Aircraft Elevators Parts

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Part Number
NSN
NIIN
1190278 Electrical Contact
004455204
1190279 Electrical Contact
002415704
11K2570PC40 Electrical Contact
000499701
11K2718PC8 Electrical Contact
000499701
11K2763PC21 Electrical Contact
000499701
1315080 Electrical Contact
005905911
1315081 Electrical Contact
000357877
153B1 Electrical Contact
000358771
174A4611G1 Electrical Contact
007255853
174A611G1 Electrical Contact
007255853
174A71611G1 Electrical Contact
007255853
174A7611G1 Electrical Contact
007255853
1JD76PC3B Electrical Contact
004455158
229B2554G4S6-5B Electrical Contact
007255853
229B3554G4AS6-5B Electrical Contact
007255853
229B3554G5AS5-5B Electrical Contact
007255853
229B3554G6AS6-5B Electrical Contact
007255853
229B3569G2AS4-5B Electrical Contact
007255853
229B3569G2S4-5B Electrical Contact
007255853
23-1570-2 Electrical Contact
005905911
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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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