Ch-53a/d/e Helicopter Parts

(Page 11) End item NSN parts page 11 of 66
Part Number
NSN
NIIN
1172015P1 Electromagnetic Relay
009994901
11722 Pressure Bellows
009422091
11789-0001 Display Handle
004890661
11796-0001 Handle Insert Assembly
004890666
117C116-2 Electromagnetic Relay
008660803
117C633-1 Electrical-electro Control Panel
007992215
117D110-1 Indicator Panel
007771704
118-21L12-10PN Electrical Plug Connector
001652514
118-22-4 Electrical Conduit Coupling Nut
002803311
11838508-1 Airframe Ball Bearing
006215240
118UC57 Transistor
009249611
119-0535-009 Semiconductor Device Retainer
007664568
119073-1 Cable Assembly
001096133
119354-01 Annular Ball Bearing
006469421
11957 Alt Control Housing
008667166
11TA-0541 Motor-tachometer Generator
010918181
11TX-300-N-22A/10 Transmitter Synchro
000188604
12-12 140138C Pipe Coupling
011965217
120-22481 Input Rod
008002942
120-45705 Feedback Cam
001017830
Page: 11 ...

Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e Helicopter

The Sikorsky CH-53E Super Stallion is the largest and heaviest helicopter in the United States military. As the Sikorsky S-80 it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor and canting the tail rotor 20 degrees. It was built by Sikorsky Aircraft for the United States Marine Corps. The less common MH-53E Sea Dragon fills the United States Navy's need for long range minesweeping or Airborne Mine Countermeasures (AMCM) missions, and perform heavy-lift duties for the Navy. Under development is the CH-53K King Stallion, which will be equipped with new engines, new composite material rotor blades, and a wider aircraft cabin.

The CH-53 was the product of the U.S. Marines' "Heavy Helicopter Experimental" (HH(X)) competition begun in 1962. Sikorsky's S-65 was selected over Boeing Vertol's modified CH-47 Chinook version. The prototype YCH-53A first flew on 14 October 1964. The first CH-53As were powered by two General Electric T64-GE-6 turboshaft engines with 2,850 shp (2,125 kW) and had a maximum gross weight of 46,000 lb (20,865 kg) including 20,000 lb (9,072 kg) in payload.

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