Mh-53e Helicopter Parts

(Page 141) End item NSN parts page 141 of 238
Part Number
NSN
NIIN
10628101 Electrical Tiedown Mounting Base
010135864
10629900-00 Transistor
004045537
10630050-137 Turnlock Fastener Stud Assembly
006395575
10631C Cable Assembly
010554844
106333 Hexagon Plain Nut
008807745
10638480 End Chain Link
012560470
10639256-1 Pipe To Boss Straight Adapter
011883184
106417 Electrical Connector Cover
011352059
10643-8-8 Tube To Hose Straight Adapter
012085863
106447 Radio Receiver Support
003980460
1064478 Annular Ball Bearing
000581682
1064478G001 Annular Ball Bearing
000581682
1064488 Shim
003332699
106464-108 Metallic Shielded Cable Ferrule
006664436
10647700-50OHM Electrical Dummy Load
011450138
1064800G1 Film Fixed Resistor
002009294
1064868G2 Cartridge Fuse
000454211
1065-1 Electrical Receptacle Connector
004783338
106500 Electrolytic Fixed Capacitor
000816159
1065082 Annular Ball Bearing
007739554
Page: 141 ...

Helicopter, Mh-53e

Picture of Mh-53e 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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