Fajr F.3
| 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— |
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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
 |
Wikimedia Commons has media related to Fajr Aviation & Composites Industry. |
- ↑ http://www.eaa.org/news/2010/2010-02-11_iranian_aircraft.asp
- ↑ Jackson 2003, pp. 271–272.
- Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.
- Exhibitors - IRAN AIR SHOW 2008
- Full Composite Aircraft FAJR-3, Manufacturer exporting direct from IRAN
External links
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