axenty.com pa24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1...

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24008 20000 t: ..:.. 15000 Q ~ ~ c ~ 12000 us :8 w.I Q IOU 4000 Sl -48 -28 1 21 II 101 41 I" TEMPERATURE. of FIGURE 5-01 P-3 I I I I I I I I I I I ALTITUDECONVERSIONCHART THISCHARTSHOULDBE USEDTO DETERMINE DENSITYALTITUDE FROMEXISTINGTEMPERATURE ANDPRESSURE ALTITUDE co.mONS FORUSEWITHPERFORMANCE CHARTS. V ----- STD. i .. -- V TEMP. '\. "t' .- \ ,\, ...-- "'-- ..;.;- ..-- -- --- '\ V "'-- ...-- ..--- ...-- --- \ ".-- -- ----- """ --- ...-- ..--- .- ...-- --- ........, V V'" - V , 1 --- .-'t ..,..-- ,......... ..,..-- \ ........- v --- ..- --- ............. - .7' -- ,.::0'1- \I ...-- """"'" v ..,..-- ........ ""'-- ..- v ...... --- - """"'" I\." ""'-- ---- - -- .- v """" --- I ---- -\ ----- .......... --- X ,1! V ...-- ..,..-- --- -- L ...-- \ V --- ".-- -----

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Page 1: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

24008

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4000

Sl

-48 -28 1 21 II 10141 I"

TEMPERATURE.of

FIGURE 5-01

P-3

I I I I I I I I I I I

ALTITUDE CONVERSIONCHARTTHISCHARTSHOULDBE USEDTODETERMINEDENSITYALTITUDE

FROMEXISTINGTEMPERATURE

ANDPRESSUREALTITUDEco.mONS

FORUSEWITHPERFORMANCECHARTS.

V-----STD.

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VTEMP.'\. "t' .-\ ,\, ...-- "'--

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..........--- X ,1! V ...--

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Page 2: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

Q)RVE NO. 11800

'f"X1';;'

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~';;"Kr"'TO OBTAIN .FUEL CONSUMPTJQN'AT>

, AIJ1n.oE, ENTEJIt, TrlSCURIJE WlTtI.~,SEA'l:EVEL' MAN., PRES$; ','"

FOR ~ ALT1iU>EPOWER.SEE'.,. "', PONT G OF EXAhIPLE, ON,AIJlTL1CE""";;, d';" .",;!,/, ,;",.: PERFORMAHCECURVEs;ltt;!:;,;1;,;t;;,;;,:\'1

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FIGURE 5-02

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Page 3: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

I-WWLL

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PIPER COMANCHE

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600 800 1000 1200 1400 1600 1800

TAKE- OFF DISTANCE, FEET

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FIGURE 5-03

P-5

Page 4: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

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RATE OF CLIMB, FEET PER. MINUTE

FIGURE 5-04

P-6

Page 5: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

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FIGURE 5-05

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Page 6: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

NOTE: FIGURES SHOWN IN THIS CHART GIVE NO CONSIDERATION TOWIND OR NAVIGATIONAL ERRORS. ALSO, NO ALLOWANCE IS ~ffiDEFORFUEL USED IN WARM-UP, TAXI, TAKEOFF OR CLIMB, AND NO RESERVEFUEL CAPACITY, AS REQUIRED BY FAA REGULATIONS, IS ALLOTTED.

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FIGURE 5-06

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Page 7: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

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FIGURE 5-07

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Page 8: axenty.com PA24-250.pdf · 24008 20000 t:..:..15000 q~ ~ c ~ 12000 us:8 w.i q iou 4000 sl-48-28 1 21 41 i" ii 101 temperature. of figure 5-01 p-3 i i i i i i i i i i i al titude conversion

LIMITATIONS

PA-24-250 * 2800 LBS. GROSS WT.

AIRSPEED LIMITATIONS - IAS

Va - DESIGN MANEUVERING SPEED/TURBULENT AIR PENETRATION SPEED

AT 2,800 LBS. GROSS WEIGHT .. 144 MPH. 125 KT.AT 1,900 LBS. GROSS WEIGHT .'..... 120 MPH. 104 KT.

** CAUTION **

MANEUVERING SPEED DECREASES AT LIGHTER WEIGHT AS THE EFFECTS OFAERODYNAMIC FORCES BECOME MORE PRONOUNCED. LINEAR INTERPOLATION MAYBE USED FOR INTERMEDIATE GROSS WEIGHTS. MANEUVERING SPEED SHOULDNOT Bi EXCEEDED WHILE OPERATING .IN ROUGH AIR.

Vc - DESIGN CRUISING SPEED ..........Vd - DEMONSTRATED DIVING SPEED....................Vfe - FLAP EXTENSION SPEED ..........Vie - RECOMMENDED..................................VIe - LANDING GEAR EXTENDED SPEED..................Vlo - LANDING GEAR OPERATION SPEED.................V10 - RECOMMENDED..................................Vne - NEVER EXCEED SPEED...........................Vne - AD 72-22-05 ..................................Vno - NORMAL OPERATING SPEED.......................

180 MPH.252 MPH.125 MPH.100 MPH.150 MPH.150 MPH.125 MPH.227 MPH.203 MPH.180 MPH.

OPERATIONAL AIRSPEEDS

Vapp- FINAL APPROACH TO LANDING SPEED ... .., 83 MPH.Vapp- FINAL APPROACH (W/ZERO DEGREES OF FLAP) ... 95 MPH.Vapp- FINAL APPROACH (IFR APPROACH/CLEAN) 120 MPH.Vh - MAXIMUM OPERATING SPEED ... 190 MPH.Vr - ROTATION SPEED (W/ZERODEGREES OF FLAP) 85 MPH.VsO - STALL SPEED (FULL FLAPS AND GEAR EXTENDED) 64 MPH.Vs1 - STALL SPEED (CLEAN) 71 MPH.Vx - BEST ANGLE OF CLIMB SPEED (AT SEA LEVEL) . 84 MPH.Vy - BEST RATE OF CLIMB SPEED (AT SEA LEVEL) ... 95/105 MPH.

** NOTE **

156 KT.219 KT.108 KT.87 KT.

130 KT.130 KT.108 KT.197 KT.176 KT.156 KT.

72 KT.83 KT.

104 KT.165 KT.74 KT.56 KT.62 KT.73 KT.91 KT.

WHILE 95 MPH WAS THE PUBLISHED FIGURE FOR Vy FOR THE EARLY MODEL250, THE OWNER'S HANDBOOK ALSO RECOMMENDS AN AIRSPEED OF BETWEEN 100TO 110 MPH. HANDBOOKS FOR LATER MODELS OF THE 250 SUBSEQUENTLYPUBLISHED A FIGURE OF 105 MPH FOR Vy. Vy OF 105 MPH IS THEREFORESUGGESTED FOR CONSIDERATION. BOTH S~EEDS ARE PRESENTED HEREIN.

EMERGENCY AIRSPEEDS

BEST ENGINE OUT GLIDE SPEED (OPTIMUM) ..., 100 MPH.BEST ENGINE OUT GLIDE SPEED (ENDURANCE) 85 MPH.

OTHER SPEEDS

87 KT.74 KT.

BEST ENROUTE RATE OF CLIMB SPEED... ... 120 MPH. 104 KT.DEMONSTRATED CROSSWIND COMPONENT 20 MPH. 17 KT.

L-1