eliteaircraft.comeliteaircraft.com/N66CC Airframe logs.pdf · 2012-01-07 · 2654.6. Painted new "N" numbers on aircraft. Adjusted voltage regulators. Removed and replaced NLG tire

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DATE

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RECORDING TACH TIME

TODAYS FLIGHT

TOTAL TIME IN SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

GREAT WESTERN AVIATION Model: Piper PA 44-180T Ogden Hinckley Airport W.O.# 5301 SIN: 44-8107042 Ogden, Utah Hobbs: 2154.6 Reg: N227ST 1-801-394-3400 Total Time: 1795.5

FAA Approved Repair Station DPOR285D

Completed annual inspection lAW Piper PA44 service information, and inspection guide. C/W AD 94-13-11 MLG trunnions, by dye penetrant inspection. No defects noted, next due @ Hobbs 225~6. C/W AD 96-20-07 Heater Decay and Combustion pressure switch. No defects noted, next due @ H.H. 1)B2.8~8/2001. C/W AD 84-26-02 Induction Air Filters. Replaced filters, next due @ 2654.6. Painted new "N" numbers on aircraft. Adjusted voltage regulators. Removed and replaced NLG tire and right wheel half. Removed and replaced left and right brake rotors and linings. Tightened b-nut on right MLG actuator. Replaced shims on right MLG torque links. Removed light corrosion from both firewalls. Serviced all landing gear struts. Removed and replaced ELT antenna, baggage door seal, left and right MLG door hinge pins, and rudder trim tab linkage bushings. Repaired nose cone fiberglass. Inspected ELT lAW FAR 91.207 Cd) 1-4, due again 9/2000. I certify that this aircraft has been inspected in accordance with an annual inspection and was determined to be in an airworthy condition. Routine servicing and functional electrical test accomplished. Run up and Ops check is ok. . J1 ff~

September 1, 1999 Signed: N ~ _ -----t------+-----f------f---------------------------------

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DATE RECORDING

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DATE

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I fi~d, that th~ .aircraft meets the requirements for the certification requested and have issued a Standard Airworthiness certificate dated /I-o.r- /9'1'1

//-0.5-/997Date{;A h: .a ?&~i-~Inspector, RK-:S -E

DATE

19__

RECORDING TACH TIME

.' .•',r;: ••

:

TODAYS FLIGHT



Inspected previously installed KXl55 Nav -com and PS1000 intercom and found both to work satisfactorly. Removed KR87 ADF indicator KI22.

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Bemis Avionics 7220 S. 4450 West

~Ordan Ut 84084 .~ "'

(RS B7~ov 5,1999

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DATE De$crlption of Inspections, Tests, Repairs and AlterationsRECORDING TODAYS TOTAL TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME19~ SERVICE Technician or Rep air Facility. (See back pages for other specific entries.)

I{(-'5-qq ,KY197, WX7 Storm Scope, EOO Removed KNS80

- NSO 360 HSI. 430 GPS, Sandel WN3308 display, Installed Garmin

WX500 Stormsc ope, JPI EDM-760, KGI02A, --- KMTl12, AK550-12, AMS-2000,KN64 DME, PA17

- vertical compass, KN72 VOR converter, RS-12

switch,FN0200 c ooling fan, OigiData Fuel flow,

overhauled OG and Horizon gyros, -

See FAA Form 3 37 Dated nov. 5,1999 Bemis Avionics

;7220 S. 4450 W est West Jordan Ut 84084

N - C@=30

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Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.) I"

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Description of Inspections, Tests, Repairs and AlterationsTOTALRECORDIIIB TODAYSDATE TIME II Entries must be endorsed with Name, Rating and Certificate Number of TACH fliGHT SERVICETIME Technici~n or Repair Facility. (See back pages for other specific entries.) 19~

DATE. Ole 26. /999 SER. tll/- B/O 70'-12TACH. 21 U ~3 N. ~27ST

AIRCRAFT INTERIOR HAS BEEN REMOVED AND ---f------+---I--- ' RE-UPHOLSTERED BY UNI-CRAFT INTERIORS.

, INTERIOR THEN RE-INSTALLED UNDER MY ------ SUPERVISION AND AT THIS TIME IS COMPLETE

• AND CORRECT. ALL MATERIALS USED HAVE MET ---------~------~---~-------- AND ARE WARRENTEED TO MEET FAR25.853 PAR.A

------------------END------------------------ ! __+--_-+--------+-- ' DCV1'n~~ ¢ t/2Ft<418i,'-,

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iJf! !G & DAERO PRODUCTS, INC. I:i ~ TINTED THERMAL PANE WINDOW iNSERTS ii,: G &. 0 AERO PRODUCTS, INC. WINDOW INSERTS Iii INSTALLED PER STet SA-,OfD3 HrtJ d IN ACC'ORDANCE WITH INSTALLATION .

. INSTRUCTIONS DATEu.D_....,Jra:~D!ttI~/"~/...I./"..I.9"J.'.L9-------

.INSTALLED BY:

AUnI.SIG:

.;&A~I82JDiil~iJ . TACH: ~'b::l.,:$DATE: /2.63h'

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. e 1991 ASA

DATE

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RECORDING TACH TIME

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TODAYS FLIGHT

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Description of Inspections, Tests, Repairs and Alteratio, Entries must be endorsed with Name. Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries


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DATE RECORDING TODAYS , Tests, Repairs and Alterations TACH FLIGHT Entries must be endorsed arne, Rating and Certificate Number of TIME Technician or Repair Facility. See back pages for other specific entries.)

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DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of f'>6() TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

GREAT WESTERN AVIATION Model: Piper PA 44-180T Ogden Hinckley Airport W.O.#: 5948 I

.\

SIN: ~107042 Ogden, Utah Hobbs: 92.3 Reg. #: N227ST 1-801-394-3400 ITA: 1895.7


C/W 100 HR/ Amma! inspection in accordance with Piper PA 44-1801' Maintenance Manual & Multi Engine Inspection Guide. C/W FAR 91.207(d) 1-4 ELT ops check requirements. No defects noted. Next due@5-2oo1. C/W AD 94-13-11 by dye penetrant inspection. No defects noted. Next [email protected]. Replaced ELT battery. Next due -@5-2oo2 Replaced manifold pressure line filters, both side aileron rod ends, both garter filters, and left side brake linings. Stop drilled cracks in dorsal fin. Paralleled alternators via voltage regulators. Ops check good. Performed routine servicing and maintenance. Run up, ops and leak checks good. I certify that this aircraft has been inspected in accordance with an ADDual inspection and determined airworthy this date.

Date: May 5, 2000 Inspector:~ (?S;', )¥o/Sfl

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--- Description of Inspections, Tests, Repairs and Anerallun.RECORDING TODAYS TOTALDATE TACH FLIGHT TIMEII Entries must be endorsed with Name, Rating and Certificate Number of ~c'I

SERVICETIME Technician or Repair Facility. (See back pages for other specific entries.)

GREAT WESTERN AVIATION W.O,#: 5961Ogden Hinckley Airport Model: Piper PA 44-180T Hobbs: 99,1 Ogden, Utah - SIN: 44-8107042

1-801-394-3400Reg. #: N227ST FAA Approved Repair Station DP0R285D

Repaired broken battery cable to right alternator. Paralleled voltage regulators/alternators lAW MIM. Replaced left halogen

landing light bulb. Run up and OpS ck good.

/' Date: 1",_'~ f2S{.. /.J'iso-'- May 13, 2000

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W.O.#: 601 Hobbs: 152.

'''P~Io'~

Logbook Entry N227ST Hobbs 181.6 June 16.2000 .,'

Replaced left engine tachometer magnetic pickup with new part # 763-504. Set clearance at .018". post.maintem engine run and operational checks OK. Icertify this aircraft was repaired LA.W. cuiTent F.A.A. regulatIons and'

detinnined to be in conditi d is ved for return to service.

GREAT WESTERN AVIATION Model: Piper PA 44·180T SIN: 44-8107042 Reg. #: N227ST

Ogden Hinckley Airport Ogden, Utah

1-80 I~394-3400

FAA Certificated Repair Station DP0R285D

Removed and replaced left alternator with new, SIN I2L000059A-1 48754. See yellow tag. Ops check good. Replaced left alternator - annuciator light resistor. Repaired fresh air vent control column. Removed and replaced oxygen system pressure gage. Leak check and ops

check good.

- Date: June 2, 2000

------'~l_~_L -Cl '991 ASA

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~odel: Piper PA 44-180T ,SIN: 44-8107042 Reg: N227ST

GREAT WESTERN AVIAT/ON Ogden Hinckley Airport

Ogden, Utah 1-801-394-3400


W.O.# 6095 Hobbs: 190.7

Total Time: 1994.1

--completed annual inspection lAW Piper PA44 service information, and inspection guide. CIW AD 94-13-11 MLG trunnions, by dye penetrant inspection. New trunnions on order. No defects noted, next due Q Hobbs 290.7.

--Removed and replaced left and right brake linings. Replaced It main tire and brake disk. Resealed It wheel brake cyl. Inspected ELT lAW FAR 91.207 Cd> 1-4, due again 6/2001. I certify that this aircraft has been

--inspected in accordance with an annual inspection and was determined to be in an airworthy condition. Rov"o' ."v"'o, 'ol '''''''0,1 ~,' t,.t ......1'..... ,., vp ,ol 0.. 'h"k ,. ,k. .

I June 30, 2000 Signed~ ___

GREAT WESTERN AVIATION Model: Piper PA 44-180T Ogden Hinckley Airport W.O.# 6216 SIN: 44-8107042 Ogden, Utah Hobbs: 246.4 Reg: N227ST 1-801-394-3400 Total Time: 2049.8

FAA· Approved Repair Station DPOR285D

Installed new brake rotors and brake linings on both . land°calipers. Flushed brake system with Mil-H-56060 and ~1~ b kIng gear wheels. Re-sealed both brake lead

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on left prop.

August 16, 2000

_--:.-[-'

Run up and Ops check is ok. l\_~' ra e system. Replaced left one~ prop de-ice

Signed: ~_ ----=-~~~----

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Ole., OfV'


GENERAL AVIATiON MAINTENANCE RELEASE L THE AIRCRAFTI APPLIANCE ~ WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FAA AND APPROVED FOR _ RETURN TO SERVICE. PE~ETAILS OF T PAIR ARE ON FILE AT THIS ~TATION UNDER ORDER NO/WS'" OAT SIGNED CRS: KD6R661N . ---


RECORDING TODAYS TACH FLIGHT TIME

DATE ~OD

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Model: Piper PA 44-180T W.O.# 6373·f SIN: 44-8107042 Hobbs: 289.4 Total Time: 2092.8>I- Reg: N227ST

Completed annual inspection lAW Piper PA44 service information, and GWA multi-engine inspection guide. C/WI -----AD 94-13-11 MLG trunnions, by replacement of trunnions with new. Replaced fwd and aft trunnion bearings of I left MLG, retraction check good. This is terminating action for this A.D. Inspected ELT lAW FAR 91.207 (d)

1-4, due again 11/2001. Replaced fwd dorsal fin cover. Replaced rear tail nav lite bulb, replaced fwd housing of lt alternator, checked brushes, and cleaned commutator. Replaced gaskets on lt and rt fuel sending units. Retorqued lt and rt engine exhaust clamps, secured wire bundle for fuel flow solenoid, replaced clamp for rt engine breather line. Replaced pressure switch for hobbs meter on rt engine, Hobbs ti_ inadvertantly advanced 66.7 hours during maintenance•. new Hobbs meter time is 356.1 Repaired broken wire on RMLG downlock switch. Replaced A/I SIN 2940A. Replaced one nose wheel bearing and race. Replaced It and rt spinner caps. C.W. A.D. 96-20-07 heater decay insp by pressure method, no defectsnext due at 556.1hobbs or 11/2002_ I certify this aircraft has been inspected in accordance with an annual inspection and was determined to be in an airworthY~C. Routin.e servicing and funct. ional electrical testondition ..accomplished. Run up and Ops check is ok. ~ ~~

Signed· ~

0, - -,_ .......-=»~_. ._~_=..,..-~_ __."'--_...- ....._.~",."" .._.~'o.~._-;"".-:~

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d Alterations te Number of pecific entries.)

