Mh-53e Helicopter Parts

(Page 75) End item NSN parts page 75 of 238
Part Number
NSN
NIIN
1-4PT, BRASS Pipe Nipple
002221837
1-4X1-8 Pipe Bushing
002783905
1-51564-1 Electrical Contact
007896272
1-51565-1 Electrical Contact
007896272
1-531984-0 Electr Receptacle Connector Body
012264298
1-531984-5 Electr Receptacle Connector Body
012264299
1-550-0009 Incandescent Lamp
000802012
1-550-0039 Incandescent Lamp
009267603
1-550-0040 Incandescent Lamp
009273180
1-5904 Manual Control Lever
010093814
1-5919 Manual Control Lever
010093814
1-5JZ15B Diode Semiconductor Device
000717429
1-5P30Z6 Paper Metallized Fixed Capacitor
009855160
1-746085-0 Electrical Plug Connector
010925028
1-746290-0 AND 499252-4 Electrical Plug Connector
010925028
1-802109-1 Electr Receptacle Connector Body
000329561
1-86016-4 Electrical Contact
007641923
1-86557-2 Electrical Contact
000096413
1-87309-4 Electrical Contact
011135316
1-87522-7 Electrical Contact
002568040
Page: 75 ...

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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