipe; all rearcylinders) .

Stud-Plain .250-20-28 thd x 1.656 in. long (deflectorfastening; all front cylinders) .004 in. oversize .

Stud sameas22673 only .008 in. oversize .Stud sameas22673 only .012 in. oversize .Coupling Assembly-Front cylinder intake pipe .Coupling Assembly sameas44046 only .010 in. oversize .Coupling Assembly sameas44046 only .020 in. oversize .Coupling-Intake pipes (all rear cylinders) .Coupling sameas43964 only .020 in. oversize ; .Stud-Plain .3125-18-24 thd x 1.312 in. long (exhaust

stack) .004 in. oversize .Stud sameas 12317 only .008 in. oversize .Stud sameas 12317 only .012 in. oversize .

ARARAR2ARARARARAR1ARARARARAR1NP1

2

6ARAR

2ARARARARAR

2ARARARARAR2

2

1ARAR1ARAR1AR1ARAR

2.33

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T.O. 2R-R2000-24

FIGURE &INDEX DESCRIPTION UNITS

NUMBER PART NUMBER 1 2 3 4 5 6 7 PER ASSY. -"-

./

10-25

10-26

10-27

10-28

10-29

10

10-30

10-31

10-32

10-33

" 10-~4

i0135

10-36

10-37

10-38

10-3910-4010-41

10-4210-43

10

10-44

1010-45

10-46

10-47

2-34

9074

MS27151-13

t71056P4

71056P871056P1271056P62t7772377723P377723P5253848

77975

48724

77688

135228

91766

10078

91767

340932

t4417044710M544770M1044770M1544770M2044770M3034755

14248428464158175

3233197126

*127918

127916

*121648t1147711477P111477P211477P4127599

9294

CYLINDERS AND PISTONS

Nut-Plain .438 Hexagon head x .250-28 thd x .188 in.thick (intake pipes; all front cylinders) .

Palnut-.438 in. hexagon x .250 -28PD (Intake pipecoupling stud; supersedes No. AAF 356-428) .

Stud-Plain .250-28 & .3i25-18 thd x 1.250 in. long(rockerbox covers) .004 in. oversize ........•......

Stud same as 71056 only .008 in. oversize .Stud same as 71056 only .012 in. oversize .Stud same as 71056 only .062 in. oversize .

Shaft-Valve rocker " .Shaft same as 77723 only .003 in. oversize .Shaft same as 77723 only .005 in. oversize .Cap-Valve rocker shaft (use No. MS20995 wire: All loca-

tions except NO.8 Cyl and outer intake side ofrear cyls.) Use (4) units on all front cyls exceptNO.8. Use (3) units all rear cyls. Supersedes No.48724 at locations indicated. . . . . . . . . . . . .. . ..

Gap-Valve rocker Shaft (front cylinder NO.8: use No.MS2Q995 wire: supersedes No. 37620; for use withPart No. 126717 cylinder assembly complete) .

Cap-Valve rocker shaft (use No. MS20995 wire: All rearcyls, intake rockerbox outer side) .

Gasket-7/8 10 xl 1/1600 x i/16 in. thick (valve rockershaft cap). .. . .

Washer-.914 ID x 1.699500 x .234 in. thick (exhaustvalve spring lower: for use with Part No. 127422guide assembly; supersedes No. 89304) .

Spring-1/688 10 x .192 in. dia Wire (exhaust valve outer:supersedes No. 59987 or 82964; for -4 & -7M2) .....

Spring-1.688 10 x .203 in. dia Wire (intake valve outer:for -4 & -7M2) .

Sprihg-1.609 10 x .170 in. dia Wire (valve inner; super-sedes No. 59986 or 82965). . . . . . . .. . .

Washer-.979 10 x 2.010 00 x .625 in. thick (exhaust valvespring upper; replaces No. 127951) .

ValveloCk-Exhaust. . . . . . . . . . . . . . .. . .Valvelock same as 44770 only .005 in. undersize. . . .. . .. ..Valvelock same as 44770 only .010 in. undersize .Valvelock same as 44770 only .015 in. undersize. . . . . .Valvelock same as 44770 only .020 in. undersize. . . . . . .Valvelock same as 4~770 only .030 in. undersize .Washer-.l9i 10 x 1.69200 x .234 in. thick (intake valve

spring lower) .Washer-Intake valve spring upper (supersedes No. 31853) .Valvelock-Intake .

Valve-Exhaust (for use with PN 127422 bronze guide (sup-ersedes 8X Valve, PN 50724). . . . . . . . . .Valve-Intake. . . . . . . . . . . . . . . . .Insert-No. 10-32 10 x .375-2400 x .500 in. long (bayonet

type thermocouples; for use on cylinders No.1 & 3on Air Force engines only) . . . .

Rocker Assembly Complete-Front intake & rear exhaustvalve. . . . . . . . . . . . .. .... ... . . .. ..

Rocker Assembly-Front intake & rear exhaust valve(super5edes No. 44051) .. . . . . . ..

Rocker-Valve .Cup-Push rod ball rocker.. . .Cup same as 11477 only .001 in. oversize. . . . . . .. ..Cup same as 11477 only .002 in. oversize. . . . . . .. ..Cup same as 11477 only .004 in. oversize. . . . . . .. . ..

Screw Assembly-Valve clearance adjusting (supersedesNo.9514) . . . . . . . . . . . . . . . . . . .. . ....

Nut-19/32-24 thd Special (valve clearance adjustingscrew) . . . . . . . . . . . . . . . . . . . . . . .. . ....

6ARARAR2ARAR

4

2

4

1

1

1

2

12ARARARARAR112

11

NP1NP1ARARAR

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T.O. 2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7_ .-CYLINDERS AND PISTONS

10

10-48

1010-49

10-50

10-51

10-52

10-53

10-54

10

10-55

10-56

10-57

10-58

10-59

10-60

10-6110-62

10-63

10-64

*127919

127917

*121647tl147711477P111477P211477P4127599

9294

68C37326-7

68C37326-9

68C37326-11

68C37326-13

68C37326-15

68C37326-17

68C37326-2168C37326-2368C37326-25MS20913-1S

MS51958-60

,~tl66313

tl19575P2W119575P3W119575P4Wtl10591P2W

110591P4W

tl10591P2W110591P4Wtl25234P2W

t125234P2W

125234P4W125234P4W

107614107614

tl07615107615P10107615

Rocker Assembly Complete-Rear intake & front exhaustvalve .

Rocker Assembly-Rear intake & front exhaust valve;supersedes No. 44052 .

Rocker-Valve .Cup-Push rod Ball rocker .Cup same as 11477 only .001 in. oversize .Cup same as 11477 only .002 in. oversize .Cup same as 11477 only .004 in. oversize .

Screw Assembly-Valve clearance adjusting (supersedesNo.9514) .

Nut-19/32-24 thd Special (valve clearance adjustingscrew) .

Spacer-Brass-Chamfered 0.704 ID x 1.094 OD x 0.0835inch thick (rocker shaft; replaces Nos. 252804 & 83484) ...

P8W Spacer same as 68C37326-7 only 0.008 in. oversizein width .

PlOW Spacer same as 68C37326-7 except 0.010 inch over-size in width .

P15W Spacer same as 68C37326-7 only 0.015 inch over-size in width .

P25W Spacer same as 68C37326-7 only 0.025 inch over-size in width .

P35W Spacer same as 68C37326-7 except 0.035 inch over-size in width .

Spacer - same as 68C37326-7 except 0.005 inch oversize .Spacer - same as 68C37326-7 except 0.020 inch oversize .Spacer - same as 68c37326-7 except 0.030 inch oversize .Plug-Square head x 125-27 pipe (cylinder head; use for

shipping spares only)(supersedes No. 17346) .Screw-machine, pan head, cross recessed x .190-32 thd x

.312 in. long (cancel on cylinders having head typethermocouples; supersedes No. AN 520-10-5) .

Piston-6.52: 1 (replaces No. 142953)(See T.O. 2R-R2000-23; para. 6-422) .

PISTON RING FOR USE IN ENGINES WITHPLAIN STEEL CYLINDERS

Piston ring-Compression vee; .002 in. oversize on width .Pistonring same as 119575 only .003 in. oversize on width .Pistonring same as 119575 only .004 in. oversize on width .Pistonring-Compression vee (for use in engines with chrome

plated Cylinder.). .Pistonring same as 110591 only .004 in. oversize on width

(for use in engines with chrome plated cylinder) .Pistonring-Compression vee, .002 in. oversize on width .Pistonring same as 110591 only .004 in. oversize on width .Pistonring-Compression vee, .002 in. oversize width (for

use in engines with chrome plated cylinder) .Pistonring-Compression vee tapered, .002 in. oversize on

width .Pistonring same as 125234 only .004 in. oversize on width .Pistonring same as 125234 only .004 in. oversize on width

(for use in engines with chrome plated cylinder) .Pistonring-Dual oil control .Pistonring-Dual oil control (for use in engines with chrome

plated cyfinder) .Pistonring-Oil scraper .Pistonring same as 107615 only .010 in. oversize .Pistonring-Oil scraper (for use in engines with chrome

plated cylinder) .

NP1NP1ARARAR1

2

ARARARARARARARAR

1

1

1ARAR

AR1AR2

1ARAR2

21AR

2-35i

.J

Page 48: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &UNITSINOEX- DESCRIPTION

PER ASSYNUMBER PART NUMBER 1 2 345 6 7

CYLINDERS AND PISTONS

10-65

10-6610

10-67

10-68

11-1

1111-211-311-4

11

11

1111-51111

11

11

1111-61111

11

11

1111-71111

11

11-8

11-9

11-10

11-11

2.36

t3587635876P535875351136

207045

103672

402987

*33645336412314498226

48164

t23145

23145P15*57383573822314498226

48164

t23145

23145P15*44594445912314498226

48164

t23145

23145P15*44595445922314498226

48164

t23145

23145P15282992

282991

32735

559886

Piston pin .Pistonpin same as 35876 only .005 in. oversize .Snapring - 10405 00 x .093 in. thick (pistonpin) .Bushing - Rocker (service fix; for use with reworked

rocker assembly) .Adapter - Thermocouple sensitive element connection

(cylinder NO.2, 8 & 14-7M2 only) .Cap, Thermocouple adapter (cylinder No.2, 8 & 14-

-7M2 only) .

CYLINDER PUSH RODS, INTAKE PIPES, ANDROCKERBOX COVERS

Packing - Preformed 4.625 10 x .113 in. dia Round (cylinderbarrel to main crankcase; supersedes No. 14438) .

Pushrod Assembly - Front intake .Push rod - Front intake .Ballend - Push rod .Spacer - Chamfered .250 ID x .5445 00 x .140 in. thick

(pushrod) .Spacer - .25010 x .5445 00 x .055-.065 in. thick (pushrod;

for optional procurement) .Spacer - .25010 x .5445 00 x .095-.105 in. thick (pushrod;

for optional procurement) .Spacer same as 23145 only .015 in. oversize .Push rod Assembly - Front exhaust .

Push rod - Front exhaust .Ballend - Push rod .Spacer - Chamfered .250 ID x .5445 00 x .140 in. thick

(push rod} .Spacer - .25010 x .5445 00 x .055-.065 in. thick (pushrod;

for optional procurement) .Spacer - .25010 x .5445 00 x .095-.105 in. thick (pushrod;

for optional procurement) .Spacer same as 23145 only .015 in. oversize .Push rod Assembly - Rear intake .

Push rod - Rear intake .Ballend - Push rod .Spacer - Chamfered .250 10 x .5445 00 x .140 in. thick

(pushrod) .Spacer - .25010 x .5445 00 x .055-.065 in. thick (pushrod;

for optional procurement) .Spacer - .250 ID x .5445 00 x .095-.105 in. thick (push rod ;

for optional procurement) .Spacer same as 23145 only .015 in. oversize .Pushrod Assembly - Rear exhaust .

Push rod - Rear exhaust. " .Ballend - Pushrod .Spacer - Chamfered .250 lOx .5445 00 x .140 in. thick

(pushrod) .Spacer - .250 ID x .5445 00 x .055-.065 in. thick (pushrod;

for optional procurement) .Spacer - .25010 x .5445 00 x .095-.105 in. thick (pushrod;

for optional procurement) .Spacer same as 23145 only .015 in. oversize .Cover Assembly - Push rod (supersedes No. 147300; for use

with Part No. 114013 washer) .Cover Assembly - Push rod (supersedes No. 147302; for use

with Part No. 114013 washer) .Ferrule - .9305 OOx .032 Wall x .875 in. long (pushrod

cover) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Packing - 1.005 10 x 1.28500 x 0400 in. thick (pushrod

cover: for spares procurement; supersedes Part No.161701, 121839 or 121834) _ ..

14AR28AR1

1

14NP12

2

14

14ARNP12

2

14

14ARNP12

2

14

14ARNP12

2

14

14AR14

14

2

56

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T.O. 2R-R2000-24

. }

12- I

4--0~-3

12

10-l'5l~-14

ll-~

&- 34-0

Hl

1-~

~-53

0-52

60 61I

~@

45-\

_-59e-55

Q-56

26 21

Figure 11. Cylinder Pushrods, Intake Pipes, and Rockerbox Covers

2-37

Page 50: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2 345 6 7 PER ASSY

11-12

11-13

11-14

11-15

11-16

11-1711-1811-1911-20

1111

11-21

11-2211,2311-2411-25

1111

11-26

11-2711-2811-2911-30

1111

11-31

11-32

11-3311-34

11-35

11-36

11-37

2-38

9265

114013

14096

88962

*96324

96316963153833634079

158188158189

*96560

96556963153833634079

158188158189

*96561

96557963163833634079

158188158189

96314

*96562

94927MS35769-11

36639

94926

3H-12-4800

CYLINDER PUSHRODS, INTAKE PIPES, ANDROCKERBOX COVERS

Nut - 1 15/32 Hexagon head x 1 3/8-20 NS thd x 27/32 in.thick (pushrod packing) (use No. MS20995 wire) .

Washer - 1.009 ID x 1,230 OD x .210 in. thick (pushrod tubeseal) .

Packing - 1.015 ID x 1.281 OD x .125 in. thick (lower pushrodlube) .

Gasket - Rockerbox cover (Only gaskets made of AMS32320.030 in. to 0.040 in. thick will be used on Air Forceengines or cylinders. Use colloidal graphite specific-ation MIL-G-26548 on gasket surfaces at assembly) .

Cover & Connection Assembly-Rockerbox (between cylindersNO.4 & 6, 10 & 12,5 & 7,9 & 11; for use with engineshaving Part No. 150246, 156075 or 164448 crankcaseassembly) .

Cover-Rockerbox front exhaust & rear intake .Cover-Rockerbox front intake & rear exhaust .Hose-Cylinder head oil drain .Clamp Assembly-1.125 in. ID Hose (cylinder head oil

drain hose) .Screw-Cylinder head oil drain hose clamp .Nut-Fibre .190-24 thd x .266 in. thick Special

(cylinder head oil drain hose clamp screw) .Cover & Connection Assembly-Rockerbox (between cylinders No.

6 & 8; for use with engines having Part No. 150246,156075 or 164448 crankcase assembly) .

Cover-Rockerbox (cylinder NO.8 exhaust) .Cover-Rockerbox (cylinder NO.6 intake) .Hose-Cylinder head oil drain .Clamp Assembly-1.125 in. ID Hose (cylinder head oil drain

hose) .Scew-Cylinder head oil drain hose clamp .Nut-Fibre .190-24 thd x .266 in. thick Special

(cylinder head oil drain hose clamp screw).Cover & Connection Assembly-Rockerbox (between cylin-

ders NO.8 & 10; for use with engines having PartNo. 150246, 156075 or 164448 crankcase assembly) .

Cover-Rockerbox (cylinder NO.8 intake) .Cover-Rockerbox (cylinder No. 10 exhaust) .Hose-Cylinder head oil drain .Clamp Assembly-1.125 in. ID Hose (cylinder head oil

drain) 'Screw-Cylinder head oil drain hose clamp .Nut-Fibre .190-24 thd x .266 in. thick Special

(cylinder head oil drain hose clamp screw) .Cover-Rockerbox (use (14) units on engines having Part No.

150246, 156075 or 164448 crankcase assembly: intakecylinders No. 1,2,3,11,12,13, & 14; exhaustcylinders No. 1,2,3,4,5, 13, & 14) .

Manifold & Covers Assembly-Rocker oil drain (for -4 &-7M2; for use with engines having Part No. 150246,156075 or 164448 crankcase assembly) .

Manifold-Rocker oil collecting .Gasket-.633 ID x .875 OD x .094 in. thick (rocker oil

collecting manifold plug; supersedes No. AN900-10) .Plug-.812 Hexagon head x .625-18 NF thd x .688 in. long

(rocker oil collecting manifold) .Elbow-.750 in. ID Hose (rocker oil collecting manifold to

rear rockerbox covers) .Hose-.750 in. ID bulk (rocker oil collecting manifold to

front rockerbox covers, Mfg Code 43999; supersedesP & W Part No. 55346; cut Part No. 3H-12-4800 hose2.500 inch length in accordance with T.O. 2R-R2000-23 figure 8.20 .

5628

56

28

NP111

21

1

NP111

21

NP111

21

1

28

NP1

2

1 ft.

Page 51: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE & .UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

CYLINDER PUSH RODS, INTAKE PIPES, ANDROCKERBOX COVERS

:A.,

11-38

11-3911-40

11-4111-4211-43

11-44

11-45

11-46

11-47

11-481111-49

11-5011-51

11-52

11-53

11

11

11-5411-5511-5611-5711-58

11-59

11-60

11-61

1212-1

1212121212

12

34079

158188158189

96315963i6NAS620-416L

156822

MS27215-2

MS29509-1MS29509-363034560-19

63034560-20

MS17840-1

483104830969034800-3

8323803

48315

48316

121830

121831

4397180380290764MS2951~-139

8323

MS35276-264

97126

*148048114672

*114671114667114670114668MS20470A03-4

114669

Clamp Assembly-1.125 in. 10 Hose (rocker oil drainmanifold elbows & hoses) .Screw-Cylinder head oil drain hose clamp .Nut.Fibre .190-24 thd x .266 in. thick Special

(cylinder head oil drain hose clamp screw) .Cover-Rockerbox (exhaust cylinder NO.9) .Cover-Rockerbox (intake cylinder No.7) .

Washer-plain .255 lOx .468 00 x .032 in. thick (rockerboxcovers; supersedes No. 12156) ....................•

Nut-non-metalic lock .438 hexagon x .250-28 thd x .312thick (rockerbox covers; supersedes 12856; replacesMS21044N4) .

Plug-18 m/m x 1.5 m/m pitch (cylinder dehydrator super-sedes No. AN4062-2) .

Plug-Vented 18 m/m x 1.5 m/m pitch .Plug-Non-vented 18 m/m x 1.5 m/m pitch .

Cover-exhaust port vented, (for use with engines preservedin a complete can) .

Cover-exhaust port non-vented (for use with engines pre-served in one half can) .

Gasket-.718 10 x .969 00 x .081 in. thick (sparkplug; super-sedes No. AN4027-1) .

Pipe Assembly-Front intake long .Pipe.Front cylinder intake 10:1g .

Pipe Assembly-Front Intake Long (No.8 cylinder only-super-sedes Part No. 48310 this location) .Nut-2 3/4-12thd xI 1/32 in. thick (intake pipe to cylinder) .Nut-2 3/4-12NS thd x 2 in. thick (intake pipe to collector;

use No. ASI00029 wire) .Packing-2.375 10 x 2.625 00 x .406 in. thick (front intake

pipe to blower) .Ring-2.331 10 x 2.573 00 x .155 in. thick (front intake

pipe to blower packing) .Spacer-Front intake pipe to collector case (for spares

procurement) '.' .Spacer-Front intake pipe to collector case (for spares

procurement) .Pipe-Rear intake ; ' .Nut-2 3/4-12NS thd x 2 in. thick (rear intake pipe to blower) .Packing-Rear intake pipe to blower .Packing-I ntake pipe to cylinder .Packing, Intake Pipe "0" Ring 102.175 in. width .103 in.

(Replaces Seal Part No. 99334) .Nut-2 3/4-12thd x 1 1/32 in. thick (rear intake pipe to

cylinder) .Screw-machine, drilled ,fillister head, slotted, .190-32

thd x .625 (supersedes Nos. 21027 and AN520-10-5; cyiinder head thermocouple wire clip) .

Insert-Cylinder head thermocouple wire clip screw .

DEFLECTORS

Deflector Assembly Complete .Oeflector-Assy Front Inter Ear, NO.4, 6,10 & 12 (-4 & -6

Engines) .Deflector-Front cylinder inter ear .Tube-I nter ear front deflector .Plate-Front cylinder inter ear baffle .Brace-I nter ear deflector left .River-Brazier head .095 dia. x .218 in. long (deflect-

or; supersedes No. 58328) .Brace-I nter ear deflector right .

81

84

842ARAR14

AR2861

11

7

7

7

777714

14

7

11

NP4NP111

351

2.39

Page 52: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

mill

40IIllll(B -j

47

41I~_.

39I(0)

38~----l

46

.. 12 DeflectorsFIgure .

1-429-l12

~_. 45

101115293233

~35

2-40

Page 53: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7 .

DEFLECTORS

1212121212-2

1212121212

121212121212-3

12121212

121212

1212-4

121212121212

12

1212

1212

1212

12-5

12121212-6

121212121212

8170991481345328171166038605

*114671114667114670114668MS20470AD3-4

11466981709914813543281711128565

*100414*128566*100415MS20470AD3-4

90093HZA008-001MS20426AD4-5

35432120412

*100414*120411100415916168171135432

91481

MS20470AD3-4

90093

HZA008-001MS20426AD4-5

35432MS20470AD3-4

128567

*128568382634764646093

*46086*46089*46090460919161691481

Clip-Deflector grommet .Rivet-.094 dia x .190 in. long Special (deflector) .Washer-.1285 10 x .15000 x .040 in. thick (deflector) .Rivet-.191 dia x .317 in. long (grommet clip) .

Deflector Assy Front Inter Ear, NO.2 & 14 (-4 Engines)(Supersedes Part No. 114672) .

Deflector-Front cylinder inter ear '1'

Tube-I nter ear front deflector .Plate-Front cylinder inter ear baffle .Brace-I nter ear deflector left ......•...................Rivet-Brazier head .095 dia x .218 in. long (deflector; super-

sedes No. 58328) .Brace-I nter ear deflector right .Clip-Deflector grommet .Rivet-.094 dia x .190 in. long Special (deflector) .Washer-.1285 10 x .250 00 x .040 in. thick (deflector) .Rivet-.191 dia x .317 in. long (grommet clip) .

Deflector Assembly-Front cylinder inter ear cylinderNO.8; for -4 only) .

Deflector-Front inter ear. .Plate-Front cylinder , ..Tube'lnter ear deflector .Rivet-Brazier head .095 in dia. x .218 in. long

(deflector. supersedes No. 58328) .Washer-.250 10 x .051 in. thick (deflector reinforcing) .Spring-Dzus fastener, deflector (supersedes No. 35431) .Rivet-100o counter sunk head, aluminum alloy .125 dia

x .312 in. long (deflector; supersedes No. AS125290) ..Washer-.1285 10 x .25000 x .040 in. thick (deflector) ....

Deflector Assembly-Front cylinder inter ear (cylinder No.8: supersedes No. 95250) .Deflector-Front cylinder inter ear .Plate-Front cylinder inter ear deflector .Tube-Front cylinder inter ear deflector : .CI ip-Deflector .Rivet-.191 dia x .317 in. long (grommet clip deflector) .Washer-.1285 ID x .250 00 x .040 in. thick (inter

cylinder deflector front) .Rivet-.094 dia x .190 in. long Special (inter cylinder

deflector front) .Rivet-Brazier head .095 in. dia x .218 in. long (inter

cylinder deflector front) .Washer-.250ID x .051 in. thick (inter cylinder deflec-

tor front) .Spring-Dzus fastener, deflector (supersedes No. 35431) .Rivet-100o countersunk head, aluminum alloy .125 dia x

.312 in. long (deflector supersedes No. AS125290) .Washer-.1285 ID x .25000 x .040 in. thick (deflector) .Rivet-Brazier head .095 in. dia x .218 in. long (inter

cylinder deflector front; supersedes No. 58328) .....Plate Assembly-Inter ear deflector (front cylinder NO.8;

for -4 only) .Plate-Front inter ear deflector .Fastener-Dzus type, deflector .Washer-21/64 ID x 7/800 x .032 in. thick (deflector) .

Deflector Assembly-Rear cylinder inter ear (cylinders No.1,3,5,7,9,11, & 13) .

Deflector-1 nter ear rear .Bracket-Inter ear rear deflector right .Bracket-I nterear rear deflector left. .Tube-Inter ear rear deflector .Clip-Deflector grommet .Rivet-.094 dia x .190 in. long Special (deflector) .

1111

2NP111

3511111

1NP

. NPNP3222

44

1NPNP111

30

22

44

30

1NP22

7NPNPNP111

2-41

Page 54: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

DEFLECTORS

1

L

12

121212121212

12-7

221212

1212121212

1212121212

12

12

12-812121212121212

121212-9

1212

12121212

12

1212-10

1212121212

2-42

MS20470AD3-4

8171135432120414

*1204133826347646

46885

*468843826347646MS20470AD3-4

46883*468823543135432AS125291

46881*468803543135432AS125291

29945

219

85866*460864608946090460919161691481MS20470AD3-4

8171135432107749

*10774890093

107781107780107772143575

AS125721

3694246857

*468564687651819820"08HZA008-001

Rivet-Brazier head .095 in. dia x .218 in. long (deflec-tor; supersedes No. 58328) .

Rivet-.191 dia x .317 in. long (deflector) .Washer-.1285 10 x .25000 x .040 in. thick (deflector) .

Plate Assembly-Front inter ear deflector (cylinder NO.8:supersedes No. 95252) .Plate-Front inter ear deflector .Fastener-Dzus type .Washer-21/64 10 x 7/800 x .032 in. thick (dzus fast-

ener retaining) .Plate Assembly-Inter ear deflector (front cylinder No.

8) .Plate-Inter ear deflector (cylinder NO.8) .Fastener-Dzus type special deflector .Washer-21/64 ID x 7/8 OD x .032 in. thick (deflector) .Rivet-Brazier head .095 in. dia x .218 in. long (deflec-

tor; supersedes Nos. 58328 and AN455AD3-4) .Bracket Assembly-I nter ear deflector plate left .

Bracket-I nter ear deflector plate left .Spring-Dzus fastener No. 100-A (deflector) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-1000 Countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector) .Bracket Assembly-I nter ear deflector plate right .

Bracket-I nter ear deflector plate right .Spring-Dzus fastener No. 100-A (deflector) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-lOOo Countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector) ......•....... , .Grommet-.438 ID x 1.062 OD x .312 in. thick (deflector;

supersedes No. 50216) .Screw-Fillister head drilled .190-32 N F thd x .625 in. long

(deflector) .Deflector Assembly-Rear cylinder inter ear .

Deflector-Inter ear rear (supersedes No. 85865) .Bracket-I nter ear rear deflector right .Bracket-I nter ear rear deflector left .Tube-I nter ear rear deflector .Clip-Deflector grommet .Riveto.094 dia x .190 in. long Special (deflector) .Rivet-Brazier head .095 in. dia x .218 in. long (deflec-

tor; supersedes No. 58328) .Rivet-.191 dia x .317 in. long (deflector) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .

Deflector Assembly-Inter cylinder left front (cylinders No.2,4,6,8,12, & 14; for -4 only) .Deflector-Inter cylinder left front. .Washer-.250 ID x .051 in. thick (inter cylinder deflec-

to reinforcing) .Strip-I nter cylinder left front deflector .Seal-I nter cylinder left front deflector .Clamp Assembly-Inter cylinder deflector left front .Rivet-Universal head .095 dia x .219 in. long (deflec-

to; supersedes No. 58328) .Rivet-Universal head, aluminum alloy .094 dia x .250

in. long (deflector; supersedes No. 57945 or 162513) .Strip-Spacer inter cylinder deflector .

Deflector Assembly-Left front inter cylinder upper (cylin-ders NO.2, 4, 6, 8, 10, 12, & 14) .Deflector-Left front inter cylinder .Clamp Assembly-Left front inter cylinder deflector .Washer-Inter cylinder deflector reinforcement .Washer-I nter cyl.inder deflector reinforcement .Spring-Dzus fastener (supersedes No. 35431) .

1611

1NP2

2

1NP22

21NP12

21NP12

2

13

41NP11111

16I-I

6NP2111

10

101

7NP1112

Page 55: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000.24

FIGURE & UNITSINDEX DESCRIPTION PER ASSYNUMBER PART NUMBER 1 2 345 6 7

DEFLECTORS

t

12

12

12

12

12-11

12121212.

121212-12

1212

12

12

121212

1212-13

12121212

12

12

12

12

12

12-14

121212

12

1212

35432

MS20426AD4-6

MS20470AD3-4

MS20426AD4-5

56027

*56026369424764547646

4764458408107753

*10775290093

107793

107782

107772143575

AS125721

3694246861

*468604687782008HZA008-001

35432

MS20426AD4-6

58408

MS20470AD3-4

MS20426AD4-5

56015

*560133694247645

47646

4764458408

Washer-.1285 10 x .250 00 x .040 in. thick (dzus fast-ener spring) .

Rivet-100o countersunk head; aluminum alloy, .125 diax .375 in. long, (dzus fastener; supersedesNo.AS125291) .

Rivet-Brazier Head .095 dia x .218 in. long (supersedesNo. 58328) .

Rivet-100o countersunk head, aluminum alloy .125dia x .312 in. long (supersedesAS125290) .

Deflector Assembly-Left front inter cylinder lower(cylinder No. 10) .Deflector-Left front inter cylinder lower .Strip-Inter cylinder deflector spacing .Fastener-.310 dia x .450 in. long (dzus type special) .Washer-21/64 10 x 7/8 OD x .032 in. thick (dzus fast-

ner retaining) .Plate-Deflector fastener ejecting .Rivet-lOOo Countersunk head .095 dia x .220 in. long .

Deflector Assembly-I nter cylinder left front (cylinder No.10; for -4 only) .......................•.......Deflector-Inter cylinder left front (cylinder No. 10) .Washer-.250 lOx .051 in. thick (inter cylinder de-

flector reinforcing) .Strip-I nter cylinder left front deflector (cylinder

No. 10) .Seal-Inter cylinder left front deflector (cylinder

No. 10) .Clamp Assembly-I nter cylinder deflector left front .Rivet-Universal head .095 dia x .219 in. long

(deflector) .Rivet-Universal head, aluminum alloy .094 dia x .250

in. long (deflector; supersedesNo. 57945 or 162513) .Strip-Spacer inter cylinder deflector .

Deflector Assembly-Right front inter cylinder upper(cylinders NO.2, 4, 6, 8,10,12, & 14) .Deflector-I nter cyl inder right front .Clamp Assembly-Right front inter cylinder deflector .Washer-Inter cylinder deflector reinforcements .Spring-Dzus fastener No. 100A (deflector; supersedes

No. 35431) .Washer-.1285 ID x .250 OD x .040 in. thick (dzus

fastener spring deflector) .Rivet-lOOo countersunk head, aluminum .125 dia. x .375

in. long (czus fastener; deflector; supersedesNo.AS125291) .

