Beech F90 King Air
Turboprop • twin engine • Low Wing • Retractable gear
Range Visualization
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Payload vs. Range
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Default: 190 lbs (FAA standard)
Default: 30 lbs
Passengers
lbs
@ lbs / pax
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Fuel on board
gal
+ Weight
Range
Available Range
/ nm
Mission capable —
Aircraft can handle the current load with full fuel tanks.
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( gal usable for nm range).
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Mission Profile
261
KTAS
Cruise Speed
10
Occupants
1235
nm
Max Range
601
lbs
Wet Payload
About the Beech F90 King Air
Twin-engine turboprop low-wing monoplane with retractable tricycle landing gear, powered by two Pratt & Whitney PT6A-135A turboprops flat-rated at 750 shp each; produced 1979–1983; seats up to 10 (including pilot); cruise 261 ktas; range 1 235 nm; service ceiling 29 802 ft; climb rate 2 380 fpm; stall speed (dirty) 77 KIAS; Vref ~100 KIAS; fuel 470 US gal; MTOW/MLW 10 950 lb.
Technical Specifications
Dimensions
- Wingspan
- 45.9 ft
- Length
- 39.8 ft
- Height
- 15.1 ft
Weights
- Max Takeoff Weight
- 10,950 lbs
- Max Landing Weight
- 10,950 lbs
- Useful Load
- 3,750 lbs
- Fuel Capacity
- 470 gal
Performance
- Cruise Speed
- 261 KTAS
- Range
- 1235 NM
- Service Ceiling
- 29,802 ft
- Rate of Climb
- 2380 fpm
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