Mh-53e Helicopter Parts

(Page 162) End item NSN parts page 162 of 238
Part Number
NSN
NIIN
111086-001 Electrical Receptacle Connector
008407152
111086-003 Connector Adapter
001054642
1110G15G Circuit Breaker
006157071
1110X4 Tube Coupling Nut
000116452
1111-0072 Abrasive Wheel
002251955
11110-001 Assembled Washer Plain Nut
008363520
11112 Pipe To Tube Straight Adapter
002891930
111126PC748 Pipe Bushing
002783167
111130PC748 Pipe Bushing
002783167
11114 Pipe To Tube Straight Adapter
002784592
111226PC748 Pipe Bushing
002783167
111230PC748 Pipe Bushing
002783167
11124-7-37 Machine Screw
000598248
1112752-81 Electrolytic Fixed Capacitor
013268362
1112906-6 Electrolytic Fixed Capacitor
004877093
1112S1-4E Fluid Pressure Dampener
008516818
1112SE Fluid Pressure Dampener
008516818
1112SE-1/4 Fluid Pressure Dampener
008516818
1113162 Electrical Engine Starter
011212577
1113250 Electrical Engine Starter
011052053
Page: 162 ...

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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