Mh-53e Helicopter Parts

(Page 178) End item NSN parts page 178 of 238
Part Number
NSN
NIIN
116584 Vent Valve
007264719
1166-36-0 Test Lead
001751431
1166-36BLACK Test Lead
001751431
1166-36BLK Test Lead
001751431
116626PC748 Pipe Bushing
002783167
116630PC748 Pipe Bushing
002783167
116695 Annular Ball Bearing
001861104
1166AS113-1 Selector Rotary Valve
013947587
11671573 Quick Disconnect Terminal
009260085
116724PC740 Pipe Bushing
002783167
116830PC740 Pipe Bushing
002783167
11689377 Annular Ball Bearing
001091157
116926PC748 Pipe Bushing
002783167
116930PC748 Pipe Bushing
002783167
11697605 Turnlock Fastener Receptacle
009820177
11697830 Electrical Contact
009379237
11697831 Electrical Contact
009379238
11698723-13 Screw Thread Insert
008037150
11699912-165 Electrical Insulation Sleeving
007816826
116CP Cotter Pin
000179252
Page: 178 ...

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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