|
Airframe / Zelle
|
|
Length
|
34' 8"
|
10.57 m
|
|
Height
|
12' 9"
|
3.89 m
|
|
Wing span
|
42' 8"
|
13.00 m
|
|
|
|
|
Gross weight
|
9,000 Lbs
|
4,086 Kg
|
|
Empty weight
|
5,018 Lbs
|
2,278 Kg
|
|
Gross weight
|
3,982 Lbs
|
1,807 Kg
|
|
|
|
|
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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|