Description of Inspections, Tests, Repa· Fntries must be endorsed with Name, Rating ~nd

r Facility. (See back pages for

7; CVI Ie ~ '-a:J./ 'Ot!L. _

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KINGS AVIONICS, INC. THIS IS A PERMANENT LOGBOOK ENTRV~l!"~~~,..-,!"'T-'7-=---,,-f

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~ /.-...}LAIR CARRIE AINTENANCERELEASE x' THEAIRCRAFTI APPUANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURR~GULATIONS OF THE FAA AND IN CONCURRENCE WITH

Co AIR CARRIER OPERATION SPECIFICATIONS,AND IS APPROVED FOR REl\JRN 10 SERVICE. PERTINENT. THE REPAIR ARE O~;J) AT THIS R:~hIATION f{ORDER NO. /b.. DAT~ SIGNE CRS:KD6R661 N

DATE

-f' I

AfR CARRIER MAINTENANCE RELEASE~ THEAIRCRAFT~-------- _ II APPUANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH i

l CUI3RENT REGULATIONS OF THE FAA AND IN CONCURRENCE WITH.-;.'oW AIRCARRIEROPERA1'ION SPECIFICATIONS,AND lsif~

~ APPROVED FOR RETURN 10 SERVICE. PER11NENT.,;;J REPAIR ARE QtVJi.:"T THIS~~TATION ! ORDER No.16L~ OAT SIGNE

..J CRS:KD6R661N . © I ItYJ REIUtl-) J((/P/lff) I(IMJ'I tIJtIJ~t/ JCRvt..J

AIR CARRIER MAINTENANCE RELEASE THE AI RCRAFTI APPUANCE WAS REPAlREDAND INSPECTED IN ACCORDANCE WITH

~spection., Te.ts,·Repairs and Alterations prsed with Name, Rating and Certificate Number of rFacility. (See back pages for other specific entries.) l i

I npt>: ~I-----.:...-------••.-J.c.;-:S~.'O;:-.--=-ll-;----

CU~~NT~GULATIONSOFTHEFAAANDINCONCURRENCEWITH Ii . 0 J T b../.{.117 AIRCARRIEROPERATIONSPECIFICATIONS,ANDIS . ~I-------------'-~----=--'--------