Rivet-100oCountersunk head .095 dia x.220 in. long(deflector) .

Rivet-Brazier head .095 dia x .218 in. long (deflector;supersedesNo. 58328) .

Rivet-100o Countersunk head, aluminum alloy .125 dia x.312 in. long (deflector; supersedesNo. AS125290) .....

Deflector Assembly-Right front inter cylinder lower (cy-IindersNo.2,4,8, 10, 12,&14) .............•......Deflector-Right front inter cylinder lower .Strip-Inter cylinder deflector spacing .Fastener-.310 dia x .450 in. long (dzus type special

deflector) .. ' .Washer-21/64 10 x 7/800 x .032 in. thick (dzus fastener

retaining deflector) .Plate-Deflector fastener ejecting deflector .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) ' ..

4

4

6

3

1NP22

213

1NP2

1

11

10

91

7NP11

2

4

3

1

2

3

6NP2

2

21

3

2-43

d

Page 56: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE & UNITSINDE5( DESCRIPTION PER ASSYNUMBER PART NUMBER 1 2 3 4 5 6 7

DEFLECTOR

12.15

121212

12

1212

12-16

1212

12121212

12

12

1212

12-17

121212

12

1212 .

12-18

1212

12121212

1212

1212

12-19

12

2.44

56016

*560143694247645

47646

4764458408

166023

*10775490093

155840107784107771143575

AS125721

MS20426AD3-4

3694258408

56029

*560283694247645

47646

4764458408

166025

*11379290093

155839113790107771143575

AS125721

MS20426AD3-4

3694258408

155537

*155536

Deflector Assembly-Left front inter cylinder lower(cylinders NO.2, 4, 6, 8, 12, & 14) .

Deflector-Left front inter cylinder lower .Strip-I nter cylinder deflector spacing .Fastener-.310 dia x .450 in. long (dzus type special

deflector) .Washer-21/64 ID x 7/800 x .032 in. thick (dzus fastener

retaining deflector) .Plate-Deflector fastener ejecting .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-I nter cyli nder right front (cylinders No.

2,4,8,10,12, & 14; for -4 & -7M2 only) .Deflector-I nter cylinder right front .Washer-.250 10 x .051 in. thick (inter cylinder

deflector reinforcing) .Strip-I nter cylinder right front deflector .Seal-I nter cylinder right front deflector .Clamp-Inter cylinder right front deflector .Rivet-Universal head .095 dia x .219 in. long

(deflector; supersedes No. 58328) .Rivet-Universal head, aluminum alloy .094 dia x .250

in. lon% (deflector; supersedes NO.5 7945 or 162513) ....Rivet-100 Countersunk head, aluminum alloy .094 dia x

.250 in. long (deflector; supersedes Nos. 166145and AS125271) .

Strip-Spacer inter cylinder deflector .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-Right front inter cylinder lower

(cylinder No.6) .Deflector-Right front inter cylinder .Strip-Inter cylinder deflector spacing .Fastener-.310 dia x .450 in .. long (dzus type special

deflector) .Washer-21/6410 x 7/800 x .032 in. thick (dzus

fastener retaining deflector) .Plate-Deflector fastener ejecting .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-Inter cylinder right front (cylinder

NO.6; for -4 & -7M2 only) .Deflector-I nter cylinder right front (cylinder NO.6) .Washer-.250 ID x .051 in. thick (inter cylinder deflec-

tor reinforcing) .Strip-Inter cylinder right front (cylinder No.6) .Seal-Inter cylinder right front (cylinder No.6) .Clamp-I nter cylinder deflector right front .Rivet-Universal head .095 dia x .219 in. long.

(deflector; supersedes No. 58328) .Rivet-Universal head, aluminum alloy .094 dia x .250 in.

long (deflector; supersedes No. 57945 or 162513) .Rivet-100o countersunk head, aluminum alloy .094 dia x

.250 in. long (deflector; supersedes Nos. 166145and AS125271) .

Strip-Spacer inter cylinder deflector .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-Left rear inter cylinder upper (cylinder

NO.9: supersedes No. 47085) .Deflector-Inter cylinder left rear upper (supersedes No.

47084) .

6NP2

2

21

3

6NP1111

6

6

31

1NP2

2

21

3

1NP

1111

6

6

31

NP

Page 57: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

DEFLECTORS

1212

1212

121212

12

12

12.

1212-20

12121212

1212

12

12

1212

12-21

12

1212

1212

121212

12

12

121212-22

12121212

1212

46878HZA008-001

35432MS20426AD4-6

7952451819MS20470AD3-4

58408

MS20470AD4-5

MS20426AD4-5

36942137486

*13748510777779524HZA008-001

35432MS20426AD4-6

MS20426AD4-5

MS20470AD3-4

3694258408

155538

*155539

46878HZA008-001

35432MS20426AD4-6

7952451819MS20470AD3-4

58408

MS20470AD4-5

MS20426AD4-5

36942137490

*13748910777779524HZA008-001

35432MS20426AD4-6

Clamp Assembly-Left rear inter cylinder deflector .Spring-Dzus fastener NO.1 OOA (deflector; supersedes

No. 35431) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-100o countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector; supersedes No. AS125291) .Bracket-I nter cylinder rear deflector upper left hand .Washer-I nter cylinder deflector reinforcements .Rivet-Brazier head .095 dia x .218 in. long (deflector;

supersedes No. 58328) .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Rivet-Brazier head .126 dia x .312 in. long (deflector;

supersedes No. AN455AD4-5) .Rivet-lOOo countersunk head; aluminum alloy .125 dia x

.312 in. long (deflector; supersedes No. AS125290) .Strip-Spacer inter cylinder deflector .

Deflector Assembly-Inter cylinder left rear upper (cylindersNO.1,3,5, 7,11,& 13;for-40nly) .Deflector-Inter cylinder left rear upper .Plate-Inter cylinder left rear deflector upper .Bracket-Inter cylinder left rear deflector upper .Spring-Dzus fastener No. 100A (deflector; supersedes

No. 35431) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-lOOo countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector; supersedes No. AS125291) .....Rivet-Brazier head .126 dia x .312 in. long (deflector;

supersedes No. AN455AD4-5) .Rivet-Brazier head .095 dia x .218 in. long (deflector;

supersedes No. 58328) .Strip-Spacer inter cylinder deflector .Rivet-100o Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-Left rear inter cylinder upper (cylinders

NO.1, 3, 5, 7,11, & 13: supersedes No. 46865) .Deflector-Inter cylinder left rear upper (supersedes No.

46864) .Clamp Assembly-Left rear inter cylinder deflector .Spring-Dzus fastener No. 100A (deflector: supersedes

No. 35431) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-1000 countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector; supersedes No. AS125291) .Bracket-Inter cylinder rear deflector upper left hand .Washer-Inter cylinder deflector reinforcements .Rivet-Brazier head .095 diax .218 in. long (deflector;

supersedes No. 58328) .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Rivet-Brazier head .126 dia x .312 in. long (deflector;

supersedes No. AN455AD4-5) .Rivet-100o countersunk head; aluminum alloy .125 dia x

.312 in. long (deflector; supersedes No. AS125290) .Strip-Spacer inter cylinder deflector .

Deflector Assembly-I nter cylinder left rear upper (cylinderNO.9; for -4 only) .Deflector-Inter cylinder left rear upper (cylinder No.9) .Plate-Inter cylinder left rear deflector upper .Bracket-Inter cylinder left rear deflector upper .Spring-Dzus fastener No. 100A (deflector; supersedes

No. 35431) .Washer-.1285 ID x .250 OD x .040 in. thick (deflector) .Rivet-100o countersunk head, aluminum alloy .125 dia x

.375 in. long (deflector; supersedes No. AS12529l) .....

1

24

411

2

3

32

6NP11

24

4

3

53

1

6

NP1

24

411

2

3

32

1NP11

24

4

2-45

Page 58: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

DEFLECTORS

12

12

1212

.12-23

121212121212

1212

12

12-24

1212121212

1212

121212

12

12-25

121212

12

1212-26

12121212

121212-27

12121 ~!.L.

'"J.L12

2-46

MS20470AD4-5

MS20470AD3-4

3694258408

137484

*137481137483137482369423826347646

107774143575

AS125721

47751

*4775036942476444764547646

58408MS35191-254

79018*73942*58751

MS20426AD3-4

83975

*839743694247645

47646

4764446867

*46866369424764547646

4764458408137488

*137487137483137482369423(~263

Rivet-Brazier head .126 dia x .312 in. long (deflector;supersedes no. AN455AD4-5) .

Rivet-Brazier head .095 dia x .218 in. long (deflector;supersedes No. 58328) .

Strip-Spacer inter cylinder deflector .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-I nter cylinder left rear lower

(cyliridersNo.1,3,5,ll, & 13;for-40nly) .Deflector-l nter cylinder left rear lower .Seal-I nter cylinder left rear deflector lower .Strip-Inter cylinder left rear deflector lower .Strip-Spacer inter cylinder deflector .Fastener-Dzus type special, deflector. .Washer-21/6410 x 7/800 x .032 in. thick (dzus fast-

ener retaining deflector) .Clamp Assembly-I nter cylinder deflector left rear .Rivet-Universal head .095 dia x .219 in. long

(deflector; supersedes No. 58328) .Rivet-Universal head, aluminum alloy .094 dia x .250 in.

long (deflector; supersedes No. 57945 or 162513) .....Deflector Assembly-Left rear inter cylinder lower (cylind-

ers NO.3 & 5) .Deflector-Inter cylinder left rear lower .Strip-I nter cylinder deflector spacing .Plate-Deflector fastener ejecting .Fastener-.310 dia x .450 in. long (dzus type special) .Washer-21/64 lOx 7/800 x .032 in. thick (dzus fast-

ener retaining) .Rivet-lOOo Countersunk head .095 dia x .220 in. long .Screw-Machine, 820 flat countersunk head, cross reces-

sed, carbon steel, .164-36 NF thd x .500 in. long(supersedes No. AN510-8-8) .

Plate Assembly-Left rear inter cylinder deflector lowerPlate-Left rear inter cylinder deflector lower .Nut-Low temperature anchor type .164-36 NF thd x

.344 in. thick .Rivet-lOOo countersunk head, aluminum alloy .094 dia

x .250 in. long (supersedes No. AS125271) .Deflector Assembly-Left rear inter cylinder lower (cylinder

No. 11) .Deflector-Left rear inter cylinder lower .Strip-Spacer inter cylinder deflector (cy.linder No. 11) .Fastener-.310 dia x .450 in. thick (dzus type special

deflector) .Washer-21/64 lOx 7/8 00 x .032 in. th ick (dzus fast-

ener retaining deflector) .Plate-Deflector fastening ejecting .

Deflector Assembly-Left rear inter cylindel' lower(cylinders NO.1, 9, II, & 13) .Deflector-Inter cylinder left rear lower .Strip-Inter cylinder deflector spacing .Fastener-.310 dia x .450 in. long (dzus type special).Washer-21/64 10 x 7/8 00 x .032 in. thick (dzus

fastener retaining) . . . . . . . . . . .. . .Plate-Deflector fastener ejecting .Rivet-lOOO Countersunk head .095 dia x .220 in. long ..

Deflector Assembly-Inter cylinder left rear lower(cylinders NO.7 & 9; for.4 only) .Deflector-Inter cylinder left rear lower .Seal-I nter cylinder left rear deflector lower .Strip-Inter cylinder left rear deflector lower .Strip-Spacer inter cylinder deflector. . . . . . .Fastener-Dzus type special, deflector .

3

53

5NP1112

21

4

3

2NP212

23

21NP

NP2

1NP2

2

21

4NP22

213

2NP1112

Page 59: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

DESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

DEFLECTORS

FIGURE &INDEX

NUMBER

_---"""T""------,r----------------------'~-"'----=>"lI UI\!ITS 1! f)ER ASSY I

12 47646

12 10777412 143575

~ 12 AS1257211\~, 12-28 46869

12 *4686812 3694212 4764512 47646

12 4764412 5840812-29 46873

12 *4687212 3694212 4764512 47646

12 4764412 5840812-30 107765

12 *10776412 90093

12 3694212 10777512 143575

12 58408

12-31 46871

12 *4687012 4687912 HZA008-00112 35432

12 MS20426AD4-6

12 7952312 8200812 MS20470AD4-5

12 5840812 MS20470AD3-4

12 MS20426AD4-5

12-32 47753

12 *4775212 3694212 4764412 4764512 47646

12 58408

Washer-21/64 lOx 7/800 x .032 in. thick (dzusfastener retaining) . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

Clamp Assembly-Inter cylinder deflector left rear. . . . . . . . 1Rivet-Universal head .095 dia x .219 in. long (deflec-

tor; supersedes Nc. 58328) , . . 4Rivet-Universal head, aluminum alloy .094 dia x .250 in.

long (deflector; supersedes No. 57945 or 162513). . . . . . 3Deflector Assembly-Left rear inter cylinder lower (:::ylinder

No.7). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Deflector-I nter cylinder left rear lower . . . . . . . . . . . . . . . NPStrip-Inter cylinder deflector spacing. . . . . . . . . . . . . . . . . 2Fastener-.310 dia x .450 in. long (dzus type special). . . . . . . 2Washer-21/64 10 x 7/8 00 x .032 in. thick (dzus fastener

reta in ing). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Plate-Deflector fastening ejecting. . . . . . . . . . . . . . . . . . . 1Rivet-lOOo Counter<;unk head .095 dia x .220 in. long. . . . . 3

Deflector Assembly-Right rear inter cylinder lower(cylinders NO.3, 5, & 7). . . . . . . . . . . . . . . . . . . . . . . . . 3Deflector-inter cylinder right rear lower. . . . . . . . . . . . . . . NPStrip-Inter cylinder deflector spacing. . . . . . . . . . . . . . . . . 2Fastener-.310 dia x .450 in. long (dzus type special). . . . . . . 2Washer-21/64 10 x 7/800 x .032 in. thick (dzus

fastener retai n ing) . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Plate-Deflector fastener ejecting. . . . . . . . . . . . . . . . . . . . 1Rivet-lOOo Counter sunk head .095 dia x .220 in. long. . . . . 3

Deflcetor Assembly-Inter cylinder right rear (cylinders No.1,3,5,11, & 13;for -4 only) .. , . . .. . .. . .. .. ... . .. . 5Deflector-Inter cylinder right rear. . . . . . . . .. . . . . . . . . . NPWasher-.250 10 x .051 in. thick (inter cylinder

deflector reinforcing). . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . 1Clamp-I nter cylinder deflector right rear. . . . . . . . . . . . . . 1Rivet-Universal head .095 dia x .219 in. long

(deflector; supersedes No. 58328). . . . . . . . . . . . . . . . . 6Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector) .Deflector Assembly-Right rear inter cylinder upper

(cylinders No. 1,3,5,7,9,11, & 13) . . . . . . . . . . . . . . . . 7Deflector-Inter cylinder right rear upper. . . . . . . . . . . . . . NPClamp Assembly-Right rear inter cylinder deflector. . . . . . . 1Spring-Dzus fastener (supersedes No. 35431) . . . . . . . . . . 2Washer-.1285 10 x .250 00 x .040 in. thick (dzus

fastener spring). 4Rivet-100 countersunk head, aluminum alloy .125 dia x

.375 in. long (supersedes No. AS125291). . . . . . . . . . . . 4Bracket-Inter cylinder rear deflector upper right hand. . . . . 1Washer-I nter cylinder deflector reinforcement. . . . . . . . . . . 1Rivet-Brazier head .125 dia x .312 in. long (supersedes

No. AN455AD4-5) . . . . . . . . . . . . . . . . . . . . . . . . . . 3Rivet-lOOo Countersunk head .095 dia x .220 in. long. . . . . 1Rivet-Brazier head .095 dia x .218 in. long (supersedes

No. 58328) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Rivet-100o countersunk head, aluminum alloy .125 dia x

.375 in. long (supersedes No. AS125290). . . . . . . . . . . . 3Deflector Assembly-Right rear inter cylinder lower

(cylinders No. 11 & 13) . . . . . . . . . . . . . . . . . . . . . . . . . 2Deflector-Right rear inter cylinder lower. . . . . . . . . . . . . . NPStrip-Inter cylinder deflector spacing. . . . . . . . . . . . . . . . . 2Plate-Deflector fastener ejecting. . . . . . . . . . . . . . . . . . . . 1Fastener-.310 dia x .450 in. long (dzus type special). . . . . . . 2Washer-21/64 10 x 7/810 x .032 in. thick (dzus

fastener retaining) . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Rivet-lOOo Countersunk head .095 dia x .220 in. long. . . . . 3

i

_______________________________________________ 2.-4_7 ••• J

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T.O. 2R-R2000-24

37

7

7

111

6

1

2

1NP2

2

21

74

NP

21NP

14

91

10C

14

213

2NP

1NP22

1141428

141414

58408

36942107775143575

*10776690093

83977

*839763694247645

4764458408

47646

4220

MS21044N4

108253

12765

AN960-416

2229082573

MS35489-19

A22707MS35489-19107619MS21044N3

3543421903

35433

121212-34

12-35

1212

121212

FIGURE & .._,----/---. ,..............-~---------------------------

INDEX' ~ DESCRIPTION UNITS

NUMBE R PA RT ~v. ..-<l '?_ "c 6 7 ,,--P_E_R_A_S_SY_

~

'J' . ~; .~ .,XEFLECTORS

12 c'4~ C '-ne, 820 flat countersunk head, cross reces--::z:: c:;.. c9 0-<,"""\Steel .164-36 NF thd x .500 in. long/ 1/ ~ '30: >-, \AN510-8-8) : .

12//'C?J ~ "'::.""lio ~ig~t rear i~ter cylinder deflector lower .12 -...p. "» ~ \ !ar Inter cylinder deflector lower .]' "'J' r-.. ' perature anchor type .164-36 NF thd x

••.••.~ c:;.. 0 ~." .....,. ~ ~ ":t ""\k head, aluminum alloy .094 dia

•••••• Cwo••••••• ",~edes No. AS125271) .~''1\er cylinder lower

~ ~:<I~~~r:: : : : : : : : : : : : : :'\..~?~s' typ~ ~pe~i'ai): : : : : : :

~ '~hick (dzus

~ ) ... 220 in. long .

Ir (cylinders/ ./' .

/:/~i~~e~ ~~I~n.d.e~~~f~e~~ .

//deflector .A",flector right .

/ .095 dia x .219 in. long/,medes No. 58328) .

/,.ntersunk head .095 dia x .220 in. long/,/) .

De .' .:isembly-Right rear inter cylinder lower(c}nrnder No.5) .Deflector-Right inter cylinder lower (cylinder No.5) .Strip-Spacer inter cylinder deflector .Fastener-.310 dia x .450 in. thick (dzus type special

deflector) .Washer-21/64 10 x 7/8 00 x .032 in. thick (dzus

fastener retaining deflector) .Plate-Deflector fastener ejecti ng .Rivet-lOOo Countersunk head .095 dia x .220 in. long

(deflector).Spacer-(9/32 10 x 1/2 aD x 5/8 in. thick (deflector) .Screw-.375 Slotted hexagon head x .190-32 NF thd x 1.310

in. long (deflector; for -4 only) .Washer-Chamfered .203 lOx .375 00 x .048 in. thick

(deflector; use (14) units for -4) .Nut-Non-metalic lock .500 Hexagon x .325-24 thd x .312 in.

thick (deflector; use (87) units supersedes No. 12856) .....Washer-Plain .266 10 x .500 00 x .062 in. thick (deflector

use (98) units for -4 & -7M2; supersedes No. 171) .Screw-Fillister head drilled .250-20 NC thd x .438 in. long

(deflector;use(7)unitsfor-4) .Screw-.375 Slotted hexagon head x .190-32 NF thd x 2.780

in. long (deflector; for -4 only) .Grommet-.688 ID x 1.312 00 x .375 in. thick (inter cylinder

deflectqr: NO.8 cylinder; for -4 & -7M2) (supersedes No.AN931-11-16) .

Grommet-deflector sparkplug lead 0.875 in. dia. hole .Grommet-deflector sparkplug lead 1.000 in. dia. hole .

Latch-Inter cylinder deflector clamp (for -4 only) .Nut-non-metalic lock 10-32 (deflector; supersedes

No. 11748) .'Screw-.375 Slotted hexagon head x .190-32 NF thd x 1.031 in.\ long (deflector) .Screw-Deflector .Spring-.312 in. 00 (deflector clamp) .

12

12-39

12121212

12

121212

12-37

12-38

12-41

12-40

1212-36

1212

12-42

12-47

12-4312-4412-4512-46

12-4812-49

2.48

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T.O. 2R-R2000-24

.",\

/~

/I

lL,/

7I\

6

/I1-

8910

19

20

21

222324

L-t -0-- 33

I"------/ c::::r>

34

35

~

37

\ (-7M2 Engines). 13 DeflectorsFigure .

2-49

j

Page 62: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

l

FIGURE &INDEX

NUMBER

-----NJ.-~.--.. r.::;ESCRIPTIOi'~ UNITS

PART ~ UMBEP--...:_'_? 3_4_!,',_6_7 __ .. PE_R_A_S_S_Y---"

DEFLECTOR (R2COO-7M2 ENGINES)

13-1 11467213 11466713 HZA008-00113 MS20426AD4-513 9009313 11466813 11466913 8170913-2 C4PI0710-1

13 C4Pl 071 09-2713 11466713 HZA008-00113 MS20426AD4-513 9009313 11466813 11466913 8170913-3 C4PHI011-3113 C4PI0710-313 C4PI07109-2713 11466713 HZA008-00113 MS20426AD4-513 9009313 11466813 11466913 8170913 C4PHI011-3313-4 4608513 3826313 4764613-5 12856513 *10041513 HZA008-00113 MS20426AD4-513 9009313-6 12856713 3826313 4764613-7 46093

13 *4608913 *4609013 4609113 9161613-8 107749

13 9009313 10778113 10778013 10777213 3694213-9 C4SCI018-17

13 9009313 10778313 10778213 3694213-10 10775313 9009313 10778313 10778213 36942

2-50

Deflector Assy-Front cyl inter ear No.2, 6, 10, & 14. . . . . . . . . . 4Tube-Inter ear front deflector 1Spring-Dzus fastener No. 100A (supersedes No. 35431) . . . . . . 2Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 2Brace-I nter ear deflector left. . . . . . . . . . . . . . . . . . . . . . . . 1Brace-I nter ear deflector right . . . . . . . . . . . . . . . . . . . . . . . 1

. Clip-Deflector grommet. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Deflector Assy-Front cyl inter ear No. 12 (Supersedes Part

No. 114672). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Deflector (Supersedes Part No. 114671) . . . . . . . . . . . . . . . . 1Tube-Inter ear front deflector. . . . . . . . . . . . . . . . . . . . . . . 1Spring-Dzus fastener No. 100A (supersedes No. 35431) . . . . . . 2Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 2Brace-I nter ear deflector left '. . . . . . . . . . . . . . . . 1Brace-I nter ear deflector right . . . . . . . . . . . . . . . . . . . . . . . 1Clip-Deflector grommet. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Fairlead. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

Deflector Assy-Front inter ear NO.4. . . . . . . . . . . . . . . . . . . . . 1Deflector (Supersedes 114671) . . . . . . . . . . . . . . . . . . . . . . 1Tube-I nter ear front deflector. . . . . . . . . . . . . . . . . . . . . . . 1Spring-Dzus fastener No. 100A (supersedes No. 35431) . . . . . . 2Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 2Brace-I nter ear deflector left. . . . . . . . . . . . . . . . . . . . . . . . 1Brace-I nter ear deflector right . . . . . . . . . . . . . . . . . . . . . . . 1Clip-Deflector grommet. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Fairlead. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

Deflector Assy-Air exhaust. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type deflector. . . . . . . . . . . .. . . . . . . . . . . . 2Washer-.2281 10 x .875 00 x .032 in. thick. . . . . . . . . . . . . . 2

Deflector Assy-Front cylinder inter ear, cylinder NO.8. . . . . . . . . 1Tube-Inter ear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1

. Spring-Dzus fastener No. 100A (supersedes No. 35431) . . . . . . 2Rivet-Solid : . . . . . . . 4

. Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 2Plate Assy-Front cylinder NO.8. . . . . . . . . . . . . . . . . . . . . . . . 1

Fastener-Dzus type deflector. . . . . . . . . . . . . . . . . . . . . . . . 2. Washer-.3281 10 x .875 00 x .032 in. thick. . . . . . . . . . . . . . 2Deflector Assy-Rear cylinder inter ear cylinder No. I, 3, 5,

7,9,11& 13 , . . . . . . . . . 7Bracket-I nter ear rear right deflector. . . . . . . . . . . . . . . . . . . 1Bracket-Inter ear rear left deflector. . . . . . . . . . . . . . . . . . . . 1Tube-I nter ear rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Clip-Deflector grommet ; . . . . . 1

Deflector Assy-Inter cylinder left front cylinder NO.4, 6, 7,12 & 14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 2Strip-Left front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Left front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp Assy-Inter cylinder deflector left front. . . . . . . . . . . . . 1

. Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Deflector Assy-Inter cylinder left front cylinder NO.2

(Supersedes 110749) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Washer-.250 10 x .05 in. thick. . . . . . . . . . . . . . . . . . . . . . . 2Strip-Inter cylinder left front deflector cylinder No. 10 . . . . . . 1Seal-Inter cylinder left front deflector cylinder No. 10. . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Deflector Assy, Inter cylinder left front cylinder No. 10. . . . . . . . 1Washer, 0.25010 x 0.051 in. thick. . . . . . . . . . . . . . . . . . . . 2Strip, I nter cylinder left front deflector cylinder No. 10 . . . . . . 1Seal, Inter cylinder left front deflector cylinder No. 10. . . . . . . 1Strip, Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Page 63: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

DEFLECTOR (R2000-7M2 ENGINES)

T.O.2R-R2000-24

UNITSPER ASSY

13-11 166023

13 9009313 15584013 10778513 10778413 10777113 MS20426AD3-413 3694213-12 C4SCI018-15

13 9009313 15584013 10778513 10778413 10777113 MS20426AD3-413 3694213-13 C4SCI018-3113-14 C4SCI018-25

13 9009313 15584013 10778513 10778413 10777113 MS20426AD3-413 3694213-15 C4SCI018-29

13 9009313 15584013 10778513 10778413 10777113 MS20426AD3-413 3694213-16 C4SC1018-21

13 9009313 15583913 11379013 10777113 MS20426AD3-413 3694213-17 137486

13 10777713 7952413 HZA008-00113 MS20426AD4-613 MS20470AD4-613 3694213-18 13749013 107777

e 13 7952413 HZA008-00113 MS20426AD4-613 MS20470AD4-613 3694213-19 137484

Deflector Assy-Inter cylinder right front cylinder NO.4, 8,& 12. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1-Stri p-R ight front deflector . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Inter cylinder right front. 1Seal-Right front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp-Inter cylinder deflecto:-. . . . . . . . . . . . . . . . . . . . . . . 1Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder right front cylinder NO.2(Supersedes 166023) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Right front deflector. . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-I nter cylinder right front. . . . . . . . . . . . . . . . . . . . . . . 1Seal-Right front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp-Inter cylinder deflector. 1Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Bracket. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . 1Deflector Assy-Inter cylinder right front cylinder No. 10

(Supersedes 166023) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Washer-.250 lOx .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Right front deflector . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Inter cylinder right front. . . . . . . . . . . . . . . . . . . . . . . 1Seal-R ight front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp-Right front deflector . . . . . . . . . . . . . . . . . . . . . . . . 1Rivet-Solid ' ~ . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 3

Deflector Assy-I nter cylinder right front cylinder NO.14(Supersedes 166023) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Right front deflector . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-I nter cylinder right front. . . . . . . . . . . . . . . . . . . . . . . 1Seal-Right front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp-Inter cylinder deflector. 1Rivet-Solid. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder right front cylinder NO.6(Supersedes 166025) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Washer-.250 10 x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Right front deflector . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Right front deflector. . . . . . . . . . . . . . . . . . . . . . . . . . 1Clamp-I nter cyl inder deflector. . . . . . . . . . . . . . . . . . . . . . . 1Rivet-Solid. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder left rear cylinder No. 1,3,5,7,11 & 13 , .. . . .. . . . . . . .. . . . 6Plate-Deflector upper left rear. . . . . . . . . . . . . . . . . . . . . . . 1Bracket-I nter cylinder rear deflector upper left-hand. . . . . . . . 1Spring-Ozus fastener No. 100A (supersedes No. 35431) . . . . . . 2Rivet-Countersunk head. . . . . . . . . . . . . . . . . . . . . . . . . . . 4Rivet-Brazier head _ _ . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1

Deflector Assy-I nter cylinder left rear cylinder NO.9. . . . . . . . . . 1Plate-Deflector upper left rear. . . . . . . . . . . . . . . . . . . . . . . 1Bracket-I nter cylinder reat' deflector upper left hand . . . . . . . . 1Spring-Dzus fastener No. IOOA (supersedes No. 35431) . . . . . . 2Rivet-Countersunk head. . . . . . . . . . . . . . . . . . . . . . . . . . . 4Rivet-Brazier head. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 3

Deflector Assy-I nter cylinder left rear lower cylinder NO.5 &13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

Page 64: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE &UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2 345 6 7 PER ASSY

DEFLECTOR (R2000-7M2 ENGINES)

I.~

13 13748313 13748213 3694213 3826313 47646

13 10777413-20 C4SC1018-27

13 13748313 13748213 3694213 3826313 47646

13 10777413-21 C4SC1018-19

13 13748313 13748213 3694213 3826313 47646

13 10777413-22 C4SC1018-11

13 13748313 13748213 3694213 3826313 47646

13 10777413-23 13748813 13748313 13748213 3694213 3826313 47646

13 10777413-24 C3SC1018-23

13 13748313 13748213 3694213 3826313 47646

13 10777413.25 107765

,13 9009313 3694213 10777513-26 C4SC1018-13

13 9009313 3694213 10777513-27 10776713 90093

2.52

Seal-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cyinder deflector. . . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 10 x .875 00 x .032 in. thick dzus fastener

retaining deflector) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-Inter cylinder deflector left rear. . . . . . . . . . . . . . 1

Deflector Assy-I nter cylinder left rear lower NO.1 (Super-sedes 137484). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 10 x .875 00 x .032 in. thick dzus fastener

retaining deflector) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-Inter cylinder deflector left rear. . . . . . . . . . . . . . 1

Deflector Assy-I nter cylinder left rear lower cylinder NO.3(Supersedes 137484) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector , . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 10 x .875 00 x .032 in. thick dzus fastener

retaining deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-Inter cylinder deflector rear left. . . . . . . . . . . . . . 1

Deflector Assy-I nter cylinder left rear lower cylinder NO.1(Supersedes 137484) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 10 x .875 00 x .032 in. thick dzus fastener

retaining deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-Inter cylinder deflector left rear. . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder left rear lower cylinder NO.9. . . . . . 1Seal-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 lOx .87500 x .032 in. thick dzus fastener

retaining deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-Inter cylinder deflector left rear. . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder left rear lower cylinder NO.7(Supersedes 137484) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Seal-Left rear deflector. . . . . . • . . . . . . . . . . . . . . . . . . . . . 1Strip-Left rear deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Fastener-Dzus type special deflector. . . . . . . . . . . . . . . . . . . 2Washer-.3281 10 x .875 00 x .032 in. thick dzus fastener

retaining deflector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Clamp Assy-I nter cylinder deflector left rear. . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder right rear lower cylinder NO.3,5, 11 & 13 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Washer-.250 lOx .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . . . . . . . . 1Clamp-Deflector inter cylinder right rear. . . . . . . . . . . . . . . . 1

Deflector Assy-Inter cylinder right rear lower cylinder NO.1(Supersedes 107765) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

Washer-.250 ID x .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1Strip-Spacer inter cylinder deflector. . . . . . . . . . . . .. . . . . . 1Clamp-Deflector inter cylinder right rear. . . . . . . . . . . . . . . . 1

Deflector Assy-t nter cylinder right rear cylinder NO.7 & 9 . . . . . . 2Washer-.250 lOx .051 in. thick. . . . . . . . . . . . . . . . . . . . . . 1

Page 65: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

DEFLECTOR (R2000-7M2 ENGINES)

131313-2813-2913-30

13-3113-3213-3313-34

13-35

13-3613-37

14

14-1

14-2

14-3

14-4

14-51414-6

14-7

14-8

14-9

14-10

14-11

14-1214-13

14-1414.15

14-1614-17

14-1814-19

3694210777522290422082573

MS21044N4AN12258212765108253

AN931-11-16

MS35489-19107619

125492

44488

57975

AN122583

MS21044N5

125491*10771457916

33146

323419

743

44492

MS20913-3S

3290947082

2604924934

4448547083

2508623996

Strip-Spacer inter cylinder deflector .Clamp-Deflector inter cylinder right rear .

