Ch-53a/d/e Helicopter Parts

(Page 5) End item NSN parts page 5 of 66
Part Number
NSN
NIIN
100476 Cable Assembly
001096133
10055 Socket Head Cap Screw
002862083
10056040 Sleeve Bearing
008195532
100696AZN006 Sleeve Spacer
008102918
100722-1 Direct Current Motor
013958532
1008 Pipe Cap
009387848
10085889 Needle Roller Bearing
002272980
100C0001-2 Electromagnetic Relay
008660803
100PD8 Weapon System Resilient Mount
000742056
100PDL-8 Weapon System Resilient Mount
000742056
10106670 Nonmetallic Bushing
005985389
10106761 Rotating Shaft Eye Bracket
011148426
10107664 Sleeve Bushing
006615422
1011 Arbitrary Scale Meter
000257110
101101-0 Fuel Control Housing
001047384
10111259 Tube Elbow
000083146
101119-2 Multiple Gears Gearshaft
013521314
101123FELE7 Ammeter
004718979
10117242 Vent Plug
000742617
10117454 Dust And Moistur Protective Plug
008041252
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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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