APPROVED FOR RETURN TO SERVoICE. PERTINENT~~~OF THE i ~

~~~~~~Jl~)AT:~:;.T~~~~ I,L

tPJ'"rt~e_s--_ CRS:KD6R641N ., .J 1'Z>l"~ L. ,~

!:~~[~~~o~~7;io~~~ ~'~. Great Western Aviation

-. Model: PA44-180T Logan-Cache Airport W.O.# 1869 -' SIN: 44-8107042 . Logan. Utah TachIHobbs: 453.5 _ Reg: N227ST 1-435-752-5955 Total time: 2 3~.1

R/R. LH brake pads, R/R. worn out disc. Cleaned and insp LH brake actuator, installed new packings and - reinstalled on ale, bled brakes. Insp RH brake operation, bled brakes. Operational and leak check good. - Serviced brake reservoir. rd., ~ - May 4, 2001 Signed/Cert#: ~. ~f:

[ I [' ." '( '«'. • ." '. ',.... •

Description of Inspections, Tests, Repairs and Alterations . Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

100 vioJion~~z= 101 Hangar Road .. .,,~ /&I:

Wilkes-Barre/Scranton International Airport. Avoca, P":>-""',~~.~~~"------------

tVaa7$T. Vta8, £/~)570) 457-3400 0//8/01. 1"TPtF G) i;:)'l. ¥' ~N5TAUEiJ 19 AJt5W PI..J, l~qOa3CJC) "BR/JI(£ ----- 7)1:S~ /M..J~ '-Iel'i>. PIJ. cP~ - 0105 LJAJ//.../6 IN A0XJ/(LJAtU:::.£ WITH ,t:Jp,oueFlSG5 PIPeR SCf:;Vlee /TJR/UU/tJL ...

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WilkeS-BarrelSCrantonlnternational Airport • Avoca, PA 18641 ~$.12. 7 r Ua;;J7$r. 7 7/9 leI (570) 457-3400 5/9....3 /t::ot31$5 t-

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Technician or Rep~ir Facility. (Seeback_pages for otherspecific entrie:

RECORDING TODAYS TOTAL TACH FUGHT TIME IN nME SERVICE

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P.O. Box 4942 Baltimore. MD 21220 (410) 514-4299 CRS #LF1 R294K

'alions :ler of ntries.)

The ATe transponder tests and inspections as required by FAR 91.413, in accordance with FAR 43, Appendix F have been performed. Transponders tested:

# 1 Model_~O---"f..?;;..~,,-----~Jo:=;..;G?Wi<..=:z:..--->Q"""Q""'-__SIN O:::::.....>ote~Q~)-"'(p'_'?'---

#2 Model tV/A SIN __L.-'~"7"0.L..rl>--

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The systems have been found airworthy for return to service. Details of this inspection are on file at this Agency under Work Order:

Number ZO(P2.3 Date 9-'-1-01

Signed ~:~::~=-:/'-I------+-'/fz.-=-~:~=---==---====~:======

19_,

=--J fJ f-"_-~~ © 1991 ASA

---------

lATE

P.O. Box 4942 Baltimore, MD 21220 (410) 574-4299 CRS #LF1 R294K

'ations :>er of ntries.)


#1 Model._-.-::(),-,&~~~-.:...J =.o"""t.?'-"z=----'Q""-o'""-__,SIN O~(p<-O""--'-I_ ...(p'___'f''--

#2 Model tV/A SIN __L-'~'¥0L.11'--

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-

The systems have been found airworthy for return to service. inspection are on file at this Agency under Work Order:

Details of this

Number 20 &> z. 3 Date 9 - '-1- 0/

Signed _ ~_,::e..:.-~,--~~'-=-:~d-=-~-~~-=-~:~-,,--==::=:======

19_,

~ 1991 ASA

-----1-- -----+---\--~--f----~---------------------

DATEions of

19__ias.)

-loll 'of

P.O. Box 4942 as. Baltimore, MD 21220 (410) 514-4299 CAS #LF1 A294K L

IThe Altirneter(s) Static and Altitude Reporting Systems test as required by FAR f-91.411 in accordance with FAR 43 Appendix E have been perfonned.

-'Altimeters tested:

LIH Model .sCf3l./PAD - I SIN ys 7:S 3 Tested To Z0lj 006 L IRIH Model_..4A.L.J1-=61I--__SIN tJjA Tested To NJA i 1-,

The systems have been found airworthy for return to service. Details of this f-inspection are on file at this Agency under Work Order: L Number ZOt.D Z3 Date __9....L.....--~'-I_-_O~/ _ ~ .~

I

Signed _-,.$~~. ~..-""'-/ ~~q.-.,-------::>7"e;..c.~c::-. _

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( DATE

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RECORDING TACH TIME

TODAYS FLIGHT

TOTAL nMEIN SERVICE

Description of Inspections, Tests, Repairs and Altera Entries must be endorsed with Name, Rating and Certificate Numb Technician or Repair Facility. (See back pages for other specific ent

P.O. Box 4942 Baltimore, MD 21220 (410) 514·4299 CRS #LF1 R294K

MAlNTENANCE RELEASE The aircraft and/or component identified above was repaired and inspected in accordance with current ederal Aviation Regulations and was found~O::tfor return to~·ce. Pertinent de . s of the ir on file at this agency under Work Order Nod'!l.tJ...6 Date: ,.. 7. IJl Signedl~~"1:!1.~~~:::::::'ftl Skytech, Inc., P.O. Box 4942, Baltimore, MD 21220 LFI 94K

N227ST Airframe Entry September 7,2001 W/O 20623 Hobbs 538.1 SIN 44-8107042 .'

la\~.8' SMo M· .: > > •• '

\. Installed 2 repaired voltage regulators, pin B-00288-1, sin 13620, pin B-00288·/. sin 80283210. Installed new fuse holder pin HRS. Adjusted voltage regulators IAW PA44-180T MM Chapter 2423-08. Ops checked satisfactory.

2. Removed CHT gauge, pin 46063, sin 168096. Reinstalled a new gauge pin 46063, sin 154849. Ops checked satisfactory.

3. Lubed overhead fresh air cable. Ops checked good. 4. Installed a new GE330 post light for Oxygen gauge. Ops checked good. 5. Troubleshot overhead cabin and map light inop. Found broken wire. Repaired wire. Ops check

light satisfactory. . 6. CIW AD 200/·17·13 Jan Aero - Comply with by removing fuel pressure ~gulatorlshut olTvalve

and sent out for testing - NON. Reinstalled valve leak check - ops checked satisfactory.-END

,-LASA

Iterations lumber of fic entries.)

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DATE

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Description of Inspections, Tests, Repairs and Alterations, Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

-:z;ltlbJ /'110

£ ,(/kK,gr HI tC. fJ"rvy

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~ MODERNAI:RO, INC.

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14801 PIONEER TRAIL _ EDEN PRAIRIE, MN 55347

. 952·941·2595 < u..- I () r) FAA APPROVED REPAIR STATION MZER198L ~ ~71). (]'..

1TA-~ J~lft.q N227ST, DAIE: 11115101 HOBBS: 596.5

RESEALED RIGHT MAIN STRUT AND SERVICED. REPLACED RIGHT' BRAKE CYLINDER, SEALED, AND REPLACED RIGHT BRAKE Lrnnms. RESEALED LEFT BRAKE CALlPER AND REPLACED LEFT BRAKE LININGS. BLED~QTIi BRAKEs JI.JJ REQUIRED. LEAK CHECK GOOD. ,~C¥MODERN AERW:0333.

,. ~!~ f - -I. '0

01991 ASA

.".

MODERN AERO,INC. , 14801 PIONEER TRAIL

. _ _ EDEN PRAIRIE. MN 55347,. • L I) 7'(/ ~ 952.941.2595~MOrr ld () . .)

FAA APPROVED REPAIR STATION MZER198L r-rftF :2~~

JiUHi'f QA'l'Ri \U'h1.iot HQ~~; ~~... \ '

~

Description of Inspections, Tests, Repairs 8nd Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

TOTAL TIMEIfII SERVICE


COMPLETED ANNUAL INSPECTION THIS DATE. PACKED WHEEL , BEARlNGS, SERVICED BATTERY, CLEANED FUEL SCREENS,

CHECKED ELT OPS. PER·FAR 91.207(d), BATT. NEXT DUE OS/02. ADJUSTED CONTROL CABLE TENSIONS. REPLACED LEFT AnnON ROD-END. REPW'a.CED NOSE TIRE. RESEALED ALL GEAR ACTUATORS. SHIMMEDeNOSE GEAR REPLACED ONE BEJI.RING AND RACE ON NOSE WHEEL. REPLACED RIGHT GEAR LOWER TORQUE LINK BOLT AND BUSHINGS. REPLACED VACUUM REGULATOR FILTER OXYGEN BOTTLE HYDRO. TESTED. GENERAL INSPECTION OF AIRCRAFT SATISFACTORY. REJiERENCE MODERN AERO W.O.# 30388,

DATE'

19__

( --i

! --i !

--;, I

i "I

J

~ i

1 I,

-< I

I 1 ---1

i -I

i

1 ~

! I

'-...

DATE RECORDING TDDAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME II Entries must be endorsed with Name, Rating and Certificate Number of

19__ 'I'IME SERVICE Technician or Repair Facility. (See back pages for other specific entries.) . ~~-

-

DATE: JANUARY 30, 2002 N66C~ (N227ST) TACH TIME: 604.5 .. ,

CHEMICALLY STRIPilED AND PAINTED' AIRCRAYf USING THE FOLLOWING MATERIALS: 570-535MATIERHORN WHITE; W00293 JADE MIST GREEN, HI0688 CARTER GOLD, HI0630 SEMINOLE RED. CHANGED REGISTRATION NUMBER FROM N227ST TO 66CC, SEE 'ASSIGNMENT OF SPECIAL REGISTRATION NUMBERS DATED: JANUARY 2,2002. BALANCED ALL FLIGHT GONTROLS PRIOR TO REINSTALLATION.

THE AIRCRAFT AIRFRAME, . AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFffiD ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENt REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETUJrn TO SERVICE. PERTINENT OF THE REPAIR ARE ON FILE AT THIS REPAIR STATION UNDER 1 . W/O NO....:8....I=:35~.---- _

S/\1.ol+ I~i'o. 2

ilAE !).¥S1. 9

DATE

19__

RECORDIIS TACH TIME

TOOAYS FLIGHT.

TOTAL TIME II SERVICE

Description of Inspections, Tests, Repairs and Alterations. Entries must be endorsed with Name. Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

i~. MODERNAERQ,INC. ~ .. •. _ 14601 PIONEER TRAIL I EDEN PRAIRIE. MN 55347

~I 952·941·2595

FAA APPROVED REPAIR STATION MZER198L HOBBS: 6S9.91 N66CC DATE: 4/11102

1 INSTALLED NEW MICHELIN AIR 6.00X6 8PLYTIRE ON RIGHT MAINJ WHEEL. SER. ED AS D. REFERENCE MODERN AER.Oj ,W1OII3IJ762

... . A"':o....(,.s. cf

. ~DERN AERO. INC. : 14801 PIONEER TRAIL .

EDEN PRAIRIE, MN 55347 ~ 952-941-2595• FAA APPROVED REPAIR STATION WlE$'W

.~

-i N66CC DATE:04'19102 80BBS:662.0

!j

~=LED AUTO !ILOT INSTALL PLACARD ON INSTRUMENT --J

·BR.EAKE~ING AUTO PILOT DISABLED" TIED OFF CIRCUIT ;, ! 0s\)!.3'S:J"r ~.

e 1991 ASA

I

Description of Inspections~Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

TOTAL TIME I. SERVICE


DATE

19__

'd Alterations ate Number of ;pecific entries.)

HOBBS: 748.5

'6~~'AlR~NC. 14801 PIONEER TRAIL

EDEN PRAIRIE. MN 55347 952-941-2595

RESET AlP CIRCUIT BREAKER, REMOVED PLACARD ON INSTRUMENT PANEL READING "AUTO PILOT DISABLED". AVIONICS OF M~~~~C _ EDEN PRAIRIE, MN 55347 CRS05VR353Y ~~ W/O#2531

FAA APPROVED REPAIR STATION __•

N66CC DATE: 09/16/02

AT6 A~~ftN~~~O~C.

14801 PIONEER TRAIL EDEN PRAIRIE. MN 55347

952-941-2595

FAA APPROVED REPAIR STATION II. N66CC 09/16102 HOBBS: 748.5

REC"---'- -- .--. TA~ TIM

DATE

19_'_

-,--_1<-_

REPLACED SANDEL SN3308 SIN 2754 EHSI PROJECTION BULB WITH NEW. PERFORMED "NEW BULB CALIBRATION" PER SANDEL INSTRUCTIONS. RAMP TESTED AND FOUND SATISFACTORY. AVIONICS OF M~ AERO, INC EDEN PRAIRIE, MN 55347 CRS 05VR 353Y Y-~~ W/O# 2531

------t----II~ I I \,

10 1991 ASA

~~":::-::--:'-":C",-C':.:-':"'-:'::::-=_,...'-t""'i Cl!l!lly.•R.l4RU.,;__II!!I_.IIIIIX.l!l!.«£llIIIlggllllllL@!II!I.ti!l'll!!'$'l!!I\l¥i-'!!!'l-MlE!l!"i'_J{~&#mlAW!!!!l$!l'!'!I",t0J';!'!J"';;.#~V!,,,,,!~g;or,,mJl3i:;!ii,illllti.':~~;9~_Nr'¥~.""' sd.

DATE RECORDING TODAYS TACH FLIGHT

19__ TIME


'~II!~ __ 76p__LL J[_~...~"'~ ffW~ ;J.., ~l


·-1

j 1

I

j----L--'-'----'-<-----,-_~~~-~~-~~---------------~

MODERN AERO, INC. 14801 PIONEER TRAIL

,........ .. ,..... EDEN PRAIRIE, MN 55347 ~ ~ 952-941-2595 ~

FAA APPROVED REPAIR STATION MZER198L N66CC DATE: 11/0112002 HOBBS: 768.7

Serviced, landing gear Hydraulic reservoir. Removed and installed in COlTed direction, main gear door, pull rod mounting bolts. Repaired by re-terminating, Left gear unsafe light wire at switch. Removed and replaced with New, 1.5 feet, X3, #22 gage ~.rires to right main gear down-lock! tLT1safe swi.tch. Installed new bulb light main gear down-lock indicator lamp. Swung landing gear several times, operation of s\!stem is n01U1a1.~ .

• J~~

'Kevm K Watrous Ref. : W.O. # 31371


DMFS DES MOINES FLYING SERVICE, INC.

~tel,up¥ ~a. . tadI.?1$l·1_ ~. ".T. a~~:l

Icertify lha! this A~'i 0' . lias beecl InspectedlnllCCllldnl... A".,,,,.,l ~~~~.L.J~~~~~~~~~~~~~ _

inspection and was dIterrnNd10 be In 81lW1l11t1y condiflon. Olher delaDs ci lhIanpeetIan..an fie at lhIa fadIItv

:::~;.O.~ ~~~1~:~. ::: .-F-'--''-=-''-''='-''''''~~=-=t-=~==-=---------Des Moines ~ . PM Fiepair Station IIG9CA485J

. ~ 1991 ASA

. ns - Stuart Aviation Services, Inc. ms Phone 561 288-5202 I 2501 SE Aviation Way )f Fax 561 288-4861 ; )Suite D, Hanger 1 I.is.) Stuart, Fl. 34996

Airframe January 27,2003

N66CC Model: PA 44- t 80T Hobbs: 811.7

Replaced gaskets in left fuel strainer. Leak check OK. With respect to this work perfonned, as mentioned above, this aircraft is approved for return to service.

EriCL.BoYdtL)AP2937667t5

e 1991 ASA

RECOROIIIIG TODAYS TOTAL TACH FLIGHT TIME 1111 TIME SERVICE


C> 1991 ASA

I

DATE

19__

3 - / -03

SERVicE

OOy..~I~'

91.,90\ o:f t .,ell. \))J

. a~"'" 6\l~uo"s;"ests, Repairs and Alterations cmn~~ must e endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

DATE

19__

RECORDING TACH TIME

lODAYS FLIGHT

TOTAL TIME iN SERVICE

Description of Inspections. Tests. Repairs and Alterations Entries mus1"oe E!ndorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

MODERN AERO, INC. . 14801 PIONEER TRAIL ••_i _

EDEN PRAIRIE. MN 55347'i:1 . 952-941-2595~ II ~ 1\ FAA APPROVED REPAIR STATION MZER198L

i

I! ~~'

DATE:6/06/Q3If

Ii',I ji

'/ JACKED AIRCRAFT, REMOVED RIGHT LANDING GEARII ~,I ----i

ACTuATOR, INSTALLED NEW SEALS IN ACTUATOR, ANDIi REINSTALLED ON AIRCRAFT, SERVICED RESERVOIR WlTIf 5606," 'I PERFORMED GEAR OPERATIONAL TEST AND FOUNDij

!, SATISFACTORY, REFERENCE ~~':1876. II il ii -

;

lj 't! "'ll '!

1'I --~--+--~---+-----,---+-----+--------------------~-~-~-----!

r> 1991 ASA

--

,I

"

!

"I

j

... '(' " i

......

TODAYS Description of Inspections, Tests, Repairs and Ai'lenition.RECORDING TOTAlDATE TACH FLIGHT TIME I. Entries must be endorsed with Name, Rating and Certificate Numb~r of

19__ TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

! , NAPLES AIR CENTER, INC.

CRS X04R655M 240 AVIATlON DRIVE NORTH :

NAPLES, FLORIDA 34104 AIRCRAFT LOG , ,

AIRCRAFT: N66CC DATE: 9-25-03 WO#: 9019 HOBBS: 911.1 RECERTIFIED TO 35,000' UNITED ALTIMETER; PIN 5934PAD-l;

SIN V5753. PERFORMED ENCODING INTEGRAnON TEST TO 25,000' \, ON NARCO BLIND ENCODER AR850. PERFORMED TRANSPONDER

RECERTIFICATION ON KING KT-76A SIN 60168. PERFORMED STATIC SYSTEM'LEAK RATE TEST. ALL lAW FAR 43 APPENDIX E AND F. ~WO# 9019 FOR PERTINENT DETAILS.

'---- '

'~' FOR NAPLES AIR CENTER CRS X04R655M. I

o LEY :-

t 1

,.,...-,1~

.'.... '".'1tA'f(....~:""'e , REC" TACH

11_,._,. y.

> "

JOIIAYS TOTAL Description of I..spections, Tests, Repairs and Alterations FlIGHT TIMEII Entries must be endorsed with Name, Rating and Certificate Number of

SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE

19__

RECORDING TACH TIME

TODAYS· FLIGHT

TOTAl TIME IN SERVICE

Description of Inspections, Tests, Repairs and Alt.,.tio"s Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

~~~~~y~s .Aircraft Registration:N66CC Total TlDle:958.7(B)

Remov~ repaired and reinstalled Sandel SN-3308 ~HSI ~IN SN~~08-OO-BL SIN 2754.Repaired Jntermitteot wmng connection on Sandel rear connector Pl-20, EIlSI ground tests good.