Spacer-.2812 10 x .500 00 x .625 in. thick .Washer-Chamfered .203 BID x .375 00 x .048"in. thick .Screw-.375 slotted hexagon head x .190-32 NF thd x 1.317 in.

long .Nut-Self-locking hexagon head (Supersedes 12856)Washer-Thrust (Supersedes 171)Screw-Fillister head drilled .250 x 20 NC thd x .438 in. long .....Screw-.375 slotted hexagon head x .190-32 NF thd x 2.780

in. long .Grommet-.688 10 x 1.31200 x .375 in. thick inter cylinder

deflector cylinder NO.8 {Supersedes 26191} .Grommet-deflector sparkplug lead 1.000 in. dia. hole .Latch-Inter cylinder deflector clamp .

MAIN OILSUMP

Sump Assembly Complete-Main oil .

ATTACHING PARTS

Washer-Plain 11/32 10 x 9/16 00 x 3/32 in. thick (main oilsump bolt) .

Bolt-Drilled .500 Hexagon head x .3125-24 NF thd x 1.940 in.long (main oil sump; uS,eNo. MS20995 wire) .

Washer-plain .328 10 x .562 00 x .062 in. thick (main oilsump; supersedes No. 172) .

Nut-non-metalic lock .500 Hexagon x .3125-24 thd x .344 in.thick (main oil sump;supersedes No. 33415) .

- - - - * - - - -Sump Machining Assembly-Main oil ; .

Sump-Main oil (supersedes No. 95211) .Bearing-Flanged .375 lOx .502 00 x 1.010 in. long

(main oil sump attaching bolt) .Pin-Straight .0947-.0951 dia x .190 in. long (main oil

sump stud) .Stud-Sump oil drain tube elbow (supersedes No. 125474

or 218863) .Gasket-.516 10 x .68800 x .078 in. thick (main oil sump

plug) .Plug-Roundhead .500-13 NC-3 thd x .625 in. long (main oil

sump) .Plug-.438 square head x .375-18 Pipe x .796 in. long

(accessory oil return connection in main sump; use No.MS20995 wire; supersedes No. AN913-35) .

Gasket-Main oil sump .Spring-1.720 00 x 1.070 in. long Free length compression

(main oil sump drain short connection) .Gland-Main oil sump drain short connection .Packing-19/32 10 x 117/3200 x 13/32 in. thick (main oil

sump connection front lower) .Tube-Main oil sump drain short .Spring-1.500 00 x 1.515 in. long free length compression

(main oil sump drain long connection) .Gland-Main oil sump drain long connection .Packing-1.031 10 x 1.265 00 x .406 in. thick (main oil sump

connection rear lower) .

11714

791987

7

11428

1

1

3

3

1NP

1

1

1

11

11

11

11

1

I

2-53. I

I

Page 66: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

I

21 ~-24I

~-24

I0_25

----..'~-11

:~~~

:l,

$-18'~~ 1°C@E;l - -'~. 12

~20-~~

I

<::)-40

~~--- i

16--

38-C)

14-~

15-S

13-8

--,

, -28

\

r----,1!C! I

I8--32

r----

&-31I

I' -30,!. 10-/D)I-t- iB . 2-nI, 1---1 i

I l ~I I

~-311I IL-_---'

...N.'

2-54

Page 67: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

j,T.O.2R-R2000-24 .1

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

MAIN OIL SUMP

"..i

14-2014-21

14-22

14-23

14-24

14-25

14-26

14-27

14-2814-2914-30

14-3114-32-,014-33

14-3414-35

14-36

14-37

14-38

14-3914-40

14-41

14

14

14

14

14

14

14

444846191

52117

47773

MIL-C-6985 &Type AMIL-H-6000

MS21044N5

4669

1254651370731254n

3708512547326196

12547598169

98168

4638

7346875-01

444877346874-01

121318

t20117

20117P335924

7437

40835

96588

20126

MS35769-21

Pipe-Main oil sump oil drain long .Gasket-.8I2 ID Pipe flanged x .031 in. thick (main oil sump

vent pipe flange to intermediate rear case) .Gasket-.813 ID Pipe flanged x .031 in. thick (main oil sump

vent pipe flange to sump) .Pipe Assembly-Main oil sump vent (cut tube in half; see T.O.

2R-R2000-23, paragraph 6-284 and figure 8-13; use 2clamps M I L-C-6985 and Type A and hoseM I L-H-60000.8751.0. at assembly) ..............•.............

Clamp-Hose, Aircraft type .

Hose-Aircraft (approximately 3 inches long, 0,875 1.0.) .

ATTACHING PARTSNut-non-metalic lock .500 Hexagon x .3125.24 thd x .344 in.

thick (main oil sump vent pipe flange to intermediate rearcase; supersedes No. 33415) .

Screw-Drilled .500 Hexagon head x .3125-18 NC thd x .938 in.long (main oil sump vent pipe flange to sump; use No.MS20995 wire) .

- - - - * - - - -Tube Assembly-Front case to sump oil drain upper .Tube Assembly-Front case to sump oil drain lower .Hose-.625 lOx 2.750 in. long (upper to lower sump oil drain

tube) .Clamp-1.000 in. ID Hose (upper to lower sump oil drain tube) .Seal-.625 in. 00 Tube (front case to upper drain tube) .Gasket-.812 lOx 1.125 00 x .078 in. thick (sump oil drain

tube) .Cap-Sump oil drain tube (use No. MS20995 wire) .

Plug-.750 Hexagon head x .750-20 NEF-3 thd x .828 in.long (main oil sump drain: for use with Part No. 107714sump) ................................•....

Insert-Flanged 3/4-10 10 x 1.000-1800 x .656 in. long(main oil sump drain plug; for use with Part No. 98169plug) .

Gasket-.750 lOx .938 00 x .078 in. thick (main oil sumpdrain plug; for use with Part No. 98169 plug) .

Washer-1.500 in. lOx 1.750 in. 00 x .075 in. thick (main oilsump connection upper front replaces No. AN900-24and MS35769-39) .

Connection-Main oil sump drain short upper (for -9A only) .Washer-1.250 in. 10 x 1.500 in. 00 x .075 in. thick (sump

connection rear upper; replaces No. AN900-20 andMS35769-41) .

Connection-Main oil sump drain long upper (replaces PartNo. 44486) .Bushing-Flanged 1.000-18 NS thd x 1.250-12 NS thd x .531

in. long (main oil sump plug; for use with Part No.95211 sump) .

Bushing same as 20117 only .003 in. oversize .Tabwasher-1.265 ID x 1.5000 x .044 in. thick (main oil

sump plug bushing; for use with Part No. 20117 bushing) ...Pin-Straight .093 dia x .266 in. long (main oil sump plug

bushing; for use with Part No. 20117 bushing) .Strainer Assembly-Main oil sump (for use with Part No.

95211 sump) .Gasket-1.438 lOx 1.64000 x .078 in. thick Special (main

oil sump strainer plug; for use with Part No. 40835strainer assembly) .

Plug-1.000 Hexagon head x No. 1-18 thd x 31/32 in. long(main oil sump drain: for use with Part No. 95211 sump;use MS20995 wire) .

Gasket-1.0075 ID x .125 Wall x .094 in. thick (main oilsump drain plug; for use with Part No. 20126 plug)(supersedes No. AN900-16) , .

1

1

1

12

3

2

11

121

21

1

1

11

1

1AR

1

1

1

2-551

.J

Page 68: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

--:T:.O~.2:R.:R:20:00=.2~4-------------------------- j

'~-34"'- ,

~-33

" 43 42

~ ~I"

12--' .~

"'" "...•

40

/Q.-23./

"

0-41

...• ...•

~""

14-< f~~>.I F~-- '-13

2.-/ .25t'__

----

Figure 15. Collector Case

2-56

Page 69: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

COLLECTOR CASE

15-115-2

15-3

15-4

15-5

15-6

151515-7

15-8

15-9

15-10

15-11

15-1215-1315-14

15-1515-16

15-17

15-18

15-19

12653586559

71454

51913

AN122583

ZEB1805-054

*93192*86558t14592P4

i4592P814592P12t3544635446P435446P835446P1235446P20t18529P4

18529P818529P12t35787

35787P335787P535787P10t15

15P1015P2015P30469137644717634

7644911523

-MS20913-1S

t19286

19286P419286P819286P1219286P62t7545P4

7545P87545P127545P62

Case & Studs Assembly-Collector (for -4 & -7M2) .Case & Studs Assembly-Collector (starting engine No. 27150:

supersedes No. 74172) .Case & Studs Assembly-Collector (for engine No. 23798 thru

27150) .Case & Studs Assembly-Collector (up to engine No. 23798) .

ATTACHING PARTSWasher-plain .328 in. 10 x .562 00 x .062 in. thick (collector

case to main crankcase; not required when nut No. ZEB1805-054 is used; supersedes NO.1 72) .

Nut'Special .3125 thd (collector case to main crankcase; use(28) units on -4 and -7M2; replace No. 33415) .

- -- - * - - - -Case-Collector (for -4 & -7M2) .Case-Collector (supersedes No. 51912, 74007 or 74571) .Stud-Plain .3125-18-24 thd x 1.688 in. long (collector to

main crankcase) .004 in. oversize ',' .Stud same as 14592 only .008 in. oversize .Stud same as 14592 only .012 in. oversize .Insert-Impeller thrust plate screw .Insert same as 35446 only .004 in. oversize " .Insert same as 35446 only .008 in. oversize .Insert same as 35446 only .012 in. oversize .Insert same as 35446 only .020 in. oversize .Stud-Plain .3125-18-24 thd x 1.531 in. long (collector oil

suction pipe) .004 ,in. oversize .Stud same as 18529 only .008 in. oversize .Stud same as 18529 only .012 in. oversize .Bushing-Flanged .740 ID x .9395 00 x .816 in. long (cam

red uction gear rear) .Bushing same as 35787 only .003 in. oversize .Bushing same as35787 only .005 in. oversize .Bushing same as 35787 only .010 in. oversize .Pin-Straight .1285 dia x .406 in. long (rear cam reduction

gear bushing) .Pin same as 150nly.Ol0in.oversize .Pin same as 15 only .020 in. oversize : .Pin same as 15 only .030 in. oversize .Elbow-I mpeller shaft air vent .Bracket-Blower oil pressure pipe .Screw-Fillister head drilled .250-20 NC thd x 1.062 in. .

long (collector oil pressure pipe bracket; use No.MS20995 wire) .

Tube-Collector oil pressure internal. .Plug-Hexagon socket .250 in. ANPT (drilled hole at co.-

lector oil pressure tube locating) .Plug-Square head .125-27 pipe thd (collector case econo-

mizer connection, use No. MS20995 wire; supersedesNo. 17346) .

Stud-Drilled .4375-14-20 thd x 1.938 in. long (enginemount brackets) .

Stud same as 19286 only .004 in. oversize .Stud same as 19286 only .008 in. oversize .Stud same as 19286 only .012 in. oversize .Stud same as 19286 only .062 in. oversize .Stud.Plain .3125-18-24 thd x 1.750 in. long (main oil sump

connection) .004 in. oversize .Stud same as 7545 only .008 in. oversize .Stud same as 7545 only .012 in. oversize .Sutd same as 7545 only .062 in. oversize .

1

1

11

30

30

NPNP28ARAR8ARARARAR2ARAR2ARAHAR

2ARARAR11

21

32ARARARAH3ARARAR

2.57

Page 70: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. ~R~R2000.24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUr.(lBER PART NUMBER 1 2 345 6 7

COLLECTOR CASE

15.20

15-21

15-22

15-23

15-2415-25

15-26

15-27

15-28

15-29

15-30

1515-3115-32

15.3315-34

15-35

15-36

15.37

15-38

15-39

15-40

15.41

15-42

15-43

151515

2.58

t656P4

656P8656P12t658P4

658P8658P12MS20913-1S

18052

7644827144

t7457774577P1074577P2074577P3083485

t35446

35446P435446P835446P1235446P2028151

184420

530153796139138

46962533

AN960-416

52819

AN960-416

AN121552

MS24665-227

24118

14591

AN960-416

8427

261612616226163

Stud-Plain .3125.18-24 thd x 1.625 in. long (collector tointermediate rear case) .004 in. oversize .

Stud sameas 656 only .008 in. oversize .Stud sameas 656 only .012 in. oversize .Stud-Plain .3125-18-24 thd x 1.938 in. long (collector to

intermediate rear case) .004 in. oversize .Stud sameas 658 only .008 in. oversize .Stud sameas 658 only .012 in. oversize .Plug-Square head .125-27 pipe thd (manifold pressure gage

connection; useNo. MS20995 wire; supersedesNo. 17346) ..Plug-.375 Square head x .250.18 Pipe x .756 in. long

(cabin heater connections; useNo. MS20995 wire) .Tube.1mpeller thrust bearing .Plug-Hexagon socket .0625 ANPT x .312 in. long Special

(impeller thrust bearing tube hole) .Liner-Front impeller shaft. .Liner sameas 74577 only .010 in. oversize .Liner sameas 74577 only .020 in. oversize .Liner sameas 74577 only .030 in. oversize .Seal-2.250 10 x .073 in. dia Round (front impeller shaft

liner) , .Insert-Collector throat & collector rim rear spark advance

tubing clamp screw (for -4 & -7M2) .Insert sameas 35446 only .004 in. oversize .Insert sameas 35446 only .008 in. oversize .Insert sameas 35446 only.012 in. oversize .Insert sameas 35446 only .020 in. oversize .Pin-Straight .072 dia x .250 in. long (collector throat &

collector rim rear spark advance tubing clamp screwinsert; for -4 & -7M2) .

Bearing Assembly-Impeller thrust (starting engine No. 27150;supersedesNo. 76452) .

Bearing Assembly-Impeller thrust (up to engine No. 27150) .Baffle-Impeller thrust bearing oil ..Screw-Fillister head drilled 1/4-28 thd x 13/16 in. long

(impeller thrust bearing plate & baffle; useNo. MS20995wire) .

Bracket-Engine mount .Nut.Castle .4375.20 thd x .454 in. thick (engine mount

bracket; useNo. MS20995 wire) .Washer.plain .266 lOx .50000 x .062 in. thick (diffuser

bolt;for-4&-7M2supersedesNo.171) .Bolt-Drilled shank .438 Hexagon head x .250-28 NF thd x- 2.080 in. long (diffuser; for -4 only) .Washer-plain .266 10 x .500 00 x .062 in. thick (diffuser to

collector; supersedesNo. 171) .Nut-Castle .250-28 thd x .282 in. thick (diffuser to

collector; supersedesNo. 502) .Cotterpin-.072-076 in. dia x .500 in. long (diffuser to

collector casenuts; supersedesNo. 7916) .Seal.16.938 ID x .070 in. dia Round (collector to intermediate

rear case) - .Seal-1.312 ID x .125 in. dia Round (collector to intermediate

rear case) .Washer-Plain .266 lOx .50000 x .062 in. thick (spark advance

tubes block bossscrew; supersedesNO.1 71) .Screw.Filiister head drilled 1/4-28 thd x 7/16 in. long

(spark advance tubes block boss) .Gasket-Collector to intermediate rear case .Gasket-Collector to intermediate rear case .Gasket.Coliector to intermediate rear case .

29ARAR1ARAR4

21

11ARARAR1

1ARARARAR

1

111

88

32

7

7

7

7

9

1

1

1111

Page 71: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000.24

'~--o0' "35..1. 41. '\~!\~~ \-13

\\ ~-17

~-16\

20_~~--21

31-D £i6~15 22 II:if: 3,I 42 I 6 r19

34 /!Jo.~ 23}-. \ \ =~-18 / / 36......"'" '\ ~:j---l\ I \ I 29 ,# / ~

~, ,33'!.'i/'/

~'';: • --> .- I / / ~

32 -=;wG 0 /. ./ _ I

••. 7

, ---~~38

8

rI

I@-9

~10

. Rear Case16 IntermedIateFigure .

.2.59

Page 72: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &INDEX- DESCRIPTION UNITS

NUMBER PART NUMBER 1 2 345 6 7 PER ASSY

INTERMEDIATE REAR CASE

16-1

16-216

16

16-3

16-4

1616-5

16-6

16-7

16-8

16-9

16-10

1616-1116-12

16-13

16-14

16-1516-16

16-17

16-18

16-19

16-20

16-21

2-60

335751

77153*77152

*77118

AN122583

MS21044N5

*102488136

AN932D4

258

335750

AN960-416

5213

*468034678443568

t33532

33532P433532P833532P12t3361633616P4AN932D2t54301

54301P1054301P4022375

t30643

30643P430643P828151

t34804

34804P534804PI0

t15

15PIO15P2015P30

Case Assembly Complete-I ntermediate rear (supersedes No.123502) . .

Case & Studs Assembly-Intermediate rear (supersedes No. 46988)Case Machining Assembly-Intermediate rear (supersedes No.

46987) .Case-Intermediate rear (supersedes No. 46772) .

ATTACHING PARTS

Washer-Plain .328 10 x .562 00 x .062 in. thick (intermediaterear case to collector case: supersedes No. 172) .

Nut-non-metalic lock .500 hexagon x .3125-24 thd x .344 in.thick (intermediate rear case to collector; supersedesNo. 33415) . .

- - - - * - - - -Case-Intermediate rear (supersedes No. 93195) .Plug-Hexagon socket .750 ANPT x .500 in. long Special

(intermediate rear case lower cored oil passage) .Plug-Hexagon socket .375 in~ ANPT (intermediate rear case

drilled oil passage; supersedes No. 15283) .Plug-Square head 1.000-11.5 00 Pipe x .875 in. long

(intermediate rear case) .Insert Machining Assembly-Supercharger intake (supersedes

No.47003) .

ATTACHING PARTSWasher-plain .366 lOx .500 00 x .062 in. thick (super-

Charger intake insert to intermediate rear case nut;supersedes No. 171) .

Nut-7 /16 Slotted hexagon head x 1/4-28 thd x 3/16 in.thick (supercharger intake insert to intermediate rearcase; use No. MS20995 wire) .

----*----Insert-Supercharger intake .Liner-Supercharger intake insert. .Pin-Straight.1285 dia x .344 in. long {supercharger. intake insert liner) . . . . . . . .. . .

Tube-.563 00 x .035 Wall x .750 in. long (intermediaterear to rear case oil pressure) .

Tube same as 33532 only .004 in. oversize .Tube same as 33532 only .008 in. oversize. . . . . . . . .. . ..Tube same as 33532 only .012 in. oversize .Tube-I ntermediate rear to rear case oil suction .Tube same as 33616 only .004 in. oversize .Plug-Hexagon socket .125 in. ANPT (intermediate rear case) .Bearing-Flanged 1.49010 x 1.75300 x 1.110 in. long

(blower intermediate shaft front) .Bearing same as 54301 only .010 in. oversize .Bearing same as 54301 only .040 in. oversize .Pin-Straight .1285 dia x .375 in. long (blower intermediate

shaft front beari ng) , .Bushing-Screw .375-24 NF 10 x .5626-18 N 00 x .688 in.

long (carburetor pad) .Bushing same as 30643 only .004 in. oversize .Bushing same as 30643 only .008 in. oversize .Pin-Straight .072 dia x .250 in. long (carburetor pad

insert) . . . . . . . . . . . . . . . . .. . .Bearing-Flanged 1.11410 x 1.37800 x .781 in. long

(generator drive idler shaft front) . . . . . .. . .Bearing same as 34804 only .005 in. oversize .Bearing same as 34804 only .010 in. oversize - .

Pin-Straight .1285 dia x .406 in. long (generator driveidler shaft bushing) ...................•........

Pin same as 150nly.010in.oversize .Pin same as 15 only .020 in. oversize .Pin same as 15 only .030, in. oversize .

11

NPNP

30

30

NP2

4

1

12

12

NP1

1ARARAR1AR4

2ARAR2

7ARAR7

1ARAR

1ARARAR

Page 73: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R.R2000.~4

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

INTERMEDIATE REAR CASE

16-22

16-23

16-24

16-25

16-26

16-27

16-28

16-29

16-30

16-31

16-32

16-33

16-34

16-35

16-36

16-37

16-38

16-39

16-40

16-41

16-42

18052

t34119P4

34119P828151

54562

96281

34834

56007

t96282P4

96282P85121

72337

t34119P4

34119P828151

4617

AN932-2

11523

91454

27143

27144

MS20913-1S

AN932-2

18052

Plug-.375 Square head x .250-18 Pipe x .765 in. long(intermediate rear case cored passage: use No.MS20995 wire; supersedes No. 129) .

Bushing-Screw .190-32 NF 10 x .3125-24 N 00 x .375 in. long(screw impeller shaft fuel feed valve diaphragm) .004in. oversize .

Bushing same as 34119 only .008 in. oversize .Pin-Straight .072 dia x .250 in. long (impeller shaft fuel

feed valve diaphragm screw insert) .Seal-1.000 10 x .065 in. dia Round (intermediate rear case

fuel intake insert: for use with case having pinnedinsert) .

Insert Intermediate rear case fuel feed (stud attachingtype insert; for use with Part No. 102489 casemachining assembly) .

Insert-Flanged .8125-16 NS & 1.125-16 NS thd x .500 in.long (intermediate rear case fuel intake pin type in-sert; for use with Part No. 93196 case machiningassembly only) " .

Pin-Straight .072 dia x .340 in. long (intermediate rearcase fuel intake insert; for use with Part No. 34834insert) " .

Stud-Drilled .3125-18-24 thd x 1.030 in. long (intermediaterear case fuel feed insert; for use with Part No. 9628"1insert) .004 in. oversize .

Stud same as 96282 only .008 in. oversize .Nut-Shear .500 hexagon head x .3125-24 NF thd x .219 in.

thick (intermediate rear case fuel feed insert stud;use No. MS20995' wire) .

Dowel-.1860-.1865 dia x .500 in. long (carburetor adapter;for use -4 & -7M2) .

Bushing-Screw .190-32 NF 10 x .3125-24 N 00 x .375 in. long(screw accelerator pump) .004 in. oversize .

Bushing same as 34119 only .008 in. oversize .Pin-Straight .072 dia x .250 in. long (accelerator pump

pad screw insert) .Dowel-Straight .1875 dia x .438 in. long (accelerating valve

to intermediate rear case locating) .Plug-hexagon socket .125 in. ANPT (intermediate rear case;

supersedes No. 11521) .Plug-Hexagon socket .250 ANPT (blower throat & blower rim

cored air passage) .Plug-Hexagon socket .125 ANPT x .375 in. long Special

(intermediate rear case) .Plug-Hexagon socket .0625 ANPT x .312 in. long Special

(intermediate rear case; supersedes No. 90553) .Plug-Hexagon socket .0625 ANPT x .312 in. long Special

(blower rim spark advance hole) .Plug-Square head x .125-27 pipe thd (intermediate rear case

cored passages; supersedes No. 17346) .Plug-Hexagon socket .125 ANPT (blower throat spark advance

hole; supersedes No. 11521) .Plug-.375 Square head x .250-18 Pipe x .765 in. long

(magneto vent hole; use No. MS20995 wire) .

7

6AR6

1

2

2AR

2

2

6AR6

2

2

1

1

1

4

1

1

2-61

Page 74: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

I

i!i~IeIi!

IIiiIII

IIIIIeI

28

I

0-27

3

'Y~_7-I

r

I~

~----25

~26I

I

II

I0-16

1]-17I1-18

;]--19

1-20

~-21

22

Figure 17 I. ntermediate R. ear Case

14

Ig,-~

T.O. 2R-R2000-24

2-62

Page 75: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

INTERMEDIATE REAR CASE

FIGURE & UNITSINDEX DESCRIPTION PER ASSYNUMBER PART NUMBER 1 2 345 6 7 -

17-1

17-2

17.3

17.4

17-5

17.6

17-7

17-8

17.917.10

17-11

17-12

17-13

17-14

17-15

273087P3

273087P6273087P9273087P12tl8515P4

18515P818515P12tl8517P4

18517P818517P12t43057P4

43057P843057P12t64

64P464P864P1264P30tl9795

19795P319795P419795P15t38299P4

38299P838299P1224652

4678552567

t11345P4

11345P811345P12t26056P4

26056P826056P1276671

.70

t26056P4

26056P826056P12AN123860

Stud-single shouldered 0.375.16-24 thd x 6.640 in. long(intermediate rear casevibration dampened; 0.003 in.oversize; for usewith part No. AN123860 seal; replacesNo. 96219 and 141375) .

Stud-same as 273087 only 0.006 in. oversize .Stud.same as 273087 only 0.009 in. oversize .Stud-same as 273087 only 0.012 in. oversize .Stud-Shouldered .3125-18NS-24NF thd x 5.312 in. long

(intermediate rear to rear case) .004 in. oversize .Stud sameas 18515 only .008 in. oversize .Stud sameas 18515 only .012 in. oversize .Stud-Shouldered .3125-18NS-24NF thd x 6.188 in. long

(intermediate rear to rear case) .004 in. oversize .Stud sameas 18517 only .008 in. oversize .Stud sameas 18517 only .012 in. oversize .Stud-Shouldered .3125-18 NS thd x 4.281 in. long

(intermediate rear to rear case) .004 in. oversize .Stud sameas43057 only .C08 in. oversize .Stud sameas43057 only .012 in. oversize .Dowel - Straight .312 dia x .625 in. long (intermediate

rear to rear case locating) .Dowel sameas64 only .004 in. oversize .Dowel sameas 64 only .008 in. oversize .Dowel sameas 64 only .012 in. oversize .Dowel sameas 64 only .030 in. oversize .Bushing - Flanged .625 10 x .877 OD x .375 in. long (oil

pressure pipe bolt) .Bushing sameas 19795 only .003 in. oversize .Bushing sameas 19795 only .004 in. oversize .Bushing sameas 19795 only .015 in. oversize .Stud - Plain .3125.18-24 thd x 1.375 in. long (main oil

sump vent pipe flange) .004 in. oversize .Stud sameas 38299 only .008 in. oversize .Stud sameas 38299 only .012 in. oversize .Seal - 2.25010 x .125 in. dia Round (impeller shaft oil

seal ring rear liner to supercharger intake insertliner) .

Liner - Impeller shaft oil seal ring rear .Screw - Flat head 10-24 thd x .500 in. long (impeller

shaft oil seal ring rear liner; supersedesNo. 34368) .

Stud - Plain .3125-18-24 thd x 1.562 in. long (clutchselector valve) .004 in. oversize .

Stud sameas 11345 only .008 in. oversize .Stud sameas 11345 only .012 in. oversize .Stud - Drilled .250-20-28 thd x 1.078 in. long

(supercharger intake insert) .004 in. oversize .Stud sameas 26056 only .008 in. oversize .Stud sameas 26056 only .012 in. oversize .Gasket - 2.906 10 x 3.625 OD x .016 in. thick (impeller

shaft rear oil seal ring) .Pin - Straight .1875 dia x .688 in. long (diffuser to

supercharger intake insert locating) .Stud. Drilled .250-20-28 thd x 1.078 in. long

(supercharger intake insert to dHfuser) .004 in.oversize .

Stud sameas26056 only .008 in. oversize .Stud sameas26056 only .012 in. oversize .

Seal."O" Ring oil resistant .234-.244 ID x .375 00 x .067-.073in. thick (intermediate rear to rear casestud: for usewith Part No. 273087 stud) .

2ARARAR

12ARAR2ARAR2ARAR2ARARARAR1ARARAR2ARAR

11

6

5ARAR12ARAR1

1

6ARAR

2

2.63

\-- .,

Page 76: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

r.o. 2R-R2000-24

"

FIGURE & ," ,IPART NUMBER

UNITSINDEX DESCRIPTIONPER ASSYNUMBER 1 2 3 4 5 6 7

INTERMEDIATE REAR CASE

17-16

17-1717-18

17-19

17-2017-21

17-2217-2317-2417-25

17-26

17-27

17.28

17-29

17-3017-311.7-32

18

18-1

18-2

18-318-418-5

18-6

18-7

18-8

18-9

18-10

18.11

18-12

2.64

30489

4468344684

89299

4468230489

8813154543114097AN960-416

5213

MS35769-31

88285

AN960-416

51911AN121552MS24665-227

156561

163287

97611

97612

4813280827174137

77117

163283

156560

163286

MS24665-151

41385

35233

Seal-.500 10 x .62500 x .047 in. thick (supercharger fueldrain outer connection to supercharger intake insert) .

Connection-Supercharger fuel drain outer .Spring-.955 00 x 4.250 in. long Free .length compression

(supercharger fuel drain outer to inner connection) .Seal-0.490 10 x 0.078 in. dia round (supercharger fuel drain

center to inner) (supersedes Part No. 49986) .Connection-Supercharger fuel drain inner .Seal-.500 ID x .625 00 x .047 in. thick (supercharger fuel

drain inner connection to intermediate rear case) .Diffuser-Intermediate rear case .Diffuser-{-7M2 only) .Shim-Diffuser (diffuser & supercharger insert) .Washer-plain .266 10 x .500 00 x .062 in. thick (intermediate

rear case to supercharger intake insert nut; supersedesNo.171) .

Nut-7/16 Slotted hexagon head x 1/4-28 thd x 3/16 in. thick(intermediate rear case diffuser to supercharger intakeinsert; use No. MS20995 wire) .

Gasket-1.133 lOx 1.500 00 x .094 in. thick (automatic fueldrain valve to intermediate rear case; supersedes AN900-20) ...

Adapter-Supercharger fuel drain valve (supersedes No. 85624,157772 or 167959) .

Washer-plain .266 10 x .500 00 x .062 in. thick (diffuserattachment bolt nut and AN122582) .

