AIRSf)EED CALIBRATION - Axenty Aviation PA44-180.pdf · pa-44-180 normal procedure-accelerate. and stop distance *standard brakes "" """lu'-'i"""" ii" '" " "ii. °1 both engines 2700

PIPER AIRCRAFT CORPOt(ATIONPA-44-180, SEMINOLE

SECTION 5PERFORMANCE

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INDICATED AIRSPEED - KNOTS

Example:Indicated airspeed: 124 knotsFlaps upCalibrated airspeed: 123 knots

AIRSPEED CALIBRATIONFigure 5-1

ISSUED: MARCH 23, 1971

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REPORT: VB-1605-11

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PIPER AIRCRt.\FT CORPORATIONPA-44-180, SEMINOLE-

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STALL SPEED VS. ANGLE OF BANKFigure 5-3

REPORT: VB-8605-12


PA-44-180NORMAL PROCEDURE- ACCELERATE. AND STOP DISTANCE

*STANDARD BRAKES"" """LU'-'I"""" II" '" " "II.

BOTH ENGINES 2700 RPM°

1'AND FULL THROTTLE

~ MIXTURE FULL RICH

g WING FLAPSO' ,. ~:! MAX. BRAKING "'"-' COWLFLAPSOPEN ~~ PAVEDLEVELDRYRUNWAY I::::I ABORT SPEED,7,6 ,KIAS

*NOTEREDUCEACCEL." STOP DIST.BY 10% IF HEAVY DUTY

BRAKES_TEI:~._~.:0

~, ~

I-I-~

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Example: ~-r-Airport pressure altitude: 680 ft.Outside air temperature: a.eWeight: 3430 Ibs.Wind component: 5 kt. headwindAcee!. 8<stop dist.: 2050 ft.

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MI.

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0 II 10 111

WIND COMPONENT - KNOTS

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PA-44-180'; Example: """,""" ,.." SHOJtTFIELDACCELE:RATEANDi AlrlX!rtpr~ss.alt.:6~ ft. I STOP DISTANCEoooj Outside air tenlp.. 8 C * STANDARD BRAKESWeight: 3430 Ibs.::2 Wind component 5 kts. headwind BOTH ENGINES 2700 RPM .. FULLTHROTTLE~ Accelerate & stop distance: 1760 ft. MIXTUREFULLRICH!:"" . ..' .-. . . WING FLAPSO' - ABORT SPEED 70 KIAS OR~ 'NOTE WING FLAPS 215' . ABORTSPEED 83 KIAS> Reduce_8'...topdlat.by10% COWLFLAPS OPEN~ Ifh8~~dutybl8k~.~..lnlt8ll8d. PAVED LEVELDRY RUNWAY~ ..". MAXIMUMBRAKIN.G.~ ' _.

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NORMAL PROCEDURE TAKEOFF GROUND ROLL (0° FLAPS)Figure 5-9

8888"'.0..PlPIPIN ~!\j INJ 1'iI\)-.N.t :"f~I"

ISSUED: MARCH 23, 1978REVISED: SEPTEMBER 14, 1979

REPORT: VB-8605-15

SECTION SPERFORMANCE

PIPER AIRCRAFT CORPORATIONPA-44-t80, SEMINOLE

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Figure 5-11

REPORT: VB-8605-16


PIPER AIRCRAFT CORPORATIONPA-44-180, SEMINOLE

SECTION SPERFORMANCE -

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ISSUED: M'ARCH 23, 1978 REPORT: VB-8605-11



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Figure5-1'

REPORT: VB-8605-18


Example:Airport press. alt.: 680 ft.Outside air temp.: aoe -Wind component 6 kt. headwind -Weight: 3430 Ibs.Total ground roll: 660 ft.

fT'

PA-44-180"""",."""""" """""

SHORT FIELD EFFORTTAKEOFF GROUND ROLL

2700 RPM . FULL THROTTLE BEFORE BRAKE RELEASEWING FLAPS - 215° COWL FLAPS OPEN

PAVED LEVEL DRY RUNWAYWEIGHT LIFT OFFPOUNDS SPEED KIAS

3800340030002800

1131101511152

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OUTSIDE AIR TEMPERATURE - °C

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PA-44-180SHORT FIELD EFFORT

TAKEOFF DISTANCE OVER 50 FT. BARRIERWING FLAPS2&' «

COWL FLAPS OPEN2700 RPM. FULLTHROTTLE

BEFORE BRAKE RELEASEPAVED LEVEL DRY RUNWAY

WEIGHT UFTOFF BARRIERPOUNDSSPEEDKIM SPEEOKIAS

3800~40031!OO2600

8380III112

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Example: ~Wind component 6 kt. headwindAirpo" press. alt.: 680 ft.FWeight: 3430 Ibs.Outside air temp.: 8'C ~Total distance over barrier. 1070 ft.