'. MAINTENANCE RELEASET!- IIirmft identified IIIbclw.. repired aid IrIIpeCt8d In ccalBiW ~ Clmlnt ITlIIirdBIIlIIC8 ruIeI d the FedrnI AWltIcn Regulations aid 18 CIJlPrfMld for reltrn to seMcia. Pertill8llt del8II d the repeIr n m file allhia repeIr staIion t.I1dlr.

Won Order N..ller: 173'1 Date: I2NOV83 , . 1

SIa··tve V\J': - For CapIWA\IIonIca, Inc. 'nfl CapItsI CIn:Ie Soufhwest

TaIIahastIee, R. 32310 0phone (IfO)675-ftJ28 0fax (BlitJ)67507441 - FAA CRS NS4R39fJII

II ~f=== _


TOTAL nMEW SERVICE

RECORDING TOOAYS TACH FLIGHT nME

DATE

19__

[iiJg~r:J~~~s Aircraft Registration:N66CC Total Time:0963.8(H)

Replaced S-200 PIT switch on copilot side. Ground tested #I1 COM with satisfactory results.

MAINTENANCE REI.J:ASE The .~ lcieRIfied IIbcMt W5 AlpIired .m In&pected In accad8IlCe with etmlI1t n&lltal8llCe rules c:I the FedenII AWItion Regul5ion8 tnj

Is IqlRMld fa I1Ihm to IIElf\Iice. Pertinent details c:l1he repIir I!I'e on tile lit this repelr I1l!ItkJn mder: Work Order N..ber: 27418 Date: 21NOV03

Slpatuft ~ f'- --.... For CapItalAi;1ca, 1nc.'3248 CBpItaJ CIrcle SouthWest

TIIIItIhassee, FL 323100 phone (160}li76-4028 0faX (l60)li76-7441 -l. FAA eRS NSfR3S9M

e ,QQ1 ASA

<1>

~

..__.__..... .0:.....-'----.--'"-_.~-_ .._....: Stuart Aviation Services, Inc. Phone 561 28&-5202 2501 SE Aviation Way FlU 561 288 4861 Suite D, Hanger I Stuart, FL 34996

Airframe Log December 5, 2003

N66CC MO(lcl:"PA44-I80T Year: 1975 SIN: 44·1807042 Hobbs: %9.0 ACTT: 2822.4 HeaterHobbs: 1510.6

Annual Inspection Complied with "customer requested" annoal inspection this date and ACTI.

RemovedlRe~laced Items See appGcab e 8130-3's

2ea Vacwnn relief filters PIN B3-5-1 2ea IndDCtion air filters PIN BA 3505 2ea Nose wheel rncesPIN LM 67010 2ea Nose wheel bearings PIN LM 67048 2ea.. Nose wheel felts PIN 154-006 lea.. Packing PIN MS 28775-110 (Rt. MlUG Actuator) 2ea Packing PIN MS 28775-113 (Rt. MlUG Actuator) 2ea Packing PIN Ms28775-222 (Lt. MlUG brake caliper) lea Switch (pitch sync.) (SPST momenlary push style)

Repairs/Maintenance Performed See applicable 8130-3's

Customer reports Rt fuel pressure indicator inoperative. Repaired Rt. Foel pressure indicating system by replacement of, right engine DlOIDl!ed. fuel pressure sender (See Rt. Engine log enlly, this date). Customer reports Lt. tach indicator needle sticks when power is rednced... Troubleshot Lt. tach indicating system and isolated fault with indicator assembly. (Customer notified) Resealed Rt. MlUG actuator, due to slight hydrau1ic leak @ output shaft. Repaired "cnlCked" Rt. MlUG door assembly. Door was CIllCked on interior side, just below hinge assy. This door was repaired using standard pnlCtices as outlined in AC 43.13. Repaired U. MlUG door hinge assembly, by removing stock diameter binge pin, tbeo over sizing both the door and fuselage mounted hinge stock #31. Completed by installing over sized binge pin. Customer reports pitch sync switch is sheered off. Removed and replaced tbi, mentioned sync switch w/new. Resealed Lt. MlUG brake caliper, doe to hydraulic leak @ lower piston.

Overhauled Items See appliC3bie 8130-3

N/A@thistime

"Airworthiness Directive5" See cmreot listings

FAR 43.9 Maintenance Entry All work performed here, as mentioned above, was dOne IIAIW the applicable manufacturers service and parts

instructions.

~_E~~-7 ~3~~

FAR 43.11 Inspection EnlTV "I certify that this aircraft was inspected IIAIW FAR 43 appendix (0) and inspection was supplemented by using

Piper model PA44-I80/180T inspection checklist, as guidelines. Aircraft was fOlDld to be in an airworthy condition, after test flight, and is approved fur return to service."

~~.~ ---~--=--'--------.END~-----------

DATE

19__

RECORDING TACH TIME

TODAYS FLIGHT

TOTAL nMEIN SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of rechnician or Repair Facility. (See back pages for other specific entries.)

Stuart Aviation Services, Inc. Phone 561 288-5202 2501 SE Aviation Way Fax 561 288 4861 Suite D, Hanger 1 Stuart, Fl. 34996

Airframe Log May 28, 2004

N66CC Model: PA44-180T Year: 1975 SIN: 44-1807042 Hobbs: 1007.3

ELT Battery Replaced Removed and replaced ELT battery PIN B82166... performed operational checks of ELT IIAIW FAR 91.207 (0) and noted no

discrepancy, operation normal.

FAR 43.9 Maintenance Entry All work performed here, as mentioned above, was done IIAIW the applicable manufacturers service and parts instructions.

------------.---------------------END---------------·---..------------

C> 1991 ASA

DATE

19 __

RECORDING TACH TIME

TODAYS FLIGHT

TOTAl TIME I. SERVICE


8-23-04 Hobbs /0J 3. J. .Removed left Brake cylinder replaced oring and reinstalled. Bled brakes. Ops check good. No leaks.

-<l .:..cr<..1.:1_ 2t--U.l..."..:. Scott Gimon 56702639AP

________---L ~~~~~_~~__

- - -"' ..

1. C/W Annual Inspection Using inspection guide from Piper M/M for PA44-180T. 2. Removed affected area of wing walk support. Riveted shim and doubler lAW AC 43.13-18

Chapter 4. 3. Applied cowl sealing material to missing sections on both engine cowls. Secured using 1300

adhesive. 4. Repositioned brake lines to preclUde further chafing. 5. Replaced vacuum gyro filter with new PIN AAOO-18-1. 6. serviced Oxygen to 1850 PSI using aviators breathing oxygen. 7. Adjusted the length of right engine throttle cable to hit stop on carburetor before stop on control

lever. lAW Piper M/M 73-20-Q1. . 8. Replaced L/H fuel sender gasket with new gasket PIN 755-049. 9. C/W ELT Inspection lAW FAR 91.207(d). Found plastic antenna tab missing. Replaced antenna

with new antenna PIN 763-019. Battery expires 6-30-06

P.O. Box 4942 Baltimore, MD 21220 (410) 574-4144 CRS #lF1 R294K

December 16, 2004 SIN 44-8107042




~~J,-;-:Jr blfi 'IlIr' -1 LOG BOOK ENTRY

N 66CC Airframe Enby W/O 23036 Hobbs: 1041.7

IT A/F: 2895.1

19__

'DATE

DATE

19__

RECORDING TACN TIME

JODAYS FLIGHT

TOTAL TIME III SERVICE

Description of Inspections, Tests. Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

P.O. Box 4942 Baltimore, MD 21220~~h--ir (410) 574-4144&1I(;,"'~'::iI'~" -, LOG BOOK ENTRY CRS #LF1 R294K

N 66CC Airframe Entry December 16, 2004 WID 23036 Hobbs: 1041.7 SIN 44-8107042

n A/F: 2895.1

10. Lubricated flap bearing blocks with 7870. Replaced retum spring with new PIN 487-377. Dps check satisfactory. r-

11. Removed existing L/H and R/H brake linil;lgs. Installed new PIN 066-10500. secured brake I !-- linnings with rivits PIN 105-00200. ,

12. Replaced R/H MLG tire SIN 1178WOOloo PIN 6.00-6, 8 Ply with new tire SIN 4199W00104 and , I....-- tube PIN 6.00-6. I

13. Replaced R/H MLG Inner bearing and race with new bearing PIN 13889 and race PIN 13836. ~ 14. Replaced L/H MLG inner and outer bearings and races with new bearings PIN 13889 and races

PIN 13836. ~ 15. Replaced NLG bearing and race with new bearing PIN LM67048 and race PIN LM67010 . 16. Replaced all wheel bearing felts with new felts PINs 154-00300, 154-00600, and 154-01300. 17. Adjusted aileron cable tension lAW M/M 27-10-05. ~ 18. Adjusted rudder trim cable tension lAW M/M 27-20-03. 19. Adjusted stabllator trim cable tension lAW M/M 27-30-02. ~

r-

~

r ~

DATE

19__

RECORDING TACH TIME

TODAYS FLIGHT

TOTAL nMEIN SERVICE

Description of Inspections. Tests. Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

P.O. Box 4942~~h~· Baltimore, MD 21220

(410) 574-4144Co p~w-'~~G BOOK ENTRY CRS #LF1 R294K

N 66CC Airframe Entry December 16, 2004 W/O 23036 Hobbs: 1041.7 SIN 44-8107042

IT AlF: 2895.1

20. C/W AD 2003-11-14C Correct quality control problems with the heater fuel pump. Does not apply per fuel pump model.

21. C/W AD 2001-17-13 Potential for fuel leakage in aircraft by following instructions in AD Cd) 1,2. NDN

22. CW AD 2004-14-12 - Control wheel attachment hardware. Does not apply per AlC SIN 448107042.

23. C/W Piper SB 1143 - Inspection of nose cone spar assembly. NDN at this time. Next inspection due at Hobbs 1141.7

24. C/W AD 2004-21-05 Prevent combustion of by products and fuel leakage from the combustion heaters. Installed overhauled heater assembly and ops checked-satisfactory. Work done lAW part 1,2 and 3 of AD. Next pressure switch inspection due at heater TIS 1613.2 or 12/16/06. Next pressure decay test of combustion chamber due at heater TIS 2013.2

25. Removed Inoperative R/H fuel boost pump and installed overhauled unit pIn 1458-00-1, sIn 0609. Ops checked - satisfactory

____I'--- ---l ..1.- • ----:--

01...DATE

19__

RECDR TACH TIME

-

.

!!JI!I

~r?~ N66CC W/O 23036

26. AID Notes Checked to Bi-weekly 2~

27. Performed post-inspection ground run

MAINTENANCE RELEASE The aircraft and/or component identified above was reIFederal Aviation Regulations and was found airwOrth1. Jar. are on ~~gen~ under ~ork Order No. ,z_{} 7(, Signed ~ P for Skytech, Inc., P.O. Box', ~,

12.

OVERHAULED

~tUed :La Block tJ ..

Ult"IUItd to alOC:k 1.1

I 14, Code ot

are APProVed tot'

APProvd I

Cet'ti.L'ieilte No.· .