Bolt-Diffuser attachment (-7M2 only) .Nut-Castillated hex, diffuser attach bolt (-7M2 only) .Cotterpin .078 dia x .500 in. long (diffuser attachment bolt

nut; supersedes No. 7916) '" .

FUEL FEED VALVE, CLUTCH SELECTOR VALVEAND ACCELERATING PUMP

Valve Assembly-I mpeller fuel feed (replaces No. 135288) (foruse with No. 98784, 10 psi spring on R2000-4 engines) ....

Valve Assembly-I mpeller fuel feed (for use with No. 134911,5 psi spring on R2000-7M2 engines) .

Seal-.445 ID x .120 in. dia Round (impeller shaft fuel feedvalve housing lower to intermed iate rear case) .

Seal-.625 10 x .147 in. dia RClund (impeller shaft fuel feedvalve housing upper to intermediate rear case) .Housing Assembly-I mpeller fuel feed valve .Valve Assembly-I mpeller shaft fuel feed .Diaphragm-Impeller shaft fuel feed valve guide (supersedes

No. 148675) .Washer-Stainless steel .031 in. base thickness (fuel feed

valve guide nut; for use with Part No. 156560 or134912 nut) .

Washer-Stainless steel .050 in. base thickness (fuel feedvalve guide nut; for use with Part No. 163286 nut) .

Nut.5.182 00 x .190-32 NF thd x .510 in. long (impeller shaftfuel feed valve guide; for use with Part No. 156561valve and housing assembly and No. 77117 washer; re-places 134912 for 156561 assy) .

Nut-I mpeller shaft fuel feed valve guide (for use with PartNo. 134911 spring and No. 163283 washer) .

Cotterpin-corr,osion resistant .058-.061 dia x .312 in. long(impeller shaft fuel feed valve guide nut; supersedesNo. AS123770) ' .

Gasket-1 1/3210 x 21/1600 x 1/32 in. thick (impeller shaftfuel feed valve flange) .

Flange-I mpeller shaft fuel feed valve housing .

11

1

21

1111

6

6

1

2077

7

1

1

111

1

1

1

1

1

1

11

"",-'.

Page 77: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

30

J31 "\ \ 2B

~ 32

29~~/;~O ~.

37 . 311~7 /~~~ )-- ----23

38~YhJ~- 36 33 //~~--40 - ",

(I 4~39' 4

.

F.Igure 18. Fuel Feed Valve Cluteand Aeeele~ating PuhSelector Valvemp ,

2.65

Page 78: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX. DESCRIPTION PER ASSYNUMBER PART NUMBER 1 2 345 6 7

FUEL FEED VALVE, CLUTCH SELECTOR VALVEAND ACCELERATING PUMP

18-13 98784 Spring.Steel .602 OD x .051 dia wire x 2.650 in. long (10 psi efuel feed valve; 22 psi fuel pressure) ................. 118-14 134911 Spring-Stainless steel .469 ID x .039 in. dia wire, 5 psi

(replaces No. 98784; 17 psi fuel pressure; for usewithPart No. 163287 fuel feed valve assembly) ............. 1

18-15 98782 Cover..Fuel feed valve diaphragm 10 psi (for usewith Part No.98784 spring) ................................ 1

8.16 34120 Cover-Impeller shaft fuel feed valve diaphragm (for usewith Part No. 134911 spring) ...................... i18.17 MS122030 Lockwasher-.194 - .205 ID x .337 OD x .047-.057 in. thick(impeller shaft fuel feed valve diaphragm cover screw;supersedesNo. AN935-10) ....................... 6

18-18 219 Screw-Fillister head drilled .190-32 NF thd x .625 in. long(impeller shaft fuel feed valve diaphragm cover; useNo. MS20995 wire) ............................ 6

18-19 83280 Seal-.375 dia x .172 in. thick (impeller shaft fuel feed valvediaphragm cover) ................................

18.20 53676 Gasket-1.910 ID x 3.130 OD x .030 in. thick (accelerating pumpto intermediate rear case) .......................... 1

18.21 36090 Seal-.750 ID x .125 in. dia Round (accelerator pump to inter-mediate rear case) ............................... 1

18.22 391601A Pump-Accelerating intermediate rear case(06848: for detailparts list seeT.O. 6Rl-3-3-34) ....................... 1

18-23 93956 Gasket-Clutch selector valve housing (-4) .................. 118 77890 Housing Assembly Complete-Clutch selector valve (-4) ......... 118.24 94188 Gasket-Clutch selector valve pad (-7M2) ................... 118,25 94189 Cover Clutch selector valve pad (-7M2) ................... 1

ATTACHING PARTS18-26 AN122583 Washer-plain .328 ID x .562 OD x .062 in. thick (clutch

selector valve to intermediate rear casenut; supersedesNo. 172) (-4 & -7M2) ............................. 5

18.27 MS21044N5 Nut-non-metalic lock .500 hexagon x .3125-24 thd x .344 in.thick (clutch selector valve to intermediate rear case;supersedesNo. 33415) {-4&-7M2) .................... 5

- - - - * • - - -18.28 77151 Housing Assembly-Clutch selector valve (supersedesNo.

40947,548060r93204) (-4) ...................... 118 *77147 Housing-Clutch selector valve (.4) ................... NP18.29 t41451P4 Stud-Plain .190-24-32 thd x .938 in. long (clutch

selector valve housing) .004 in. oversize (-4) .......... 341451P8 Stud sameas 41451 only .008 in. oversize (-4) .......... AR41451P12 Stud sameas41451 only .012 in. oversize (-4) .......... AR

18-30 16804 Dowel-Shouldered .182-.192 dia x .500 in. long (clutchselector vavle housing) (.4) ..................... 1

18.31 MS20913-1S Plug-Squarehead x .125-27 pipe thd (clutch selectorvalve low oil pressurechecking gageconnection; useMS20995 wire; supersedesNo. 17346) (.4) ...........

18.32 18052 Plug-.375 Square head x .250-28 Pipe x .765 in. long(dri lied high 0iI pressurechecki ng gageconnection;useNo. MS20995 wire enclosed by spaghetti) (-4) ...... 1

18 92285 Spaghetti-Clutch selector valve plug safety wire .......... 6 in.18-33 143745 ShaH-Clutch selector valve (supersedesNo. 93206 or 40944) ... 118.34 287788 Seal Option-CI utch selector valve shaft support (procure-

ment number consists of: Part No. 14538 Seal-Oil .500ID x 1.00400 x .375 in. thick (optional to Part No. .e287778) Part No. 287778 Seal.Oil .500 ID x 1.004 OD x.375 in. Wide (optional to Part No. 14538) (-4) .......... 1

18-35 40943 Support-Clutch selector valve shaft .................... 118.36 40946 Gasket-Clutch selector valve support to clutch selector

valve housing) (-4) ............................. 118.37 40945 Washer-Plain .328 ID x .75000 x .0937 in. thick (clutch

selector valve lever) ............................ 1

2.66

Page 79: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITS

INDEX (' DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

FUEL FEED VALVE, CLUTCH SELECTOR VALVEAND ACCELERATING PUMP

18-3818-39

18-40

18-41

1818

18-42

18-43

18-4418-45

18-46

18.47

18-48

18

19-1

19-2

19

19

1919

19-319-419-5

19-6

19-7

19-819-919-1019-1119-1219-1319-14

33605MS21044N4

11618

MS21044N3

143744143747

234

131

96997AN122583

18380

26196

38666

78261

202999

212383

202877

*81113

*202684*81112

2090517045543568

46779

41452

469124678046776716574678211394447970

Lever-Clutch selector valve (-4) .Nut-non-metalic lock .438 hexagon x .250-28 thd x .312 in.

thick (clutch selector valve lever: supersedesNo.12856) (-4) .

Washer-Plain .203 ID x .375 OD x .0315 in. thick (clutchselector valve shaft support to housing nut) (-4) .

Nut-non-metalic lock .375 hexagon x .190-32 thd x .234 in.thick (clutch selector valve shaft support to housing;supersedesNo. 11748) (-4) .

Stud-Clutch selector valve shaft (for service procurement) .Pin-Straight .1572-.1577 dia x .440 in. long (clutch selector

valve shaft stud; for service procurement) .Gasket-.625 ID x .938 OD x .078 in. thick (intermediate rear

casethermometer connection) .Plug-Round head .625-18 NF-3 thd x .562 in. long (intermediate

rear casethermometer connection) .Gasket-Intermediate rear to rear case .Washer-plain .328 ID x .562 OD x .062 in. thick (blower oi'l

suction bolt; supersedesNo. 172) .Bolt - Shouldered .500 Hexagon head x .3125-24 NF thd

x 6.219 in. long (blower oil suction: useNo. MS20995 wire) .Gasket - .812 ID x 1.125 OD x .078 in. thick (intermediate

rear casefuel intake bolt; for usewith shippingplug also) .

Plug - 1.125 Hexagon head x .8125-16 NS thd x .688 in. long(intermediate rear casefuel intake insert: forshipping only) .

Plug - .375-18 in. NPT (supercharger fuel drain valve adapter;for shipping only; useNo. MS20995 wire) .

IMPELLER SHAFT, ACCESSORYDRIVE SHAFT AND STARTER JAW

Impeller & Shaft Balancing Assembly -7.15:1 & 9.52:1(usewith creeper desludging type clutches only:supersedesNo. 81814 or 195189) (-4 only) .

Impeller & Shaft Balancing Assembly -7.15:1 & 9.52:1(usewith desludging type clutches only; supersedesNo. 81114) (-4 only) .

Shaft Assembly - Impeller 7.15:1 & 9.52:1 (supersedesNo. 81813) .

Shaft Assembly - Impeller 7.15: 1 & 9.52:1 (usewithdesludging type clutches only) .Shaft - Impeller 7.15:1 & 9.52:1 (supersedesNo. 81812) .Shaft - Impeller (usewith desludging type clutches

only) .Impeller and Shaft Balancing Assy-(-7M2 only) .

Carrier - Impeller shaft oil seal ring rear .Pin - Straight .1285 dia x .344 in. long (impeller

shaft oil seal ring rear carrier) .Bearing - 1.344 ID x 1.471 OD x 1.250 in. long

(impeller shaft front & rear) .Pin - Straight .1285 dia x .156 in. long (impeller

shaft front & rear bearings) .Carrier - Impeller shaft fuel seal ring .SIinger - Impeller fuel. .

Impeller - (-7M2 only) .Impeller-(-4 only) .Spacer - Impeller .Carrier - Impeller shaft oil seal ring front .Spannernut - 1.843-20.NS thd x 2.313 x .500 in. thick

(impeller shaft front) .

1

3

31

1

11

1

1

.'\

1-:?

1

NPNPNP11

2

2

4111111

1

2.67

Page 80: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

L

T.O. 2R-R2000-24

Figure 19. Impeller Shaft, Accessory Drive Shaft,and Starter Jaw

2-68

Page 81: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

IMPELLER SHAFT, ACCESSORYDRIVE SHAFT AND STARTER JAW

19-15

19-16

19-17

19.19-1819-19

19-201919-21

19-22

19-23

19-24

19-2519-2619-27

107425

t26475

26475P526475P5W26475P5P2W

26475P5P5W

26475P5P10W

26475R1

26475P1026475P10W26475P10P2W

26475P10P5W

26475P10P10W

26475R2

26475P1526475P15W26475R3

t51807

51807P551807P5W51807P5P5W

51807R1

51807P1051807P10W51807P10P5W

51807P10P10W

*1520633480620303

138609*13691424077

147620

96138

78282

453751341720298

Rivet - Flat head, slotted .093 dia x .350 in. long (impellershaft front nut) .

Ring - Oil seal 2.501 00 x .078 in. thick (impeller shaft oilseal ring front carrier) .

Ring same as 26475 only .005 in. oversize .Ring same as 26475 only .005 in. oversize on width .Ri n'g same as 26475 only .005 in. oversize on 00 & .002

in. oversize on width .Ring same as 26475 only .005 in. oversize on 00 & .005

in. oversize on width .Ring same as 26475 only .005 in. oversize on 00 & .010 in.

oversize on width .Ring same as 26475 only .005 in. oversize on 00 & .015 in.

oversize on width .Ring same as 26475 only .010 in. oversize .Ring same as 26475 only .010 in. oversize on width .Ring same as 26475 only .010 in. oversize on 00 & .002 in.

oversize on width .Ring same as 26475 only .010 in. oversize on 00 & .005 in.

oversize on width .Ring same as 26475 only .010 in. oversize on 00 & .010 in.

oversize on width .Ring same as 26475 only .010 in. oversize on 00 & .015 in.

oversize on width .Ring same as 26475 only .015 in. oversize .Ringsameas264750nly.015 in. oversize on width .Ring same as 26475 only .015 in. oversize on 00 & .015in.

oversize on width .' .Ring - Oil seal 2.53200 x .078 in. thick (impeller shaft

ring carrier; use (4) units for oil seal ring rear & use(2) units for fuel seal ring) .

Ring same as 51807 only .005 in. oversize .Ring same as 51807 only .005 in. oversize on width .Ring same as 51807 only .005 in. oversize on 00& .005 in.

oversize on width ....................•........Ring same as51807 only .005 in. oversize on 00 & .010 in.

oversize on width .Ring same as 51807 only .010 in. oversize .Ring same as 51807 only .010 in. oversize on width .Ring same as 51807 only .010 in. oversize on 00 & .005 in.

oversize on width .Ring same as 51807 only .010in. oversize on 00 & .010 in.

oversize on width .Shaft Assembly Complete - Accessory drive .

Gear - Accessory drive shaft floating .Bearing - 1.685 ID x 1.936500 x .796 in. long (accessory

drive shaft spring drive gear floating) .Shaft Assembly - Accessory drive .

Shaft- Accessory drive (supersedes No. 46783) .. Stud - 1-14 NF thd x 1 27/32 in. long (accessory drive

shaft starter jaw drive; for use with PartNo. 137547 jaw & 27646 nut) .

Shaft Assembly - Accessory drive (for use with PartNo. 134877 jaw & 96137 nut; supersedes No. 96141) ...

Stud - 1-14 N thd x 1.734 in. long (accessory driveshaft starter jaw drive; for use with PartNo. 134877 jaw& 96137 nut) .

Pin - Straight .093 dia x .188in. long (accessory driveshaft starter jaw drive stud) - .

Plate Assembly - Accessory drive shaft spring drive fixed .Spring - .84800 (accessory drive shaft blower drive gear) .Button - Accessory drive shaft blower dr,ive gear spring

retainer. . . . . . . . . . . . . . . . . . . . . . . . . . .

4ARARARARARARARARARAR

ARARARARAR

6ARARAR

ARARAR

ARAR11

11NP

1

1

116

12

rl

Page 82: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2 3 4 5 6 7PER ASSY

IMPELLER SHAFT, ACCESSORY DRIVE SHAFTAND STARTER JAW

l

19-28

19-29

19-3019-31

19-32

19-3319-3419-3519-36

19-37

19-38

19-39

19-40

19-41

19-42

19-43

19-44

19-45

19-46

202020

20

20-1

20-2

20

20

20-3

20-4

20

2-70

20297

137547

27646134877

96137

142142192190192189184428

138547

136915

MS-24665-151

t24075

24075P2W24075P4Wt2407624076P2W24076P4W

. AS123790

28462

24234

24248

MS20913-1S

*146111*146112163820

163824

163819

163823

*163818

*163822

39323

77342

*54170

Pin - .4375 d ia x .594 in. long (accessory drive shaft blowerdrive gear spring) .

Jaw - Starter 3 tooth (for use with Part No. 27646 nut &24077 stud) .

Nut - 3/8-24 thd Special (starter jaw) .Jaw - Starter 3 tooth (for use with Part No. 96137 nut &

96138 stud; supersedes No. 96140) .Nut - .375-24 thd Special (starter jaw; for use with

Part No. 134877 jaw & 96138 stud) .Spacer Assembly - Accessory drive shaft coupling .Coupling - Outer (accessory drive shaft; replaces No. 136913) .Coupling - Inner (accessory drive shaft; replaces No. 136913) .Snapring - 2.32500 x .035 in. thick (accessory drive shaft

coupling; for use with Part No. 192189 & 192190coupling) .

Washer - 2 00 x .093 in. thick (accessory drive shaft adapternut) : ' .

Spannernut - 1.1875-24 thd x .310 in. thick (accessory driveshaft coupling; supersedes No. 24050) .

Cotterpin-.078 in. dia x .500 in. long (trim to .312 in. long;accessory drive shaft nut washer; supersedes No. AS123770) .

Ring - Oil seal 1.70010 x 1.87300 x .123 in. thick(accessory drive shaft rear at starter jaw) .

Ring same as 24075 only .002 in. oversize on width .Ring same as 24075 only .004 in. oversize on width .Retainer - Accessory drive shaft oil seal ring .Retainer same as 24076 only .002 in. oversize on width .Retainer same as 24076 only .004 in. oversize on width .Cotterpin - Corrosion resistant .086-.090 dia x .625 in. long

(starter jaw nut) .Bushing-1/4-18 NPT to 1/8-27 NPT (oil pressure intake to

blower bolt) .Gasket-.641 ID x .93800 x .032 in. thick (oil pressure intake

to blower bolt) .Bolt-5/8-18 NF thd x 6 3/8 in. long (oil pressure intake to

blower) .Plug-Square head x .125-27 pipe thd (oil pressure intake to

blower bolt; use No. MS20995 wire; supersedes No. 17346)

CREEPER DESLUDGING CLUTCHES (-4 only)

Clutch Assembly Complete-Left hand (supersedes No. 91064) .Clutch Assembly Complete-Right hand (supersedes No. 91062) .

Shaft & Clutch Cones Assembly-Left hand (supersedes No.1459780r91063) .

Shaft & Clutch Cones Assembly-Right hand (supersedes No.145977or91061) .Shaft Assembly-Blower intermediate drive left (super-

sedes No. 77344) .Shaft Assembly-Blower intermediate drive right (super-

sedes No. 77343) .Shaft-Blower intermediate drive left (supersedes No.

77341) .Shaft-Blower intermediate drive right (supersedes

No. 77340) .Pin-Straight .204 dia x .109 in. long (intermediate

drive shaft drilled oil passage) .Spacer-Blower intermediate drive shaft high ratio

clutch thrust) .Plug-.204 dia x .410 in. long (blower intermediate

drive shaft) .

6

11

1

1111

2

1

1

1ARAR1ARAR1

1

1

1

NPNP

1

1

1

NP

NP1

NP

Page 83: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

18

26

27

31

~J

34

2524

T.O. 2R-R2000.24

7

9

21

11

Figure 20 Cr. eeper D 1es udging Cl tu ches

2-71

Page 84: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000-24

FIGURE &INDEX- DESCRIPTION UNITS

NuMBER PART NUMBER 1 2 3 4 5 6 7 PER ASSY

CREEPER DESLUDGING CLUTCHES (-4 only)

I

20-5

20-620.720.8

20.920.1020-11

20-12

20.13

20-142020202020-15

20.16202020

20

20-17

20.18

20.19

20-20

20.21

20.22

2.72

168049

1679365980346149

54114393224617

t5979859798M20t5979959799M2083217*83216*59796*50527

*59793

47036

83219*83215*59801*50527

*59806

47036

t59808

59808P559808P5P2W

59808P1059808P1bW59808P10P2W

t34732

34732P534732P5P2W

34732P1034732P10W34732P10P2W

39325

t54169

54169P10t29273

29273P529273P5P2W

29273P1029273P10W29273P10P2W

Cone-Low ratio clutch (supersedesNo. 59794,134840 or163817) .

Cone-High ratio clutch (supersedesNo. 59805) .Spring-2.634 00 (blower drive clutch) .Washer-1.373 ID x 1.91500 x .080 in. thick (high ratio

cone stop) .Spacer-Blower intermediate shaft .Retainer-Blower intermediate shaft oil ring carrier .Dowel-Straight .1875 dia x .438 in. long (blower

intermedate shaft oil ring carrier retainer) .Facing-Low ratio clutch cone .Facing sameas 59798 only .020 in. undersize .Facing-High ratio clutch cone .Facing sameas 59799 only .020 in. undersize .Gear Assembly-Low ratio clutch 7.15:1 .

Gear-Low ratio clutch 7.15:1. .Liner-Low ratio cone seal ring .Rivet-Countersunk head .1235 dia x .590 in. long (low

ratio cone seal ring liner) .Ring-4.120 10 x 4.740 00 x .280 in. thick (low ratio

desludging) .Bearing-Flanged 1.490 lOx 1.626500 x .670 in. long

(low ratio clutch gear) .Gear Assembly-High ratio clutch 9.52: 1. .

Gear-High ratio clutch 9.52: 1 .Liner-High ratio cone seal ring .Rivet.Countersunk head .1235 dia x .590 in. long (high

ratio cone seal ring liner) .Ring-4.40 ID x 5.0300 x .260 in. thick (high ratio

desludging) .Bearing-Flanged 1.490 10 x 1.626500 x .670 in. long

(high ratio clutch gear) , .Ring. Oil seal 4.375 00 x .093 in. thick (high ratio

clutch cone) .Ring sameas 59808 only .005 in. oversize .Ring sameas 59808 only .005 in. oversize on 00 & .002 in.

oversize on width .Ring sameas 59808 only .010 in. oversize .Ring sameas 59?08 only .010 in. oversize on width .Ring sameas59808 only .010 in. oversize on 00 & .002 in.

oversize on width .Ring. Oil seal4.093 00 x .093 in. thick (low ratio

clutch cone) .Ring sameas 34732 only .005 in. oversize .Ring sameas 34732 only .005 in. oversize on 00 & .002 in.

oversize on width .Ring sameas 34732 only .010 in. oversize .Ringsameas34732,only.010in.oversizeonwidth .Ring sameas 34732 only .010 in. oversize on 00 & .002

in. oversize on width .Spring - .156 00 (blower intermediate shaft oil ring

carrier retainer pinion) .Pin - Straight .3405 dia x 1.120 in. long (blower clutch

shaft oil control) .Pin sameas 54169 only .010 in. oversize .Ring - Oil seal 1.39800 x .078 in. thick (low ratio

clutch cones center) .Ring sameas 29273 only .005 in oversize .Ring sameas 29273 only .005 in. oversize on 00 & .002 in.

oversize on width .Ring sameas2'9273 only .010 in. oversize .Ring sameas 29273 only .010 in. oversize on width ' .Ring sameas 29273 only .010 in. oversize on 00 & .002 in.

oversize'on width .

.•.-,." ~~--~------- ..._" ._- ." --~._._.- --

Page 85: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R.R2000.24

FIGURE & UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2,3 4 5 6 7PER ASSY

CREEPER DESLUDGING CLUTCHES (-4 only)

20-23

20-2420-25

20-2620-2720-28

20-29

20-30

20-31

20-32

20-33

20-34

39324

3846037413

430594306018460

17783

t199721

199721M5199721M10tl37264

137264P5W137264P10Wt126215

126215M5126215M10t137265

137265P5W137265P10WMS24665-300

Pin - .125-,196 dia x 1/2 in, long (blower intermediateshaft 0 iI ri ng carrier retainer). , .

Pinion - Fuel pump drain left hand .Nut - Shear .812 Hexagon head x .500-20 NF thd x .328

in. thick (fuel drain.pinion left hand) .Spacer - Hydraulic pump drive gear right hand .Gear - Hydraulic pump driving right hand .Washer - Plain .328 10 x .8125 00 x .0937 in. thick

(hydraulic pump drive gear screw right hand) ..... ; ...Screw - Drilled .500 Hexagon head x .3125-24 NF thd

x .625 in. long (hydraulic pump drive gearright hand; useNo. AS100029 wire) .

Gear - High ratio clutch desludging 9.52: 1 (supersedesNo. 83212) .

Gear sameas 199721 only .005 in. undersize .Gear sameas 199721 only .010 in. undersize .Ring - Retaining 5.420 00 x .080 in, thick (high ratio

clutch desludging gear; supersedesNo. 83213) .Ring sameas 137264 only .005 in. oversize on width .Ring sameas 137264 only .010 in. oversize on width .Gear - Low ratio clutch desludging (supersedesNo. 59791

or 137796) , .Gear sameas 126215 only .005 in. undersize .Gear sameas 126215 only .010 in. undersize .Ring - Retaining 5.120 00 x .080 in. thick (low ratio

clutch desludging gear; supersedesNo. 59797) .Ring sameas 137265 only .005 in. oversize on width .Ring sameas 137265 only .010 in. oversize on width .

Cotterpin-.093-.098 in. dia x .750 in. long (fuel drive pinion;supersedesNo. 20545) .

11

111

1

1ARAR1ARAR1ARAR1ARAR1

1

6

-~

4

Figure 21. Impeller Intermediate Drive Gear Assembly (-7M2 Only)

2.73 ,

)

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T.O.2R-R2000-24

FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

IMPELLER INTERMEDIATE DRIVEGEAR ASSY (-7M2 ONLY)

UNITSPER ASSY

2121-121-221-321-421-521-621-721-821-9

22-1

22-2

22-3

2222-4

22-5

22-6

22-7

22-8

22.9

22-10

22-11

22-12

2.74

88738*8873746342463434306018460NAS565-215761218460NAS565-21

102795

AN122583

MS21044N5

*102561t3858P4

43858P843858P12

AN932-2

t29280

29280P329280P529280P1029280P40t15

15P1015P2015P30t48996P4

48996P848996P12t28255P4

28255P828255P1212211

39899

t18491P4

Gear Assy-Impeller intermediate drive (-7M2 only) .Gear -I mpeller (-7M2 only) .Pin-Straight headless (-7M2 only) , ..Plug (Available in .005 in. oversize AR) (-7M2 only) .

Gear-Hydraulic pump .Washer-Flat .Bolt-Machine (supersedes No. 17368) .Gear-Spur (-7M2 only) .Washer-Flat .Bolt-Machine (supersedes No. 17368) .

REAR CASE

Case & Studs Assembly-Rear .

ATTACHING PARTSWasher-plain .328 10 x .56200 x .062 in. thick (rear case to

intermediate rear case nut; use 14 units -4 and -7M2; super-sedes NO.1 72) .

Nut-Non-metalic lock .500 in. hexagon x .3125-24 thd x .344in. thick (rear case to intermediate rear case; use (14)units for -4 and -7M2; supersedes No. 33415) .

- - - - * - - --Case-Rear .Stud-Plain .375-16-24 thd x 1.938 in. long (generator

drive; supersedes No. 96197) .004 in. oversize .Stud same as 43858 only .008 in. oversize .Stud same as 43858 only .012 in. oversize .

REAR CASE

Plug - Hexagon socket .125 in. ANPT (generator drive padrecess; removable for accessory oil drain whenrequired; supersedes No. 11521) .

Bearing - Flanged 1.052 ID x 1.315500 x 1.063 in. long(blower intermediate drive shaft rear) ; .

Bearing same as 29280 only .003 in. oversize .Bearing same as 29280 only .005 in. oversize .Bearing same as 29280 only .010 in. oversize .Bearing same as 29280 only .040 in. oversize .Pin - Straight .1285 dia x .406 in. long (blower

intermediate drive shaft rear bearing) .Pin same as 150nly.010in.oversize .Pin same as 15 only .020 in. oversize .Pin same as 15 only .030 in. oversize " .Stud - Plain 3/8-16-24 thd x 1.98 in. long (starter drive)

.004 in. oversize .Stud same as 48996 only .008 in. oversize .Stud same as 48996 only .012 in. oversize .Stud - Plain .250-20-28 thd x 1.188 in. long (right & left

hand side vacuum pump spacer) .004 in. oversize .Stud same as 28255 only .008 in. oversize .Stud same as 28255 only .012 in. oversize .Dowel- Straight .1875 dia x .375 in. long (right & left

hand side vacuum pump drive spacers to rear caselocating) .

Dowel - Stepped .2495 dia x .531 in. long (right & lefthand vacuum pump drives & tachometer driveadapter to rear case locating) .

Stud-Plain .3125-18-24 thd x 2.094 in. long (main oilscreen cover) .004 in. oversize .

2222111111

17

15

NP4ARAR

1

2ARARARAR

2ARARAR

6ARAR

14ARAR

4 e~J

2

4

Page 87: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

\;-45

I I33 I L--.r62

46 L 48 L@-J:3

@/40 fJ.I /2-;';2 /~- 6123 / ~

~ // ,./'~ 27~ ~ u-28

~/ ...~ 14]-17 '". _----~-[1358 59 60 61 16I I I~~iv

ff.{;;. - - r 53~-49 ----0 .•i- 32 L

_ -~31 54

----,,---- -\

~ ... ----',,- -{43 tiU@-39

\ ~ ~\ "4l'-{41 51

\~34 52

Figure 22 R. ear Case

2-75

Page 88: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

FIGURE &INDEX- DESCRIPTION UNITS

NUMBER PART NUMBER 1 2 3 4 5 6 7 PER ASSY

REAR CASE

22.13

22-14

22-15

22.16

22-17

22-18

22-19

22-20

22-21

22-22

22-23

22-24

22-25

22-26

22-27

18491P818491P12t43042

43042P543042P1043042P1543042P2043042P30tl5

15P1015P2015P30MS51981-59

43042

43042P543042P1043042P1543042P2043042P30tl5

15P1015P2015P30MS51981-59

t39079P4

39079P839079P12t84568P4

84568P884568P12t43056P4

43056P843056P12t35807P4

35807P835807P12t14592P4

14592P814592P1243052

AN932D2

tl8524P4

18524P818524P12t24073

24073P324073P524073P1024073P40

Stud same as 18491 only .008 in. oversize ~ .Stud same as 18491 only .012 in. oversize .Bushing - Flanged .864 ID x 1.0645 OD x .630 in. long

(hydraulic pump drive shaft front) .Bushing same as 43042 only .005 in. oversize .Bushing same as 43042 only .010 in. oversize .Bushing same as 43042 only .015 in. oversize .Bushing same as 43042 only .020 in. oversize .Bushing same as 43042 only .030 in. oversize .Pin - Straight .1285 dia x .406 in. long (hydraulic pump

drive shaft front bushing) .Pin same as 15 only.010 in. oversize .Pin same as 15 only .020 in, oversize .Pin same as 150nly.030in.oversize .Plug - .156 Hexagon head x .3125-18 NC-3 thd x .312 in.

long (hydraulic pump drive shaft front bushingdrilled oil passage, supersedes No. 15842) .

Bushing - Flanged .864 ID x 1.064500 x .630 in. long(oil & fuel pump drive shaft front) .

Bushing same as 43042 only .005 in. oversize .Bushing same as 43042 only .010 in. oversize .Bushing same as 43042 only .015 in. oversize .Bushing same as 43042 only .020 in. oversize .Bushing same as 43042 only .030 in. oversize ; .Pin - Straight .1285 dia x .406 in. long (oil & fuel pump

drive shaft front bushing) .Pin same as 15 only .010 in. oversize .Pin same as 15 only .020 in. oversize .Pin same as 15 only .030 in. oversize .Plug - .156 Hexagon head x .3125-18 NC-3 thd x .312 in.

long (oil & fuel pump drive shaft front bushingdrilled oil passages, supersedes 15842) .

Stud - Plain .3125-18-24 thd x 1.438 in. long (oil inlet &outlet connection) .004 in. oversize .

