Aérospatiale N 262

· Aérospatiale · 2 × Turbomeca Bastan

Airplanes

Length

19.28 m

Flat Wing Span

21.9 m

Height

6.21 m

Flat Wing Area

55 m²

Flat Wing Aspect Ratio

8.72

Max Seating

Cruise Speed

360 km/h

Max Speed

385 km/h

Max Ceiling

7300 m

Number of Engines

Aircraft Engine

First Flight

1962-12-24

Entry Into service

1964-01-01

Number Built

110

Maximum Take-Off Weight

10.3 t (paragliders: kg)

Total Fuel Capacity

2000

Maximum Range

1110 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Aérospatiale N 262	10.3	2000	1110

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All data (30 fields)

Name: Aérospatiale N 262
Manufacturer: Aérospatiale
Description: The Aérospatiale N 262 is a French twin-turboprop high-wing airliner built first by Nord Aviation (merged into Aérospatiale in 1970).
ICAO Code: N262
First Flight: 1962-12-24
Entry Into service: 1964-01-01
Production End: 1976-01-01
Designer: Aérospatiale
Type: Turboprop airliner
Length (m): 19.28
Height (m): 6.21
Cockpit Crew: 2
Max Seating: 29
Max Speed (km/h): 385
Cruise Speed (km/h): 360
Min Speed (km/h): 128
Max Ceiling (m): 7300
Rate of Climb (m/s): 6.35
Capacity Description: 29 passengers
National Origin: France
Number Built: 110
Powerplant Description: 2 × Turbomeca Bastan VIC turboprops, 794 kW (1065 hp) each
Primary Users: French Air Force, French Navy , Allegheny Airlines
Wikipedia Article (URL): en.wikipedia.org/wiki/A%C3%A9rospatiale_N_262
Flat Wing Span (m): 21.9
Flat Wing Area (m²): 55
Flat Wing Aspect Ratio: 8.72
Wake Category: M
Aircraft Engine: Turbomeca Bastan
Number of Engines: 2