BEECHCRAFT 65-90
The Beechcraft 65-90 (also known as the King Air 90) is a twin-turboprop aircraft with a length of about
35.535.5
35.5
ft and a wingspan of
50.350.3
50.3
ft. It is powered by two Pratt & Whitney Canada PT6A-6 turboprop engines, each producing
550550
550
hp, and has a maximum takeoff weight of around
9,3009 comma 300
9,300
lbs. Key performance figures include a maximum speed of approximately
243243
243
knots, a service ceiling of about
27,000−27,40027 comma 000 minus 27 comma 400
27,000−27,400
ft, and a maximum range of around
1,3601 comma 360
1,360
nautical miles.
Key specifications
- Type: Twin-engine turboprop business aircraft
- Length:
35.535.5
35.5
ft (
10.810.8
10.8
m)
- Wingspan:
50.350.3
50.3
ft (
15.315.3
15.3
m)
- Height:
1414
14
ft
33
3
in (
4.44.4
4.4
m)
- Engines: 2 × Pratt & Whitney Canada PT6A-6 turboprops,
550550
550
hp each
- Maximum Takeoff Weight:
9,3009 comma 300
9,300
lbs (
4,2184 comma 218
4,218
kg)
- Empty Weight:
5,6805 comma 680
5,680
lbs (
2,5762 comma 576
2,576
kg)
- Crew: 1-2
- Passenger Capacity: 6-8
- Beechcraft Queen Air - Wikipedia
General characteristics. Crew: 1–2. Capacity: 4–9 passengers. Length: 35 ft 6 in (10.82 m) Wingspan: 50 ft 3 in (15.32 m) Height:
Wikipedia
Performance
- Maximum Speed:
243243
243
knots
- Normal Cruise Speed:
235235
235
knots at
10,00010 comma 000
10,000
ft
- Service Ceiling:
27,40027 comma 400
27,400
ft
- Rate of Climb:
1,9001 comma 900
1,900
fpm
- Maximum Range:
1,3601 comma 360
1,360
nmi
Dimensions and cabin
- Cabin Height:
44
4
ft
1010
10
in
- Cabin Width:
44
4
ft
66
6
in
- Cabin Length:
1212
12
ft
44
4
in
- Cabin Volume:
227227
227
cu ft
- Internal Baggage:
5454
54
cu ft
Other details
- Construction: Aluminum alloy semi-monocoque fuselage, aluminum alloy wings with magnesium ailerons, and all-metal cantilever tail
- Landing Gear: Retractable tricycle gear
- Electrical System:
2828
28
VDC system