Stud same as 39079 only .008 in. oversize .Stud same as 39079 only .012 in. oversize .Stud - Plain .3125-18-24 thd x 3.962 in. long (fuel pump

drive pad) .004 in. oversize .Stud same as 84568 only .008 in. oversize .Stud same as 84568 only .012 in. oversize .Stud-Plain .3125-18-24 thd x 1.625 in. long (fuel pump

adapter; use (4) units for -9A) .004 in. oversize .Stud same as 43056 only .008 in. oversize .Stud same as 43056 only .012 in. oversize .Stud - Plain .3125-18-24 thd x 1.390 in. long (fuel pump

adapter) .004 in. oversize .Stud same as 35807 only .008 in. oversize .Stud same as 35807 only .012 in. oversize .Stud - plain 0.3125-18-24 thd x 1.688 in. long (hydraulic

pump adapter) 0.004 in. oversize, supersedes No. 43056 ..Stud same as 14592 only 0.008 in. oversize .Stud same as 14592 only 0.012 in. oversize .Dowel - Flat head .251 dia x .250 in. long (fuel pump

single adapter to rear case locating) .Plug - Hexagon socket .125 in. ANPT (drilled oil holes

near starter drive pad) .Stud - Plain .3125-18-24 thd x 1.625 in. long (rear case to

intermediate rear case) .004 in. oversize .Stud same as 18524 only .008 in. oversize .Stud same as 18524 only.012 in. oversize .Bearing - Flanged 1.864 ID x 2.129 00 x .5632 in. long

(accessory drive shaft rear) .Bearing same as 24073 only .003 in. oversize .Bearing same as 24073 only .005 in. oversize .Bearing same as 24073 only .010 in. oversize .Bearing same as 24073 only .040 in. oversize .

ARAR1ARARARARAR1ARARAR

2

1ARARARARAR1ARARAR

2

6ARAR

2ARAR5ARAR1ARAR5ARAR1

2

3ARAR2ARARARAR

Page 89: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000.24

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7

REAR CASE

22-28

22-29

22-30

22-31

22-32

22-33

22-34

22-35

22-36

22-37

22-38

22.-39

22-40

22-41

22-42

22-43

22-44

22-45

22-46

22-47

t15

15P1015P2015P30t34773

34773P334773P534773P10t15

15P10

15P2015P30t75597

75597P1075597P20103711

t84567P4

84567P884567P1218461

AN122718

t9385P4

9385P89385P12t12102P4

12102P812102P12104228

27143

MS20913-3S

AN932D4

18052

MS20913-1S

41514

20178

t41815P4

41815P8t77914P4

77914P877914P12

Pin - Straight .1285 d ia x .406 in. long (accessory driveshaft rear bearing) .

Pin same as 15 only .010 in. oversize .Pin same as 15 only .020 in. oversize .Pin same as 15 only .030 in. oversize. .. . .Bearing - Flanged 1.052 ID x 1.3155 OD x 1.562 in. long

(generator drive idlegear rear) .Bearing same as 34773 only .003 in. oversize .Bearing same as 34773 only .005 in. oversize .Bearing same as 34773 only .010 in. oversize .Pin - Straight .1285 dia x .406 in. long (generator drive

idlegear rear bearing) .Pin same as 15 only .010 in. oversize .

Pin same as 15 only .020 in. oversize .Pin same as 150nly.030 in. oversize .Bushing - 1.115 ID x 1.315500 x .750 in. long (generator

drive shaft) .Bushing same as 75597 only .010 in. oversize .Bushing same as 75597 only .020 in. oversize .Pin -Straight .1260-.1270 dia x .380 in. long (generator

drive shaft bushing) .Stud - Plain .3125-18-24 thd x 1.531 in. long (lower

vacuum pump drive) .004 in. oversize .Stud same as 84567 only .008 in. oversize .Stud same as 84567 only .012 in. oversize ..........•....Pipe - 3/32 ID x .156 OD x 1 5/8 in. long (generator drive

shaft bushing oil) ~ .Pin - Straight, headles~ .250 dia x .625 in. long (rear

oil pressure pump to rear case locating;supersedes No. 62) .

Stud - Plain .3125-18.24 thd x 2.281 in. long (rear caseoil pressure pump) .004 in. oversize .........•.....

Stud same as 9385 only .008 in. oversize .Stud same as 9385 only .012 in. oversize .Stud - Plain .3125-18-24 thd x 2.938 in. long (rear case

oil pressure pump .004 in. oversize .Stud same as 12102 only .008 in. oversize .Stud same as 12102 only .012 in. oversize .Pin - Straight .1260-.1270 dia x .250 in. long (dr.illed

oil passage rear tachometer drive shaft; supersedesNo. 102905) .

Plug - Hexagon socket .0625 ANPT x .312 in. long Special(oil passage near lower vacuum pump drive boss) .

Plug - .438 Square head x .375-18 Pipe x .796 in. long(rear case cored oil passage; use No. MS20995 wire,supersedesNo.AN913-35) .

Plug - Hexagon socket .375 in. ANPT (cored passage neargenerator drive bushing) .

Plug - .375 Square head x .250-18 Pipe x .765 in. long(rear case high oil pressure; use No. MS20995 wire) .....

Plug-Square head x .125-27 pipe (vacuum pump oil return;supersedes No. 17346 and AN913-1S) .

Plug - .4375 Square head x .750-14 Pipe x 1.0625 in. long(tank vent to engine right & left hand side) .

Pin - Straight .165 dia x .250 in. long (drilled oilpassage to generator drive bushing) .

Stud - Drilled .3125-18-24 thd x 1.719 in. long (generatordrive shaft support) .004 in. oversize .

Stud same as 41815 only .008 in. oversize .Stud - Plain .250.20-28 thd x 1.469 in. long (tachometer

drive cover right & left hand side) .004 in.oversize .

Stud same as 77914 only .008 in. oversize .Stud same as 77914 only .012 in. oversize .

4ARARAR1ARARAR1ARARAR1ARAR1

4ARAR1

1

5ARAR2ARAR

2

2

1

2

1

2

4AR

8ARAR

. 2.77

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-----------------------._~,., ..,...:.~~---~~~=-----------------

T.O.2R-R2000-24

-FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7REAR CASE

I

22-48

22-49

22-5022-51

22-52

22-5322-54

22-5522-56

22-57

22-58

22-5922-60

22-61

22-62

22-6322-64

23-1232323

23-2

23-3

23-423-5

23-6

23-7

2323-8

23-9

2-78

43085

27144

58660MS20913-1S

AN932D4

234131

3235832359

4218

59243

5778814591

32164

40989

13844143084

43094*43061*43062*19788

43064

7435

4308693809

AN122583

MS21044N5

*93788t43066

43066P343066P5t15

15P10

Dowel - .220 dia x .438 in. long (generator drive shaftsupport to rear case locating) .

Plug - Hexagon socket .0625 ANPT x .312 in. long Special(generator pad; top left plug is removable foraccessory oil supply when required) .

Plug - .3025 dia x .500 in. long (starter stud oil hole) .Plug-Square head x .125-27 pipe (cored passage for rear

case high oil pressure; supersedes Nos. 17346 andAN913-1S) .

Plug - Hexagon socket .375 in. ANPT (drilled oil passagesabove oil inlet connection) .

Gasket - .62510 x .93800 x .078 in. thick (rear case plug) .Plug - Round head .625-18 NF-3 thd x .562 in. long (right

hand side of rear case; use No. MS20995 wire) .Gasket - Relief valve to pump inlet oil pressure pipe .Pipe Assembly - Pump inlet oil pressure to relief valve .

ATTACHING PARTScrew - Flat fillister head drilled .250-20 NC thd x .656 in.

long (relief valve to pump inlet oil pressure pipeflange; use No. MS20995 wire) .

- - - -* - - - -Gasket - 1.200 ID x 1.40000 x .031 in. thick (thermostat to

rear case; supersedes No. 28956) .PIug - Thermostat control replacement .Seal - 1.312 10 x .125 in. dia Round (thermostat plug; for

-9A only) .

Plug - Plain, slotted 1-9/16-16 thd x 35/64 in. long(thermostat) .

Gasket - 1 in. 10 Special (scavenge strainer plug to rearcase) .

Strainer Assembly - Rear oil scavenge .Pipe - Rear oil suction .

HYDRAULIC PUMP DRIVE

Gear Assembly-Tachometer & gun control drive .Gear-Hydraulic pump drive .Gear-Tachometer & synchronizer driven .Plug-.749 dia x .062 in. long (tachometer & synchronizer

driven gear) .Tube-.1885 00 x .028 Wall x 1.1094 in. long (tachometer &

synchronizer driven gear & shaft) .Cork-Tapered 00 1 1/16 in. & 7/8 in. 00 x .625 in. long

(hydraulic drive gear shaft) .Gasket-Hydraulic pump adapter .Adapter Assembly-Hydraulic pump (supersedes No. 43095) .

ATTACHING PARTSWasher-Plain .328 10 x .562 00 x .062 in. thick (hydraulic

pump adapter to rear case nut) (supersedes No. 172) .Nut-Non-metalic lock .3125-24 thd x .344 in. thick, .500

hexagon (hydraulic pump adapter to rear case; supersedesNo. 33415) .

- - - - * - - - -Adapter-Hydraulic pump .Bushing-Flanged 1.11410 x 1.31400 x 1.407 in. long

(hydraulic pump adapter rear) .Bushing same as 43066 only .003 in. oversize .Bushing same as 43066 only .005 in. oversize .Pin-Straight .1285 dia x .406 in. long (hydraulic pump

adapter rear bushing) .Pin same as 150nly.010in.oversize .

2

22

1

21

111

2

1

1

111

1NPNPNP1

111

5

5

NP1ARAR1AR

Page 91: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O.2R-R2000-24

•:~.t .~

512

4

~---13

Figure 23. Hydraulic Pump Drive

FIGURE & UNITSINDEX DESCRIPTION

NUMBER PART NUMBER 1 2 345 6 7PER ASSY

HYDRAULIC PUMP DRIVE

15P2015P30

23-10 t43065

43065P543065P10

23-11 16276

23-12 t84567P4

84567P884567P12

23-13 MS20913-1S

23-14 355281

--,~,23-15 MS9135-01

23-16 33201

23-17 AN122583

23-18 MS21044N5

Pin same as 15 only .020 in. oversize .Pin same as 15 only .030 in. oversize .Bushing-Flanged 1.114 ID x 1.314 OD x 1.0362 in. long

(hydraulic pump adapter front) .Bushing same as 43065 only .005 in. oversize .Bushing same as 43065 only .010 in. oversize .Pin-Straight .1285 dia x .750 in. long (hydraulic pump

adapter front bushing) .Stud-Plain .3125-18-24 thd x 1.531 in. long (hydraulic

pump adapter) .004 in. oversize .Stud same as 84567 only .008 in. oversize .Stud same as 84567 only .012 in. oversize .Plug-Square head x .125-27 pipe (hydraulic pump adapter;

drilled oil passage to rear bushing; use No. MS20995wire; supersedes No. 17346 and AN913-1S) .

Seal-Oil 1.125 ID x 1.832 OD x .437 in. Wide (hydraulic pumpadapter; supersedes No. 87552 & 241592) .

Gasket - 3.750 :in. OD X 0.15 in. thick (accessory pad; hy-draulic pump drive cover; supersedes No. 32386 andAN4044-1) .

Cover-5.000 ID x .280 in. thick (accessory pad; hydraulicpump drive) .

Washer-plain .328 ID x .562 OD x .062 in. thick (hydraulicpump cover nut; supersedes No. 172) ..... ! ••••••••••••••

Nut-Non-metalic lock .500 in. hexagon x .3125-24 thd x .344in. thick (hydraulic pump drive cover; supersedes No.33415) .

AI'<AR

1ARf.R

1

4ARAR

1

1

1

4

4

Change 1 < 2-79

~I

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T.O. 2R-R2000-24

'\

5 ,," \~':'L=:A,,/q/" 3 l_~~-{4 ~-27

6

2:}-~ ~-[23 tt-28I- 26

~ ~---14 1--2915_~./? 10 cQr--308-~1 ~-31

9--~. "--11

12~~~ @~16

17~~~ /20f--~ ~ ,2119 ----i- 22

Figure 24. Side Accessory Drives

SIDE ACCESSORY DRIVES

.,',7)..~-

24-124-2

24.3

24-4

24

24

24-5

24.6

24-724-8

24

2."0

4306387107

t24169

24169P15t8711487114P1526328

24684

281

28848

4167318005

43130

Gear-Tachometer & synchronizer driven right hand .Shaft-Vacuum pump & tachometer drive left hand (for -4 &

-7M2) .Support-Vacuum pump drive & tachometer drive right hand (for

-4 & -7M2) .Support same as 24169 only .015 in. oversize .Support-Vacuum pump drive & tachometer drive left hand .Support same as 87114 only .015 in. oversize .Pin-Straight .204 dia x .281 in. long (side auxiliary drive

recessed; for service fix) .Pin-Straight .188 dia x .250 in. long (vacuum pump support:

use (2) units with Part No. 24169 & 87114 support; forservice fix) .

Serew-Fillister head drilled .250-20 NC thd x .875 in. long(vacuum pump drive & tachometer drive right & left support;use No. MS20995 wire) .

Gear-Vacuum pump drive left hand .

Shaft-Vacuum pump drive driven left hand .Gasket-2 13/32 ID x 419/64 OD x 1/64 in. thick (accessory

drive adapter) .Cover-Vacuum pump location right hand .

1

1

1AR1AR2

4

41

1

21

-",'"".',,

~L •.

~~.

/

I

Page 93: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

FIGURE &INDEX DESCRIPTION

UNITS

NUMBER PART NUMBER 1 2 345 6 7PER ASSY

SIDE ACCESSORY DRIVES

".

24-924

24-10

24-11

2424-1224-13

24

24-14

2

24-15

24-16

24-17

24-1824-19

24-20

24-21

24-22

24-2324-2424-25

24-2624-2724-2824-2924-30

24-31

24-32

84587121904

AN960-416

MS21044N4

*33885119849t77913P4

77913P877913P12tAN126216

AN126217AN126218AN126219AN126220t24714

24714P324714P524714P10t33813

33813P333813P533813P10287780

MS9134-01

77909AN100043

AN960-416

MS21044N4

AN121552

24172121569MS35769-18

5255228781183501835217354

99642

93715

Adapter Assembly-Accessory drive left hand .Adapter Assembly-Accessory drive right hand (for -4 & -7M2

only) .

ATTACHING PARTSWasher-Plain .266 ID x .500 in. OD x .062 in. thick (accessory

drive adapter to rear casenut; supersedesNO.1 71) .Nut-Non-metalic lock .438 hexagon x .250-28 thd x .312 in.

thick; accessorydrive adapter to rear case; (supersedesNo. 12856) .

- - - - * - - - -Adapter-Accessory drive .Pin-Straight .1577 dia x .120 in. long (drilled oil hole) .Stud-Plain 1/4-20-28 thd x 1.380 in. long (accessorydrive

adapter; for usewith Part No. 84587 adapter assembly).004 in. oversize .

Stud sameas77913 only .008 in. oversize .Stud sameas 77913 only .012 in. oversize .Stud- Straight .250-20-28 thd x 1.250 in. long (accessory

drive adapter: supersedesNo. 121903; for usewith PartNo. 121904 adapter assembly) .

Stud sameasAN126216 only .003 in. oversize .Stud sameasAN126216 only .006 in. oversize , ..Stud sameasAN126216 only .009 in. oversize .Stud sameasAN126261 only .012 in. overszie .Bushing-Flanged .470 ID x .689 OD x .5005 in. long (gun

drive shaft) .Bushing sameas24714 only .003 in. oversize .Bushing sameas 2471'4 only .005 in. oversize .Bushing sameas24714 only .010 in. oversize .Bushing-Flanged .861 ID x 1.064 OD x .500 in. long (vacuum

pump driven shaft) .Bushing sameas33813 only .003 in. oversize .Bushing sameas33813 only' .005 in. oversize .Bushing sameas33813 only .010 in. oversize .

Seal-Oil .875 ID x 1.379 OD x .375 in. Wide (accessorydriveadapter; supersedesNo. 30684) .

Gasket-.016 in. thick (accessorydrive adapter cover; super-sedesNo. AS100001) .

Cover-.250 in. thick (accessorydrive adapter; for -4 & -7M2) .Cover-.359 in. thick (vacuum pump drive left hand: supersedes

No. 9632 and 91972) .Washer-plain .266 ID x .500 in. OD x .062 in. thick (accessory

drive adapter cover; supersedesNo. 171) .Nut-non-metalic lock .438 hexagon x .250-28 thd x .312 in.

thick; accessorydrive adapter cover; supersedesNo. 12856) ...Nut-Castle .250-28 thd x .282 in. thick (vacuum pump drive

cover: useNo. MS20995 wire: supersedesNo. 502) .Gear-2:1 Gun synchronizer (for -4 & -7M2) .Shaftgear-Tachometer drive (for -4 & -7M2) .Gasket-0.883 ID x 1.125 OD x .0.094 in. thick (oil pressure

relief valve; supersedesNo. AN900-14) .Valve Assembly-Oil pressure relief .

Body-Oil pressure relief valve .Plunger-Oil pressure relief valve .Spring-oil pressurerelief valve .Gasket-.688 ID x .875 OD x .078 in. thick (oil pressure

relief valve cap) .Plug-Drilled hexagon head .6875-16 thd (oil pressure relief

valve; supersedesNo. 18351) .Plug-Vacuum pump dr. bushing right hand (for enginesequipped

with right hand auxiliary vacuum pump drive) .

1

1

14

14

NP1

4ARAR

4ARARARAR1ARARAR1ARARAR2

22

1

8

8

411

11111

1

1

2.81

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T.O. 2R-R2000-24

3-~

4-~

5-1' ~,...6-.7-l.-8

9

29T 31o 28

23 .~2027

2624

),

Figure 25. Tachometer, Fuel, and Oil Pump Drives

TACHOMETER, FUEL, AND OIL PUMP DRIVES

25-5 MS9134-01

25-6 7790925-7 AN960-416

25-8 12856

25-9 8711625 *87108.25 *25153825 *4304625-10 8011

25 *1978825 251543

25-125-225-325-4

2.82

9345610126534065431936

Shaft-Tachometer drive right hand & left hand .Shaft-Dummy, (Tach drive left hand side; -4 engines) .Liner-Tachometer drive right hand & left hand shaft oil seal .Seal Option, Tachometer drive shaft right hand and left hand

(supersedes No. 25618 and 287790; procurement number con-sists of: Part No. 287781, Seal, Oil 0.687510 x 1.50400x 0.375 in. wide (optional to Part No. 287782 Part No. 287782, Seal, Oil 0.687510 x 1.50400 x 0.375 in. side(optional to Part No. 287781) .

Gasket-.016 in. thick (accessory pad tachometer drive cover;supersedes AS100001) .

Cover-.250 in. thick (accessory pad tachometer drive) .Washer-plain .266 10 x .50000 x .062 in. thick; (Tach drive

cover nut; use (8) units on -4 and -7M2; supersedes No. 171) ...Nut-Fibre .438 Hexagon head x .250-28 thd x .312 in. thick

(tachometer drive cover; for -4 & -7M2) .Shaft Assembly-Oil & fuel pump drive .

Shaft-Oil & fuel pump drive .Gear-Oil & fuel pump drive (replaces No. 87115) .Gear-Fuel pump drive intermediate .Pin-Straight .125 dia x 1.375 in. long (oil & fuel pump

drive shaft & gear) .Plug-.749 dia x .062 in. long (oil & fuel pump drive shaft) .

Screw-flat fillister head drilled 0.190-32 thd x 0.365 in.long (for use on oil & fuel pump drive gear assy No. 87115;Use No. MS20995 dia. 0.040 in. lockwire: Screw No. 251543replaces screw No. 87112) .

212

2

22

16

81NPNPNP1NP

6

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FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2. 3 4 5 6 7TACHOMETER, FUEL, AND OIL PUMP DRIVES

T .0, 2R-R2000.24

UNITSPER ASSY

25-112525-1225-1325-1425-15

25-16

25-17

252525-18

25-19

25-20

25-21

25-22

25-23

25-24

25-25

25-26

25-2725-28

25-29

25-30

25-31

26.126-22626-326-4

43103*4304843092430518458843097

AN122583

MS21044N5

*46800*4305043047

t27549

27549P527549PI027549P1543049

t27549

27549P527549PlO27549P15t84569P4

84569P8t43054P4

43054P843054P1253331

43093MS9137-01

ASI00039AN122583

AN121553

AN122583

MS21044N5

13467957092*567823098733829

Gear Assembly-Fuel pump drive .. Gear-Fuel pump driven .

Plug-.608 dia x .062 in. long (fuel pump driven gear) .Gasket-Fuel pump adapter .Adapter Machining & studs Assembly-Fuel pump drive .Adapter Assembly-Dual fuel pump .

ATTACHING PARTSWasher-plain .328 ID x .562 00 x .062 in. thick (fuel pump

single adapter nut; suoersp.desNo. 172) .Nut-non.metalic lock .500 in. hexagon x .3125-24 thd x .344 in.

thick (fuel pump single adapter; supersedesNo. 33415) .- - - - * - - --

Adapter-Fuel pump single .Adapter-Fuel pump dual .Bearing-Flanged .739 10 x .939 00 x .9112 in. long (oil &

fuel pump drive gear rear) .Pin-Straight .1285 dia x .188 in. long (oil & fuel pump

drive gear rear bushing) : .Pin sameas 27549 only .005 in. oversize .Pin sameas27549 only .010 in. oversize .Pin sameas 27549 only .015 in. oversize .Bushing-Flanged .864 lOx 1.064 00 x 1.2505 in. long (fuel

pump driving gear) .'Pin-Straight .1285 dia x .188 in. long (fuel pump driving

gear bushing) .Pin sameas 27549 only .005 in. oversize .Pin sameas 27549 only .010 in. oversize .Pin sameas27549 only .015 in. oversize .Stud-Plain .3125-18-24 thd x 1.687 in. long (fuel pump

single adapter; for -4 & -7M2) .004 in. oversize .Stud sameas84569 only .008 in. oversize .Stud-Drilled .3125-18-24 thd x 1.656 in. long (fuel pump:

supersedesNo. 48111) .004 in. oversize .Stud sameas43054 only .008 in. oversize : .Stud sameas43054 only .012 in. oversize .

Seal-Oil .875 10 x 1.50400 x .312 in. thick (fuel pump.driving gear) .

Lubricator-Fuel pump driving gear .Gasket-.016 in. thick (accessory pad fuel pump drive cover;supersedesNo. AN4059-1) .Cover-.375 in. thick (fuel pump drive) (supersedes35961) .Washer-plain .328 lOx .562 00 x .062 in. thick (fuel pump

drive covers) (supersedesNo. 172) .Nut-castled .3125.24 thd x .328 in. thick; fuel pump drive

covers. (supersedesNo. 511) .Washer-plain .328 10 x .562 00 x .062 in. thick (fuel pump

drive cover nut; supersedesNO.1 72) .Nut-non-metalic lock .500 hexagon x .3125-24 thd x .344 in.

thick (fuel pump drive cover; supersedesNo. 33415) .

GENERATOR DRIVE

Shaft - Generator drive idler 3: 1 .Shaft Assembly - Generator drive 3: 1 .

Shaft - Generator drive 3: 1 .Plug - Cup. 702 in. dia (generator drive shaft) .Pin - Straight .125 dia x 1.156 in. long (generator drive

shaft plug) ., .

1NP1111

7

7

NPNP

1ARARAR

1

1ARARAR2AR4ARAR11

11

8

8

2

2

11Np.1

1

2.83

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T.O. 2R.R2000.24

13

26-5 4309926 *4307726 *4307826-6 t43080

43080P526-7 43081

26-8 134914

26-9 AN122583

2.84

7-c:?

"fA3--~

Figure 26. Generator Drive

GENERATOR DRIVE

Gear Assembly - Lower vacuum pump intermediate drive.Gear - Lower vacuum pump intermediate drive .Gear - Lower vacuum pump intermediate drive driving.Bushing - Flanged 1.11510 x 1.31400 x .780 in. long

(lower vacuum pump intermediate drive gear) .Bushing same as 43080 only .005 in. oversize .Pin - Straight .095 dia x .391 in. long (lower vacuum pump

intermediate drive gear bearing) .Support Assembly - Generator drive shaft .

ATTACHING PARTSWasher-Plain .328 10 x .562 00 x .062 in. thick (generator

drive shaft support nut; supersedes No. 172) .

1NPNP

1AR31

4

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T.O.2R-R2000-24

.•. 1

FIGURE &INDEX

NUMBERDESCRIPTION

PART NUMBER 1 2 3 4 5 6 7

GENERATOR DRIVE

UNITSPER ASSY

26-10 AN121553~.26 *43074

'-'26-11 t134913

134913P5134913P40

26-12 33602•26-13 t15

15P10, 15P2015P30

26-14 5678326-15 43072

26-16 43071

26-17 355281

26-18 88798

26-19 AN10004126-20 AN122584

26-21 D52EE064TF

Nut-Castled .3125-24 thd x .328 in. thick; generator driveshaft support; (supersedes No. 511) 4

.. - - * - - - -Support-Generator drive shaft NPBearing-Flanged 1.115 ID x 1.314 OD x .626 in. long

(generator drive shaft support). . . . . . . . . . . . . . . . . . . . . 1Bearing same as 134913 only .005 in. oversize. . . . . . . . . . . . ARBearing same as 134913 only .040 in. oversize. . . . . . .. . . . . ARPin-Straight .1285 dia x .203 in. long (generator drive

shaft support bearing) .Pin-Straight .1285 dia x .406 in. long (generator drive

shaft support). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Pin same as 15 only .010 in. oversize. . . . . . . . . . . . . . . . . . . ARPin same as 150nly.020 in. oversize. ARPin same as 150nly.030in.oversize. AR

Gear-Generator driven 3: 1 1Tabwasher-.750 ID x 1.125 OD x .062 in. thick (generator

driven gear plug) .Plug.Round head .625-18 NF-3 thd x .750 in. long (generator

driven gear retaining) .Seal-Plain, encased 1.125 ID x 1.832 OD x .437 in. thick (oil

generator drive shaft; supersedes No. 404553) .Gasket-4.160 ID x 6.000 OD x .011 in. thick (accessory pad

generator drive cover; for Air Force engines only) . . . . . . . . . . 1Cover (accessory pad generator drive; supersedes No. 12874). . . . . 1Washer-plain .391 ID x .688 OD x .062 in. thick (generator

drive cover nut; supersedes No. 173). . . . . . . . . . . . . . . . . . . 4Nut-non-metalic lock .562 hexagon x .375-24 thd x ;453 in.

thick (generator drive cover; supersedes No. 26432). . . . . . . . . 4

LOWER VACUUM PUMP DRIVE

Gear Assembly-Vacuum pump drive driven (replaces 126121which can be reworked to No. 43141) (See T.O. 2R-R2000-23, Paragraph 6-555) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Gear-Vacuum pump drive driven . . . . . . . . . . . . . . . . . . . . . NPPlug-Cup .702 dia x .310 in. thick (vacuum pump drive

driven gear: for use with Part No. 126121 gearassembly; for Navy only) .

Plug-Cup.702 in. dia (vacuum pump drive driven gear: foruse with Part No. 43141 gear assembly; for Air Forceonly) .

Pin-Straight, headless .125 in. dia x .875 in. long(vacuum pump drive driven gear plug; supersedes No. 37) . . . 1

Pin same as AN122696 only .002 in. oversize. . . . . . . . . . . . . ARPin same as AN122696 only .005 in. oversize. . . . . . . . . . . . . AR

Plug-.lI5 dia x .125 in. long (vacuum pump driven gear: foruse with Part No. 126121 gear assembly; for Navy only) .

Adapter Machining Assembly-Vacuum pump drive .

ATTACHING PARTScrew-Flat head .250-20 NC thd x .781 in. long (vacuum pump

drive adapter to rear case). . . . . . . . . . . . . . . . . . . . . . . . . . 2

- - - - * - - - -

2-85

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T.O. 2R.R2000.24

-,--:;:.". ... --"":'".,--------,.~.,....,_ ..

..'

..

Figure 27. Lower Vacuum Pump Drive

FIGURE & UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 345 6 7

LOWER VACUUM PUMP DRIVE

II

27 *9936427-7 43082

27-8 4229

27-9 431937

27-10 MS9135-01

27-11 33201

27-12 AN122583

27-13 MS21044N5

2-86 Change 1

.'......~

Adapter-Vacuum pump drive .......•................Bushing-Flanged .865 lOx 1.03300 x 1.0552 in. long

(vacuum pump drive adapter) .Pin-Straight .1285 dia x .281 in. long (vacuum pump drive

adapter bushing) .Seal Option-Vacuum pump drive (procurement number consists of:

Part No. 287783 Seal-Oil .875 lOx 1.50400 x .375 in. Wide(optional to Part No. 287784) Part No. 287784 Seal-Oil .87510 x 1.50400 x .375 in. Wide (optional to Part No. 287783) ..

Gasket -:3.750 in .• 00 x 0.015 in. thick (accessory pad;vacuum pump drive cover to rear case; supersedesNo. 32386 and AN4044-1) .

Cover-5.000 lOx .280 in. thick (accessory pad vacuum pumpdrive) .

Washer-plain 328 10 x .562 00 x .062 in. thick (vacuum pumpdrive cover nut; supersedes NO.1 72) .

Nut-non-metalic lock .500 hexagon x .3125-24 thd x .344 in.thick (vacuum pump drive cover; supersedes No. 33415) .

NP1

1

1

4

4

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/

T.O.2R-R2000-24

2

----1

~-13

21 =- ,-- 1~~ 1 If,,,! ~6 -= . ~ @,;;>17 II I5- tI9@1,ll--15

1

1/ Iil I

3~~_2:V! .,.,10--~ 14 lfj ~~

~~-J ~. .'1£-

/111 '~IJVI

10-C":) /25-1J fIJ-24 Ifij_. ;'

2~I_iii_26 !VUlt ~30

W ~--9 / ~-31 JI _J G-32_.

L___ ,Figure 28. Rear Oil Pump

2-87

-- .;

Page 100: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

FIGURE &INDEX'~ DESCRIPTION

NUMBER PART NUMBER 1 2 3 4 5 6 7

UNITS"'PER'ASSY;

REAR OIL PUMP

2ARARARARAR

1ARAR2ARAR

1ARARARARARARARARARAR

4

3

2

2

AR1ARAR1NP

ARARAR

1111

2AR

11111

Gasket- 31/410 x 4 3/8 00 x 1/32 in. thick (rear oil pumpbody: use colloidal graphite specification M IL-G-26548

, on gasket surfaces at assemb'ly). .Pump AssemblYCon'lplete - Rea(oil (supersedes No. 87118) .

Shaft Assembly - Oil scavenge"pump idler .Plate - Oil 'scavenge pumpe~d. ; .Shaft - Oil s'cavenge pump'idler : .Pin - Straight, he'adless, lock;125.dia x .812 in. long

. (oil scavenge pump id,ler shaft; supersedesNo. 35568) .!, . :.. ~ ( .

