Piper Cherokee 140 Guida utente

O!av Kieserud

CHEROKEE I 40

OWNER'S HANDBOOK

753-584

Olav K jesecud

CHEROKEE 140

PA.28.l 40

Owner's Hondbook

Piper Aircraft Cotporotion, Vero Beoch, FlorUo

u.5. A.

NOTICI]

TIIIS IIANDI}OOK IS NO't DESIGNIiD, NOR CAN ANY

H^NDDOOK SERVE, ^S A SUBSTTTUTE FOR ADEQU^TE ^ND

coMpETENT FLIGHT INSTRUCTION, OR KNOWLEDGE OF THE

CURRENT AIRWORTHINES§ DIRECTIVES, THE APPLICABLE

FEDERAL AIR REGULATIONS, AND ADVISORY CTRCULARS. IT

IS NOT INTENDED TO IIE A GUIDI' OF ITASIC }'LIGHT

INSTRUCTION, NOR A TRAINING MANUAI,.

'l'ilrt il^NDD(x)K ls Drist(.;Ntil):

I. TO IIELID YOU OI'IiRA'I'E YOUR CHIIROKIiI' WITII

SA I.'ETY AND CONIIIDENCE.

2, TO MORE FULLY ^CQU^rNT yOU WITH THE BASIC

PERFORMANCE AND HANDLING CHARACTERISTICS

OFTHE AIRPLANE.

3. TO MORE FULLY EXPLAIN YOUR CHEROKEE'S

OPERÅTION THAN IS PERMISSIBLE TO SET FORTH IN

THE AIRPLANE FLIGHT MANUAL.

IF THERE IS ANY INCONSISTENCY BETIVEEN THIS

HANDBOOK AND THE AIRPLANE FLIGHT MANUAL APPROVED

BY THE F.A,A., THE AIRPLANE FLIGHT MANUAL SHALL

GOVERN.

Revised text and illustrations shall be indicated by a

black vertical line in the margin opposite the change,

A line opposite the page number will indicate that

materi al was relocated.

Additional copies of this manual, Part No. 753 584,

may be obtained from your Piper Dealcr.

Published by

PUB UCATIONS DEPARTMENT

Piper Aircraft Corporation

753 5U

Issu«l: Febnrary 1964

Revised: March l. l99l

SECT|ON I

SPECIFICATION FEATURES

Performance .

Weights

Power Planc.

FueI and Oil

Baggage

Dimens ions.

Landing Gear .

THE PIPER CHEROKEE SECTION

sEcfloN I

SPECIFICATION FEATURES

PERFORMANCE

Tetc-off Di.Btaræ Over 50 ft. Obsracle (fr.) (fl8ps up) lsm I r?00

Best Rate of CUmb Spæd (hph) 85 I Ss

Rrte of CUmD (ft. per mln.) I 820 i 660

Scrvtce Cetllug (ft.) 15, O0O r4,3OO

Absolute Ceiltng f7, OOO ,U. U*

Top $ced (mph) r r4t (r44.) i t39 (r42.)

ClutslnB Sp€ed (75% power, sea level) (mph) 'l r20 (f23.) ' tZt 1tU.1

Optlmum Crulstng Speed pSS potuer, 7000 It., mph) f30 (f33.) I f30 (f33.)

The gross $reighr o, l95O Pq.rnds ln the following perlårmance chÅrts appll,es ,o S{rUf Nos, 28-2OOOO

to 28-20939, uleas the airpleqe has been modilled t

Nos, 28-20940 snd llp hsvc bcen llcenircd from the fa

Perforrutrcq flgues ere for strnderd alrplanes

Ievel or ståld flhltudc. Any dcvistldl from Sta

GRO§S WEIGHTS

Telc-off Ru (It,) (flaps 14)

wer, sea level) 100 (102+) .l r00 (r02r)

. 7.e i 8.4

s.3 I s.o

) 5r5, { hEs. (r20, 6 hr8...) +fO, n frru[ (680, 6 hrs.rr)

) 560 (780..) i 535 (725.+)

Opttmu$ Grulslng Renge (55$ powrr, 10, 0m ft, ) 600 (840..) I 570 (790.r)

'\iltren Fenders Instålled

"With 50 gal. Resene Fæl

730I I 5

SECTION ITHE PIPER CHEROKEE

SPECIFICATION FEATURES: (cont)

PERFORMANCE

: lnetruciloul Pover Crutsltrg Range

(50%,pqwer, sea level)

Sta[ln-gSpeed (flaps doyn, mFh)

Landlng Roll (flaps down, fr.)

WEIGHTS

Gross U,eight (lbq. )

Empcy Wetght (Standard) (Ibs.)

USEFUL LOAD (Standard) (lbs.)

Empcy \Yeighr (AutoFlight) (lbs.)

UsEFUl, LOAD (Åu.oFligtrr) (lbs.)

POWER PI.ANT

EEgtne - L}æomlng

Rated Horsepryer md Speed (rpm)

Bore (lo:hes)

Stroke (inches)

. Displaæmetrt (cubic incheE)

CompEesslotr Ratib

Dry Weighr (poutrds)

Oit Sump Capaqity (qts. )

Propeller (Sensentch)

"Wirh 50 gal, Resefle Fuel

aRosri TErGr{Ts

640,1 6.s hrs. (89s,

t hrs. ti) d50, 6.5 hrs, (910, t hrs. r.)

52 54

48s 53s

r9 50 2r50

650630

o-320-E2A

140 ei 2450

5. r25

3.875

319.8

7:\

272

M74DM

2150

l20l

949

t24l

909

o-x20-E2A

150 at 2700

5, t25

3.875

319.8

7i7

M74DM

1950

,.180

770

1220

730

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