279L

late ~ (II/dly)

/04

1certify that this in8peeted in accordance w'th a_ k'lspectlon ana was determined to ~

in alrworth conaillOn.

DATE RECORDING TODAYS TOTAl Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME I. Entries must be endorsed with Name. Rating and Certificate Number of

19__ TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

- -

MAINTENANCE RELEASE " 'The aircraft and/or component Identified above was repaired and Inspected In accordance with current . ,Federal Aviation Regulations and was found alrwo~ for retum to service. Pertinent etails of the repair are

on flle.~V'f0ryt)rderNo. ;2 3~ Of' Date. '-~',¥-..z~.e..lI{.'o"J !. Slgne~~ for Skytech, Inc., P.O. Box 4942, Baltimore, MD 2122 I

I-I

1--~ 1-

___ If-----

June 21, 2005 SIN 44-8107042

P.O. Box 4942 Baltimore, MD 21220 (410) 574-4144 CRS #lF1 R294K

Airframe Entry ACTT. 2934.3

··END--. ~. • _ ------~--,---

C!W Piper SB 1156 Nose gear drag link, dated April 7, 2005, steps 1-8, Installing new bolt P/N: NAS464P4-27. Bushings found within limits at this time. Next bushing Inspection and bolt/pin replacement due at ACTT 3434.3. C/W Jan Aero AD 2004-25-16Rl Fuel regulator valve, para (e), parts (1) and (2), dated June 20,' 2005. Also referenced Kelly Aerospace Power Systems SB A-l07A, steps 1, 2, and 5, dated September 6, 2002. No signs of leakage found at this time. Next, Inspection due at ACTT 3034.3, or June 2006, whichever occurs first.

1.

2.

-...:........ _-- ....~ "-

DATE

19__

I I

RECORDING TACH TIME

TODAYS FLIGHT

TDYAL TIME IN SERVICE

Description of Inspections, Tests, Repairs and Alterations' Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

..~.--

-P.O. Box 4942

.J __ ;,.0......OJ! Baltimore, MD 21220 c:::- , .

~.Ar (410)574-4144 c- ? LOG BOOK ENTRY CRS #LF1 R294K -

-I

Aircraft Reg. No. 6'Ccoe Serial No. ~1'-,g/tf)rtP-f~ . -


-#1 Model IC'T:?/// SIN Nt!?d.J'

#2 Model /;# SIN ~d -

I I

-The systems have been found airworthy for return to s~ Details of this ~ection , are on file a.fbis Agen<:y~ND' £3 Date: ~~. o,.r-

-Signed

-

~ - -- . -I I 1

I

i

DATE

19__

RECORDING TACH TIME

TODAYS FLIGHT


Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name. Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)


Aircraft Reg. No. 8'i?~C Serial No. f.f- J(tJIt¥'z The Altimeter(s) Static and Altitude Reporting Systems test as required by FAR 91.411 in accordance with FAR 43 Appendix E have been performed. Altimeters tested:

LIH Model 57'3yP'#fJ-1 SIN_v'---..:=3_ .t!&. tJttJI} I

.... '---.1-=-5-=3::::...--Tested To

R/H Model ~ /,4 SIN /V.....£.0~~'-----__Tested To ________

The systems have been found airworthy for return to service. Details of this inspection are on filo at !hi, Ago"y ~0:-;2J,.7'{" Dato, ,f!,t'S. (') 0;

Signed /. . -----

-I)ns )f IS.)

"- .,~

~~ _ ~",_", ••_"'~ __ ""'fI"lI.~r~~~F ... -;,,"

DATE

19__

RECORDING UGH TIME

TODAYS FLIGHT·

TOTAL TIME III SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating,and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

-'

P.O. Box 4942 Baltimore, MD 21220 (410) 574-4144 CRS #LF1 ~294K

December 09, 2005 SIN 44-8107042

1. Complied with Annual Inspection lAW Piper PA-44-180T M/M 5-21-00 2. qw ELT inspection lAW FAR 91.207(d) NDN. Battery expires June '06 3. Removed combustion heater ignition vibrator, and installed new vibrator PIN: 14EOO-1, per

Janitrol Overhaul and Maintenance Manual section 3.9. Ops checked - satisfactory 4. Adjusted cabin air valve cable as nece$ary to provide complete closure of. valve. 5. Fabricated two .5" X 7.75" doublers from .032" aldad; and riveted in place at upper and lower

attatch flanges of aft R/H oil cooler baffle using AN470AD3-3.S rivets. 6. Adjusted LH nose gear door linkage to allow door to close tighter to fuselage lAW Piper PA44

180T MM chapter 32-23-04. Operational retract check satisfactory. 7. Adjusted elevator autopilot servo bridle cable tension lAW Piper PA44-180T MM 8. Adjusted stabilator control cable tensions lAW Piper PA44-180T MM chapter 27-30-00.' 9. qw AD 2005-15-10 Correct quality con~1 problems with the heater fuel pump, effecive date

August 26, 2005. Does not apply per fuel pump model.

P.O. Box 4942 ,--f r3altimore,MD 21220 ltlons . DATE r ".. (410) 574-4144··'" erof

19 I CRS #LF1 R294'K !tries.) December 09, 2005

SIN 44-8107042 ==I

10. C/W AD 2004-25-16 Rl, effective date June 20,2005, parts (1) and (2). Referenced Kelly Aerospace Power Systems SB No. A-l07A, issue date September 6,2002, steps 1, 2, 5, 6, and 7. NON at this time. Next Inspection due at AClT: 3097.6, or December 2006, Whichever occurs first.

11. Replaced bulb in sandel SN330S-QO-BL sIn 2754 i/a/w sandel Installation Instruction SPN90122 Ufe limitation of projection lamp-200 hours or calendar year,whichever comes first.

12. Removed KX155 p/n069-1024-3, sin 4321. Bench checked, verified problem and replaced Display pin 037-00073-0000. Reinstalled unit

'. 13. Removed LMlG Super Hawk tire PIN: 53-1055, SIN: HE6039, and installed new Michelin Air tire PIN: 070-317-0, SIN: 4335WOO88, with new Michelin Airstop tube PIN: 092-315-0, per Piper MIM Ch. 32-42-03.

14. Removed and inspected hydraulic pump brushes for condition lAW Piper PA-44-1BOT 29-11-04. NON

15. AID Notes Checked to Bi-weekly 2005-24. See AD log dated 12-9-05.I,· ~"'.-""'- ,-. .~--_ ..._--_...._""'-~"--~" -- ---.~_ ..... , ... Ii 16. Performed post-inspection ground run operational and leal< checks ar~ satisfactory.

--.-----.--------------.------------------------------ END -------------------------------------------------------Ii _

=J MAINTENANCE RElEASE The aircraft andlor component identified above was repaired and inspected in accordance with current Federal'Aviation Regulations and w.as found a}.r:wq$h.n;or ~tum to service.ijP~@)e.n~tJdetails of the repairI are on file.-pt ~.Lg~C¥J.Inder Work Order No. P.ft.1L . Date:-J.t.""'_r---'Wl'_..."..&I_~,-signed,~~ "lOr Skytech, Inc., P.O. Box 4942, Baltimore, M 1220 CRS lF1R294K .

thIs aIrcraft hos been inspected kl occordanr:e with on annual Inspection and has been deemed airworthy at thi' time,

C 1991 ASA

19__

DATE RECORDING TACH TIME

TODAYS FLIGHT


Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Reoair Facilitv. (See back paces for other specific entries.)

Airframe Entry Hobbs: 1189.9


N66CC May 5, 2006 W/O 24107 S/N 44-8107042

1. Performed Piper mandatory SB 1161 - Aft wing, WS 49.25, rib assembly inspection & modification per the Instructions step 3.a. by the installation of kits p/n's 767-397 (left) and 767-398 (right). This is considered terminating action for the repetitive inspection required by this SB. SB dated March 8, 2005.

2. Removed strobe power pack s/n DA-14-1 1914. Installed a rebuilt (Whelen Engineering Co. Inc. CRS#PQ061 ONE W /0#44765) p/n 01-0770028-05 s/n 31437. Installed a new strobe light p/n A61 0 on the right hand wing.

3. Installed a new ElT antenna p/n 110-324. 4. Inspected the ElT per FAR 91.207(d).lnstalied a new battery p/n 1152166 in the elt, expiration date is

June 2008. 5. Installed an alternator capacitor p/n 63897-006 on the left alternator and repaired the field wire by

splicing in a new section of #20 wire. ----------------------------------------------------END--------------------------------------------------------------

MAINTENANCE RELEASE The aircraft and/or component identified above was repaired gnd. inspected in accordance with current Federal Aviation Regulations and was found airworThy for return to service. Pertinent details of the repair are on file ~~y~de~rder No. 24107 Date: May 5. 2006 Signedr~~for Skytech, Inc., P.O.llox 4942, Baltimore,MD 21220 CRS LF1R294K

19

.~ ~'

-p.o. Box 4942 '~er, Baltimore, MD 21220 \umt (410) 574-4144 licel CRS #LF1R294K

January 15, 2007 5/N44-8107042

_I_1. Performed an annual inspection of the airframe per Piper PA-44-180T MM 5-21-00. 2. Removed right vacuum pump P# 212CW 5# 2374 and replaced with new vacuum pump P#

216CW-WIP 5# 48224. , 3. qw AD 2004-25-16 Rl, effective date June 20, 2005, parts (1) and (2). No discrepandes

noted at this time. Next inspection due at heater hobbs: (1649.1), or 12/31/07, whichever occurs first. Removed combustion pressure switch for testing by Harold Haskins CRS#IS4R269M W/O#32259 and reinstalled. Combustion pressure switch tested JAW Janitrol S8 A-102.

4. qw AD 2004-21-05 Prevent combustion by-products and fuel leakage from the combustion heaters effective date 11/19/2004 part (e) (1) (I) , JAW Janitrol Maintenance and Overhaul Manual 24E25-1, Section 3.3.1. No leaks noted at this time.

5. Removed vacuum filter and replaced with new MOO-1S-1 filter. 6. Installed new vacuum regulator filters.

7. Installed new rotors pin 164-02300 and new brake linings pIn 066-10500 on left and right hand main wheels. .

8. Installed a new fire extinguisher pin RTA600 in aircraft. 9. Installed a repaired (AMSAFE AVIATION CRS#529R829J W/O#25233) lap bet pin 449965-201

37TN on the pilot side. 10. Rigged rudder control system JAW Piper PA44-1S0T MM chapter 27-20·02. Adjusted cable

tensions to within limits using tensiometer 5KY0077 and safetied using 4 each M521256-1 dips. 11. Installed a new gasket pIn 755-049 on left hand fuel sender. . 12. Removed ElT, opened and inspected. Installed a new battery pIn 452-0130. Tested ELT lAW

FAR 91.207(d) and unit was found to be in satisfactory condition. ElT expires 8 299~ ~/tJ' e/OA 13. Repaired broken wire CD102 on pilot's trim S\vitch 52 pin N.O. Ops check Autopilot and Electric

Trim-satisfactory.

r

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FAAIUnned States FAA Form 8130-3, AIRWORTHINESS APPROVAl TAG AA rYtlfJo 4. ~endAdlhls 5. WOIIl 0rderIC0ntJacUI NumIler.