Body - Oil scavenge pump upper." ~ .Body - Oil scaven'ge pump !ower. '•. :. : .Body - Oil. scavenge pump,~ . "'. :' .. ".' : : .Ring - Seal 3.216'00 'X .101 thick x .093 in. Wide (oil

scavenge pump sections; supersedes No. 8138) . ' .Ring same as 314047 only .005 in,:ollersize on 00 .Ring same as 314047 o'nly .005,'ih. oVersize'on.OO &

.010 in. oversize on width ..• : .Ring same as 314047 only .0lD in~ oversize on 00 .Ring same as 314047 only .010 in. oversizeon width ..•......Ring same as 314047 only .0lD in, oversize on 00 &

.010 in. oversize on width ' .Ring - Seal 3.21600 x .101 thick x,.2480in.Wide (oil. scavenge pump secti.ons; supersedes NO..30805) .Ring same as 314055 only'.005 in. oversize on 00 .Ring same as 314055 only .010 in. oVersize on 00 ..Cover Assembly - Rear oil pump ',.. '.:: .

Cover - Rear oil pump , ...•. ',: .;' .Bushing - Flanged .590 10 x .81400 x .442Jn. long

(rear oil pump drive gear) .. :: .Bushing same as.37527 only .005 in. oversize':- .Bushing same as37527 only .010 in:oversize. ;' .Stud-Shouldered.250-20NC-28N F Hid x 5.906 in. long

(rear oil pump cover) .004 in. oversize.': ,.': .Stud same as 33035 only .008 in. oversize .. .'."'., : :Stud same as 33035 only .012 in. oversize .

Screw - Fillister head 1/4-28 thd x 5 45/64 in; long(rear oil pump sections attaching). . . .. . •. . .

Washer - Plain .266 lOx .50000 x .062 in. thick(rear,,,,' oil pump cover nut; supersedes No ..171Y .-.'." .Washer - Plain .25510 x .468 00 x .032 in. thick (rear, oil pump cover nut; supersedes No. 12156). , .< .Nut -Castle .250-28 thd x .282 in. thick (rear ail pump

-co'ver; supersedes No. 502) .KeY - Flat .750 x .1275 x ,150 in. (oil scavenge pump , ',upp'ergear; supersedes No. 87) ~: ;." .

.' Key.- Flat same as 224883 'only .002 in. oversize .,Key- F'lat same as 224883 only .005 in. oversize , ..'Key- Flat same as 224883 only .010 in. oversize: .Key - Flatsame as 224883 only .020 in:'oversize: : .Key - Stepped,same as 224883 only .020 in. oversize .Key" Hit sam'e as 224883 only .030 in. oversize , .•....Key - Steppeds,ame as 224883 only .030 in. oversize ' .K~y '~.Stepped s'ame as 224883 only .040 in. oversize, ' .Key. Stepped same as 224883 only .050 in. oversiZi;! ',' .Key - Stepped same as 224883 only .060 in. oversize .Key - Flat 1.060 x .1275 x .150jn. (oil scavenge pump

lower gear; supersedes No. 20759) .Key - ~Iatsame as.224882 only .002 in. oversize '.' .Key. Flat same as 224882 only .005 in. oversize '0 •••

Key - Flat same as 224882 only .010 in. oversize .' .Key. Flat saine as 224882 only .020 in. oversize .Key - Stepped same as 224882 only .020 in. oversize .

29815

1356321383468711333017MS9486-58

3301813563433020t314047

314047P5314047R1

314047P10314047PIOW314047R2

t314055

314055P5314055P10.37587*36932t37527

37527P537527P10t33035P4

33035P833035P1233036

AN960-416

N AS620-416 L

AN121552

t224883

224883P2224883P5224883P10224883P20224883P20S224883P30224883P30S224883P40S '..224883P50S224883P60St224882

224882P2. 224882P5224882P10224882P20224882P20S

28-20 '

28-11

28-16

28-17

28-18

28-19

28-122828-13

28-15

28-14

28-1

28-228.328-428-528-6

28-728-828-928-10 :

.2.88

L

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T.O.2R-R2000.24 ;'T.O.;2R-R2000:24

,-FIGUHE,& '.t. ,~",' .. ,,",~ .. ~._.' -,~-~ _. "--~•..•.. ,._' . ,- ~" ..,._. ~,"~~ - -_.~ '. .. ....•.. ..... '.. •.. .>--. ,~- ..~.." . ...UNITSINDEX DESCRIPTION PER ASSY

NUMBER PART NUMBER 1 2 3 4 5 6 7 .

REAR OIL PUMP

28-21'

-" .•..~~~•. :.:Q::.~~l.'28-22;;-

28-23

28-24

28-25

28-26

28-27

28-28

28-29

28-30

28-31

28-32

29-129.229-329.429-5

29.6

29.729-8

29-9

29-10

29-11

29.12

2929-13

29-14-29-15

29-16

224882P30224882P30S224882P40S224882P50S224882P60S87109,'"

L ->•••.".~..

1841120763

20764

29781

29782,

MS20913'3SI' '.;,;

20189'; x;:MS246,65-227

.. t<.-:)AN12258'~

MS210M,N5........,...""--',-~"'. ;:

10485874693215771048388698

MS35769-29

57790 .AN121502

234

183748

22053

AN123884

206849206848

152599152633"

152617

Key. Flat sameas 224:882 only .030'in. oversize .Key - Stepped sameas'224882.orily .030 in. oversize'. .. : .Key.-..5tepped sameas:224882.onIY'.040 in. oversize .... ; :.. (

. Key-Stepped same.:as224882 only.050 rn.~oyersize:",. ; .,,;,'Key'~Stepped sameas 224882 only.060in: oversize ..,;'Shaft-Oilpurt,pdrive 'r: ? :'.: ' .

REAR'qILPUMP

Gear - Keyed .6025.dia x 1.0605in.ibrig~(OiLsCave~gepump uppe'r) " :,".' :'., .•... ': :.

Gear - Drilled hole .561 dia x 1.0605 in. long (oil ','scavengepump upper 'idiet) .. ' '.,•. " ' : ; .• : .. ::

• J' ' ••• ~- :: ~ '.

Gear- Keyed .6025 dia x 1.4065 in.lon'g(oil scavenge ,., jpumplower) '," ' : ' , , .Gear - Drilled hole .561 dia x 1.4cj'65 in. long (oLi ", .

. scavengepump lower) : , 'Gear - Keyed .6025 dia x 1.7485 in. long (oil pre?surE! .

pump) '..c. •. : •••Geilr - Drilled hole .561 dia x 1.7485 in. long (oil ' .' .

Ii pressure pump) ". : . , .PIYJg- .438 Sq'udrehead x .375-18 Pipe x .796 in. long

. (rear oil pump cover at idler shaft, supersedesAN913-3S).Plug - .375 Square head x .500-14 Pipe x .8750 in. long

(rear oil pump cover at oil pump drive shaft) ..C6tterpin-.078 dia x .500 in. long (rear oil pump to rear

,'. casenut;supel'sedes No. 7916) .Washer" Plain .328 ID x .562 OD x .062 in. thick (rear oil

•' ,pump to rear casenut; supersedesNo. 172) ; .Nut~nori'-il\etalic lock .500 hexagon x .3125-24 thd x .344

. :in. rhick (rear oil pump to rear case;supersedesNo .3'3415) .

MAIN OIL SCREEN, REAR BREATHER,AND OIL PRESSURE RELIEF VALVE

Va:lveAssembly - Relief ; ..Body' -'Oil pressure relief valve '.' , •......Plunger - Oil pressure relief valve : ', . :' !,. : ..Spring - .470 OD (oil pressure relief valve pL\Jnger) :,.:Screw- 1j4-28 thd x 1 3/32 in. long (oil pressure reli,ef

valve adjusting) , >':' : : ..Gasket -'1.195 ID x 1.438 OD x .094 in. thick (oil pressure

, '. relief valve cap to rear case;supersedesNQ. AN900'19) ....Housing": Oil pressure relief valve '.':'. , <" .

. Nut - Pla(n, hexagon head .438 x .250-28NF-3 'th~' .. 'x .219 in. thick (oil pressure relief valve'" ; .

,. acorn cap; supersedesNo. 501) ; ; .'.::.Gasket ,::,625 ID x .938 OD x .078 in. thick (oiipr~ssure'.,

re}ief valve acorn cap) ,. -Cap~.'625-18 NS thd (oil pressure relief valve': 'use:", ..

No. MS20995wire;supersE!d~sNo. 8699) .. '." ',' ..Pin - Straight.Oq4idiax .375 ih;.long (oil,pressurerel,ief 11,

valvebody"r6'rear,case,).; (0': .:: ::;.:- .... :",0 .. '.:( .....Seal - "0" Ring oifresistant-L724-L744;ID x 2.000:0D

x .135-.143 in. thick (outer oil'scree'n upper .ferrule to inner rear case) ': ';:> .

Screen Assembly - Main oil (supersedesNo. 152064 or 152618) .Body Assembly - Oil return check valve (supersedes

No. 152597) .Valve - Oil return check .

.Spring', .3500Dx 1.117 in. long Free length compression". (oil retu.rn check valve) .. '.' , , .

Washer- .400 ID x .500 OD x .120 in. thick (oil returncheck valve spring retaining) , .

ARARARARAR1

1

1

.1

..;.' ,.

