Beechcraft King Air C90A

Beechcraft

ICAOBE9L
Beechcraft King Air C90A aircraft
BeechcraftBeechcraft King Air C90A
Photo: James from Cheltenham, Gloucestershire · CC BY-SA 2.0 · Modified

About

The C90A is the smallest King Air EASA still certifies: 4,581 kg on a pair of PT6A-21s, a 15.32 m wing and the conventional tail the 90 series kept while every larger King Air went to a T-tail. IM.A.503 tabulates it by serial number and the later block is the one stored here — the earliest C90As stopped at 4,377 kg. Thirteen seats including both pilots, 1,454 litres of usable fuel, and a 30,000 ft ceiling where the 200 and 300 series are cleared to 35,000.

Weightscompared to Airbus A318

MRW (Maximum Ramp Weight)

4,609kg
0
25k
50k
68k

MTOW (Maximum Takeoff Weight)

4,581kg
0
25k
50k
68k

MLW (Maximum Landing Weight)

4,355kg
0
25k
50k
56k

Capacitycompared to Airbus A318

Passenger Capacity

11passengers
0
100
132

8% of A318 maximum capacity

Crew

Total
1
Cockpit
1

Dimensions

Length

10.8m

Wingspan

15.3m

Height

4.3m

Wing Area

27.3m²

Engine Specifications

Engine Count

2×

Engine Model

Pratt & Whitney Canada PT6A-21 turboprop

Fuel & Cargo

Fuel Capacity

1,454 L

Production & History

Production Status

Out of production

Business jets and the API are coming

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