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Lockheed P-38 Lightning lower rudders now in production. These are available as complete, airworthy, bolt on assemblies including led counterweights. In production now for a limited time, they are provided with a full set of certifications (heat treatment, material, machining etc).
Preview of the Parts Catalog for P-38H, P-38J, P-38L, and F-5B Airplanes document available on the AirCorps Library
The Lockheed P-38 Lightning is an American single-seat, twin piston-engined fighter aircraft that was used during World War II. Developed for the United States Army Air Corps (USAAC) by the Lockheed Corporation, the P-38 incorporated a distinctive twin-boom design with a central nacelle containing the cockpit and armament.
General Servicing Coolant Systems for P-38, F-5, P-40 (except F and L), P-51, P-51A, P-63 and A-36
The Lockheed P-38 Lightning was originally designed as a bomber-interceptor and was never intended to be a fighter. Weight was kept to a minimum and it was far more advanced and faster than its U.S. counterparts, the Bell P-39 Airacobra and Curtiss P-40 Warhawk .
"The P-38 was a large fighter with much mass. 52' wingspan and long, wide-chord ailerons contributed to slow response along the longitudinal axis of the early airplanes. The higher the indicated airspeed, the slower the response. At very high IAS it took plenty of muscle to roll the airplane.
The Lockheed P-38 Lightning was an American heavy fighter aircraft that was deployed in World War II. The P-38 has an unusual design, the fuselage consists of two engine nacelles, each topped with a rudder and connected by an elevator.