IAR 825 | |
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General information | |
Type | Trainer aircraft |
National origin | Romania |
Manufacturer | Industria Aeronautică Română |
Status | Prototype only |
Number built | 1 |
History | |
First flight | 12 June 1982 |
Developed from | IAR-823 |
The IAR-825 Triumf is a Romanian-designed 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. The IAR-825 is equipped with the Canadian Pratt & Whitney Canada PT6 turboprop engine. The type's first flight took place on the 12 June 1982.
Only one prototype aircraft exists, formerly registered YR-IGB. It was sold and registered in the US in 2006 as N825BA. It was damaged in a forced landing on July 15, 2012. It is currently registered by the Federal Aviation Authority as airworthy and active on the US civil aircraft register website as at November 2019.
Operators
Specifications (IAR-825)
Data from Jane's All The World's Aircraft 1988-89
General characteristics
- Crew: 2
- Length: 8.99 m (29 ft 6 in)
- Wingspan: 10 m (32 ft 10 in)
- Height: 3.2 m (10 ft 6 in)
- Wing area: 15 m (160 sq ft)
- Airfoil: NACA 23012 (modified)
- Empty weight: 1,250 kg (2,756 lb)
- Max takeoff weight: 2,300 kg (5,071 lb)
- Powerplant: 1 × Pratt & Whitney Canada PT6A-15AG turboprop engine, 507 kW (680 hp)
- Propellers: 3-bladed constant-speed propeller
Performance
- Maximum speed: 470 km/h (290 mph, 250 kn)
- Cruise speed: 440 km/h (270 mph, 240 kn)
- Stall speed: 105 km/h (65 mph, 57 kn)
- Never exceed speed: 550 km/h (340 mph, 300 kn)
- Range: 1,400 km (870 mi, 760 nmi)
- Service ceiling: 9,000 m (30,000 ft)
- Rate of climb: 16 m/s (3,100 ft/min)
See also
Aircraft of comparable role, configuration, and era
References
- ^ Taylor, John W.R., ed. (1988). Jane's all the World's Aircraft 1988–89 (79th ed.). London: Jane's Information Group. p. 200. ISBN 0-7106-0867-5.
- "CEN12LA446: Full Narrative". National Transportation Safety Board. Retrieved 13 April 2016.
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