Aero Ac«:eaorIIe, Inc. 0 1240 SprIngwood Avenu. 0 GlbIonvIIIe, NC 27'249 USA SYIJ'OFAA-PMA (PQ1208CE)

fllem 7. DeIcIiIlInn 8. t.

EIailIiIY ~lv 11. SerlII'BelcII fobrCler 12. S1atutIIW<llk PIIlNlmllr

1 Dry Air Pump NJA 1 Newly

Z,~cw f/tzzv Overhauled

13. RtII8Ib Overhauled &Tested in accordance with FAA approved data

14. CeItIlea Ile I\Inw IdontIIod obow ...... 1IIIIlIlfIctuII II CllIl!olmIy Ill: 19. 1114 CFR 43.1 IIIlurnTD SIrvIGt

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c.-. ............. qilalldln'*"*tl ....ddlldlnblock12n1011C*diltlbclU_C)llloQ NorHpprovlli _ dIlIa apdIed II BIoc:Ill3. _._..."""'Colt~. ___.poIC3 .... _ ...._ .._ .._

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15. Aud1o!IZId Siphn 18. AppnlvaVAlIhorizIIIon 20. AuI1orIlId~ J-L. 21. Appova¥Certlllcale No.: No. YV4R688M

17. Neme (TYpIdorPrtnflld): 18. OllIe (M I 0 I Y) 22. Neme (7YpId or PrInIId}

K1M CI.Ml\ SEp(M2'l 20£ ReeponIIbIIlIIoe

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Projection Lamp kit SPN90122 Iia Iw Sandel SN3308 installation manual Document No. 901061M.Reinstalled unit and reset the lamp-hoUl'S counter.Cps check-satisfactory.

15. Removed the corrosion from the aileron counter weights. Primed and painted and reinstalled. 16. Removed the corrosion from the nose structure support brackets. Treated with extend and

dinotrol. 17. AID Notes Checked to B1-weekly 2006-23. See AD Log dated 12-26-06. 18. Perfonned post-inspection ground run operational and leak checks ,are satisfactory. ---~---. ---:---.--~----"-----" END --:--------------:,-.--------------------------

MAII'ITENANCE RELEASE (. " The airaaft: and/or ponent identified above was repaired and inspected in accordance with current Federal A' on Rations and was found airworthy for retum to servic:~fertinent details of the repair are on e this ntV under Wor1c: Order No. U331 . Date: 11~ Sign for Skytech, Inc., P.O. Box 4942, Baltimore, MD 21220 CRS LF1R294K

ThI. afl'a'aft hal &.en FnspecHd in accordOl'lCe wfth an _11nspectlon and hOI b_d_a1rwanhy at litis If....

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Ir= , j<e 1991 ASA

. ......c:rI-PtJcm of 1"8»0c:tlon8. Teata. ReDaln and Alteratiel,ber o· entrie~

P.O. Box 4942 Baltimore, MD 21220 (410) 574-4144 CRS #LF1 R294K ~ Airframe Entry January 15,2007

Hobbs: 1269.6 SiN 44-8107042-I 1. Removed autopilot computer pin: 10757·1001001, sin: 13630G and autopilot controller p/n:1C771, sin: 583 and sent to Autopilots Central (certificate#: CM2R747K, trocklng #: SH07I 138211 for repair. Reinstalled unlts s/n:1363OG and 583. Ops check satisfactory.

2. Performed Roll steering adjustments on Autopilot Mode Programmer In flight. Ops check satisfactory. .

~~ 3. Replaced strobe power supply, old, PIN: 01-0770028-05, SIN: 31437. Rebuilt power supply: P/N: 01-0770028-05, SIN: 34700. Operates satisfactory.

•• Replaced filters on both left and right engine altemators. 5. Installed new transistor pin: 2N3055 on lighting meostat panel acqUired from Cessna Aircraft

Company, Cessna Ports Distribution Dept. 702; 5800 Pawnee, Wltchita, KS. 67218 on PO# I 25457. All lighting works satisfactory.

6. Installed a new OV window pin 65896-00-I I

--------·---------·-------·-·---------------:·------END-._--------.--.--.---.---------.---.-----.---------..--.-----.MAINTENANCE RELEASE

The aircraft and/or compont;nt identified above was repaired and inspected in accordance with current Fed~ral AVI.ation ~tion and was found ~¥ for reium.lO servIce. Pertin~details of the repair are o~ fole a~ '~!Jge;~f~~ ~.?rder No. ~ I Date: I 'S1'",Jfil.n. 4'1 Sign (/1:. /' ' - ·for Skytech, Inc., P.O. 80x 4942, 8altimore, MD 21220 CRS LFI R294K

RECORDING. TODAYS I TO.TP TACH FUGHT '"'" '. II n. !,dlVICE

DATE

19__

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Techniciaf' "'-·lepair Facility. (See back pages for other specific entries.)

-r------1--~

'ations ber of ntries.)

P.O. Box 4942 Baltimore, MD 21220 (410) 574·4144 CRS #LF1 R294K

Airframe Entry ... September 11, 2007 Hobbs: 1354.8 . SIN: 44-8107042

1. The A1timeter(s) Static and Altitude Reporting Systems test as required by FAR 91.411 in accordance with FAR 43 Appendix E have been performed. Altimeters tested: . UH Model: 5934PAD-1 SIN: V5753 Tested To: 20,000« R1H Moder: NIA SIN: NIA Tested To: .

MAINTENANCE RELEASE The aircraft and/or component identified above was repaired and inspected in accordance with current Federal Aviation Regulations and found airworthy for return to service. Pertinent details of the repair are on file . ency under W Order No. 24852 Date: September II. 2007 Signed orSkytech, Inc., \ppox 4942, Baltimore, MD 21220 CRS LFIR294K

I I I r= I

~ I I

t=

DATE .

19___..

1lECORDlIG . TODAYS ·TOTAL Descrlptlo'n of Inspections, Tests, Repairs and Alterations TACH TIME

FUGHT nME lit SERVICE

Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other speCific entries.)

