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Aérospatiale N 262

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Top speed
  
385 km/h

Length
  
19 m

Manufacturer
  
Wingspan
  
22 m

First flight
  
December 24, 1962

Aérospatiale N 262 Nord 262 Wikipedia

The Aérospatiale N 262 is a French twin-turboprop high-wing airliner built first by Nord Aviation (merged into Aérospatiale in 1970). The aircraft was also known as the Nord 262.

Contents

Aérospatiale N 262 Aerospatiale N 262 Fregate Flight Simulator Aircraft Catalog

Design and development

Aérospatiale N 262 Aerospatiale N262 Mohawk 298 Lloyd Aviation Aviation Photo

Originally designed to replace the Douglas DC-3/C-47 Skytrain, the prototype utility transport aircraft was designed by Max Holste and designated the Max Holste MH.250 Super Broussard it first flew on 20 May 1959. The initial design had the aircraft rather square in shape, and fitted Pratt & Whitney Wasp radial engines to the aircraft. The second prototype, known as the MH.260, was equipped with 980 hp Turbomeca Bastan turboprop engines and eventually took its flight just over a year later on 29 July 1960.

Aérospatiale N 262 Aerospatiale N262 Fregate amp Mohawk 298 picture 03 Barrie

Eventually, wholly state-owned Nord Aviation (later renamed Aérospatiale) took over the further development of the aircraft. The new changes that Nord brought to the aircraft were a rounded, pressurized cabin and the new name Nord 262. The new cabin design enabled the aircraft to carry between 24-26 passengers.

Aérospatiale N 262 Nord Aviation SNCAN Aerospatiale N 262 Frgate Specifications

The first prototype since the changes by Nord took to the skies for the first time on 24 December 1962 and the aircraft was exhibited at the June 1963 Paris Air Show. The aircraft received its certificate on 16 July 1964 and entered its initial commercial service with Air Inter of France.

Aérospatiale N 262 Aerospatiale N262 Specifications Photo

Four of the first aircraft 262A, 262B, 262C, and 262D were built, the first two fitted with Bastan IVC engines, while the C and D models were fitted with the higher-powered Bastan VIIC. Of these four aircraft, the latter two saw their first air time in July 1968. Most sales of the initial aircraft were not in the passenger field, but rather the military field. The 262D was the most popular and marketed as Frégate.

Aérospatiale N 262 httpsuploadwikimediaorgwikipediacommonsthu

As for the American designation, the "Mohawk 298" airplanes were modified Nord 262s and first flew on 7 January 1975, equipped with Pratt & Whitney Canada PT6A-45 turboprops. Built in order to meet United States FAR 298 regulation, the modification of the aircraft was overseen by Mohawk Air Services and outsourced to Frakes Aviation. Allegheny Airlines was the initial operator of the aircraft.

Joel Krane, the chairman of the FOEB (Flight Operations Evaluation Board) determined that a common type rating could be issued for the Nord 262 and Mohawk 298. Appropriate differences training would be required for transitioning pilots.

Variants

Max Holste MH.250 Super Broussard
Prototype 17-seat transport first flown in 1959.
Max Holste MH.260 Super Broussard
23 passenger production variant of the MH.250, ten ordered but not completed before development handed over to Nord Aviation.
N 262
Prototypes and initial production version
N 262A
Early standard production version (preceded by N 262B). Powered by Turbomeca Bastan VIC engines. Certified 15 March 1965 with first delivery to Lake Central Airlines on 17 August 1965.
N 262B
Initial production version for Air Inter, powered by two Bastan VIC turboprops. Four built, with first example flown 8 June 1964, certification 16 July 1964 and delivery 24 July 1964.
N 262C Frégate
Bastan VIIC engines and greater wingspan
N 262D Frégate
French Air Force version of N-262C
N 262E
A maritime patrol and training version used by the Aviation navale (French Navy).
Mohawk 298
Nine aircraft updated by Frakes Aviation for Allegheny Airlines between 1975 and 1978. Powered by Pratt & Whitney Canada PT6A-45 engines driving five-bladed propellers.

Operators

As of July 2011 a total of three Nord 262 aircraft remain in airline service with the following airlines:

  • Equatorial International Airlines (1),
  • International Trans Air Business (1)
  • RACSA (1).
  • Former Operators

  • Aerovias
  • Air Ceylon
  • Air Florida Commuter (operated by National Commuter Airlines)
  • Air Inter
  • Alisarda
  • Allegheny Airlines (Mohawk 298 conversion)
  • Altair Airlines
  • B.C. Air Lines (acquired by Pacific Western Airlines)
  • Cimber Air
  • Crown Airways
  • Dan-Air
  • Filipinas Orient Airways
  • Golden Gate Airlines (former Swift Aire aircraft)
  • IFG Interregional Fluggesellschaft
  • Indonesia Airlines
  • Japan Domestic
  • Lake Central Airlines
  • Linjeflyg
  • Malu Aviation
  • Mohawk Air Service
  • National Commuter Airlines (NATCOM) (operated both the Nord 262 and Mohawk 298 in Air Florida Commuter feeder service)
  • Pacific Western Airlines (former B.C. Air Lines aircraft)
  • Pocono Airlines
  • Queensland Pacific Airlines
  • Rhein Air (Switzerland)
  • Swift Aire Lines (San Luis Obispo, CA, USA)
  • Tempelhof Airways
  • Trans Service Airlift
  • Wideroe
  • Military Operators

     Angola
  • National Air Force of Angola
  •  Burkina Faso
     Republic of the Congo
  • Congolese Air Force
  •  France
  • French Air Force
  • French Navy
  •  Gabon

    Specifications (Nord 262A)

    Data from Jane's All The World's Aircraft 1965–66

    General characteristics

  • Crew: two
  • Capacity: 29 passengers
  • Length: 19.28 m (63 ft 3 in)
  • Wingspan: 21.90 m (71 ft 10 in)
  • Height: 6.21 m (20 ft 4 in)
  • Wing area: 55.0 m² (592 sq ft)
  • Airfoil: NACA 23016 at root, NACA 23012 at tip
  • Empty weight: 6,654 kg (14,669 lb)
  • Max. takeoff weight: 10,300 kg (22,710 lb)
  • Powerplant: 2 × Turbomeca Bastan VI C turboprops, 794 kW (1,065 ehp) each
  • Performance

  • Never exceed speed: 498 km/h (269 knots, 309 mph)
  • Maximum speed: 385 km/h (208 knots, 239 mph)
  • Cruise speed: 360 km/h (194 knots, 223 mph)
  • Stall speed: 128 km/h (69 knots, 79 mph)
  • Range: 1,110 km (600 nmi, 690 mi)
  • Service ceiling: 7,300 m (24,000 ft)
  • Rate of climb: 6.3 m/s (1,250 ft/min)
  • References

    Aérospatiale N 262 Wikipedia