Mh-53e Helicopter Parts

(Page 114) End item NSN parts page 114 of 238
Part Number
NSN
NIIN
10135444 Connector Adapter
003376770
10135447 Electrical Plug Connector
003619542
10135450 Electrical Plug Connector
004174208
10135457 Electrical Plug Connector
004304107
10135476 Electrical Plug Connector
004878019
10135484 Electrical Plug Connector
005254260
10135498 Receptacle Dummy Connector
009471036
10135500 Electrical Connector Cover
009592610
10135522 Electrical Plug Connector
010327783
10135527 Electrical Plug Connector
010354722
10135529 Electrical Plug Connector
010381577
10135557 Electrical Plug Connector
010497912
10135610 Electrical Plug Connector
011084485
10135698 Electrical Plug Connector
011418193
10135707 Electrical Connector Cover
011613379
10136-1 Electrical-electron Mounting Pad
009582673
10136945 O-ring
011074961
10137-1 Safety Relief Valve
008810994
10138010 Dust And Moisture Protective Cap
001914898
10138033 Timer Housing
002395743
Page: 114 ...

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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