Puneet Varma (Editor)

NDN Firecracker

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Top speed
  
367 km/h

Length
  
8.33 m

Wingspan
  
7.92 m

First flight
  
May 26, 1977

NDN Firecracker NDN Firecracker Turbo Firecracker

The NDN Firecracker is a single-engine aircraft designed as a military trainer.

Contents

Design and development

NDN Firecracker NDN 1T TurboFirecracker

In 1976, Nigel Desmond Norman, one of the founders of Britten-Norman, the manufacturers of the Islander, set up NDN Aircraft to build the Firecracker, a single piston engined trainer designed to replicate the handling of a jet trainer. It was intended that the Firecracker would be built under license by third world countries to help start up local aviation industries. As such the structure was simple. The first prototype, powered by a Lycoming O-540 piston engine flew on 26 May 1977.

NDN Firecracker NDN 1 Firecracker

The aircraft configuration is a tandem two seat aircraft with retractable tricycle landing gear. It has a low aspect ratio wing in order to give fighter like handling and is fitted with an airbrake.

NDN Firecracker httpsuploadwikimediaorgwikipediacommonsthu

After producing a single piston-engined prototype, NDN developed the aircraft by fitting a Pratt & Whitney Canada PT6 turboprop engine, producing the NDN-1T Turbo-Firecracker. Three NDN-1Ts were built for the British commercial flying school, Specialist Flying Training, who used them for contract training of foreign military students, the first one flying on 1 September 1983. The Firecracker was entered into the competition to replace the BAC Jet Provosts used by Britain's Royal Air Force as a basic trainer, it being proposed to fit the aircraft for the RAF with a more powerful engine and ejection seats. Although the Firecracker, which was planned to be built by Hunting Group if successful, was one of the four shortlisting aircraft (the others being the Pilatus PC-9, Embraer Tucano and AAC A20 Wamira), ultimately a much modified version of the Tucano, the Shorts Tucano was chosen.

NDN Firecracker Norman NDN1 Firecracker Untitled Aviation Photo 0562626

Although NDN, which renamed itself the Norman Aircraft Company (NAC) in 1985, continued to try to sell the Firecracker, no further production ensued, and NAC went into receivership in 1988.

Specifications (Turbo Firecracker)

Data from Jane's All the World's Aircraft 1988-1989

General characteristics

NDN Firecracker WINGS PALETTE NAC Firecracker Great Britain others

  • Crew: Two
  • Length: 8.33 m (27 ft 4 in)
  • Wingspan: 7.92 m (26 ft 0 in)
  • Height: 3.25 m (10 ft 8 in)
  • Wing area: 11.89 m² (128 ft²)
  • Airfoil: NACA 23012
  • Empty weight: 1,117 kg (2,462 lb)
  • Max. takeoff weight: 1,633 kg (3,600 lb)
  • Powerplant: 1 × Pratt & Whitney Canada PT6A-25 turboprop, 533 kW (715 ehp)
  • Performance


  • Never exceed speed: 533 km/h (288 knots, 331 mph)
  • Maximum speed: 367 km/h (198 knots, 228 mph)
  • Cruise speed: 333 km/h (180 knots, 207 mph)
  • Stall speed: 111 km/h (60 knots, 69 mph)
  • Range: 1,158 km (625 nm, 720 mi) with maximum standard fuel
  • Service ceiling: 8,260 m (27,100 ft)
  • Rate of climb: 10.5 m/s (2,060 ft/min)
  • Wing loading: 137 kg/m² (28.1 lb/ft²)
  • Power/mass: 0.33 kW/kg (0.20 hp/lb)
  • Armament

  • Hardpoints: 4 with a capacity of 181 kg (400 lb) each
  • References

    NDN Firecracker Wikipedia