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IAR-825TP Triumf - Retaining the wing and landing gear of the IAR-823, the turboprop powered Triumf has a new fuselage with two seats in tandem, and a new swept fin. Two underwing hardpoints are provided. The IAR-825TP first flew on June 12, 1982, and series production for the Romanian Air Force, using uprated 559kW Pratt & Whitney Canada PT-6A-25C engines, was due to begin in 1986.

IAR-825TP Triumf
Engine: 1 x P&WAC PT6A, 560 kW.
Span: 10.3 m.
Length: 8.9 m.
Wing area: 15 sq.m
Empty wt: 1200 kg.
MTOW: 2300 kg.
Max speed: 470 kph.
Initial ROC: 960 m / min.
Ceiling: 9000 m.
T/O run (to 15m): 250 m.
Ldg run (from 15m): 300 m.
Fuel internal: 360 lt.
Range/Endurance: 1400 km / 3 hr.


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