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| Fajr3 |
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| Type |
Training aircraft |
| Manufacturer |
Fajr Aviation & Composites Industry |
| Maiden flight |
1995 |
| Introduced |
Iran |
| Status |
Active service |
| Primary user |
Iran |
The Fajr-3 (فجر-3)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.
[edit] Specifications (Fajr-3)
Data from {name of first source}
General characteristics
- Crew: One, pilot
- Capacity: 3 passengers
- Length: 8.07 m (26 ft 6 in)
- Wingspan: 10.5 m (34 ft 5 in)
- Height: 3.05 m (10 ft 0 in)
- Wing area: 14 m² (150.6 ft²)
- Empty weight: 1,100 kg (2,420 lb)
- Max takeoff weight: 1,580 kg (3,483 lb)
- Powerplant: × Six-cylinder air-cooled horizontally-opposed piston engine, 201 kW (270 hp) each
- * Cabin Width: 1.25 m (4 ft 1 in)
- MAC: 1.4 m (4 ft 7 in)
- Fuel Capacity: 212 litres
Performance
- Maximum speed: 326 km/h (176 knots, 203 mph)
- Cruise speed: 275 km/h (148 knots, 170 mph)
- Stall speed: 104 km/h (56 knots, 65 mph)
- Range: 1,300 km (701 nm, 808 mi)
- Service ceiling 5,791 m (19,000 ft)
- Rate of climb: 5.23 m/s (1,030 ft/min)
- Wing loading: 112.8 kg/m² (23.06 lb/ft²)
- Power/mass: 7.85 kg/kW (12.9 lb/hp)
- Take-off Run: 310 m (1,017 ft)
- Landing Distance Roll: 330 m (1,083 ft)
[edit] See also
[edit] References
[edit] External links
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