Piper CHEROKEE ARROW 200 Guide de l'utilisateur

CHEROKEE

ARROW

.__

PA-28R-200

., .

This

handbook

for

airp

anes

with

serial

nos

28R-35001

through

28R

35392

Owner's

Handbook

Piper

Aircraft

Corporation,

Vero

Beach,

Florida

U.S.

NOTICE

THIS HANDBOOK

NOT DESIGNED,

NOR

CAN ANY

HANDBOOK SERVE,

A SUBSTITUTE

FOR

ADEQUATE AND

COMPETENT FLIGHT INSTRUCTION,

KNOWLEDGE

THE

CURRENT AIRWORTHINESS DIRECTIVES,

THE

APPLICABLE

FEDERAL AIR REGULATIONS, AND ADVISORY CIRCULARS. IT

NOT INTENDED TO

A GUIDE

BASIC FLIGHT

INSTRUCTION, NOR A TRAINING MANUAL.

THE HANDBOOK

DESIGNED:

1. TO HELP YOU OPERATE YOUR CHEROKEE WITH

SAFETY AND CONFIDENCE.

2. TO MORE FULLY ACQUAINT YOU WITH

THE

BASIC

PERFORMANCE AND HANDLING CHARACTERISTICS

THE

AIRP~ANE.

MORE FULLY EXPLAIN YOUR CHEROKEE'S

OPERATION THAN

PERMISSIBLE

SET

FORTH

THE AIRPLANE FLIGHT MANUAL.

IF THERE

ANY INCONSISTENCY BETWEEN THIS

HANDBOOK AND THE AIRPLANE FLIGHT MANUAL APPROVED

THE F.A.A., THE FLIGHT MANUAL SHALL GOVERN.

Revised

text

and illustrations shall

indicated

black venical line in the margin opposite

the

change.

Additional copies

this manual, Pan No. 753

795,

may

obtained from

YO':'.!'

Piper Dealer.

Published

·PUBLICATIONS DEPARTMENT

Piper Aircraft Corporation

753

795

Issued: February 1969

Revised: January

1987

Performance

Weights.

Power

Plant

Fuel

and

Oil

Baggage

Dimensions

Landing

Gear

SECTION

SPECIFICATIONS

CHEROKEE

"ARROW"

SECTION

SPECIFICATIONS

PERFORMANCE

Performance figures are for

airplanes

equipped for

cross-

country transportation and flown

gross

weight under standard

conditions

sea

level

stated

altitude.

Any changes in equip-

ment

may

result

changes

in performance.

Take-off Run (maximum effort,

25°

flap) (ft)

Take-off over 50-ft barrier (maximum effort,

25°

flap)

(ft)

Best

Rate

of Climb Speed (mph)

Rate

of Climb (ft per min)

Service

Ceiling

(ft)

Absolute

Ceiling

(ft)

Top Speed {mph)

Optimum Cruising Speed

(75%

power, optimum

altitude)

(mph)

Cruising Range

(75%

power, optimum altitude)(mi)

Optimum Cruising Range

(55%

power, optimum

altitude)

(mi)

Stalling Speed (flaps down, gear down) (mph)

Stalling Speed (flaps and gear up) (mph)

Landing

Roll

(flaps down) (ft)

Landing

Roll

aver 50-ft barrier (ft)

i690203

770

1600

910

16,000

18,000

176

166

810

950

780

1380

SECTION

SPECIFICATIONS

(cont):

WEIGHTS

Gross Weight

(lbs)

Empty Weight (Standard)

(lbs)

USEFUL

LOAD

(Standard) {lbs)

POWER

PLANT

Engine {Lycoming)

Rated

Horsepower

Rated Speed (rpm)

Bore

(in.)

Stroke

(in.)

Displacement (cu

in.)

Compression

Ratio

Dry Weight

(lbs)

Propeller

FUEL

AND

OIL

Fuel

Capacity

(U.S.

gal)

Oil Capacity

(qts)

Fuel,

Aviation Grade (min

octane)

BAGGAGE

Maximum

Baggage

(lbs)

Baggage Space (cu

ft)

Baggage Door Size

(in.)

CHEROKEE

"ARROW"

2600

1450

1150

10-360-ClC

200

2700

5.125

4.375

361.0

8.7:1

326

HC-C2YK-1/7666A-2

100/130

200

. 690203

CHEROKEE

"ARROW"

SPECIFICATIONS

(cont):

DIMENSIONS

Wing

Span (ft)

Wing

Area

(sq

ft)

Wing

Loading (lbs per

ft)

Length

(ft)

Height (ft)

Power Loading (lbs per

hp)

LANDING

GEAR

Wheel

Base

(ft)

Whee

Tread

(ft)

Tire

Pressure

(psi)

Nose

Tire

Size

690203

Main

Nose (4 ply

rating)

Main (4 ply

rating)

SECTION

160

16.3

24.2

8.0

13.0

7.4

10.5

5.00 X 5

6.00

X 6

SECTION

CHEROKEE

''ARROW''

.___10'10.0"-____.

...,.._--------30'-------___.

690203

SECTION

DESIGN

INFORMATION

Engine

and

Propeller

Induction

System.

Structures . .

Landing

Gear .

Control Systems .

Fue

1 System .

Electrical

System

Heating

and

Ventilating

System .

Cabin

Features

. 16

Ce manuel convient aux modèles suivants

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