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 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.
Evolution of United States Air Force uniforms in the United States. A captain in the 1917 uniform walks towards a French Nieuport fighter aircraft. He inspects the propellers and the engine of the aircraft. The captain climbs into the cockpit and adjusts his eye gear. The aircraft taxis on a field.
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