Ch-53a/d/e Helicopter Parts

(Page 31) End item NSN parts page 31 of 66
Part Number
NSN
NIIN
3096 Directional Coupler
002645504
30A4-050 Calibrated Flow Valve
011084547
31-E5-56-638-9 Electrical Wire
013139878
31-E5-56-639-9 Electrical Wire
013164050
310162 Gasket
009421487
310D010 Air Sleeve Assembly
011811972
310D010-3 Air Sleeve Assembly
011811972
310D038-19 Liquid Quantity Transmitter
011741919
310D258-1 Fire Sprinkling Automatic Drain
012204650
311-7013-000 Plain Tapered Pin
001873218
31150 Electrical Receptacle Connector
000614641
31162-55 Annular Ball Bearing
009980540
31162-88 Annular Ball Bearing
009980540
3120-686-1011 Sleeve Bearing
006861011
3120006861011 Sleeve Bearing
006861011
3120718 Valve Body
000227586
3157251 Servo Valve Cover
009452397
3157252 Cable Assembly
009452396
3157687 Servo Valve Damper
009437886
Page: 31 ...

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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