T25 Universal C military training Two versions of the Neiva Universal trainer aircraft are used by the Air Force Academy. This T-25A is used for basic training whereas instrument and navigation training is performed with the T-25C variant.

Especifications and limits Wide 36,8 feet Lenght 24,6 feet Height 9,84 feet Empty weight 2 292 lb Stall speed / retracted flaps 67 knots Stall speed / full flaps 59 knots Maximum weight 2 792 lb Maximum power 300 HP / 2700 RPM Flaps extend max speed 105 knots Gear down max speed 104 knots Cuise speed 120 knots Cruise speed during turbulent flight 90/170 knots Pitch down maximum speed 240 knots Fuel capacity 310 lts Range 600 nm Maximum speed 240 knots Rate of climb at sea level 800 feet / minute Rate of climb at 10.000 feet 300 feet / minute Ceilling 13.000 feet Basic procedures to fly T-25 Take off - full acelleration - 2650 RPM Climbing 90 kt - full acelleration, 2450 RPM, very rich mixture Cruise - wait until 100 kt and reduce to 20 pol (this procedure is the correction mixture before flight exercices and acrobatic events). Cruise (trip) - wait until 100 kt and reduce 1 pol on the gas, then reduce mixture to 60 h/lt Descent - 20 pol in the gas, 140 kt induced, rich mixture Traffic circuit - 100 kt - 17 pol Gear down while on wing leg -engine 23 pol Flaps down 30 degrees at base leg, engine 15 pol and ajdust to 2650 RPM

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