Nord N 262 Civil Aircraft Model Details

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General Information of Nord N 262

First Flight : MH.250: 20 May 1959 ; N 262: 24 December 1962

Introduction : 1964

Manufacturer : AErospatiale

National Origin : France

Number Built : 110

Primary Users : French Air Force; French Navy; Allegheny Airlines

Produced : 1962-1976

Role : Turboprop airliner

General characteristics of Nord N 262

Airfoil : NACA 23016 at root, NACA 23012 at tip

Capacity : 29 passengers

Crew : 2

Empty Weight : 6,654 kg (14,669 lb)

Height : 6.21 m (20 ft 4 in)

Length : 19.28 m (63 ft 3 in)

Max Takeoff Weight : 10,300 kg (22,710 lb)

Powerplant : 2 × Turbomeca Bastan VI C turboprops, 794 kW (1,065 ehp) each

Wing Area : 55.0 m² (592 sq ft)

Wingspan : 21.90 m (71 ft 10 in)

Performance of Nord N 262

Cruise Speed : 360 km/h (194 knots, 223 mph)

Maximum Speed : 385 km/h (208 knots, 239 mph)

Never Exceed Speed : 498 km/h (269 knots, 309 mph)

Range : 1,110 km (600 nmi, 690 mi)

Rate Of Climb : 6.3 m/s (1,250 ft/min)

Service Ceiling : 7,300 m (24,000 ft)

Stall Speed : 128 km/h (69 knots, 79 mph)

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