.40 .20 0 20OUTSIDE AIR TEMPERATURE - ac

- -- --

40 31500 3000 21500 0 15 10 115WEIGHT - POUNDS WIND- KNOTS

- '- ..-

3000Ii:i

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CLIMBPERFORMANCE-BOTH ENGINES OPERATlNG-GEAR DOWN

Figure 5-21

ISSUED: MARCH 23,1978 REPORT: VB-8605-21

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Example:Press. alt.: 680 It.Outside air temp.: aoeWeight: 3430 Ibs.Rate of climb: 1570 It.! min.

~d-L!o'...

-BEST POWER MIXTUAE L_ANED<2S0F ~ ~\'f,!~\~RICHOFPEAKE.G.T.. ~ ~~~X~!

~~~~~~

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40 -30 .20 .10 0 0 20 30 40OUTSIDE AIR TEMPERATURE - °C

1Z00 1800 20000 400 BOO

------PIPER AIRCRAFT CORPORATIONPA-44-180, SEMINOLE


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CLIMB PERFORMANCE -ONE ENGINE OPERATING -GEAR UPFigure 5-25

ISSUED: MARCH 23, 1978REVISED: APRIL 10, 1981

REPORT: VB-860S.13

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PA.44..180FUEL, TIME AND DISTANCE TO CLIMB

E'NGINES2700 RPM . FULLTHROTTLEWINGFLAPSO' - COWL FLAPS OPEN' ':j:j:j::I:j:1

LANOI.r.aGG~I:t.I:I~'t:M8W.~OCLIMB SPEEO 88 KIAS

-:;:;:z.,

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Example:Airportpre... Ih.: 880 ft.

, Airportoutllde lir temp.: a.c

II Crulle prell. Ih.: 6800 ft.Crull' outsld. Ilr temp.: -2.CFuel to climb: 2.6 minul 1.0 =Time to dimb: 4.6 minus 1.2 =DI..ln08 to climb: 7 minul 1.4.", rrnn'

j:.i

laf'j_nIofJdC:»c:»

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OUTSIDE AIR TEMPERATURE - .C0 10" 20--- 30 40

TIME DISTANCE AND FUEL TO CLIMB

1.6118"3.3 min.=5.8 NM

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F1!EL AND POWER CHART. LYCOMING (L) 0-366-E SERIES (PER ENGINE)

NOTE: To maintain constant power, add approximately I% manifold pressure for each 6° C abovestandard, subtractapproximately I% for each 6°C belowstandard.

*Best Power

~

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Press. Std. Alt. 99 BHP - 55% Rated Power 117 BHP - 65% Rated Power 135 BHP - 75% Rated Power Press.Alt. Tel1)p. Approx. Fuel Flow-9.3 Gall Hr.. Approx. Fuel Flow-IO.3 Gall Hr.- pprox. Fuel Flow-I 1.2 Gall Hr. * Alt.Feet °C RPM AND MAN. PRESS. RPM AND MAN. PR'£SS. RPM AND MAN. PRESS. Feet

2100 2200 2300 2400 2100 2200 2300 2400 2200 2300 2400

SL 15 22.2 21.7 21.2 20.7 24.5 24.0 23.4 22.9 26.4 25.8 25.2 SL1000 13 21.9 21.4 21.0 20.4 24.2 23.7 23.1 22.6 26.1 25.5 24.9 10002000 II 21.6 21.1 20.7 20.2 23.9 23.4 22.9 22.3 25.8 25.2 24.6 20003000 9 21.3 20.8 20.4 19.9 23.6 23.1 22.6 22.1 25.4 24.9 24.4 3000

4000 7 21.0 20.6 20.1 19.7 23.2 22.7 22.3 21.8 FT 24.7 24.1 40005000 5 20.8 20.3 19.9 19.4 22.9 22.4 22.0 2J.5 - FT 23.8 50066000 3 20.5 20.2 19.6 19.2 22.6 22.1 21.7 21.3 - - FT 60007000 I 20.2 19.7 19.3 18.9 FT 21.8 21.5 21.0 7000

8000 -I 19.9 19.5 19.1 18.6 FT 21.2 20.7 80009000 -3 19.6 19.2 18.8 18.4 - - FT 20.5 9000

10,000 -5 19.3 18.9 18.5 18.1 - - - FT 10,00011,000 .7 FT 18.6 18.3 17.9 11,000

12,000 -9 - FT 18.0 17.6 12,00013,000 -II - - FT 17.4 13,00014,000 -13 - - - FT 4,000

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~"»."!'!tOo!.-~000~"rJ)~~O::"->ZOo!0-~O~Z

.40 .30 .20 .10 0 10 20 30 40

OUTSIDE AIR TEMPERATURE - °C

140120 180 180

TRUE AIRSPEED - KNOTS

----------------

- , +<-SPEED POWER" --.- --. -- - -_.- -.- -

- --

---'h"- ---

APPROX.FUEL FLOW%PWR.'

PERF.CRUISE ECON. CRUISEH 18.80PH 14.80PH 58

.,... 20.8 OPH 17.0GPH 6822.4 OPH IS.3GPH ., 78

-.

. --

ECON MY CRUISE MIXTURELEAN EO TO PEAK E.O.T.

fI

----..". -.- . ,- ----.- -, -

.-,..

"a\. -- ..' -.... .--..

..-. -. 'b"" --,

PA-44-180'STANDARD TEMPERATURE

