Normal and emergency operating characteristics of United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. Three P-38 aircraft fly in formation. A P-38 Lightning aircraft in flight. Animation depict bail out techniques from the aircraft. The aircraft flies low over a shoreline. The P-38 aircraft accelerates while in flight. The propellers of the aircraft rotate. Cockpit panel of the aircraft.
A film about the United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. A P-38 Lightning aircraft lifts in air. American aviator Milo Garrett Burcham applies brakes. Revolutions per minute ( RPM ) gauges show reduced speed of the aircraft. The aircraft in flight. The aircraft tilts while taking a sharp turn. A temperature gauge on a panel of the aircraft.
A film about the United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. Landing light of an aircraft. American aviator Milo Garrett Burcham applies brakes to reduce the speed before landing. Manifold Pressure Gauge on the panel of the aircraft. The landing gear of the aircraft is lowered. The pilot applies the brakes. The landing gear of the aircraft is pulled up. The pilot operates auxiliary hand pump. A bypass valve is closed. The landing gear is lowered. The pump is operated. A selective valve is closed. Flaps are put in position. The aircraft lands on two main gears. The nose wheel touches down while the landing.
A film about the United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. An aircraft taxis after landing. Other aircraft parked in the background. Animation depicts problems of nose wheel landing and the problems faced by a pilot while studying the single seat fighter.
A film about the United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. The instruction version of the P-38 aircraft. A new recruit talks to American aviator Milo Garrett Burcham. Burcham sits in a cockpit. He operates the brakes to control the speed of the propellers. Propeller switches are operated to control revolutions per minute (RPM ) of the aircraft. Warning lights glow. A circuit breaker trips up as a short circuit occurs. The circuit breaker is pushed down. The aircraft taxis. Propeller system is operated, a booster pump is switched on and toe brakes are held. The brakes are applied to get the desired speed. Manifold Pressure Gauge on a panel. The aircrafts takes off. The warning lights blink. The circuit breakers trip. The RPM gauge shows increased propeller speed. The RPM is reduced to desired value. A circuit breaker switch is pushed. The aircraft in flight. The pilot operates handles and switches for single engine operation in case of an engine failure.
A film about single engine operation of a United States Army Air Force Lockheed P-38 Lightning aircraft in the United States. A P-38 Lightning aircraft in flight. One of the propellers of the aircraft stops. The booster pump of the aircraft is put on. The rudder tap and the selector valve are operated. The oil cooled switch is put on. The aircraft in flight. The tank selector valve is operated and the booster pump is put on. The governor control operated to reduce speed. Switches operated for cut off. The feather switch is operated. The rudder tab and the oil switch are operated. The feather switch is put to normal position. The governor control is operated. The manual propeller switch is operated to resume two engine operation. Temperature and fuel pressure gauge. Manifold Pressure Gauge, Revolutions per minute ( RPM ) gauge and temperature gauge show readings.
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