PIPER, Cheyenne II, PA31-T
General Information

Airframe / Zelle

Length

34' 8"

10.57 m

Height

12' 9"

3.89 m

Wing span

42' 8"

13.00 m

Fuel  

382 Gal

1,445 l

Gross weight

9,000 Lbs

4,086 Kg

Empty weight

5,018 Lbs

2,278 Kg

Gross weight

3,982 Lbs

1,807 Kg

First certified

05/03/72

Pressurized Cabin / Druckkabine

Height

4' 3"

1.30 m

Width

4' 2"

1.27 m

Passengers (maxi, including crew)

8

Propulsion / Triebwerke

Number of engines

2

Type of engines

Turbine

Make & Model

Pratt & Whitney PT6A-28

Power

620 Hp

Total fuel for both engines

63 Gal/h

238 l/h

Performances / Leistung

Maximum speed

283 Kts

325 Mph

524 Km/h

Cruise speed

269 Kts

309 Mph

498 Km/h

Stall speed

75 Kts

86 Mph

138 Km/h

Service ceiling

31,600 Ft

9,631 m

Engine out service ceiling

14,600 Ft

4,450 m

Rate of climb

2,710 Ft/mn

13.7 m/s

Engine out rate of climb

660 Ft/mn

3.3 m/s

Takeoff over 50 Ft (15m)

1,980 Ft

603 m

Takeoff ground run

1,410 Ft

429 m

Landing over 50 Ft (15m)

2,480 Ft

755 m

Landing ground roll

1,430 Ft

435 m

Range

1,444 Nm

1,662 Sm

2,674 Km

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