IAR 825
From Wikipedia, the free encyclopedia
| IAR 825 | |
|---|---|
| Role | Trainer aircraft |
| National origin | Romania |
| Manufacturer | Industria Aeronautică Română |
| First flight | 12 June 1982 |
| Status | Prototype only |
| Number built | 1 |
| Developed from | IAR-823 |
The IAR-825 Triumf is a Romanian tandem multirole trainer aircraft based on the IAR-823 built for the Romanian Air Force. The aircraft is roughly in the same class with the Brazilian EMBRAER Tucano. IAR-825 is equipped with the Canadian Pratt & Whitney Canada PT6 turboprop engine. First flight took place on the 12 June 1982.[1] Only one prototype exists, former YR-IGB, sold and registered in the USA in 2006 as N825BA.
[edit] Operators
[edit] Specifications (IAR-825)
Data from Jane's All The World's Aircraft 1988-89 [1]
General characteristics
- Crew: 2
- Length: 8.99 m (29 ft 6 in)
- Wingspan: 10.00 m (32 ft 9¾ in)
- Height: 3.20 m (10 ft 6 in)
- Wing area: 15.00 m² (151.5 ft²)
- Airfoil: NACA 23012 (modified)
- Empty weight: 1,250 kg (2,756 lb)
- Max. takeoff weight: 2,300 kg (5,070 lb)
- Powerplant: 1 × Pratt & Whitney PT6A-15AG turboprop, 507 kW (680 hp)
Performance
- Never exceed speed: 550 km/h (296 knots, 341 mph)
- Maximum speed: 470 km/h (254 knots, 292 mph)
- Cruise speed: 440 km/h (237 knots, 273 mph)
- Stall speed: 105 km/h (57 knots, 66 mph)
- Range: 1,400 km (755 nm, 870 mi)
- Service ceiling: 9,000 m (29,525 ft)
- Rate of climb: 16 m/s (3,150 ft/min)
[edit] See also
- Aircraft of comparable role, configuration and era
[edit] References
- Taylor, John W R. (editor). Jane's All The World's Aircraft 1988-89. Coulsdon, Surrey, UK: Jane's Information Group, 1988. ISBN 0 7106-0867-5.
|
|||||||||||||||||||||||
|
||||||||||||||
