Piper CHEROKEE D Benutzerhandbuch

CHEROKEE

PA-28-180

Owner's

Handbook

Piper

Aircraft

Corporation,

Vero

Beach,

Florida

U.S. A.

NOTICE

THIS HANDBOOK

NOT DESIGNED,

NOR

CAN ANY

HANDBOOK SERVE, AS A SUBSTITUTE

FOR

ADEQUATE AND

COMPETENT FLIGHT

INSTRUCfiON,

KNOWLEDGE

THE

CURRENT AIRWORTHINESS

DIRECfiVES,

THE

APPLICABLE

FEDERAL

AIR

REGULATIONS, AND ADVISORY CIRCULARS. IT

IS NOT INTENDED TO

A GUIDE

BASIC FLIGHT

INSTRUCTION, NOR A TRAINING MANUAL.

THE HANDBOOK

DESIGNED:

HELP YOU OPERATE YOUR CHEROKEE WITH

SAFETY AND CONFIDENCE.

MORE FULLY ACQUAINT YOU WITH THE BASIC

PERFORMANCE AND HANDLING CHARACfERISTICS

THE

AIRPLANE.

MORE FULLY EXPLAIN YOUR CHEROKEE'S

OPERATION THAN

PERMISSIBLE

SET FORTH

THE AIRPLANE FLIGHT MANUAL.

THERE

ANY INCONSISTENCY BETWEEN THIS

HANDBOOK AND

THE

AIRPLANE FLIGHT MANUAL APPROVED

BY THE F.A.A., THE FLIGHT MANUAL SHAI.L GOVERN.

Revised

text

and illustra;tions shall

indicated

black vertical line in

the

margin opposite the change.

Additional copies

this manual, Part No. 753 765

may be obtained from

your

Piper Pealer.

Published

PUBLICATIONS DEPARTMENT

Piper

Aircraft Corporation

753 765

Issued:

November 1967

Revised: January 1973 ·

Performance

Weights.

Power

Plant

Fuel

and Oil

Baggage

Dimensions

Landing

Gear .

671101

SECTION

SPECIFICATIONS

CHEROKEE

"D"

SECTION

SPECIFICATIONS

PERFORMANCE

Performance

figures

are

fcir

airplanes

equipped

for

cross-

country

transportation

and flown

gross

weight

under

standard

conditions

sea

level

stated

altitude.

Any

changes

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) (mph)

Stalling

Speed

(flaps

up)

(mph)

Landing

Roll

(flaps

down)

(ft)

Landing

Roll

over 50-ft

barrier

(ft)

681115

720

1625

750

13,000

15,000

152

143

725

845

600

1150

SECTION

SPECIFICATIONS

(c:ont}:

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)

Pro

"Peller

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

"D"

2400

1294

1106

0-360-MA

180

2700

5.125

4.375

361.0

8.5:1

285

M76EMMS60

91/96

200

X 22

671101

CHEROKEE

~·o"

SPECIFICATIONS

(cont):

DIMENSIONS

Wing

Span

(ft)

Wing

Area

(sq

ft)

Wing

(lbs

per

ft)

Length

(ft)

Height

(ft)

Power

(lbs

per

hp)

LANDING

GEAR

Wheel

Base

(ft)

Wheel

Tread

(ft)

Tire

Pressure

(psi)

Nose

Main

Tire

Size

671101

Nose

ply

rating)

Main (4 ply

rating)

SECTION

160

15.0

23.5

7.3

13.3

6.2

6.00

SECTION

CHEROKEE

"D"

1+------------30'--------_,

671101

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