Aircraft Elevators Parts

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Part Number
NSN
NIIN
1190280 Electrical Contact Assembly
002330255
1265913 Electrical Contact Assembly
000694321
200-VC-1004 Electrical Contact Assembly
000694321
23-2912 Electrical Contact Assembly
002620828
23-2999 Electrical Contact Assembly
008166440
23-29999 Electrical Contact Assembly
008166440
272083PC3 Electrical Contact Assembly
002330255
302-6293694 PC 38 Electrical Contact Assembly
009412114
365751PC3 Electrical Contact Assembly
002330255
36J643PC13 Electrical Contact Assembly
002330255
423481PC13 Electrical Contact Assembly
002330255
6-4035-101 Electrical Contact Assembly
009412114
6-4035-101A Electrical Contact Assembly
009412114
6956ED518 PC 1C Electrical Contact Assembly
002620828
6962ED3446 PC 1D Electrical Contact Assembly
002620828
6962ED3446 PC 2A Electrical Contact Assembly
002620828
6962ED3449 PC 1C Electrical Contact Assembly
002620828
6962ED3453 PC 1D Electrical Contact Assembly
002620828
6962ED3453 PC 2A Electrical Contact Assembly
002620828
6963ED233-1D Electrical Contact Assembly
002620828
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Elevators, Aircraft

Picture of Aircraft Elevators

Elevators are flight control surfaces, usually at the rear of an aircraft, which control the aircraft's pitch, and therefore the angle of attack and the lift of the wing. The elevators are usually hinged to the tailplane or horizontal stabilizer. They may be the only pitch control surface present, sometimes located at front (early airplanes) or integrated into a rear "all-moving tailplane" also called a slab elevator or stabilator.

The horizontal stabilizer usually creates a downward force which balances the nose down moment created by the wing lift force, which typically applies at a point (the wing center of lift) situated aft of the airplane's center of gravity. The effects of drag and engine thrust may also result in pitch moments that need to be compensated with the horizontal stabilizer.

Both the horizontal stabilizer and the elevator contribute to pitch stability, but only the elevators provide pitch control. They do so by decreasing or increasing the downward force created by the stabilizer :

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