Piper AZTEC D PA-23-250 Benutzerhandbuch

ZTEC

OWNER'S

HANDBOOK

AZTEC

'D'

PA-23-250

{Six

Place)

Owner's

Handboo"'

;

Piper

Aircraft

Corporation,

Lock

Haven,

Pa.

5. A.

Assurance

that

the

airplane

airworthy

condition

the

responsibility

the owner.

The

pilot

command

responsible

for determining

that

the

airplane

safe

for flight.

The

pilot

also

responsible

for remaining

within

the

operating

limita-

tions

outlined

the

Flight

Manual, instrument

markings and

placards.

inconsistency

information

exists

be-

tween

this

handbook and the

Flight

Manual approved

the

FAA,

the

Flight

Manual

shall

be the

authority.

Additional

copies

this

manual,

Part

No. 753

772

may

obtained

from your

Piper

Dealer.

Published by

PUB

TIO

DEPARTMENT

Piper Aircraft Corporation

753

772

Issued: May 1968

Revised: May 1972

Perfonnance

Weights . •

Power

Plant

Fuel

and

Oil

Baggage

Dimensions

Landing

Gear

680501

SECTION

SPECIFICATIONS

THE

PIPER

AZTEC

"D"

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

equip-

ment may

result

changes

performance.

Take-off Run (max

effort,

ft)

Take-off

Distance

Over 50-ft

Barrier

(max

effcrt,

ft)

Accelerate-Stop

Distance

(ft)

Minimum

Controllable

Single Engine Speed (mph)

Stalling

Speed (gear down,

flaps

down

50°,

power

off, mph)

Stalling

Speed

(gear

and

flaps

up, power off, mph)

Best

Rate

of Climb (ft per min)

Best

Rate

of Climb Speed (mph)

Best

Angle of Climb Speed (mph)

Single

Engine

Rate

of Climb (ft per min)

Best

Single

Engine

Rate

of Climb Speed (mph)

Best

Single Engine Angle of Climb Speed (mph)

Absolute

Ceiling

(ft)

Service

Ceiling

(ft)

Single

Engine

Absolute

Ceiling

(ft)

Single

Engine

Service

Ceiling

(ft)

Altitude

Cruising

Speeds

(mph)

RPM

26.0" 2400

24.0" 2400

24.0" 2200

20.0" 2200

680501

Normal

Intermediate

Economy

Long

Range

Altitude

4000

6000

6400

10,200

820

1250

2220

1490

120

107

240

102

21;100

19,800

6,400

5,000

Speed

210

208

204

195

SECTIONJ

THE

PIPER AZTEC

"D"

SPECIFICA!IONS (cont):

PERFORMANCE

Altitude

Cruising

Range (No

Reserve)

:·

RPM Altitude

26.0"

2400 4000

24.0"

2400 6000

24.0

2200 6400

20.0"

2200 10,200

Fuel

Consumption (both

engines,

gph)

RPM GPH

26.0"

24.0"

2400

34.0

27.0

24.0

. 2200

25.0

20.0"

. 2200 21.0

Range

830

1080

1110

1210

Top

Speed (mph) 216

Landing

Roll

(flaps down,

max

effort, ft) 850

Landing

Distance

Over 50-ft Barrier (flaps down,

ft)

1620

WEIGHTS

Gross Weight

(lbs)

Maximum

Landing Weight (lbs)

Zero

Fuel

Gross

Weight

(ll~s)

Empty Weight (Standard,

lbs)

USEFUL LOAD (Standard,

lbs)

POWER

PLANT

.Engine (Lycoming)

Rated

Horsepower

Rated

Speed (rpm)

Bore

(inches)

5200

4940

4400

3006'

2194

I0-540-C4B5

250

2575

5-1/8

690505

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