7

NP111

11

11

11

1

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ToO. 2R.R2000.24

~--9

20-0~

r/,23 21 ~~ --2% 8-- 8I 119-~ c::»

~~~_22L ~-10

, '24

27-0 ~-29

28-01S-30

25-0

Malon01"1Screen, Rear Breather, and Oil Pressure Relief ValveFigure 29.

2.90

L

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T.O. 2R-R2000-24

FIGURE & UNITSINDEX DESCRIPTION

.NUMBER PART NUMBER 1 2 345 6 7

PER ASSY

29-17

29-1829-1929-2029-212929-22

29-23

29-2429-2529-2629-27

29-28

29-2929-30

29-3129-3229-33

29-34

29-35

29-36

29'37

29-38

29-39

29-4029-41

29-42

29-43

2929-4429-45

29-46

29-47

MS9486-28

317029317028185006152825*152598152625

. 119407

169355 4'126512152634AN122583

MS21044N5

t 4098920126

470574705247059

47061

47056

AN122583

AN121553

MS'24665-227

MS9136-01

ANI00041AN122584

D52EE064TF

84107

AN4171-2428595MS21044N5

AN122584

D52EE064TF

MAIN OIL SCREEN, REAR BREATHER,AND OIL PRESSURE RELIEF VALVE

Lockpin - Steel .0938 dia x .375 in. long (oil returncheck valve; supersedes NO.AN150233) .

Spacer - Oil screen outlet (supersedes No. 151443) .Spacer - Oil screen inlet (supersedes No. 151442) .Screen - Oil (supersedes No. 152536) .Support Assembly - Oil screens & spacers .

Support - Oil screens & spacers .Pin - Headed .120 dia x .135 in. long Special (oil

screens & spacers support) .Plug - Hexagon head 1.062-12 thd x .680 in. long (use

No. MS20995 wire) .Spring-Oil return check valve (supersedes No. 152619) .Gasket-3.401 ID x .067 in. thick (main oil screen cover) .Cover-Oi I screen .Washer-plain .328 ID x .562 OD x .062 in. thick (main oil

screen cover nut; supersedes No. 172).Nut-non-metalic lock .500 hexagon x .3125-24 thd x .344 in.

thick (main oil screen cover; supersedes No. 33415) .

Gasket-1.000in. ID Special (main oil screen cover plug) .Plug-1.000 Hexagon head x No. 1-18 thd x 31/32 in. long (main

oil screen cover; use No. MS20995 wire) .Shim-Rear breather body .Body-Rear breather .Gasket-1.000 ID Pipe flanged x .018 in. thick (rear breather

pipe to rear breather body) .Pipe Assembly-Rear breather '.-;, '.

ATTACHING PARTScrew-Fillister head drilled .250-28 N F thd x 1.688 in. long

(rear breather pipe flange to rear case; use No. MS20995wire) .

*Washer-plain .328 ID x .562 OD x .062 in. thick (fuel pump

drive to intermediate rear case nut; supersedes No. 172) .Nut-castled .3125-24 thd x .328 in. thick (fuel pump drive to

intermediate rear case nuts; supersedes 511) .Cotterpin-.078 dia x .500 in. long (fuel pump drive to inter-

mediate rear case nut; supersedes No. 7916) .Gasket-.016 in. thick (accessory pad starter drive cover to

rear case) (supersedes 93695, AS100003 and AN4047) .Cover-accessory pad (starter drive; supersedes No. 12874) .Washer-plain .391 ID x .6B8 OD x .062 in. thick (starter drive

cover nut; supersedes No. 173). . . . . . . . . .. . .Nut-non-metalic lock .562 hexagon .375-24 thd x .453 ir. thick

(starter drive cover; supersedes I\Jo. 26432). . . .....Gasket-1 3/8 in. OD Pipe flanged (oii inlet. fi. outlet cove!'

shipping) , . , .. . .Gasket-.016 in. thick (flange oil connection;flight) .Cover-2.312 ID x .250 in. thick (oil inlet & outlet, shiplJing) .Nut-non-metalic lock .500 hexagon x .3125-24 tha x .344 in.

thick (oil inlet and outlet cover; shipping; supersedes No.33415) .

Washer-Plain .391 ID x .688 OD x .062 in. thick (rear case tointermediate rear case at generator drive cover nut;supersedes No. 173)., .

Nut-non-metalic lock .562 hexagon x .375-24 thd x .453 in.thick (rear case to intermediate rear case at generatordrive cO,ver; supersedes No. 26432) .

126255011

1111

1

4

1

111

11

2

2

2

2

11

6

6

222

6

2

2

..,I

/

!'-.-q

2..91 .J

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T..O:2RJt2000.24,

:",j , '.

".1-, .:t _;

,';'

' ..•. '

.'- , .....

. ;., :~.~,

\':'"

,-{~;>.•.-, -,'-'---'" - "~~ ... ,~

. " ~,-

"J,.;o

.J _ ",

! ~ '-•. ..:..

30.1

30-2

30118

442390

IGNftlON SYSTEM

Ignition Harness Assembly Complete (78570;fb'r detail parts-list 'see T.O;8E2.4"3-94;'for -4 engines) '.-'. ';~';.<' ';

!~:' "..' . j, 'l...' i.- 'h:.- ..-:-: ;:

Ignition Harness,Assembly Complete (785'70;fbr detail parts• 'list see t.O.8E2:.4-3'94 for "7M2erigines:onty) ! .'.~

. ; ~,.

,.\.

-, I.

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3 4

,;'

.,..,...

"...t.

31-1

31-2

31-3

10-37700

10-81725-1or

10-27625-4AN912-lD

3200X2

Figure 31. Magneto Vent System

MAGNETO VENT SYSTEM

. )V~ritilafor-magneto (77820: use antiseYz~i:bmp<;>~nd;s~~ecifica~. ; tion M I L-A-907D for threaded fittings) , " : " :- .Magneto Assy (77820: for detail parts list see T.O. 8E2-5-5-44;

for -4 and -7M2) .

Bushing-reducer (user antiseize compound specification M I L-A-9070 for threaded fittings) .

or

Adapter-.125 in. female & male pipe thread (use antiseize com-,poundspecification MI L-.A-907D for threaded fittings) .

. : ,,;-I , ",'. • -,' ~.'L ": ,<" ~'_ ,<0 .'.' .£.:": r:" .;. : ".:.).

8

2

8

4

2-9B

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T.O. 2R-R2000-24

II

Ie

I~e

---------1

I

DISTRIBUTOR BLOCK(11 HOLE)

(5 HOLE)S~LNTILLA SF14RN 8 M___ __ - AGNETO

.------

DISTRIBUTOR BLOCK(11 HOLE)

Figure 32 M. agneto to Distributor Block Atta h"c mg Parts

2.94 I

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T.O.2R-R2000-24

FIGURE &INDEX

NUMBER

DESCRIPTIONPART NUMBER 1 2 3 4 5 6 7

MAGNETO TO DISTRIBUTOR BLOCK ATTACHING PARTS(For R2000-4 and -7M2 Engines)

UNITSPER ASSY

ELEVEN HOLE CONFIGURATION

32-4 MS21044N4

'.32-5 MS20073-04-11

32-6 AN960-416

FIVE HOLE CONFIGURATION

32-7 AN4.17A

e 32-8 AN960-416

32-9 NAS620-416L

32-10 MS21044N4

32-11 MS51976-46

Bolt-machine hexagon drilled head .250-28 thd x 1.906 in. long(magneto to distributor block; 5 hole configuration) . . . . . . . . 5

Washer-plain .266 10 x .50000 x .062 in. thick (magneto todistributor block; 5 hole configuration; supersedes Nos.171 and A-24582). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

Washer-plain .255 10 x .468 00 x .032 in. thick (magneto todistributor block; 5 hole configuration; use 1 unit undernuts; supersedes No. 12156) . . . . . . . . . . . . . . . . . . . . . . . . 5

Nut-non-metalic lock .438 hexagon x .250-28 thd x .312 in.thick (magneto to distributor block; 5 hole configuration;supersedes Nos. AN365-428A and A-22646) .. -. . . . . . . . . . . . 5

Setscrew, hexagon socket 0.250-28 x 0.375 in. long Dist blkunused open holes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

18

9

9

2

2

9

Bolt-Machine, drilled hexagon head .250-28 thd x 2.031 in.long (magneto to distributor block attaching, 11 hole con-figuration; supersedes No. A-25233) .

Washer-plain .266 lOx .500 in. 00 x .062 in. thick (magnetoto distributor block; 2 units under each bolt head; 11 holeconfiguration; supersedes Nos. 171 and AN 122582) .

Washer-plain .266 in. 00 x .500 in. 00 x .062 in. thick(magneto to distributor block; use 1 unit under nuts nextto block; 11 hole configuration; supersedes Nos. 171, AN122582 and A-24577) , .

Nut-non-metalic lock .438 hexagon x .250-28 thd x .312 in.thick (magneto to distributor block; 11 hole configuration;supersedes Nos. AN365-';'28A and A-22646) .

Bolt-Machine hexagon head .250-28 thd x 1.156 in. long;magneto to distributor block; use 2 units; 11 hole con-figuration supersedes No. A-25232) .

Washer-plain .266 10 x .500 00 x .062 in. thick (magneto todistributor block; use 1 unit under bolt heads supersedesNos. 171 and A24582) .

AN4-20A

AN960-416

AN960-416

32-1

32-3

32-2

CARBURETOR AND ATTACHING PARTS - 06848(For -4 and -7M2 Engines)

For detail parts list see T.O. 6Rl-3-3-34

33-1 390926

33-2 10472133-3 77295

33 92870

33 D52EE064TF

33 MS51957-79

e 33 94870

33-4 4017633 *3560533-5 3837533-6 3837733-7 153

33-8 4222033 776633 P832033 AN7513-2

Carburetor - PD-12F-13 (06848; for detail parts list seeT.O. 6Rl-3-3-34) .

Gasket - Carburetor adapter to intermediate rear case .Bolt - .550-.564 Hexagon head x 8.500 in. long

(carburetor holddown; shipping & installation) . . . . . . 4Washer - .375 Bolt size special cupped (carburetor

holddown nut) . . . . . . . . . . . . . . . . . . . . . . . . . . . 4Nut-non-metalic lock .562 hexagon x .375-24 thd x .453 in.

thick (carburetor holddown; supersedes No. 26432). . . 4Screw-Round head .250-20 thd x .500 in. long (carbure-

tor air screen shipping; supersedes No. AN515-416-8) .. '. . 4Tube-1.8125 10 x 1.562 in. long x .062 Wall (automatic

mixture control protector; shipping). . . . . . . . . . . . . . . 1Screen Assembly-Carburetor air intake NO.4 mesh. . . . . . . 1

Screen-Carburetor air NO.4 mesh. . . . . . . . . . . . . . . . . NPWasher-Carburetor air screen packing . . . . . . . . . . . . . . 1Packing-Carburetor air screen. . . . . . . . . . . . . . . . . .. . 1Rivet-Round head .095 dia x .375 in. long

(carburetor air screen packing). . . . . . . . . . . . . . . . . 5Gasket-Carburetor air screen. . . . . . . . . . . . . . . . . . . . . . 2Tag-Carburetor warning ..... ; . . . . . . . . . . . . . . . . . . . 1Dehydrator-Storage, carburetor (supersedes No. 80003) . 1Indicator-Humidity (supersedes No, 55705) , . , .... , .. , . 1

2-95

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-.~

",;e~)l'C)',,:P~il,O ,f"

~;

,'<,3(; ' .•'.,. j i .~":__,..) 'i/j l-:l"""~ :.t -it" ~t ~.~

''''''.0-,- ,','",.. ,_.~t.,"~'. 'v"~::=:!'1'~'T;_="~~~~:-'.~~._,~15-~

@-6

", ", , ) -" ",J", ',,' "~~~_4

~-8

3

L12

; I,~

13,~!; - ", ,:: ".:, ),-.-,

, ;.....

..~u

~.

" >. .~

., .•..-".':-,

. J:-~~ ~l. r

-:; -:;"t.,",'," i';.

co' :"f ,','

. ,' .. "' , ,. '- ~\"~

' ••• ~ ' I"

"

C~.RBU.Rf::TORANb;ATT~C,H"NGPARTS - 06848" "~';:(FoJ,4:a,nd:71\i12Ellginesr _.,' 'Fordetail parts list's,ee,Tog: 6Rr3.3:34 '

. ,

.. ;..'

7

2

22761219 ft311

11

1

940203430126196

34835

49710

29085

Band;Rippled paper (c~rburetor shipping) 0 • 0 •••

': \ ,:.': "Gasket.Carburetcrr fuiil'feed' pipeb'r'citket. .. 0 ••• 0 • 0 ••• 0

-Gasket~;812 lD'x'1.125'OD x .078 in. thick (interme-".~ diater-ear fuel feed Pipe)' ..... 0 '. 0 ••••••••• 0 0 • 0 • 0

,,', ,Bolt-13/16.16 NS thd x 13/8 in.,1oqg (intermed iate rear " .', "case fue(jntaket::: '," :, . ,",' .";' ;" 7'.":"

" MS20913-1S ~'c; c., _, ~Lug,S.quar,ehead xo125~~t'pipe thd)~ .,578 in. long . ',r'"(conneCtor-assembly),:,,,' : '.: 00 0 0 •••• 0 • ~.,

111075 .,' .,. ',cchn.ector'Assemhly-Blow:edtiroateriginepriming :'; ~78187 "'Pr,ot~ftor.~,c,:or.~er~~rb,~r~~?rcartori: .. < ','/,,0 ......•. 0 "

,~ 54442 Cleat,Carload Ing carburetor cart(:m 0 0" •• 0 • 0 ••••••• 0 ••• :'. --

56572 ' " ; i S~rev~-Drive,No. 10 X}Yl)ri:)ong (carlciading~arburetor c~rtpn) : ','"54434 .' ,'" ' . v.Strap.-5/8 WidEix,Q15 iri~(car-lciading,carburetor carton). 0 : '0 0 -. ". '. '

54437 ,,' Se~I:3/4 'in.,Wide (carloading" carburetor carton) .. 0 •••• , ••• ,. ','

94190. H,':;(:dver_Carburetorpad(shippin'g).:';,:,: .. ,:-: 0 •••••• : ;:".:

94191 i.<'",', Coiier-lndudion"poi:+diH:ivdrator:. ,0' :'" ',0 •••••• 0 ••••• 0.0

AN122584 \. 'Washer,plairi .391IDx.6880l:>' x :062 in. thick (carburetor pad ,;. ',' s~ip'pin'g:tover;superseMs No;:173):'. :"'" '. '"Bolt-Shouldered .562 Hexagon h'ead x•.375:24 NF thd x 1.0625 in> ' , '

long (cad:iuretor p~d ~hipi:>ingcoveriuse No. MS20995 ,.u, '

Wire).: '.~ ',:::' ... ,",'::",'.:,;:0 :.'. :":',. ••• •••• • 0 0... 7~ .","" "ITag:Warning, fue,I,.',," •. ,""," '.co.',' .... . . . . . . ... 0 ••• 0 ,33

33

3333.933-10

33-11

33-12

33.133333333333333333

-::.""• i -~

. ,1:;'

: ,;""". - .

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Page 110: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

NJMERICAL INDEX (cont)

T.O. 2R-R2000-24

PART NllMBER FIG. ~AND qry rz:lU H

INDEX PER ~~<rz:l

NO. ARI'.~8~8PART NUMBER FIG. rz:l ~

AND (Jr"l U H

~~<rz:lINDEX PER 00 ~8m. ARI'. tl)U

(AN900-18) 8-6.(AN900-19) 29-6 (AS123791)(AN900-20) 14-40

17-27 (AS123806)AN912-1D 32-3 8(AN913-3S) 14-11

22-40 (#AS125271)28-28

(AN931-11-16) 12-4213-35

AN932-2 16-35 4 PI S (AS125290)16-4122-5

AN932D2 2-21 96-1816-1522-25

AN932D4 16-6 4 #AS12529122-41 (#AS125291)22-52

(AN935-10) 18-17AN960-416 2-34 236 PI S

7-687-7212-3915-35 #A.S12572115-3715-4216-917-2524-1024-20 AS195860R425-7 C4PHlOll-3128-16 C4PHlOll-3332-2. C4P10710-132-3 C4P10710-332-6 C4P107109-2732-8

(AS100001) 24-17 C4SC1018-11i,;}2:\4 25-5 C4SC1018-13~t~";;(AS100003) 29-39 C4SC1018-15

AS100039 25-27 1 C4SC1018-17(AS123770) 18-10 C4SCI018-19

19-39 C4SC1018-21(AS123773) 6-33 C4SCI018-23AS123775 8-5 8 C4SC1018-25AS123788 3-26 1 C4SC1018-27(AS123790) 6-23 C4SC1018-29

7-532-446-166-299-139-5212-1612-1812-2412-3212-312-412-1012-1312-1912-2012-3112-7 14012-1012-1312-1912-2012-2112-2212-3112-912-1212-1612-1812-2312-279-51 AR13-2 213-3 213-2 113-3 113-2 213-313-22 113-26 113-12 113-9 113-21 113-16 113-24 113-14 113-20 113-15 1

Ii

I 3-2

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tlJMERICAL INDEX (cant)

T.O. 2R-R2000-24

PARI' NUMBER FIG. ~ P:::AND ('frY U HP:::~ <~INDEX PER ~A p..,A

00 ~8ID. ARI'. (l)U

C4SCI018-31D52EE064TF

H2A008-001

MIL-C-6985AND,TYPE A

(r-tIL-G-26458)MIL-H-6000MS122030HS122122f>1S17840-1r1S20073-04-11MS20426AD3-4

MS20426AD4-5

PART NUMBER FI<:,. ~ P:::AND qry U HP:::~ <~INDEX PER ~A p..,A

00 ~oNO. ARI'. (l)U P:::U

13-13 1 ~1S20426AD4-5 13-34-55 34 pI S 13-55-16 ~1S20426AD4-6 12-10 2826-21 12-1329-42 12-1929-47 12-2034-3 12-2112-3 82 PI S 12-2212-4 12-3112-10 13-1712-13 13-1812-19 ~1S20470AD3-4 12-1 657 PI S12-20 12-212-21 12-312-22 12-412-31 12-613-1 12-713-2 12-813-3 12-1013-5 12-1313-17 12-1913-18 12-2014-24 2 PI S 12-21

12-2211-15 AR pI S 12-3114-25 AR pI S HS20470AD4-5 12-20 63 PI S18-17 6 12-227-10 2 12-3111-47 28 pI S ~1S2047OAD4-6 13-17 82 PI S32-5 2 PI S 13-1812-16 44 PI S ~1S20913-lS 6-24 32 PI S12-18 la-5312-24 15-1712-32 15-2213-11 16-4013-12 18-3113-14 19-4613-15 22-4313-16 22-5112-3 100 PI S 23-1312-4 HS20913-3S 14-11 4 PI S12-10 22-4012-13 28-2812-19 r'LS20913-6S 5-12 1 pI S12-20 (HS20995) 2-6 AR P1 S12-31 2-3513-1 2-3913-2 2-42

3-3

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~1EB.ICAL, IND~-(GontJ, ,-' /.' '. "'. . ,. ,.,

"

122 PI S

AR-, .'~~i,'s..35 "" PI S'"

23 ,PI"S

6 pI S19 PI S

:i'.:':~''pi s,.i "'Pl'S"5 . PI S

. ,

18

1 PI S224 pI S281 PI SARAR

33-13. .'. '-;" ...

" 9-4512-46

", _.' 18-41(;t-: 12-38

18-39.}...• ---. -

24-11" +-.1

24-21." 2-43-35•. f -'

, ". 5-10i 5-2114-414-2616-418-2722-323-7

" 23 ..-18t - ( :

. , 25-1725-3127-13

, 28-3229-28'29-45 (5-285-116-3318-1019-39

',. 6-38,; 15-39

17-3228-306-47

I' 2-446-166-237-5320-346-299-5210-2610-411-454-411-4511-45

( ~.

.." '-~

~1S24665-229~1S24665-300

~1S21044N4

~1S21044N7MS21083N5MS24665-151

(MS20995) ,(MS20995N51)HS21044N3'

MS24665-370

~1S27151-13~1S2715i-19~1S27215-2MS27423-4~1S29509-1~1S29509-3

HS21044N5

MS24665-227

~C' \ •• <

•• J i.,' , .•_

'. , '.. " ..L _.

"

,,) .,,'. \- ,',;

"r ..FIG., ,1 ANDi INDEX00.

.. ->

, " ~~

3-14~ .• or:

3-155-12

:-- i 5-14'~ i •. ,., •

5-20p t. ~'.<.f 7-5~'.~"::~~. ".7-61

CI. _'

7-65{,~~- ':" 7-69f: - ~. 7-73'\ " ....~. l. 9-29('.: .~.; 9-31- " 10-29~,~....."."! 10-30F- ". f 11-12~,:~.~.14-2

14-11'., ,< ' 14-27,. , 14-34, 14-41

15-14":.J 15-17

'. 15-22,-'; 15-23. ",~ .. -

15-3215-34

" 16-1016-2216-3016-4217-2618-1818-3218-4618-4819-46

.•.. r'. '

" 22-40.~; & •• :.

22-42" ;. 22-54

22-5723-1324-524-2225-1029-10

'.~-"29-2529-3029-35

- ".)

(HS20995)

.3-4

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tU1ERICAL INDEX (cont)

T.O. 2R-R2000-24

HS35769-21MS35769-26MS35769-29~1S35769-31(MS35769-39)(MS35769-41)MS51957-79

e MS51958-60t-tS51976-46MS51981-59MS9018-01MS9018-02MS9018-03MS9018-04MS9018-09MS9018-10r-1S9122-04t.1S9134-01MS9135-01

MS9136-01MS9137-01MS9164-009

Ie MS9164-029

MS9486-28MS9486-58NAS565-21NAS620-416L

PARI'Nur1BBR FIG. r~AND qry ~UINDEX PER p::~ <~~e:l p.,e:l00. ARI'.00 ~8tf.lU

I.

MS29513-139MS3397-13MS35191-254MS35276-264MS35489-19

MS35769-11MS35769-18

11-58 145-13 1 PI S12-24 10 PI S12-3211-60 14 PI S12-42 1412-4413-3611-34 1 PI S5-3 4 PI S8-98-3224-258-6 1 PI S2-38 1 PI S29-6 1 pI S17-27 1 PI S14-3814-4033-3 4 PI S10-54 14 PI S32-11 422-16 322-1810-18 1410-18 AR10-18 AR10-18 AR10-18 AR10-18 AR5-26 2 PI S8-2224-17 4 PI S25-523-15 2 PI Z.27-1029-39 1 PI S25-26 1 PI S2-26 AR3-2027-32-26 AR3-2027-329-17 1 Pl-S28-621-6 221-911-43 92 PI S28-17

PART NUMBER FIG. I~~AND (]IT Up::~ <~INDEX PER ~e:l p.,e:l00 ~8NO. ARI'. tf.lU

32-9(P-6792) 8-11P8320 34-8 1ZEB1805-054 15-6 30 PI SIDI09 2-43 18 PI S*100414 12-3 NP

12-4#100415 12-4

13-5*100415 12-3 NP#100536 9-21 110078 10-34 14(100949) 9-47tl01116 8-2 1101116P4 8-2 AR101116Rl .8-2 AR*101234 9-1 NP(101236) 9-1101265 25-2 1 PI S*102488 16-4 NP*102561 22-3 NP#10-27625-4 31-2102795 22-1 1(102905) 22-38103672 10-68 3103711 22-32 110-37700 31-1 810-81725-1 31-2 2104228 22-38 2104721 33-2 1104838 29-4 1104858 29-1 NP(105264) 9-32105731 9-15 2106319 5-32 4#tl06749 7-33 4 PlDS1C6749PI0 7-33 AR106749P15 7-33 AR106749P40 7-33 AR#tl06750 7-33 3 PIDS106750PI0 7-33 AR106750P15 7~33 AR106750P40 7-33 ARtl06751 7-33 4106751PIO 7-33 AR106751P15 7-33 AR106751P40 7-33 AR#tl06753 7-33 5 PlDS

OIange 1 3-5

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T.O. 2R-R2000-24

N.Jr>1ERICALINDEX(cant)

PARTNUMBER FIG. w P::;AND QrY U HP::;W <wINDEX PER ;::l~ P-<~

00 ~8NO. ART. UlU

PARTNUMBER FIG. w p::;AND ~f u Hp::;w <wINDEX PER ;::l~ P-<~

-" 00 woID. ARI'. UlU P::;U

106753PI0 7-33 AR106753P15 7-33 AR #107774106753P40 7-33 AR#tl06754 7-33 4 PIDS106754PI0 7-33 AR106754P15 7-33 AR106754P40 7-33 AR#tl06756 7-33 4106756PI0 7-33 AR106756P15 7-33 AR #107775106756P40 7-33 AR*106757 7-58 NP106758 7-58 28106759 7-67 1106760 7-71 1 #107777*106957 9-46 NP106965 9-46 12107425 19-15 1107614 10-61 28 PI S #107780107615 10-63 .14 PI S

10-64 #107781107615PI0 10-63 AR pI S107619 12-45 61 #107782

13-37*107714 14-5 NP107718 5-24 1 #107783*107748 12-9 NP107749 12-9 11

13-8 107784*107752 12-12 NP107753 12-12 2

13-10*107754 12-16 NP*107764 12-30 NP 107785107765 12-'30 9

13-25*107766 12-34 NP107767 12-34 4 107794

13-27 108203#107771 12-16 12 108253

12-1813-11 10873313-12 *10927013-14 10927113-15 10927213-16 10<)273

#107772 12-9 9 (109273)12-12 109274

3-6

13-812-23 1312-2713-1913-2013-2113-2213-2313-2412-30 1012-3413-2513-2613-2712-20 912-2213-1713-1812-9 213-812-9 213-812-12 313-913-1012-1213-913-10.12-16 613-1113-1213-1413-1513-1113-1213-1413-155-35 15-19 112-41 1413-345-8 13-5 NP3-11 13-13 13-2 13-13-28 1

I

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( .

...~.--~--~-_._------_.-----c-~~~~~~~~~~~~--------------.--- __

T.O. 2R-R2000-24

NUMERICAL INDEX (cant)

PARI' NUMBER FIG. f;Ll ~A\JD QJY U H

~f;Ll <t:f;LlINDEX PER ;::JO p-<O

00 f;Ll000. ARr. CIlU ~U

---_.PART NUMBER FIG. f;Ll ~

AND qry U H~f;Ll <t:f;Ll

INDEX PER ;::JO p-<O00 ~8 iNO. ARr. CIlU

Page 116: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

NUMERICAL IND)'.X(cent)

t12102P4 22-37 2 125392M11W 4-25 AR12102P8 22-37 AR 125392M13W 4-25 AR#121049 5-14 8 12539~1l5W 4-25 AR121318 14-41 1 125392Ml7W 4-25 AR121319 7-38 2 125392Ml9W 4-25 AR121323 7-35 6 125392M21W 4-25 AR121325 8-14 1 125392t-123W 4-25 AR121332 8-29 1 125392M5W 4-25 ARt121336P4 7-43 3 125392M7tv 4-25 AR121336P62 7-43 AR pI S 125392M9W 4-25 AR121336P8 7-43 AR 125392P15\'l 4-25 AR121337 7-34 14 125465 14-28 1(12156) 11-43 125471 14-30 1

28-17 125473 14-32 1121569 24-24 1 (125474) 14-8121573 9-11 8 125475 14-34 1121574 9-12 8 125491 14-5 1tl21575 9-10 R 125492 14- 1121575P10 9-10 AR (125809) 7-55*121647 10-48 NP 125810 7-54 1*121648 10-44 NP #12584 8-36 1#121830 11-53 7 t126056 7-15 168#121831 11-53 7 126056P10 7-15 AR(121839) 11-11 126056P20 7-15 AR(121903) 24-13 126056P30 7-15 AR PD S#121904 24-9 1 126056P40 7-15 AR PD S(122) 2-30 (126121) 27-112211 22-10 4 tl26215 2()-32 112317P12 10-24 AR 126215MI0 20-32 ARtl2317P4 10-24 14 126215M5 20-32 AR12317P8 10-24 AR tl26239 9-8 2(123502) 16-1 126239P10 9-8 AR#123554 5-14 4 126239P2 9-8 ARtl25072 4-23 6 126239P20 q-8 AR125072Pl 4-23 AR 126239P5 9-8 AR125072P5 4-23 AR (126375) 9-45125072P7 4-23 AR #126419 2-30 1125208 8-24 1 126440 5-34 1125234P2~1 10-58 28 pI S 126512 29-25 1

10-59 28 126535 15-1 110-60 14 12669 10-19 14

125234P4W 10-58 28 PI S 126874 7-49 110-59 28 tl27097P4 7-45 110-60 14 127097P62 7-45 AR pI S

125310 8-19 1 127097P8 7-45 AR*125353 8-28 NP (127139) 7-1125391 4-31 246 *127140 7-1 NPt125392 4-25 6 127145 7-12 112

PART NLlMBER FIG. ~ ~AND \!fY U H~~ <t:~INDEX PER ::JO P-lO00 ~8N). ARl'. CflU

3-8

PART NUMBER FIG. ~ ~AND (frY U H

~~ <t:~INDEX PER ::JO P-lO00 ~8NO. ART. CflU

Page 117: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

NJJI1ERICALI~EX (cant)

T.O. 2R~R2000-24

PART NUMBER FIG. ~ ~AND qry U H

~~ <~INDEX PER :=>0 P->O00 ~o

m. ARI'. CJ)U ~u

127146tl27170127170P10(127247)(12734)#t127422127422M30127422P10127422P20127422P3127422P30127422P40127422P5127422P50127422P60127422Rl127422R2127422R3127422R4127422R5127422R6127422R7127422R8127422R9127599

12765

127880127916127917(127942)(1'27944)(127951)(128290)(12856)

12856128565

*128566128567*128568(12874)

PART NillffiER FIG. ~ ~AND qry U H~~ <~INDEX PER :=>0 P->O00 ~oNO. ART. CJ)U ~u

7-13 56 (129) 16-227-7 4 131 18-43 27-7 AR 22-547-1 13417 19-26 62-3 20 134448 2-18 110-9 14 134679 26-1 110-9 AR (134840) 20-510-9 AR 134869 4-16 110-9 AR 134870 9-29 110-9 AR 134877 19-31 110-9 AR 134911 18-14 110-9 AR (134912) 18-810-9 AR tl34913 26-11 110-9 AR 134913P40 26-11 AR10-9 AR 134913P5 26-11 AR10-9 AR 134914 26-8 110-9 AR 134944 8-21 210-9 AR 8-2310-9 AR (135011) 4-110-9 AR 135180 9-3 110-9 AR 135228 10-32 1410-9 AR (135413) 9-910-9 AR 135632 28-2 110-9 AR P1DS 135634 ' 28-8 110-46 28 *135705 4-30 NP10-50 135822 7-50 112-40 14 135903 7-51 113-33 24 *135982 6-3 NP27-4 1 PI S #135983 6-3 110-44 14 135984 6-2 110-48 14 136 16-5 27-63 t13618 10-12 287-63 13618P12 10-12 AR10-36 13618P30 10-12 AR5-7 13618P4 10-12 AR12-38 13618P62 10-12 AR18-39 13618P8 10-12 AR24-11 136249 5-30 124-21 (136913 ) 19-3425-8 8 19-3512-3 2 *136914 19-20 NP13-5 136915 19-3812-3 NP 137073 14-29 112-5 2 (137233) 9-813-6 t137264 20-31 212-5 NP 137264P10W 20-31 AR26-19 137264P5W 20-31 AR29-40 t137265 20-33 2

3-9

Page 118: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

~

T.O. 2R-R2000-24

nm1EPICAL INDEX (cant)

PARTNUHBER FIG. w ~ PARTNill1BER FIG. ~wAND Q'IY u H AND QI'Y u H~w <w ~w <wINDEX PER ::':>0 P-<O INDEX PER ::':>0 P-<O

00 WO 00 gaSNO. ARl'. CIlU ~U NO. ART. CIlU

137265P10v7 20-33 AR 142641P8 7-46 AR137265P5W 20-33 AR tl42642P4 7-39 6*137481 12-23 NP 142642P60 7-39 AR#137482 12-23 13 142642P62 7-39 AR

12-27 142642P8 7-39 AR13-19 (142643) 7-4213-20 (142953) 10-54 ~ j

13-21 143519 8-8 113-22 #143575 12-9 18213-23 12-1213-24 12-16

#137483 12-23 13 12-1812-27 12-2313-19 12-2713-20 12-3013-21 12-3413-22 #143744 18-41 113-23 143745 18-33 113-24 #143747 18-41 1

137484 12-23 7 (143991) 2-613-19 *143992 7-1 NP

*137485 12-20 NP *143993 7-1 NP137486 12-20 12 tl44355 10-8 14

13-17 144355PI0 10-8 AR*137487 12-27 NP 144355P20 10-8 AR137488 12-27 3 144355P30 10-8 AR

13-23 144355P40 10-8 AR*137489 12-22 NP 144355P5 10-8 AR137490 12-22 2 144355P50 10-8 AR

13-18 (14438) 11-1137547 19-29 1 144542 9-6 4(137796 ) 20-32 144722 4-28 1138346 28-3 1 (14538) 18-34138441 22-63 1 #t145899 2-24 1138547 19-37 1 145899P10 2-24 AR138609 19-20 1 14591 15-41 2138863 8-28 1 22-60139275 2-15 14592P12 15-7 AR13940P12 10-17 AR 22-23 ARtl3940P4 10-17 77 tl4592P4 15-7 3313940P8 10-17 AR 22-23 AR14096 11-14 56 14592P8 15-7 ARt(141375) 17-1 22-23 AR142142 19-33 1 (145977) 20-142484 10-39 14 (145978) 20-t142641P4 7-46 2 145996 7-6 14142641P60 7-46 A,-q (145997) 7-6142641P62 - 7-46 AR *145998 7-1 NP

}-10

Page 119: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

NUHERICAL INDEX (cant)

T.O. 2R-R2000-24

PART NUHBER FIG. >x.l ~Al\ID (]I'Y U H

~>x.l ~>x.lINDEX PER ~~ P-<~00 ~8m. ARI'• CIlU

(146035)*146111*14611214634(147300)(147302)147620*148048(148675)149533*149697149698t15

15PI0

15P20

15P30

PART NUMBER FIG. >x.l ~AND (]rY U H~>x.l ~>x.lINDEX PER ~~ P-<~00 >x.l0NO. ARr. CIlU ~U

7-1 16-2120- NP 22-720- NP 22-149-50 12 22-1711-8 22-2811-9 22-3019-22 1 23-912- NP 26-1318-5 (150246) 7-12-5 1 tl50755 9-18 1

8-7 tIP 150755P5 9-18 AR8-7 1 #150932 9-15 16-10 17 #150933 9-15 19-4 150934 9-19 115-11 150935 9-14 116-21 (150936) 9-122-7 151037 6-13 122-14 (151442) 29-1922-17 (151443) 29-1822-28 (151733) 9-122-30 *152063 19-17 NP23-9 (152064) 29-1226-13 152224 ' 4-59 16-10 AR (152536) 29-209-4 (152597) 29-1315-11 *152598 29-21 NP

16-21 152599 29-14 122-7 152617 29-16 122-14 (152618) 29-1222-17 (152619) 29-2422-28 152625 29-22 122-30 152633 29-15 -.J.

23-9 152634 29-26 126-13 152814 3-28 16..10 A,.~ 152815 3-29 19-4 152816 3-8 1

15-11 152817 3~30 116-21 152818 3-4 122-7 152819 3-1 122-14 152820 3-21 122-17 152821 3-10 1

22-28 152822 3-9 122-30 152824 3-12 ,

.L

23-9 152825 29-21 1

26-13 (15283) 16-66-10 AR 152848 3-16 19-4 153 34-7 515-11 tl53071 10-5 7

3-11

Page 120: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

-24

NT.H1ERICALINDEX (cant)

FIG. w IX: PART NUMBER FIG. w IX:AND QrY U H AND ('frY U HIX:w <w IX:w <wINDEX PER O~ P-<~ INDEX PER o~ P-<~00 WOCf)U IX:U 00 ~8N). ARI'. NO. ART. Cf)U

10-5 AR 160637P15W 4-29 AR e10-5 7 160637P30W 4-29 AR10-5 AR (161701) 11-1110-1 7 (162513) 12-910-1 7 12-123-22 1 12-1612-19 NP 12-18 Ii

12-19 1 12-2312-21 6 12-2712-21 NP tl62625 7-59 28 ~12-18 1 162625P10 7-59 AR13-16 tl6268 4-58 212-16 4 16268P10 4-58 AR13:...11 16268P10P10W 4-58 AR13-12 16268P10P20W 4-58 AR PI S13-14 16268P10W 4-58 AR13-15 16268P20W 4-58 AR2-16 1 16268P5 4-58 AR2-15 16268P5P10W 4-58 AR PI S7-33 3 P1DS 16268P5P20W 4-58 .A.-q PI S e7-33 AR (16274) 7-627-33 AR 16276 23-11 17-33 AR 163283 18-7 1 pI S7-33 3 P1DS 163286 18-9 17-33 AR 163287 18- 17-33 AR (16330) 3-37-33 AR 163540 4-51 17-1 163817 20-518-8 1 *163818 20-2 NP18- 1 163819 20-1 17-61 163820 20- 111-44 84 PI S *163822 20-2 NP4-32 6 163823 20-2 13-23 1 163824 20- 117-28 164448 7-110-41 14 166023 12-16 611-20 28 13-11 911-25 166025 12-18 111-30 166131 9-44 411-39 (166145) 12-1611-20 28 PI S 12-18 e11-25 #166313 10-54 1411-30 166582 9-32 211-40 16681 9-2 14-30 6 (16715) 10-U~22-15 167936 20-6 222-18 (167959) 17-274-29 6 16804 18-30 1

PART NUHBER

15307lRl#t153072153072Rl153084#153085154965*155536155537155538*155539#155839

#155840

T.O. 2R-R2000

t160637

156010156011#t156072156072P10156072P15156072P40#t156073156073P10156073P15156073P40(156075)156560#156561(15670)156822157247157741(157772)158175#158188

158189

158403(15842)

3-12

Page 121: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

NUMERICAL INDEX (cent)

T.O. 2R-R2000-24

,- i

e (17346)

PART NUMBER FIG. ~ ~AND gry U H

~~ <~INDEX PER Pt=l P-<t=l

00 ~8ro. Am'. Cf.lU

168049169355(171)'

17187(172)

(172254)(173)

PART NUMBER FIG. ~ ~AND OJY U H~~ <~INDEX PER Pt=l P-<t=l

00 ~8NO. ARr. Cf.lU

20-5 2 19-4629-24 1 22-432-34 22-517-4 23-137-68 17354 24-30 17-72 (17368) 21-612-39 21-915-35 174137 18-5 115-37 (174576) 9-2215-42 (17490) 5-416-9 (175599) 7-6 1417-25 t175993 4-21 624-10 175993P1 4-21 AR24-20 175993P5 4-21 AR25-7 175993P65 4-21 AR28-16 17634 15-14 22-27 1 17783 20-29 12-3 178027 4-22 63-34 (17930) 10-85-9 18005 24-814-3 18052 15-23 1315-5 16-2216-3 16-4218-26 18-3218-45 \ 22-4222-2 (18185) 7-523-6 18350 24-28 123-17 (18351) 24-3125-16 18352 24-2925-28 183748 29-10 125-30 18380 18-46 126-9 184420 15-30 127-12 184428 19-36 228-31 18460 20-28 429-27 21-529-36 21-84-1 18461 22-34 14-54 29 18470 28-22 126-20 18471 28-23 129-41 18491P12 22-12 AR29-46 t18491P4 22-12 433-13 18491P8 22-12 AR6-24 32 185006 29-20 5010-53 18502 8-13 115-17 (18502) 8-915-22 18515P12 17-2 AR16-40 t18515P4 17-2 1218-31 18515P8 17-2 AR

3-13

Page 122: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

NmlERICAL INDEX (cant)

