Mh-53e Helicopter Parts

(Page 70) End item NSN parts page 70 of 238
Part Number
NSN
NIIN
0M028 V Belt
005284451
0N057136 Incandescent Lamp
009267603
0N064070 Transistor
007525362
0N064104-14 Electrical Plug Connector
011093787
0N064104-22 Electrical Plug Connector
011104744
0N064104-25 Electrical Plug Connector
011077294
0N084015 Turnlock Fastener Receptacle
002820629
0N091366-2 Electrical Plug Connector
009310412
0N169628-3 Electrical Contact
000397481
0N173879-1 Electrolytic Fixed Capacitor
008725152
0N205436 Transistor
010114957
0N270638-3 Electronic Equipmen Hardware Kit
010572216
0N27413-1 Electrical Wire
010464014
0N287298-9 Electrical Plug Connector
010925028
0N295165-2 Tip Jack
007295559
0N316819 Film Fixed Resistor Network
010517994
0N419040-1 Electrical-electronic Heat Sink
009385157
0N436281-1 Dust And Moisture Seal Boot
010979929
0N501397-1 Extractor Post Fuseholder
007855471
0N507756 Incandescent Lamp
004910402
Page: 70 ...

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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