Beechcraft Queen Air

· Beechcraft · 2 × Lycoming O-540

Airplanes

Length

10.668 m

Flat Wing Span

15.24 m

Height

4.2672 m

Flat Wing Area

27.3042 m²

Max Seating

Cruise Speed

294.4677 km/h

Max Speed

398.1797 km/h

Max Ceiling

8168.64 m

Number of Engines

Aircraft Engine

First Flight

1958-08-28

Entry Into service

1960-01-01

Number Built

1005

Maximum Take-Off Weight

3.9916 t (paragliders: kg)

Total Fuel Capacity

810.0781

Maximum Range

2439.084 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Beechcraft Queen Air	3.9916	810.0781	2439.084

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Lockheed Model 12 Electra Junior		10.9728	14.9352	6	Compare
Dornier Do 28	Lycoming O-540	11.41	15.55	12	Compare
Airspeed Consul		10.668	16.1544		Compare
Barkley-Grow T8P-1		10.668	15.24	6	Compare
Savoia-Marchetti SM.85		10.4	14		Compare
Hirtenberg HV.15	Siemens-Halske Sh 14	10.65	15	4	Compare

All data (26 fields)

Name: Beechcraft Queen Air
Manufacturer: Beechcraft
Description: The Beechcraft Queen Air is a twin-engined light aircraft produced by Beechcraft in numerous versions from 1960 to 1978.
First Flight: 1958-08-28
Entry Into service: 1960-01-01
Production End: 1978-01-01
Designer: Beech Aircraft Corporation
Type: Utility aircraft, Airliner
Length (m): 10.668
Height (m): 4.2672
Cockpit Crew: 1
Max Seating: 9
Max Speed (km/h): 398.1797
Cruise Speed (km/h): 294.4677
Min Speed (km/h): 131.4919
Max Ceiling (m): 8168.64
Rate of Climb (m/s): 6.477
Capacity Description: 4–9 passengers
Number Built: 1005
Powerplant Description: 2 × Lycoming IGSO-540 A1D supercharged, air-cooled flat-6 engines, 283 kW (380 hp) each
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Beechcraft_Queen_Air
Flat Wing Span (m): 15.24
Flat Wing Area (m²): 27.3042
Aircraft Engine: Lycoming O-540
Number of Engines: 2