P.O. Box 4942

~~~~ Baltimore, MD 21220 G - ,i#tD' . (410) 574-4144& ~, , LOG BOOK ENTRY CRS #LF1R294K

N66CC Airframe Entry September 11, 2007

WID: 24852 Hobbs: 1354.8 SIN: 44-8107042

The ATC transponder tests and inspections as required by FAR 91.413, in accordance with FAR 43, Appendix F have been perfonned. Transponders tested: #1 Model: KT-76A SIN: 060168

I I MAINTENANCE RELEASE

The \4iJcrafi and/or component identified above was repaired and inspected in accordance with current Federal~und airworthy for return to service. Pertinent details of the repair are on file .s ency under Wo er No. 24852 Date: September 11, 2007 Signed or Sk:ytech, Inc., P.O. Box 4942, Baltimore, MD 21220 CRS LFIR294K

DATE

19__

RECORDING TACH TIME

TODAYS FLIGHT

TOTAL 'I'IMEIN SERVICE


PO. Box 4942 Baltimore, MD 21220 (410) 574-4144 r.~S #LE1 ~?Q~K $eplember 20;2007

SiN 44-8107042

1. Removed aircraft battery ./n 4009347. Installed a new battery p/n RG35AXC ./n 40201507. 2. Removed Shodin Digidata indicator p/n: 912602, ./n: 681 and .ent to Shadin for repair. Installed

repaired unit pin 912602 & sin 681. Performed pltot/static leak test. NDF. (Shadin Avionics, Repair Station #: K5NR335Y, WO#: 09130701)

3. Replaced pltot/static tube with new tube, p/n 96392-007. Leak check in tolerance. 4. Cleaned connector at antenna, power output tested within tolerance at 125Wctts. ----------------------------------------------------END------------------------------------------------------------.-

MAINTENANCE RELEASE The aircraft and/or component . entified above was repaired and inspected in accordance with current Federal Av' ion Regulati an was found airworthy for return to service. Pertinent details of the repair are on file at Is aqe~cy er W. rk Order No. ~ Date: _September 20, 2007_ Signed .;(t'?; r Skytech, Inc., P.O. Box 4942, Baltimore, MD 21220 CRS LFI R294K

-----'.~-----------

·DAlE .'

11__, _

',REC._ TACH TIME

TODAYS FLIGHT

TOTAL TIME II SERVICE


Registration: N66CC Make: PIPER Model: PA44-180T SIN: t/f-aJ01 0'/2.-

AlC tfoBas:I3I:3.1 AlC Landings: Work Order: N/A Date: 10-4-07

REPLACED BUSHINGS AND HARDWARE FOR NOSE GEAR TORQUE LINKS.

Signature, ~ "-t2I.- 'Certificate #, 73707471AP

--_.-Richmor Aviation Inc. Maintenance Record

/

FAA-PMARosen P/N-:-RPF-300-2 {PQ2393NM) i Description: PlPER-2 SYSTEM

customer PIN: N/A Model: PIPER-2 ' STC No: SEE STC .

• Insp: C£> ;'5 2oorClliiiiiu_-- ----.,.--

""""

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ons-' DATE Description of Inspections, Tests, Repairs and Alterations of Entries must be endorsed with Name, Rating and Certificate Number of ~s.) Technician or Repair Facility. (See back pages for other specific entries.)

'1

10-30-07; N66CC Airframe Hobbs: 1372.1

Removed and replaced left fuel sending unit gasket PIN 755-049 lAW Piper PA 44- 18QT MIM. Repaired right engine mag cooling duet. . The aircraft, aircraft engine, propeller or appliance identified above was repaired and inspected in aceordance with current maintenance rules of the Federal Aviation Regulations and is approved for return to service. "Pertinent details of the repair are on file at this repair station under

Work Order: AJ3947 Date: 10-30-07

Signed~~r?~-Michael ~i;ato

For ALOETS OPERATIONS,LLC INC. Certificate 2501 S.E. Aviation Way Suite D Stuart, FL 34996

Description of Inspections, Tests, Repairs and AlterationsRECORDING TODAYS TOTAL TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of

19__ nME SERVICE Technician or Repair Facility. (See back pages for other specific entries.) ! ----+----~.

DATE RECORDING TACH TI~IE HOBBS TI~IE TOTI~L TIME IN SEF<VICE _ 11/09/07 0.0 1376.6 ,3I7U# p.u

AIRCRAFT LOG BOOK ENTR~f N66CC PIPER SEMINOLE PA44-180T \ RECORDING HOBBS TIME = 1376.6 AIRCRAFT TOTAL TIME IN SERVICE :::3'-f1Z. q'tMk· ====:=====::::=====:=::::::====::::=::====::-.:=::::::==::::==:::::::::=================:::=-:... ;;;..-==::::~::;:::: l

.,:$'"

THE FOLLOWING MAINTENANCE WAS PREFORMED THIS DATE: LOW OIL JPRESSURE INDICATION NOTED BY PILOT ON LEFT ENGINE GUAGE.

VERIFIED GUAGE IS OPERATING NORMALLY. RUN UP INSPECTION REVEALED f

iLEAKING AROUND OIL SENDING UNIT. REMOVED AND REPLACED WITH NEW ISENDING UNIT PART #587-956. RUN UP TO VERIFY OIL PRESSURE ~ INDICATOR WORKING PROPERLY, LOW OIL PRESSURE STILL INDICATED,

REMOVED OIL PRESSURE RELIEF VALVE FOR INSPECTION, SPRING AND BALL INCORRECTLY INSTALLED. CLEANED AND REINSTALLED SPRING AND I BALL CORRECTLY. RUN UP STILL INDICATING LOW OIL PRESSURE AFTER. ALL ADJUSTMENT LIMITS WAS REACHED. REPLACED OIL PRESSURE IRELIEF VALVE ASSEMBLY WITH NEW PIN 77808 ,SPRING PIN 61084, BALL , PIN 1028-B. ADJUSTED PRESSURE RELIEF VALVE. INSTALLED NEW CLEVIS jPIN PIN MS20392-1C19 ON NOSE WHEEL. CHANGED OIL IN L/H AND R/H ENGINES. CUT OPEN OLD FILTERS, AND INSPECTED FOR EVIDENCE OR METAL OR EXCESS CARBON AND NONE WAS FOUND. OIL SOAP SAMPLES ITAKEN AND MAILED FOR PROCESSING TO AVIATION LABORATORIES.

1REPLACEDL/H AND R/H OIL FILTERS WITH PIN CH48103. SERVICED ENGINES WITH 120TS AEROSHELL 15W-50 DET. OIL. RUN UP,NO LEAKS FOUND AND OIL PRESSURE NORMAL. *-*END*.* l/~

DATE RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of

19 __ TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

;~0_l ~**~)~~J~~~*~,~~~*~~ji-**~)~~~~~~*~)~)~~f~!(~~*i*~(jf' ~:~A:;l·.~~·~~A~~)~~1t~~·~}t~~ t

[ [FRTIFY rHAT rHE ~AINTENANCE AND REPAI~S PERFOP~EO eN fHIS tl.r::;~cr;.:(lrT i\tl l.)[ B[Cr··1 L~'I~~';F'[C.T[li U(···!:C~[I~: CUPF-:F!··iT F('i (I l·,~rl.:j:.JL.f\ r :.C'j-··:::.:; ···"'i.

:,:';\ F: E. ,"~ r> \:-, i"\ Ur) F" [I ::' C· F;~ r:: 1::. T\ Jr;~ I"'; T0 ~:~: FF:!.) ICC THT~::; U('j r[, r:' cr;.: T r. ;·ll-~. ;.\ :" :i'~ E:: ; ;'::1 :

~. 11 E: i'1 (':1 J NT f~ r! til-,j CE (11-,·1 Ii h' [. F' (1 Tj~: S (:i r-;.: F C) 1···j F T1._ [ ti T THT':) r' I : I t Ll "r (:'\ "T J :J!

IjriD[F~ ',)i]. :?1~.. .. It'\j rEn .111C!3/~-!. Ii~':::~'I'C rUF~ .. ~~.. FOR TNGLEWUOD ~VIATION INC. FAA eRS ZA4RSSJM PO ~nx l~?O U (, L PFI,'I (,0:1_. C 'c:; T,';hl!. '/ CUIJr,! '1\' (~r i~:P Cf;:T, tiL ;:~[i'1(II~:L~:' : Ie .• iL'') i,.,

1 __ L ~ . .

DATE RECORDING TACH TIME HOBBS TIME TOTAL TIME IN SERVICE 2/08/08 0.0 1391. 3 3487.1

AIRCRAFT LOG BOOK ENTRY: N6&CC PIPER PA-44-180T, SIN 44-8107042 TOTAL TIME AIRCRAFT .... :3487" 1 TOTAL TIME HOBBS METER '" 13')10 3

i HEATER HOBBS METER ::: 1563.8 ==:==========;===:=:==:============================:::::::=::====:::=:==:::::::::= COMPLETED A ANNUAL INSPECTION THIS DATE PER INSPECTION GUIDE AND PIPER MM. OPENED PLATES AND PANELS REQUIRED BY THIS INSPECTION. LUBED AND SERVICED PER PIPER MM GUIDE. INSPECTED STRUCTURE AND CABLES. LUBED PULLEY AND ROTATED. JACKED AIRCRAFT REMOVED ALL WHEELS. CLEANED AND REPACKED LH AND RH MAIN WHEEL BEARINGS. CLEANED AND REPACKED NOSE WHEEL BEARINGS, REMOVED WORN NOSE TIRE AND INSTALLED NEW CONDOR TIRE 5.00-5 f.,PLY SIN 6254W00134. BALANCED AND REINSTALLED ALL WHEELS. REPLACED LH AND RH LANDING GEAR BRAKE HOSE WITH NEW HOSE PIN 565-148. BLED BRAKE SYSTEM ~z '~ 1991 ASA

DATE. "

19__

aCORD. TACH TIME

AND GEAR EXTENT ION REPLACED FILTERS

TESTED DUE FEB.

05,2008. FEBUARY 1663.8 DUE

INTERIOR. THRU R03 I WITH APPROVED THE NO ~ FOR ALBEMARLE

OR

~---

ELT

---

TODAYS TOTAl Description of Inspections, Tests, Repairs and Alterations FU6HT nME III Entries must be endorsed with Name, Rating and Certificate Number of


SERVICED WITH HYDRAULIC FLUID. RETRACTION TESTED LANDING THRU 4 CYCLES AND OPERATIONS WERE NORMAL. EMERGENCY

WAS OPERATIONALLY CHECKED AND OPERATIONS WERE NORMAL. HOSE ON BRAKE RESERVOIR. REPLACED INSTRUMENT AIR

AND VACUUM FILTER. REPLACED LH MAIN GEAR SCISSOR BOLT PIN 691-308 • . REPLACED LH MAIN GEAR SCISSOR BUSHING PIN 453721.

AND REPLACED BATTERY PIN BS2166. ELT BATTERY NEXT 2010. REMOVED SANDEL HSI, PIN 3308 REINSTALLED AFTER .

BULB REPLACEMENT BY CAROLINA AVIONICS ON WO"4446 DATED FEBUARY C/W AD 2004-25-16R NEXT DUE @ HEATER HOBBS 1663.8 OR -_.

08,2009. C/W ~D 2004-21-05 NEXT DUE @ HEATER HOBBS FEBUARY 08,2009.C/W OXGEN BOTTLt HYDRO TEST, NEXT

FEBUARY 08, 2013. SERVICED WITH OXYGEN TO 1750 PSI. REINSTALLED ~LATES AND PANEL. WASHED EXTERIOR·AND CLEANED

LUBED ALL EXTERIOR CONTROLS. AD COMPLIANCE REVIEWED ISSUE JANUA~Y 25, 2008.

************************************************************ CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE .

A ANNUAL INSPECTION UNDER CURRENT FAA REGULATIONS AND IS FOR RETURN TO SERVICE THIS DATE. PERTINENT. DETAILS OF

INSPECTION ARE ON FILE AT THIS REPAIR STATION UNDER WO DATED ~/~i INSPECTOR ~ ~

INGLEWOOD AVIATION INC. FAA CRS ZA4R693M PO BOX.1~0 STANLY COUNTY AIRPORT, ALBEMARLE NC 28002 "liz . , ,

DATE -

19__

RECORDING TOOAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT nMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE RECORDING TACH TIME HOBBS TIME TOTAL TIME IN SERVICE '12/03/08 6.0 1477.6 3573.4

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AIRCRAFT LOG BOOK ENTRY HGGCC.:" PIPER PA-44-180T, SIN 44-8107042 AIRCRAFT TOTAL TIME IN SERVICE = 3573.4 AIRCRAFT RECORDING HOBBS ~ETER = 1477.6 ----. HEATER HOBBS METER = 1577.9

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~===========;===~================================================ A ANNUAL INSPECTION WAS COMPLETED THIS DATE: REMOVED PLATES AND PANELS REQUIRED BY THIS INSPECTION. INSPECTED STRUCTURE AND CABLES. LUBED PULLEYS AND ROTATED. LUBED AIRCRAFT PER SERVICE GUIDE. JACKED AIRCRAFT REMOVED ALL WHEEL ASSEMBLIES. CLEANED AND CHECKED BRAKE DISC AND LININGS FOR WEAR. BRAKE DISC AND

~---'LININGS OK TO CONTINUE IN SERVICE. CLEAN, INSPECTE[I AND ----- REPACKED ALL WHEEL BEARINGS. REINSTALLED ALL WHEEL ASSEMBLIES --

SERVICED BRAKE RESERVOIR WITH HYDRAULIC GEAR RETRACTION TEST AND EMERGENCY III

AFTER BEING BALANCED. - FLUID. PERFORMED LANDING -- f..--

EXTENSION WAS OPERATIONAL CHECKED. NO DISCREPANCIES FOUND. ...- -a_ions )er of

DATE LOWERED AIRCRAFT FRO~ JACKS. SERVICED BRAKE RESERVIOR WITH

