BEECHCRAFT 65-A90-2
The Beechcraft 65-A90-2 is a variant of the King Air 90. Key specifications include a maximum takeoff weight of
9,3009 comma 300
9,300
lbs, a fuel capacity of
384384
384
US gallons, and a maximum payload of
2,9762 comma 976
2,976
lbs. It is powered by two
550550
550
shp Pratt & Whitney PT6A-6 turboprop engines. Its dimensions include a wingspan of
4545
45
ft
1111
11
in, a length of
3535
35
ft
66
6
in, and a height of
1414
14
ft
88
8
in.
General
- Crew: 1-2
- Passengers: Up to 7
- Dimensions:
- Length:
3535
35
ft
66
6
in (
10.810.8
10.8
m)
- Height:
1414
14
ft
88
8
in (
4.44.4
4.4
m)
- Wingspan:
4545
45
ft
1111
11
in (
13.913.9
13.9
m)
- Cabin Dimensions:
1212
12
ft
44
4
in (length) x
44
4
ft
66
6
in (width) x
44
4
ft
1010
10
in (height)
Performance
- 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)
- Maximum Payload:
2,9762 comma 976
2,976
lbs
- Max Speed:
223223
223
kts (normal cruise)
- Rate of Climb:
1,9001 comma 900
1,900
ft/min
- Service Ceiling:
30,20030 comma 200
30,200
ft
- Takeoff Distance:
1,7301 comma 730
1,730
ft
- Landing Distance:
1,2501 comma 250
1,250
ft
- 1966 - 1967 BEECHCRAFT A90 King Air - Plane PhD
Performance specifications. Horsepower: 2 x 550 HP. Best Cruise Speed: 216 KIAS. Best Range (i): 1,160 NM. Fuel Burn: 71.0 GPH. St...
Plane PhD
Powerplant
- Engines: 2 x Pratt & Whitney Canada PT6A-6 (or similar)
- Horsepower:
550550
550
shp each
- Fuel Capacity:
384384
384
US gallons