18517P12 17-3 AR 20178 22-45 1t18517P4 17-3 2 20180 28-29 118517P8 17-3 AR (201991) 5-718524P12 22-26 AR (20218) 4-36t18524P4 22-26 3 *202684 19-2 NP18524P8 22-26 AR 202877 19-2 118529P12 15-9 AR 20297 19-28 6tl8529P4 15-9 2 20298 19-27 1218529P8 15-9 AR - 202999 19-1 1192188 9-30 1 20303 19-19 1192189 19-35 1 203170P12 7-42 AR192190 19-34 1 t203170P4 7-42 6tl9286 15-18 32 203170P62 7-42 AR19286P12 15-18 AR 203170P8 7-42 AR19286P4 15-18 AR 20362 4-24 619286P62 15-18 AR t20363 4-20 219286P8 15-18 AR 20363P2 4-20 AR(195189) 19-1 20363Rl 4-20 ARtl95860 9-51 4 PIDL t204506 4-27 6195860Ml 9-51 AR 204506P15~'J 4-27 AR195860MlO 9-51 AR 204506P30W 4-27 AR195860M12 9-51 AR (204529) 4-36195860M14 9-51 AR 20543P12 2-10 AR195860Ml6 9-51 AR t20543P4 2-10 8195860M18 9-51 AR 20543P8 2-11 AR195860M2 9-51 AR (20545) 20-34195860M20 9-51 AR 206848 29-13 1195860M4 9-51 AR #206849 29-12 1195860M6 9-51 AR 207045 10-67 1195860M8 9-51 AR 20731 2-12 10195860P10 9-51 AR (20759) 28-20195860Rl 9-51 AR 20763 28-24 1195860R2 9-51 AR 20764 28-25 1195860R3 9-51 AR #207888 7-62 AR*19788 23-1 NP 209051 19-3 1

25-10 (21027) 11-60tl9795 17-6 1 212383 19-2 119795P15 17-6 AR *213527 4-18 NP19795P3 17-6 AR (213528) 4-1819795P4 17-6 AR 214091 4-18 1(198220) 9-51 (214092) 4-18199721Ml 20-30 1 215 2-17 419972lM10 20-30 AR 21577 29-3199721M5 20-30 AR *21779 9-32 NP#t20117 14-41 1 218 27-6 220117P3 14-41 AR (218863) 14-8#20126 14-41 2 219 #12-7 10

29-30 18-18

3-14

PART NUMBER FIG. ~ ~AND ([IT U H

~~ ~~INDEX PER ;::>A p-<A

00 ~o!\D. ARr. trlU ~U

PART NUMBER FIG. ~ ~AND qry U H

~~ ~~INDEX PER ;::>A p-<A

00 ~oNO. ARI'. trlU ~U

Page 123: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

NUMERICAL INDEX (cant)

T.O. 2R-R2000-24

.'

PART NUHBER FIG. ~ P:::AND QrY u HP:::>:il <tJ>:ilINDEX PER ;::JO P-<O00 ~8NO. ARI'. oou

21903 12-49 1422053 29-11 1(22118) 9-5222157 4-35 622290 12-35 7

13-2822375 16-17 2(22473) 6-47t224882 28-20 2224882PI0 28-20 AR224882P2 28-20 AR224882P20 28-20 AR224882P20S 28-20 AR224882P30 28-20 AR224882P30S 28-20 AR224882P5 28-20 AR224882P50S 28-20 AR224882P60S 28-20 ARt224883 28-19 1

. 224883PI0 28-19 AR224883P2 28-19 AR224883P20 28-19 AR224883P20S 28-19 AR224883P30 28-19 AR224883P30S 28-19 AR224883P40S 28-19 AR224883P5 28-19 AR224883P50S 28-19 AR224883P60S 28-19 ARt224886 3...;27 1224886PI0 3-27 AR224886P2 3-27 AR224886P20 3-27 AR224886P20S 3-27 AR224886P30 3-27 AR224886P30S 3-27 AR224886P40S 3-27 AR224886P5 3-27 AR224886P50S 3-27 AR224886P60S 3-27 AR224999 7-55 1225634 7-62 12225635 8-26 2225636 8-27 1225637 7-61 622673P12 10-21 ARt22673P4 10-21 722673P8 10-21 AR

PART NUMBER FIG. >:il P:::AND QrY u HP:::>:il <tJ>:ilINDEX PER ;::JO P-<O00 >:il0NO. ARr. oou P:::u

22744P12 7-16 ARt22744p4 7-16 222744p8 7-16 AR(230625) 5-7 123144 11-3 56

#11-5#11-6#11-7

#t23145 11-4 5623145P15 11-4 AR234 18-42 3

22-5329-9

23407 9-9 2(23964) 8-1023996 14-19 1(24050) 19-38t24073 22-27 224073P10 22-27 AR24073P3 22-27 AR24073P40 22-27 AR24073P5 22-27 ARt24075 19-40 124075P2W 19-40 AR24075P4W 19-40 ARt24076 19-41 124076P2W 19-41 AR24076P4W 19-41 AR24077 19-21 124118 15-40 1(241592) 23-14t24169 24-3 124169P15 24-3 AR24172 24-23 124234 19-44 124248 19-45 1(24304) 4-1424305 4-12 124306 4-11 124652 17-8 1#24684 24-4 4t24714 24-14 224714P10 24-14 AR24714P3 24-14 AR24714P5 24-14 ARt24856 7-23 4

7-2424856P10 7-23 AR

3-15

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NUHERICAL INDEX (cant)

T.O. 2R-R2000-24

PART NUMBER FIG. ~ ~AND ('!JY U H

~~ <t:~INDEX PER ~~ p..,~

00 ~o00. ARl'• CfJU ~u

7-2424856P3 7-23 AR

7-2424856P5 7-23 AR

7-24#t24919CL A 9-42 424919CL B 9-42 AR24919CL C 9-42 AR24919P1D 9-42 AR24919piE 9-42 AR24919P1F 9-42 AR24919P10A 9-42 AR24919P10B 9-42 AR24919P10C 9-42 AR24919PllD 9-42 AR24919PllE 9-42 AR24919PllF 9-42 AR24919P15A 9-42 AR24919P15B 9-42 AR24919P15C 9-42 AR24919P16D 9-42 AR24919P16E 9-42 AR24919P16F 9-42 AR24919P5A 9-42 AR24919P5C 9-42 AR24919P6D 9-42 AR24919P6E 9-42 AR24919P6F 9-42 AR*24920 9-42 NP249280 2-6 224934 14-15 125 7-26 125070 7-27 125086 14-18 1*251538 25-9 NP#251543 25-10 6(252804) 10-5225336 10-15 14253848 10-29 4525618 25-4 2258 16-7 4(25850) 3-11

3-1325855 5-20 225858 4-34 625869 5-23 2

8-18I 25870 5-22 2

l 3-16

PART NUMBER FIG. ~ ~AND ('fr':l U H

~~ <t:~INDEX PER ~~ p..,~

00 ~oNO. ARl'. CfJU ~U

8-1726049 14-14 126056P12 17-12 AR

17-15t26056P4 17-12 18

17-1526056P8 17-12 AR

17-15*260877 4-1 NP260899 4-1 1#26161 15-43 1#26162 15-43 1#26163 15-43 126196 14-33 5

18-4733-10

26198 6-14 1t26199 6-6 126199P10 6-6 AR26199P3 6-6 AR26199P30 6-6 AR26199P5 6-6 AR26240 9-41 10

#9-429-43

#26328 24-4 2(26432) 4-55

5-1626-2129-4229-4733-3

26448 9-39 5#9-42

t26475 19-16 426475P10 19-16 AR26475P10P10W 19-16 AR26475P10P2W 19-16 AR26475P10P5W 19-16 AR26475P10W 19-16 AR26475P15 19-16 AR26475P15W 19-16 AR26475P5 19-16 AR26475P5P10W 19-16 AR26475P5P2W 19-16 A.~26475P5P5W . 19-16 AR26475P5W 19-16 AR26475R1 19-16 AR

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NJMERICAL INDEX (cant)

T.O. 2R-R2000-24

PART NillffiER FIG. r:il ~AND (frY U H~r:il ~r:ilINDEX PER ::;JP p..P

00 r:il0NO. ARI'. cnU ~U

PART NUMBER FI~. ~r:ilAND (m.' U H~r:il ~r:ilINDEX PER ::;JP p..p

NO. 00 woART. cnu ~u

26475R2 19-16 AR 28462 19-43 126475R3 19-16 AR 28464 10-40 2826486 9-31 8 28595 29-44 226553 7-22 1 287778 18-34 126689 4-53 10 287780 24-16 2t27 6-5 4 (287783) 27-9.II 27P11 6-5 AR (287784) 27-927P6 6-5 AR 287788 18-34 127143 16-38 3 28781 24-27 1:~ 22-39 (28822) 8-9 127144 4-57 5 28848 24-6 115-25 (288904) 2-3016-39 (288917 ) 6-34

22-49 (288918) 6-34(27144) 9-15 (288922) 4-51(27190 ) 4-49 288936 2-30 427191 4-56 1 288949 ~34 1273087P12 17-1 AR 288952 4-51 1#t273087P3 17-1 2 (28956) 22-58273087P6 17-1 AR #29085 34-13 7273087P9 17-1 AR t29273 20-22 4t27549 25-}9 2 29273P10 20-22 AR25-21 29273P10P2vv 20-22 AR27549P10 25-19 AI~ 29273P10W 20-22 AR25-21 29273P5 20-22 A.~27549P15 25-19 AR 29273P5P2W 20-22 AR25-21 t29280 22-6 227549P5 .25-19 AR 29280P10 22-6 AR25-21 29280P3 22-6 AR(27592) 10-7 29280P40 22-6 AR27646 19-30 1 29280P5 22-6 AR(27843) 7-63 1 29614 4-10 127956 7-64 7 29615 4-7 1281 24-5 4 29781 28-26 128151 2-24 32 29782 28-27 16-40 29815 28-1 17-29 #29945 12-7 137-32 29981P12 7-17 AR15-29 t29981P4 7-17 216-19 29981P8 7-17 ARe 16-24 3H-12-4800 11-37 1 FT.16-33 30118 30-1 128255P12 22-9 AR 302561 4-8 1t28255P4 22-9 14 30489 17-16 228255P8 22-9 AR t30643 16-18 7282991 11-9 14 30643P4 16-18 AR282992 11-8 14 30643P8 16-18 AR#283110 9-32 2 (30684) 24-16

3-17

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T.O. 2R-R2000-24

NJHERIC'AL INDEX (cant)

(30805) 28-11 32336P4 7-28 AR30987 26-3 2 32336P8 7-28 AR

#27-2 323419 14-8 131153 2-11 10 32358 22-55 13115Q 6-21 2 32359 22-56 131157P12 2-9 AR (32386) 23-15t31157P4 2-9 8 27-1031157P8 2-9 AR t32544 10-6 14t314047 28-10 2 32544PI0 10-6 AR314047PI0 28-10 AR 32544P3 10-6 AR314047PI0vl 28-10 AR 32544P5 10-6 AR314047P5 28-10 AR 32735 11-10 56314047R1 28-10 AR #t32818CL A 9-42 4314047R2 28-10 AR 32818CL B 9-42 ARt314055 28-11 2 32818CL C 9-42 AR314055PI0 28-11 AR 32818PID 9-42 AR314055P5 28-13 P-R 32818PIE 9-42 AR31416P12 7-19 AR 32818PIF 9-42 ARt31416P4 7-19 16 32818PI0A 9-42 AR31416PB 7-19 AR 3281BPIOB 9-42 AR31537 6-3 3 32818PI0C 9-42 ARt31538 7-21 1 32818PllD <)-42 AR31538P4 7-21 AR 32818P11E 9-42 AR31538P8 7-21 AR 32818PllF 9-42 AR(31540) 7-11 32818P15A 9-42 AR

31541P12 7-11 AR 32818P15B 9-42 AR

t31541P4 7-11 18 32818P15C 9-42 AR31541P8 7-11 AR 3281SP16D 9-42 AR

(31542) 2-6 32818P16E 9-42 AR31543 8-31 1 32818P16F 9-42 AR

317028 29-19 25 32818P5A 9-42 AR317029 29-18 26 32818P5B 9-42 AR

(31706) 4-32 32818P5C 9-42 ARt31707 4-26 6 32818P6D 9-42 AR31707H13W 4-26 AR 32818P6E 9-42 AR31707Ml5W 4-26 AR 32818P6F 9-42 AR31707Ml7VJ 4-26 AR 32820 7-66 131707Ml9VJ 4-26 AR 32909 14-12 131707M41W 4-26 AR 32971 2-39 131707M23W 4-26 AR 33017 28-5 131707P15W 4-26 AR 33018 28-7 1*31776 9-42 NP 33020 28-9 1(31853 ) 10-39 33035P12 28-14 AR3200X2 31-4 4 t33035P4 28-14 2

32164 22-61 1 33035P8 28-14 AR32331 10-42 14 33036 28-15 2t32336 7-28 1 33146 14-7 132336P2 7-28 AR 33201 23-16 2

3-18

PART NUMBER FIG. >il p:::AND QrY

u HP:::>il <>ilINDEX PER :;:JP p.,P00 >il0NO. ARI'• CJ)U p:::u

PART Nill1BER FIG. >il P:::AND ('frY U HP:::>il <>ilINDEX PER :;:JP p.,P00 gagNO. ART. CJ)U

.,

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- -- ------~~~~~~~~~~~~~~~~~~~~~~~~~--------

T.O. 2R-R2000-24

NUMERICALINDEX (cont)

PART NUHBER FIG. ~ p:::

AND ('frY U Hp:::~ ~~

INDEX PER :::>0 0.-.000 ~o

NJ. ARl'• rf.lU P:::U

#t332403332403PI0332403P20332403P30332403P40332403P5033254133254233254433254633254733254833334(33415)

t3353233532P1233532P433532P83357503357513360233605t3361633616p433641*33645*33663337475

t33813

PART NUMBER FIG. ~ P:::A..1'ID QrY U HP:::~ ~~

INDEX PER :::>0 0.-.000 ~oNO. ART. CIlU p:::u

27-11 33813PI0 24-15 AR10-13 14 PD S 33813P3 24-15 A.R.10-13 AR 33813P5 24-15 AR10-13 AR 33829 26-4 110-13 A..R. *33885 24-11 NP10-13 AR 339764 5-29 110-13 AR (34020) 8-264-45 1 34065 25-3 25-2 1 34079 11-20 14 PI S2-29 1 11-254-47 1 11-304-46 1 11-384-48 1 340932 10-36 14 PI S10-16 28 t34119P4 2-23 182-4 16-233-35 16-325-10 34119P8 2-23 AR5-21 16-238-16 16-3214-4 34120 18-16 114-28 34137 10-20 1416-4 34194 4-50 118-27 34207 6-20 122-3 t34212 6-4 123-7 34212P10 6-4 AR23-18 34212P5 6-4 AR25-17 34212P62 6-4 AR25-31 (34218) 6-3427-13' 34301 33-9 128-32 (34368) 17-1029-28 t34732 20-19 229-45 34732PI0 20-19 AR16-13 1 34732P10P2~il 20-19 AR16-13 AR 34732pI0Vl 20-19 AR16-13 AR 34732P5 20-19 AR16-13 AR 34732P5P2~il 20-19 AR16-8 1 34755 10-38 1416-1 1 34770PI0 2-8 AR26-12 1 34770P5 2-8 AR18-38 1 34770P62 2-8 AR P1DL16-14 1 t34773 22-29 116-14 AR 34773PI0 22-29 AR11-2 7 34773P3 22-29 AR11-1 NP 34773P5 22-29 AR10-14 NP t34804 16-20 12-28 2 34804PI0 16-20 AR4-43 34804P5 16-20 AR24-15 2 34806 19-18 1

3-19

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T.O. 2R-R200Q-24

NUB ERICAL INDEX (cont )

34834 16-27 1 t35787 15-10 234835 33-11 1 35787PI0 15-10 AR#351136 10-66 AR 35787P3 15-10 AR352143 4-36 2 35787P5 15-10 A.-q(352144) 4-36 35807P12 22-22 AR35233 18-12 1 t35807P4 22-22 1#(35431) 12-3 35807P8 22-22 AR.

12-4 35875 10-66 2812-10 t35876 10-65 1412-13 35876P5 10-65 AR12-19 (359233) 2-3012-20 (359239) 6-3412-21 35924 14-41 112-22 (35961) 25-2712-31 36061 2-41 113-1 36088 6-8 213-17 36088P5 6-8 AR13-18 36090 18-21 1

35431 12-7 1 36103 4-6 2#35432 12-1 167 (36113 ) 4-8

12-2 36115 2-33 812-3 36130 4-39 112-4 36132 4-42 112-6 36252 2-31 212-7 *36444 4-55 J'JP12-10 36445 4-52 112-13 (36227) 2-2312-19 #36639 11-35 112-20 36640 4-44 112-21 *36700 9-32 NP12-22 #t367350 7-33 212-31 367350PI0 7-33 AR

35433 12-47 14 367350P15 7-33 AR35434 12-48 14 367350P40 7-33 ARt35446 15-8 #t367351 7-33 3

15-28 367351PI0 7-33 AR35446P12 15-8 AR 367351P15 7-33 AR

15-28 3fi7351P40 7-33 AR35446P20 15-8 AR *36932 28-12 NP

15-28 #36942 12-9 14435446P4 15-8 AR 12-11

15-28 12-1235446P8 15-8 AR 12-14

15-28 12-15355281 23-14 2 12-16

26-17 12-17(35568) 28-6 12-18*35605 33-4 NP 12-19

3-20

PART NUH...J:3ER FIG. w P:::AND CJrY u H

INDEX PER P:::w <t:w~o ~ot-n. ARl'. 00 wocnU P:::U

PAAT NUMBER FIG. P:::QI'Y wAND U HP:::w <t:wINDEX PER ~o ~o

NO. 00 gagART. cnu

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NUMERICAL INDEX (cant)

T.O. 2R-R2000-24

PART NUMBER FIG. f;<:l P:::AND qry U HP:::f;<:l<f;<:lINDEX PER O~ p..~

00 f;<:l000. ARr. cnu p:::u

(37)

3708537413*374384t374385374385Pll374385P14374385P17374385P2374385P25374385P27374385P5

12-2012-2112-2212-2312-2412-2512-2612-2712-2812-2912-3012-3212-3312-3412-3513-813-913-1013-1113-1213-1413-1513-1613-1713-1813-1913-2013-2113-2213-2313-2413-2513-2613-272-263-2027-314-3120-259-219-219-219-219-219-219-219-219-21

21NP1ARARARARARARA.R.

PART NUMBER FIG. f;<:l P:::AND (JrY u Hp:::f;<:l <f;<:lINDEX PER O~ p..~00 f;<:l0

, NO. ART. cnu p:::u

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T.O. 2R-R2000-24

NUMERICA.L INDEX (cent)

39324 20-23 2 4229 4-2 339325 20-20 2 27-839899 22-11 2 42745 6-45 240176 33-4 1 t43042 22-13 2402888 7-3 1 22-16402987 11-1 14 43042P10 22-13 AR(404553) 26-17 22-1640500 6-36 4 43042P15 22-13 AR40606 9-35 2 22-16#40835 14-41 1 43042P20 22-13 AR40943 18-35 1 22-16(40944) 18-33 43042P30 22-13 AR40945 18-37 1 22-1640946 18-36 1 43042P5 22-13 AR(40947) 18-28 22-1640989 22-62 2 *43046 25-9 NP

29-29 43047 25-18(41017) 4-51 *43048 25-11 NP41385 18-11 1 43049 25-20 141451P12 18-29 AR *43050 25-17 NPt41451P4 18-29 3 43051 25-13 141451P8 18-29 AR 43052 22-24 141452 19-7 4 43054P12 25-23 AR41514 22-44 2 *43054P4 25-23 4t41624 4-33 6 43054p8 25-23 AR41624P30vJ 4-33 A...~ 43056P12 22-21 AR41673 24-7 1 43056P4 22-21 1#41764 9-29 4 43056P8 22-21 ARt41815P4 22-46 4 43057P12 17-4 AR41815P8 22-46 AR t43057P4 17-4 2(41861) 6-45 43057P8 17-4 AR41862 6-43 43059 20-26 1(41863) 6-45 43060 20-27 2t41870 6-11 2 21-441870P10 6-11 AR *43061 23-1 :NP41873 6-46 2 *43062 23-1 NP42 7-25 1 43063 24-1 142038 9-:-17 2 43064 23-2 1t42039 9-16 2 t43065 23-10 142039P3 9-16 AR 43065P10 23-10 AJ~42039P6 9-16 AR 43065P5 23-10 AR42042 9-5 2 t43066 23-8 142051 4-17 1 43066P3 23-8 AR42117 4-5 1 43066P5 23-8 AR4218 22-57 2 43071 26-16 14220 12-37 88 43072 26-15 1

13-29 *43074 26-10 NP42220 33-8 1 *43077 26-5 NP

3-22

--~- ------

PART NillffiER FIG. ~ p,:jAND (lr'f U Ho::~ <~INDEX PER ;:JO P-+O00 gagNO. ARr. CfJU

PART NUMBER FIG. ~ 0::AND (lr'f U H

INDEX PER o::~ <~;:JO P-+ONO. ARI'.00 gagCfJU

1

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T.O. 2R-R2000-24

Nill1ERICALINDEX (cent)

NUHBER FIG. ~ P:: PART NUMBER FIG. ~ P::j'lND (]IT U H AND QI'Y U Hp::;~ <~ p-::~ <~INDEX PER ::::Ji=l P-<i=l INDEX PER ;::Ji=l P-<i=l

NO.00 ~o 00 ~8ARI'. cnU P::U NO. A~T. cnu

78 26-5 NP 44096P10 6-9 AR79 27-1 NP 44096P5 6-9 AR

080 26-6 1 442390 30-2 1OP5 26-6 AR 44484 14-20 11 26-7 3 44485 14-16 12 27-7 1 (44486) 14-414 22-64 1 44487 14-41 15 22-48 2 44488 14-1 16. 23-4 1 44492 14-10 12 25-12 1 44509 10-14 13 25-25 1 44588P12 2-22 AR4 23-1 1 t44588P4 2-22 895) 23-5 1 44588P8 2-22 AR7 25-15 1 44591 11-6 79 26-5 1 44592 11-7 13 25-11 1 *44594 11-5 NP0 24-8 1 *44595 11-6 NP41 27-1 1 44682 17-20 136 25-4 2 44683 17-17 137 27-9 1 44684 17-18 19 7-30 1 446867 3-35 18 7-47 3 446868 2-1 116 9-29 4 t44689 9-48 18 6-7 4 44689PI0 9-48 AR

16-12 *44731 4-42 NP19-5 t44770 10-37 28

58 9-47 NP 44770MI0 10-37 AR9 9-36 8 44770M15 10-37 AR1 8-33 1 44770M20 10-37 AR2 8-30 1 44770H30 10-37 AR81) 5-25 44770M5 10-37 AR8P12 22-4 AR t45078 3-6 158P4 22-4 45078PI0 3-6 AR8P8 22-4 AR 45078P20 3-6 AR905) 10-14 (45094) 3-524 9-47 12 t45173 3-7 224) 9-46 45173PI0 3-7 AR4R1 9-47 AR 45173P5 3-7 AR64 10-23 7 (452243) 4-364P20 10-23 AR 45375 19-25 11 11-54 7 *45415 6-38 NP8 9-37 4 45416 6-35 246 10-22 7 45417 6-39 26PI0 10-22 AR (45476) 2-366P20 10-22 AR (45477) 2-3751) 10-44 (457059) 4-5152) 10-48 *46040 2-25 NP96 6-9 2 46050 2-25 1

3-23

PART

*430*430t43430843084308430843084308430943094309(4304309430943104313#4314319431943194340#4354356

*436436543664366(4374385t4384385(t43t439(4394392t439439643974397t44044044404(440(440t440

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T .0. 2R-R2000-24

NlJr1ERICALINDEX (cant)

PART NillffiER FIG. ~ ~ PA..R.TNUl'1BER FIG. ~ ~AND (YIY U H AND QI'Y u H~~ ~~ ~~ ~~INDEX PER :::'>0 P-<O INDEX PER :::'>0 P-<O00 ~o 00 ~o e00. ART'• u)u ~u NO. ARI'• u)u ~u

46085 13-4 1 *46870 12-31 NP*46086 12-6 NP 46871 12-31 7

12-8 *46872 12-29 NP*40689 12-6 NP 46873 12-29 3

12-8 *46874 12-33 NP13-7 46875 12-33 1

(*46090 12-6 NP #46876 12-10 712-8 #46877 12-13 713-7 #46878 12-19 7

#46091 12-6 3 12-21 ,12-8 #46879 12-31 713-7 *46880 12-7 NP

46093 12-6 #46881 12-7 113-7 *46882 12-7 NP

460992 7-1 1 #46883 12-7 146149 20-8 2 *46884 12-7 NP4617 6-42 6 46885 12-7 1

16-34 46912 19-8 120-11 46913 15-12 1

46342 21-2 2 46962 15-33 8 e46342P5 21-3 . 2 (46987) 16-24638 14-37 1 (46988) 16-2(464772) 10-18 47036 20-15 4(46557) 3-5 20-17t46575 2-13 1 47052 29-32 146575P10 2-13 AR 47056 29-35 246575P5 2-13 AR 47057 29-31 14669 14-27 2 47059 29-33 1(46772) 16-2 47061 29-34 146776 19-10 1 47082 14-13 146779 19-6 2 47083 14-17 146780 19-9 1 (47084) 12-1946782 19-12 1 (47085) 12-19(46783) 19-20 #47644 12-11 1246784 16-11 1 12-1446785 17-9 1 12-15*46800 25-17 NP 12-17*46803 16-10 NP 12-24*46856 12-10 NP 12-2546857 12-10 7 12-26*46860 12-12 NP 12-28 e46861 12-13 7 12-29(46864 ) 12-21 12-32(46865) 12-21 12-33*46866 12-26 NP 12-3546867 12-26 4 #47645 12-11 24*46868 12-28 NP 12-1446869 12-28 1 12-15

3-24

"-'.""' ---

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NIJHERlCAL INDEX (cant)

T.O. 2R-R2000-24

PART Nill1BER FIG. ~ p:::AND (JfY U Hp:::~ <:t:~

INDEX PER ~o p-.O00 ~oNO. ARI' • r:J)U p:::u

#47646

*4775047751*47752477534777347970(48111)48132#48164#4830948310(48310)4831548316(48724 )

PART NUHBER FIG. ~ p:::

AND CYrY U Hp:::~ <:t:~

INDEX PER ~O P-.O00 ~8NO. ART. r:J)U

12-17 48724 10-30 112-24 48996P12 22-8 AR12-25 t48996P4 22-8 612-26 48996P8 22-8 AR12-28 49107 3-24 112-29 (49482) 8-2712-32 (49624) 5-1112-33 #49710 33-13 112-35 (49986) 17-19 212-5 48 *50034 7-3 NP12-6 (501) 29-812-7 t501782 9-22 112-11 501782P20 9-22 AR PIDS12-14 50195 4-15 212-15 9-2412-17 (502) 2-3512-23 7-6912-24 7-7312-25 15-3812-27 24-2212-28 28-1812-29 (50216) 12-712-32 (50279) 10-812-33 *50527 20-14 NP12-35 20-1613-4 (507) 6-3213-6 (50724) 10-4113-19 51C9610-1 8-11 1 PI S13-20 (511) 25-2913-21 26-1013-22 29-3713-23 5121 8-4 1013-24 16-3012-24 NP 514 6-37 612-24 2 6-4412-32 NP *51778 9-42 NP12-32 2 t51807 19-17 614-23 1 51807P10 19-17 AR19-14 1 51807PI0PI0v.7 19-17 AR25-23 518D7PI0W 19-17 AR

18-3 1 51807PI0P5"1J 19-17 AR11-4 14 51807P5 19-17 AR11-48 1 51807P5P5W 19-17 AR11-48 6 51807P5W 19-17 AR11-49 51807Rl 19-17 A.-q

11-52 7 #51819 12-10 311-53 7 12-1910-29 12-21

3-25

..".

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T.O. 2R-R2000-24

NUMERICAL INDEX (cant)

#t51894CL A 9-42 4 54140 5-5 151894CL B 9-42 AR 54141 5-6 151894CL C 9-42 AR t54169 20-21 151894PID 9-42 AR *54170 20-4 NP51894PIE 9-42 AR t54301 16-16 251894PIF 9-42 AR 54301pI0 16-16 AR51894PI0A 9-42 AR 54301P40 16-16 AR51894PI0B 9-42 AR (54430) 4-1951894PI0C 9-42 AR (54431) 7-1151894PIID 9-42 AR #54434 34-13 19 FT.51894P11E 9-42 AR #54437 34-13 351894P11F 9-42 AR 54543 17-23 151894P15A 9-42 AR 54562 16-25 151894P15B 9-42 AR 54609 2-32 251894P15C 9-42 AR (54806) 18-2851894P16D 9-42 AR (55346) 11-3751894P16E 9-42 AR (55705) 34-851894P16F 9-42 AR #559886 11-11 56 Pl S51894P5A 9-42 AR 56 6-12 251894P5B 9-42 AR 56007 16-28 251894P5C 9-42 AR *56013 12-14 NP51894P6D 9-42 AR *56014 12-15 NP51894P6E 9-42 AR 56015 12-14 651894P6F 9-42 AR 56016 12-15 651911 17-30 7 *56026 12-11 NP(51912) 15-6 56027 12-11 151913 15-4 1 *56028 12-17 NP(521) 2-42 56029 12-17 152117 14-22 1 (56131 ) 7-595213 7-65 25 t56132 7-60 28

16-10 56132P10 7-60 AR17-26 #56572 34-13 12

(52144) 4-18 *56782 26-2 NP#523 9-29 4 56783 26-14 1(524) 6-22 57092 26-2 152552 24-26 1 57382 11-5 152567 17-10 6 *57383 11-4 NP(52791) 4-23 t57580 10-10 252819 15-36 7 57580PI0 10-10 AR#53015 15-30 1 57580P15W 10-10 AR(53032) 2-28 57580P2 10-10 AR

4-43 57580P2P15 10-10 AR(533) 7-37 57580P2P15W 10-10 AR

7-48 57580P5 10-10 AR533 15-34 32 57580P5P15W 10-10 AR53331 25-24 1 t57581 10-11 253676 18-20 1 57581P10 10-11 AR54114 20-9 1 57581P15 10-11 AR

3-26

PART NUl'ffiER FIG. ~ p:::AND QrY u H

~~ <:~INDEX PER :=>0 p.,o00 ~oNO. ART. CIlU p:::u

PART tUffiER FIG. ~ p:::AND QrY U Hp:::~ <:~INDEX PER :=>0 p.,o00 ~8NO. ART. CIlU

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Nut-mRICALINDEX (cent)

T.O. 2R-R2000-24

PART NUHBER FIG. ~ p::AND ('frY. U. Hp::~ <t:~INDEX PER PO P-<O

00 ~8NO. Am' • u)u

57581P15W57581P257581P2P15W57581P557612577885779057916(57945)

5795957975(#58328 )

(58328)

#58408

PART NUHBER FIG. ~ p::AND (JrY U Hp::~ <t:~INDEX PER PO P-<O

00 ~oNO. ART'• u)u P::U

10-11 AR 12-2910-11 AR 12-3010-11 AR 12-3110-11 AR 12-3221-7 1 12-3322-59 1 12-3429-7 1 12-3514-6 1 58660 22-50 212-9 *58751 12-24 NP

12-12 12-3212-16 59243 22-58 112-18 (59297) 9-1312-23 9-5212-27 #t59417 10-18 27-31 2 59417P15 10-18 AR14-2 1 59417P20 10-18 AR12-1 59417P3 10-18 AR12-3 59417P30 10-18 AR12-6 59417P5 10-18 AR12-8 (59791) 20-3212-10 *59793 20-14 NP

12-13 (59794) 20-512-19 *59796 20-14 NP

12-20 59797 20-3312-21 t59798 20-12 1

. 12-22 59798M20 20-12 AR12-31 t59799 20-13 1.12-9 59799~120 20-13 AR12-16 *59801 20-16 NP

12-18 59803 20-7 112-23 (59805) 20-612-27 *59806 20-16 NP12-30 t59808 20-18 112-34 59808PID 20-18 AR12-11 41 59808P10P2W 20-18 AR12-13 59808P10vJ 20-18 AR12-14 59808P5 20-18 AR12-15 59808P5P2VoJ' 20-18 AR12-16 (59812) 4-1812-17 59837 5-1 112-18 (59986) 10-3512-19 (59987) 10-3312-20 6191 14-21 112-21 (62 ) 22-3512-22 63D34560-19 11-46 1412-24 63D34560-20 11-46 AR12-26 637P12 6-41 AR12-28 t637P4 6-41 4

3-27

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T.O. 2R-R2000-24

NUHERICAL INDEX (cant)

PART NUMBER FIG. w ~ PART NUMBER FIG. .w ~AND gry U H AND (]rY U HP:::w <t:w ~w <t:INDEX PER pp p...p INDEX PER pp p...

00 ~8 00 w00. ARr. U)u NO. ARI'• u)u ~

637P8 6-41 AR 71601P2 9-33 ARt64 7-20 3 71601P3 9-33 AR

17-5 71601P4 9-33 AR64P12 7-20 .M 71601p5 9-33 AR

17-5 71657 19-11 164P30 7-20 AR 72337 16-31 2

17-5 72624 7-44 364P4 7-20 AR 73092 6-19 1

17-5 73137 6-26 264P8 7-20 A."R 9-41

17-5 *73153 9-42 NP64406 7-56 1 *73154 9-38 NPt6467 8-34 2 *73155 9-40 NP6467P30W 8-34 AR 733 7-5 26558 5-17 2 t73340CL A 9-42 4

8-12 73340CL B 9-42 AR656P12 15-20 AR 73340CL C 9-42 ARt656P4 15-20 29 73340PID 9-42 AR656P8 15-20 AR 73340P1E 9-42 AR6560 7-8 3 73340P1F 9-42 AR

9-7 73340P10A 9--42 AR658P12 15-21 AR 73340PI0B 9-42 ARt658P4 15-21 1 73340P10C 9-42 AR658P8 15-21 AR 73340PllD 9-42 AR66D3805 12-2 2 73340P11E 9-42 AR68C37326-11 10-51 AR 73340P11F 9-42 AR68C37326-13 10-51 AR 73340P15A 9-42 AR68C37326-15 la-51 AR 73340P15B 9-42 AR68C37326-17 10-51 AR 73340P15C 9-42 AR68C37326-21 10-51 AR 73340P16D 9-42 AR68C37326-23 10-51 AR 73340P16E 9-42 AR68C37326-25 10-51 AR 73340P16F 9-42 AR68C37326-7 10-51 28 73340P5A 9-42 AR68C37326-9 10-51 AR 73340P5B 9-42 AR69D34800-3 11-49 1 73340P5C 9-42 AR69E35002-1 7-63 1 73340P6D 9-42 AR70 17-14 1 73340P6E 9-42 AR(70230) 4-43 73340P6F 9-42 AR70455 19-4 1 t73341CL A 9-38 470464 2-40 1 73341CL B 9-38 AR71056P12 10-27 AR 73341CL C 9-38 ARt71056P4 10-27 6 73341pID 9-38 AR71056P62 10-27 AR 73341PIE 9-38 AR71056P8 10-27 AR 73341pIF 9-38 AR71454 15-3 1 73341PI0A 9-38 AR71547 8-25 1 73341PI0B 9-38 ARt71601 9-33 2 73341P10C 9-38 AR71601Pl 9-33 AR 73341P11D 9-38 AR

3-28

L

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NUHERICAL INDEX (cant)

T.O. 2R-R2000-24

PART NUMBER FIG. >il ~AND (]rY U H~~ <>ilINDEX PER PO p..o

00 gagNO. ARI' • ct:lU

PART NillffiER FIG. >il ~AND . 0I'Y U H~>il <>ilINDEX PER PO p..O

00 gagNO. ARr. ct:lU

Page 138: AIRCRAFT ENGINES - aeroconsultores.com · (usaf) t.o. 2r-r2000-24 technical manual illustrated parts breakdown aircraft engines usaf models r-2000-4 r2000-7m2 (pratt & whitney aircraft)

T.O. 2R-R2000-24

NU~1ERICALINDEX (cant)

PARTNUMBER FIG. roa P::: PARTNUMBER FIG. roa P:::AND QIY U H' AND QIY U Hp:::roa <t:roa P:::roa <t:roaINDEX PER ~~ p..~ INDEX PER ~~ ~@00 roao 00NO. ARr. Cf)U p:::u NO. A-qrr • Cf)U P:::u et77914P4 22-47 8 827 5-18 1

779141'8 22-47 AR (82964 ) 10-33#77975 10-29 2 (82965) 10-35#78187 34-13 7 83104 6-17 2#78261 18-48 1 8323 11-50 878282 19-24 1 11-59

I

79018 12-24 1 (83212) 20-30 ~#79019 12-32 1 (83213) 20-31(7916) 6-38 *83215 20-16 NP

15-40 *83216 20-14 NP17-32 83217 20-14 128-30 83219 20-16 129-38 83280 18-19 1

#79523 12-31 (83320 ) 9-51#79524 12-19 7 (83484) 10-52

12-20 83485 15-27 112-21 *83974 12-25 NP12-22 83975 12-25 113-17 *83976 12-35 NP13-18 83977 12-35 1

79747 5-31 4 84058 7-52 1(*0003) 34-8 84107 29-43 28011 25-10 1 84237 8-10 1802 11-56 7 t84251 9-34 2803 11-51 8 9-49

11-55 842511'10 9-34 AR80827 18-4 1 9-49*81112 19-2 NP 842511'5 9-34 AR*81113 19-2 NP 9-49(81114 ) 19-2 8427 15-43 181439 8-35 2 (84477) 2-15(81441) 3-23 (84478) 2-17#81709 12-1 2 (84560) 2-18

13-1 845671'12 22-33 AR81711 12-1 5 23-12

12-2 t84567P4 22-33 812-3 23-1212-5 845671'8 22-33 AR12-8 23-12

(81812) 19-2 845681'12 22-20 AR(81813) 19-2 t84568P4 22-20 2(81814) 19-1 845681'8 22-20 AR(81885) 3-2 t84569P4 25-22 2#82008 12-10 3 845691'8 25-22 AR

12-13 84587 24-9 112-31 84588 25-14 1

82573 12-36 14 846921'12 2-19 AR13-30 t84692P4 2':"19 3

3-30

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NUMERICALINDEX (cant)

T.O. 2R-R2000-24

J

,I

PARTNUHBER FIG. W P::AND QrY u HP::W ~WINDEX PER ;:Jt=l p...t=l

00 woNO. ART'• u)u P::U

84692P8 2-19 AR85039 5-27 185594 5-38 2(85624) 17-28(85865) 12-885866 12-8 1*86558 15-6 NP86559 15-2 18698 29-5 1(8699) 29-12(87) 28-1987107 24-2 1*87108 25-9 NP87109 28-21 1(87112) 25-1087113 28-4 1t87114 24-4 187114P15 24-4 AR(87115) 25-987116 25-9 1*87511 10-5 NP*87512 10-5 NP88131 17-22 188285 17-27 188737 21-1 288738 21- 288798 26-18 188962 11-15 2889299 17-19 2(89304) 10-32#90093 12-3 34

12-412-912-1212-1612-1812-3012-3413-113-213-313-513-813-913-1013-1113-1213-14

PARTNUMBER FIG. W P::AND QI'Y U HP::W ~WINDEX PER ;:Jt=l p...t=l

00 ~oNO. ARr. u)u P::U

13-1513-1613-2513-2613-27

(90553 ) 16-389074 10-25 190764 11-57 149085P12 7-18 l\Rt9085P4 7-18 29085P8 7-18 AR*90962 4-18 NP(91061) 20-(91062) 20-(91063) 20-(91064 ) 20-91454 16-37 1#91481 12-1 4

12-212-412-8

#91616 12-4 412-612-813-7

(91735) 10-5(91736) 10-591766 10-33 191767 10-35 2(91972) 24-19#92285 18-32 6 IN.9252P12 2-13 AR#t9252P4 2-13 29252P8 2-13 AR(92527) 4-1*92533 6-25 NP*92534 6-26 NP92535 6-25 1t92541 9-20 192541P20W 9-20 AR92541P40W 9-20 AR92541P75W 9-20 AR92555 7-70 19265 11-12 56#92661 3-29 192870 34-3 492892 6-28 192893 6-27 3

3-31

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FIG.AND

PART Nill1BERFIG.AND

PART NUMBER

T.O. 2R-R2000-24

NUr1ERICAL INDEX (cont)

~~ <t:~ .. ~~ <t:~INDEX PER PO p.;O INDEX PER PO p.;o00 ~o 00 ~oNO. ART'• U'lU ~U NO. ART. U'lU ~U e(92938) 5-26 96282P8 16-29 AR

8-22 96314 11-31 19294 10-47 2 #96315 11-18 3 pI S

10-51 11-23*93192 15-6 NP 11-41(93195) 16-4 #96316 11-17(93204 ) 18-28 11-28 t 1:;,(93206) 18-33 11-42 ~93406 6-30 1 (9632) 24-19 ~.93407 6-31 1 *96324 11-16 NP " I

93456 25-1 2 #96556 11-22 1 pI S(93695) 29-39 #96557 11-27 1 PI S93714 6-1 1 *96560 11-21 NP93715 24-32 1 *96561 11-26 NP*93788 23-7 NP *96562 11-32 NP93809 23-7 1 #96588 14-41 19385P12 22-36 AR 96639 8-1 2t9385P4 22-36 5 #96643 7-2 19385P8 22-36 AR 96643P10 7-2 AR93956 18-23 1 96643P5 7-2 AR e9400 7-41 2 96656 9-2R 19401 7-36 25 96657 9-27 1#94020 34-8 1 #96675 7-9 294032 8-3 8 96675~no 7-9 AR94033 4-38 1 96675H2 7-9 AR94034 4-37 1 96675M5 7-9 AR94188 18-24 1 96675P10 7-9 AR94189 18-25 1 96675P20 , 7-9 A..~#94190 34-13 1 96675P30 7-9 AR#94191 34-13 1 96675P30H5 7-9 AR(94715) 10-18 96675P40 7-9 AR#94870 34-3 1 96675P5 7-9 AR94926 11-36 2 pI S 96675P50 7-9 AR#94927 11-33 1 96675Rl 7-9 AR94930 5-37 1 96675R2 7-9 AR94931 5-36 1 96675R3 7-9 AR(9514) 10-46 96675R4 7-9 AR

10-50 96675R5 7-9 AR(95211) 14-5 96675R6 7-9 AR(95250) 12-4 96675R7 7-9 AR(95252) 12-6 (96724) 9-21 e96137 19-32 1 (96725 ) 9-2196138 19-23 1 , 96997 18-44 1(96140) 19-31 97126 11-61 1(96141) 19-22 (97254) 9-23(96197) 22-4 (97255) 9-2296281 16-26 1 97257 9-15 1#96282P4 16-29 2 97258 9-26 1

3-32l

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NtmERIC'AL INDEX (cent)

T.O. 2R-R2000-24

97259 9-25 1 9876 5-15 8(97282) 5-7 98782 18-15 1(97283) 10-5 98784 18-13 1(97284 ) 10-5 98872 10-5 1 P1DL97611 18-1 1 98872P20 10-5 AR P1DL97612 18-2 1 98873 10-5 1 PIDL97738 5-28 1 98873P20 10-5 AR PIDL97946 4-9 1 98874 10-5 1 P1DL98168 14-36 1 98874P20 10-5 AR p1DL98169 14-35 1 *99364 27-5 NP98226 #11-4 99409 27-5 1

#11-5 99541 8-20 3#11-6 99642 24-31 1#11-7 99889 5-14 2

PART NmffiER FIG. ~ P:::AND ('frY U HP:::~ ~~INDEX PER :::>0 P-<O

00 ~oNO. ARI' • CflU P:::U

PART NWl'ffiER FIG. ~ P:::AND (lIT U HP:::~ ~~INDEX PER :::>0 P-<O

00 ~oNO. I\.t{r • r:f'J ... P:::U

"r u.s. GOVERNMEN ~ PRI•• riNG OFFICE:1980-671-150 11438

3-33/(3-34 blank)

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::(

I~-'

r.'

/"/.: