Design Philosophy
IRAN-140 Versatile Performance
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| High wing monoplane , pressurized , wing mounted twin turboprop. | |
| Designed according to AP-25, FAR-25 & JAR-25. | |
| Passenger/Cargo for Hot & High , Adverse Weather Conditions. | |
| Operable in small airfield , short soft surface low LCN. | |
| High level cabin comfort ,low noise. | |
| Low maintenance , low Direct Operating Cost. | |
| Fast reconfiguration capability. | |
| APU
permanently installed . spacious baggage compartments. |
DESIGNED TO PERFORM
Full
IFR flight with GPS/RADIO NAV auto-pilot,
designed for "hot and high " performance
Modern and specious crew-convenient cockpit layout ,
half ton fuel consumption per hour,
highest lift to drag ratio for flight with single engine,
and lowest sink speed with all inoperative.
Fail-safe primary structure designed for a fatigue life of 50,000 flights
of1 hour .
Convertible
for various roles and missions Operation from short ,
unprepared airfields Independence from ground equipment Low internal and
external noise levels system for maximum dispatch rates High passenger-appeal
interior.
IRAN-140 Engine
Most reliable maintainable engine ,with more than 7 million safe flying hours with a long MTBF( 3 in 100,000 FH).
| Motorsich the largest engine manufacturer of Ex-Soviet Union and one of the largest Aero-Engine maker in the world produces TV3-117 VMA-SBM1 which is superior to Canadian PW127 with TBO of more than 4000 hours and a life expected to reach 20,000 flying hours. |
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