'--"'PERFORMANCECRUISE RANGE'T'JT MIXTURE LEANED TO 1250 F RICH OF PEAK E.G.T.

-. +~ 3800 POUNDS. 108 GAL. USABLE FUEL-. . NO WIND

ti~:i . . ADDO"E NZ~~I~ALMILEFOR :;::SUBTRACU%FROMTHER~NO'E', .I . EACH OEGREE CENTIGRADE ::: WITH THE 3 BLAOE PROP INSTAL."" ~""" ABOYE STANOARD AND SUB. LATION.

~, 000", ~H- , . 1 c~, TRACT1.1 NAUTICALMILES:)1RANGEWITH41 MIN. FOREACHDEGREECENTI.t:

1

RESERVE AT 15% POWER GRADE BELOW STANDARD.!:i.. BEST ECONOMY MIX. EXAMPLE:

" .. LU C TURE. . CRUIS~PR,E8S.,ALT.. 1100ft.~BOO5j~ ~(i~~R"~21~~8BELOW8TD.,

i ' RANGE W/RE8ERYE. 70211.1.81."

ffJ 75%, =::~~ :~:~S~;:.E:7~~~~5~il' ' "f .65%1 -i-:-'::i::.. RANGEWINO RES..778 N.M.

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, A,EeERYE

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65%II, ,

56% POWER56% POWER

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660 700 760 700 750RANGE. NAUTICAL MILES

(INCLUDES CLIMB AND DESCENT DISTANCE)

800 860600

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SECTION SPERFORMANCE


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STANDARD TEMPERATUREECONOMY CRUISE RANGE

Figure 5-35

REPORT: VB-8605-28

ISSUED: MARCH 23, 1978REVISED: MARCH 14,1983



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PERFORMANCE CRUISE ENDURANCEFigure 5-37

'.1:1 - 30n.1l1", 31!nSS311d

ISSUED: MARCH 13, 1978REVISED: MARCH 14, 1983

...

II>

...

0

REPORT: VB-8605-19

...

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PIPER AIRCRAFT CORPORATIONP A-44-180, SEMINOLE

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80

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00

51

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ECONOMY CRUISE ENDURANCEFigure 5-39

REPORT: VB-8605-30

iii~t=I-Z

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a::I-'U~

III

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ISSUED: MARCH 13, 1978REVISED: MARCH 14, 1983

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FUEL, TIME AND DISTANCE TO DESCENDFigure 5-41

ISSUED: MARCH 23, 1978REVISED: SEPTEMBER 14, 1979

REPORT: VB-8605-31

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0

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e.'Iample:

Airpon press. alt: 6S0 ft.

Outside lIir temp.: S"C

Wind component: 5 ktl.heldwindWeight: 3430 Ibs.Landing ground roll: 480 ft.

"NOTEREDUCE LANDINO GROUND ROLLIIY 311" IF OPTIONAL LANDINGGEAR HEAY'/' DUTY GROUP NO.1IS INIITALLED. (SIE EDUIPMENTUIITI

PA-44-180LAN~~G"G'~~~OLL3t*STANDARD BRAKES!:t': SHORT FIELDEFFORTm:t: WING FLAPS 40° - POWER OFF33IE COWL FLAPS OPEN

PAVED LEVEL DRY RUNWAYFULL STALL TOUCHDOWN-~..

.,. fi..t."'" Ii. @!.~' :s..< I-

.--40 -30 -20' .10 I) 10 20

OUTSIDE AIR TEMPERATURE - .C WEIGHT - POUNDS

wZ::::J

..:wII:

"'.iI.o.',A-

~

30 40 3IlOO 3000 2100 ci

i i-jj:j~4f"i'

tt.j:L:t

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-------------------------.....----

& 10 15400.J..L.U.J


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PA-44-180. ilillill-r-LANDING'DISTANCE OVEFfsoFT:BAR'RIERExample, T

~ .. *STANDA D .". "".Airportpreas.alt.:680 ft. . R BRAKESOutsideair temp.:a.c . - SHORT FIELD EFFORT :i 'Wind component: 6 kts. headwind, WING FLAPS40. - POWER OFF - COWLFLAPSOPENWeight: 3107 Ibs. PAVEDLEVELDRY RUNWAYApproach speed: 68 KIAS FULLSTALLTOUCHDOWNTotal landing distence: 1200 ft. APPROACHSPEED AS SCHEDULED"""",,

.:...-wT""r-W...

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16oo~i::;:to(

ID

°NOTEReduce totllilanding dlltance by1S%lfoptlonallandlngg88rhaavy .dutyGroupNo.1Iainltallad.(S.. p.\,.~'Equlpma~t.~I~I.. . . . . . . . ,~t,~'" .

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