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FFT Eurotrainer 2000

The FFA 2000, FFT Eurotrainer 2000, Eurotrainer 2000 is a low wing two seat training aircraft developed by Gyroflug. A prototype was tested and displayed throughout Europe, but the project was canceled.[1]

FFT Eurotrainer 2000
Role Trainer
National origin Germany
Manufacturer Gyroflug, (Flugzeug und Faserverbund Technologie mbH)
Number built 1
Developed from FFA AS-202 Bravo

Development edit

The Eurotrainer 2000 was developed as a modern low cost trainer for military and civilian pilots developed from AS-202 metal design. The first launch customer was to be Swissair.[2] FFT went out of business in 1992 with one prototype produced.

Design edit

The aircraft is a four-seat, retractable tricycle gear design. The fuselage and wings are all composite construction. The landing gear uses a trailing link layout.[3][4]

Operational history edit

The prototype has been displayed in Paris, France in 1991 at Le Bourget airfield.

Variants edit

FFA 2000
FFA Flugzeugwerke project developed in 1985 with a Porsche PFM 3200-T03 engine. Production delays of Porsche engine prompted switch to Lycoming AEIO-540-X100 engine in 1989.[5]
FFT 2000
Gesellschaft für Flugzeug- und Faserverbund-Technologie mbH version (no differences)
Eurotrainer 2000A
Renamed product

Specifications (FFT Eurotrainer 2000) edit

Data from Flight International

General characteristics

  • Capacity: 4
  • Length: 8.10 m (26 ft 7 in)
  • Wingspan: 10.4 m (34 ft 1 in)
  • Width: 1.15 m (3 ft 9 in)
  • Height: 3.2 m (10 ft 6 in)
  • Wing area: 14 m2 (150 sq ft)
  • Empty weight: 920 kg (2,028 lb)
  • Max takeoff weight: 1,300 kg (2,866 lb)
  • Fuel capacity: 260 liters
  • Powerplant: 1 × Lycoming AEIO-540-L , 200 kW (270 hp)
  • Propellers: 3-bladed

Performance

  • Cruise speed: 324 km/h (201 mph, 175 kn)
  • Stall speed: 93 km/h (58 mph, 50 kn)
  • Never exceed speed: 417 km/h (259 mph, 225 kn)
  • Service ceiling: 7,000 m (23,100 ft)
  • Rate of climb: 6.6 m/s (1,300 ft/min)

Notes edit

  1. ^ Flight International. 23 May 1990. {{cite journal}}: Missing or empty |title= (help)
  2. ^ Flight International. 23 May 1990. {{cite journal}}: Missing or empty |title= (help)
  3. ^ "FAA certification". Retrieved 22 November 2010.
  4. ^ Air Progress. February 1989. {{cite journal}}: Missing or empty |title= (help)
  5. ^ Flight International. 24 June 1989. {{cite journal}}: Missing or empty |title= (help)

References edit

eurotrainer, 2000, 2000, eurotrainer, 2000, wing, seat, training, aircraft, developed, gyroflug, prototype, tested, displayed, throughout, europe, project, canceled, role, trainer, national, origin, germany, manufacturer, gyroflug, flugzeug, faserverbund, tech. The FFA 2000 FFT Eurotrainer 2000 Eurotrainer 2000 is a low wing two seat training aircraft developed by Gyroflug A prototype was tested and displayed throughout Europe but the project was canceled 1 FFT Eurotrainer 2000 Role Trainer National origin Germany Manufacturer Gyroflug Flugzeug und Faserverbund Technologie mbH Number built 1 Developed from FFA AS 202 Bravo Contents 1 Development 2 Design 3 Operational history 4 Variants 5 Specifications FFT Eurotrainer 2000 6 Notes 7 ReferencesDevelopment editThe Eurotrainer 2000 was developed as a modern low cost trainer for military and civilian pilots developed from AS 202 metal design The first launch customer was to be Swissair 2 FFT went out of business in 1992 with one prototype produced Design editThe aircraft is a four seat retractable tricycle gear design The fuselage and wings are all composite construction The landing gear uses a trailing link layout 3 4 Operational history editThe prototype has been displayed in Paris France in 1991 at Le Bourget airfield Variants editFFA 2000 FFA Flugzeugwerke project developed in 1985 with a Porsche PFM 3200 T03 engine Production delays of Porsche engine prompted switch to Lycoming AEIO 540 X100 engine in 1989 5 FFT 2000 Gesellschaft fur Flugzeug und Faserverbund Technologie mbH version no differences Eurotrainer 2000A Renamed productSpecifications FFT Eurotrainer 2000 editData from Flight InternationalGeneral characteristicsCapacity 4 Length 8 10 m 26 ft 7 in Wingspan 10 4 m 34 ft 1 in Width 1 15 m 3 ft 9 in Height 3 2 m 10 ft 6 in Wing area 14 m2 150 sq ft Empty weight 920 kg 2 028 lb Max takeoff weight 1 300 kg 2 866 lb Fuel capacity 260 liters Powerplant 1 Lycoming AEIO 540 L 200 kW 270 hp Propellers 3 bladed Performance Cruise speed 324 km h 201 mph 175 kn Stall speed 93 km h 58 mph 50 kn Never exceed speed 417 km h 259 mph 225 kn Service ceiling 7 000 m 23 100 ft Rate of climb 6 6 m s 1 300 ft min Notes edit Flight International 23 May 1990 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Flight International 23 May 1990 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help FAA certification Retrieved 22 November 2010 Air Progress February 1989 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help Flight International 24 June 1989 a href Template Cite journal html title Template Cite journal cite journal a Missing or empty title help References edit Retrieved from https en wikipedia org w index php title FFT Eurotrainer 2000 amp oldid 1092486813, wikipedia, wiki, book, books, library,

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