Britten-Norman Defender

· Britten-Norman

Airplanes

Length

12.2 m

Flat Wing Span

16.15 m

Height

4.4 m

Flat Wing Area

32.6 m²

Flat Wing Aspect Ratio

Max Seating

Cruise Speed

277.7998 km/h

Max Speed

325.9517 km/h

Max Ceiling

7620 m

Number of Engines

First Flight

1970-05-01

Maximum Take-Off Weight

3.8555 t (paragliders: kg)

Total Fuel Capacity

1131

Maximum Range

1863.112 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Britten-Norman Defender	3.8555	1131	1863.112

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
GAF Nomad		12.4968	16.4592	12	Compare
Dornier Do 28	Lycoming O-540	11.41	15.55	12	Compare
Messerschmitt Me 410 Hornisse		12.192	16.1544		Compare
De Havilland Dove		11.8872	17.3736	8	Compare
Airspeed Consul		10.668	16.1544		Compare
Avro Anson		12.8016	17.0688		Compare

All data (27 fields)

Name: Britten-Norman Defender
Manufacturer: Britten-Norman
Description: The Britten-Norman Defender is a multi-role utility transport aircraft, manufactured by Britten-Norman of the United Kingdom.
ICAO Code: BN2P
First Flight: 1970-05-01
Designer: Britten-Norman
Type: Transport, patrol, reconnaissance
Length (m): 12.2
Height (m): 4.4
Cockpit Crew: 2
Max Seating: 16
Max Speed (km/h): 325.9517
Cruise Speed (km/h): 277.7998
Min Speed (km/h): 87.0439
Max Ceiling (m): 7620
Rate of Climb (m/s): 6.35
Capacity Description: Up to 16 troops in transport role
Endurance (h): 8
National Origin: United Kingdom
Powerplant Description: 2 × Rolls-Royce 250 B17F turboprops, 298 kW (400 hp) each
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Britten-Norman_Defender
Flat Wing Span (m): 16.15
Flat Wing Area (m²): 32.6
Flat Wing Aspect Ratio: 8
Wake Category: L
Number of Engines: 2