19__ ntries.)HVDRALIC FLUID. SERVICED LANDING GEAR RESERVOIR WITH HVDRALIC -----I. FLUID. CIW ELT IHSPECnOH PER FAR 91.207(D) NO DISCREPANCIES

NOTED. ELT BATTERV NEXT DUE ON OR BEFORE 02/2010. INSTALLED NEW LANDING LIGHT LA~P~ OPS CHECKED OK. INSTALLED NEW TAIL NAV LAMP. OPS CHECKED. OK. INSTALLED NEW CAPACITOR PIN 51915-1 ON LH ALTERNATOR. TROUBLE SHOOT LH WING FUEL WEEPING. FOUND SEAL BAD AT LH SENDING UNIT. REPLACED LH FUEL SENDING UNIT GASKET. CIW AD 2004-2'-05 CO~BUSTION DECAY TEST PER AD INSTRUCTIONS AND lAW JANITRDL ~AINTENANCE AND OVERHAUL MANUAL 24E24-1. NO DISCREPANBIES FOUND. CIW AD 2004-25-16Rl COMBUSTioH PRESSURE SWITCH TEST PER JANITROL SB A-I02. NO LEAKS NOTED. HEXT DUE HHM 1677.9 OR DEC 03, 2008. CIW SB "1188 EMERGEHCY GEA~ EXT.CAB~E, PER MOD KIT PIN 88433-002 DRAWING AND INSTRUCTIOHS.' CHECKED CABLE TENSIOHS AND ALL TRAVEL LIMITS. WE~GHTE{) FIRE EXnHGUISHERS~ SERVICED 02 TO 1750 PSI. REIHSTALLED ALL PANELS AND PLATES. WASHED EXTERIOR AND CLEANED INTERIOR. LUBED ALL EXTERIOR CONTROLS. AD COMPLIANCE REVIEWED

______~ T~RU ISSUE NOVERMBER 28, 2008. ***END*** R03 ************************************************************ I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION UNDER CURRENT FAA REGULATIONS AND IS APPROVE' FOR RETURN TO:SERVICE THIS DATE. PERTINENT DETAILS OF THE INS.ECTION ARE ON tILE AT THIS REPAIR STATION UNDER WO NO 35f5l. :DATEDc2/0"4/'UJt)"$ INSPECTOR rfA.tt f'/IAJh/ FOR INGl.EWOODAVIATION'INC. FAA CRS ZA4R693M PO BOX17fO ALBEMARLE STANLV COUNTY AIRPORT, ALBEMARLE Ne 28002

Zfz--

Description of Inspections, Tests, Repairs and AlterationsRECORDINI TODAYS TOTALDATE TACH TIME I. Entries must be endorsed with Name, Rating and Certificate Number ofFLIGHT

19__ SERVICETIME Technician or Repair Facility. (See back pages for other specific entries.)

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TOTAL TIME IN SERVICEDATE· RECORDING TACH TIME HOBBS TIME 12/15/09 0.0 1572.2 3&&8.0

AIRCRAFT LOG BOOK ENTRY N6&CC. PIPER PA-44-180T, SIN 44-8107042 AiRCRAFT TOT~L TU1E IN SERV1CE = 3668.0 AIRCRAFT RECoRDING HOBBS "ETERe' =1572.2 AIRCRAFt HEATER HOBBS ftETER. =1597.5 ================================================================= A ANNU~ INSPECTION WAS COMPLETED THIS DATE: REMOVED PLATES AND PANELS REQUIRED BV THIS INSPECTION. INSPECTED STRUCTURE, CABLES AND TURNBUCKLES. LUBED PULLEYS AND ROTATED • LUBED AIRCRAFT PER

. SERVICE GUIDE. JACKED AIRCRAFT REMOVED ALL WHEEL ASSEMBLIES. CLEANEn AND CHECKED BRAKE DISC AND LININGS FOR WEAR. BRAKE DISC AND LININGS OK TO CONTINUE IN SERVICE. CLEANED, INSPECTED AND REPACKED ALL WHEEL BEARINGS. REINSTALLED ALL WHEEL ASSEMBLIES AFTER BEING BALANCED. . SERVICED BRAKE RESERVOIR WITH HVDRAULIC FLUID• REPLACED ALL LANDING GEAR HVDRAULIC ACTUATOR HOSES. I/~.i .. - .-.

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DATE

19__

SERVICED LANDING GEAR HYDRAULIC RESERVOIR. PERFORMED LANDING GEAR RETRACTION TEST AND EMERGENCY EXTENSION WAS OPERATIONAL CHECKED. NO DISCREPANCIES FOUND. LOWERED AIRCRAFT FROM JACKS. CIW ELT INSPECTION PER FAR 91.207(D). ELT BATTERY DUE ON OR BEFORE 02/2012. CHECKED CABLE TENSIONS AND ALL TRAVEL LIMITS. WEIGHT FIRE EXTINGUISHERS. REMOVED JPI EDM 760. REINSTALLED JPI EDM 760 SIN 2402 AFTER BEING OVERHAULED BY JPI INSTRUMENTS INC. ON WO" RMA28687 DATED NOVEMBER 23, 2009. TOUCHED UP PAINT ON NOSE GEAR LOWER STRUT FORK AND WHEEL. REMOVED LH ENGINE ALTERNATOR PIN ALY6421RX S/N.A148754. INSTALLED OVERHAULI EXCHANGE ALTERNATOR PIN ALY6521R SIN J100089 OVERHAULED BY KELLY AEROSPACE ON WO" M247650 DATED OCTOBER 13, 2009. CIW AD 2004-25-16Rl BY INSPECTION PER AD INSTRUCTIONS AND SB A-l07A. NO LEAKS FOUND. SERVICED OXYGEN TO 1750 PSI. INSTALLED NEW CLAMP ON RH ALTERNATOR NOISE REGULATOR. REMOVED SANDEL EHSI SIN 2754. REMOVED RACK FOR SANDEL EHSI. INSTALLED NEW RACK PER SANDEL TECH REP INSTRUCTION PIN 82113-A. REINSTALLED SANDEL EHSI SIN 2754 AFTER CASE REPLACEMENT BY SANDEL TECH REP. ALL OPERATIONS AND FUNCTION CHECK NORMAL. REINSTALLED PANELS AND PLATES. WASHED EXTERIOR AND CLEANED INTERIOR. LUBED ALL EXTERIOR CONTROLS. AD COMPLIANCE REVIEWED THRU ISSUE NOVEMBER 27, 2009. ***END*** R03 ************************************************************ I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION UNDER CURRENT FAA REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE THIS DATE. PERTINENT DETAILS OF THE INSPECTION ARE ON FILE AT THIS REPAIR STATION UNDER WO NO "$mR.. DATED /:J./IS/Jooq INSPECTOR AA fI'1AJn-/ FOR INGLEWOOD AVIATION MAINTENANCE SERVICES INC. IFAA!CRS ZA4R693M.

.tlons )er of ntries.)

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-~

I

: ALBEMARLE STANLY COUNTY AIRPORT, PO. BOX 1720 ALBEMARLE NC 28002 q&

- rOTAl r H1E IN SERl)lCEI DATE RECORDING TACH rIME HOBBS r [I'IE 3684.11/18/10 0.0 1588.3

1!

AIRCRAFT LOG BOOK ENTRY N66CC: PIPER PA-44-180T, SIN 44-8107042 AIRCRAFT TOTAL TIME IN SERVICE = 3684.1 AIRCRAFT RECORDING HOBBS METER :;:: 1~S88.3

================~=====================:==:======================~

GENERAL MAINTENANCE PERFORMED fHIS DArE: REMOVED UPPER AND LOWER COWLING ON lH & RH ENGINES. REMOVED AND INSTALLED NEW TIT PROBE PIN 86143 ON LH ENGINE. REMOVED AND INSTALLED NEW fGT PROBE PIN M7111 ON NUMBER 1 CYLINDER ON RH ENGINE. OPS TESTED BOTH PROBES AND NO DISCREPANCIES FOUND. REINSTALLED COWLING ON LH & RH ENGINES. ***END***

R01 ************************************************************ I CERTIFY THAT THE MAINTENANCE AND REPAIRS PERFORMED ON THIS AIRCRAFT HAVE BEEN INSPECTED UNDER CURRENT FAA REGULATIONS AND ARE APPROVED FOR RETURN TO SERVICE THIS DATE. PERTINENT DETAILS OF THE MAINTENANCE AND REPAIRS ARE ON FILE AT THIS REPAIR STATION UNDER WO 3WS(( DATED ot1(2~10 INSPECTOR~~ FOR INGLEWOOD AVIATION MAINTE~E SERVICES INC. FAA CRS ~A4R693M ALBEMARLE STANLY COUNTY AIRPORT, ALBEMARLE NC 28002

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nd Alterations cate Number of specific entries.)

\

1

TOOAYS TOTAL Description of Inspections, Tests, Repairs and Alterations FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of


1(

I

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1

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TOTAL Description of Inspections, Tests, Repairs and AlterationsRECORDING TODAYSDATE TIME INTACH FLIGHT Entries must be endorsed with Name, Rating and Certificate Number of SERVICE19 {lOIO TIME Technician or Repair Facility. (See back pages for other specific entries.)

F.A.A. - P.M.A. AIRTEX PRODUCTS, INC.

NUMBER q31/7 1'/0'1 PART ~~ CARPET

PART COWL PAD PART CUSHION UPHOLSTERY PART HEADLINER PART WALL PANELS PART BAGGAGE COMPARTMENT PART FIREWALL COVER PART SEAT SLINGS PART HAT Sl1JiLF PAD

ELIGIBILITY /9y/ f,f~r fA 4 fI --~--~-----

to 1991 ASA

4-:..--- ::::-.. __ .c __.==-~~. .__. ~~._:~:-:~.:_: ._. :__ ._::~~-. :.-.._- ..--_.:. ~.'. =_ ._.. :==:: =:-._ .. . "Dl~ ~East Coast Cirrus Factory Authorized Service Center'

1. I·~ ..I? AVIAT"I1N SERVICE. Cessna, Beech, Piper Piston Singles &Twins<<'.0-1 -- _ INC. 2580 SE Aviation Way Ste 102----l ".' Stuart, FL 34996 PH (772) 781-0610 ~ .....-./ [email protected]

I 5/21/10 N66CC PA-44·180 SN#4481 07042 H.M.1631.7 .~,I Removed 10 amp circuit breaker from bottom of panel for the KX 155 Nav/Com, replaced circuit breaker PN#7274-2- !-_; 10 operational checks ok no discrepancies noted. . A 31 -i

8092 Memphis Avenue, Millington, TN. 38053 PH. 901-873-4780 eRS # T8BD652N

June 30, 2010 Hourmeter: 1640.6 N66CC SIN 448107042

Removed attitude gyro PIN lU3 7-203-3 SIN 4437A and installed overhauled exchange PIN lU367-203-3 SIN 400 Groun.d ops checked good. A;( c::s

William A Dean N ..11'tI-Details on file under W.O.# 26118

I

8092 Memphis Avenue, Millington, TN. 38053 PH. 901·873-4780 eRS # T8BD652N [email protected] July 28,2010 Hounnctcr: 1643.1 N66CC SIN 448107042

Replaced #2 KXI55 power supply wires and circuit breaker supply wire to correct intennittent operation caused by poor installation practices. Sent KX155 NAV/COM PIN 069-1024-31 SIN 4231 to ASI for repair. ASI found broken circuit board runs caused by excessive current at switched power out P401-12 and N. Found unused wire spliced into switched power output of KX 155 to be shorted to airframe ground. Isolated unused wire and capped and stowed. Reinstalled repaired KX155. Ground ops checked good.

Avionics bus voltage low caused by loose wire tenninals at avionics master relay. Wires and terminals heat damaged from arcing. Replaced wi~resan~tr~=d ops check of avionics master good.

William A. Dean IV ~ \ :5 Details on file under . .# 261794

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DATE

19__ CSG AVIATION

Airframe log entry for an Annual Inspection. N-66CC Piper PA-44 Seminole SN 44-8107092

Aircraft Hour meter 1713.5 Airframe Total Time 3809.3 An Annual Inspection has been completed this date lAW FAR43 [a][d] and applicable service instructions.

Tested E.L.T.IAW FAR 91.207[a][d] and is found to be airworthy for continued service, with battery expiration of Feb 1011 Airworthiness Directives checked through Dec 1010 I certifY this aircraft has been inspected lAW an annual inspection and is found to be airworthy at this time.

l. R&R B3-5-1 filter. L& R 2. Acft lube clw 3. . R&R Rt & Lt brake pads (8 ea) with new pin 66-105 4. OIH Lt brake assy with new 0 rings pin MS28775-222 (2ea) 5. ACF 50 treatment c/w. 6. AD 2004-21-05 24mth I 100 hr heater decay insp c/w. Next due 1717.1 on htr hr mtr or Dec 15

2012 7. AD2010-15-10 One time insp of L &R yoke U joints clw 8. AD 2004-25-16R I 1001 annual insp of heater fuel shut off. Next due 1717.1 on htr hr meter or

Dec -15-2011 9. R&R rt and It main tires with 6-6.00/8/120 Michelin tires

~i~~:;P13r;:;::vts Dare 12I2JaOlO

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€I 1991 ASA

Documents

eliteaircraft.comeliteaircraft.com/N66CC Airframe logs.pdf · 2012-01-07 · 2654.6. Painted new "N" numbers on aircraft. Adjusted voltage regulators. Removed and replaced NLG tire