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Fajr F.3
Role Training aircraft
Manufacturer Fajr Aviation & Composites Industry
First flight 1995
Introduction Iran
Status Active service
Primary user Iranian Air Force
Produced 2001—

Fajr F.3 (Persian: فجر اف.۳‎) is an Iranian full composite four-seat training/touring aircraft built by Fajr Aviation & Composites Industry. First flown in 1995, production commenced in 2001 after the aircraft was certified to JAR-23 standard. It has been speculated that it is a copy/modification of the Cirrus SR-20.[1]

Specifications (Fajr F.3)[]

Data from Jane's All The World's Aircraft 2003—2004[2]

General characteristics

  • Crew: One, pilot
  • Capacity: 3 passengers
  • Length: 8.07 m (26 ft 5¾ in)
  • Wingspan: 10.50 m (34 ft 5½ in)
  • Height: 3.05 m (10 ft 0 in)
  • Wing area: 14.02 m² (150.9 ft²)
  • Airfoil: Horstmann-Quast HQ-42E
  • Empty weight: 1,100 kg (2,425 lb)
  • Max. takeoff weight: 1,580 kg (3,483 lb)
  • Powerplant: 1 × Lycoming AEIO-540-L1B5 Six-cylinder air-cooled horizontally-opposed piston engine, 201 kW (270 hp)
  • Cabin Width: 1.25 m (4 ft 1 in)
  • Fuel Capacity: 212 litres (56.0 US Gallons)

Performance

  • Never exceed speed: 370 km/h (200 knots, 230 mph)
  • Maximum speed: 296 km/h (160 knots, 184 mph)
  • Cruise speed: 267 km/h (144 knots, 166 mph)
  • Stall speed: 104 km/h (56 knots, 65 mph)
  • Range: 1,129 km (610 nmi, 702 mi)
  • Endurance: 6 hr 15 min
  • Service ceiling: 5,480 m (18,000 ft)
  • Rate of climb: 5.2 m/s (1,030 ft/min)
  • Take-off Run: 310 m (1,020 ft)
  • Landing Distance Roll: 370 m (1,180 ft)

See also[]

References[]

  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.

External links[]

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The original article can be found at Fajr F.3 and the edit history here.
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