Mh-53e Helicopter Parts

(Page 2) End item NSN parts page 2 of 238
Part Number
NSN
NIIN
000-8002-337 Incandescent Lamp
004910402
000-8002-430 Tube To Hose Straight Adapter
010878886
000-8002-757 Tip Jack
007295559
000-8002-788 Electrical Contact
007896272
000-8002-810 Electrical Contact
003389875
000-8002-811 Electrical Plug Connector
010476313
000-8003-293 Electrical Wire
010464014
000-8003-316 Electrical Wire
010464014
000-8003-875 Film Fixed Resistor
002368118
000-8003-922 Film Fixed Resistor
010520978
000-8004-029 Film Fixed Resistor
001374511
000-8004-033 Film Fixed Resistor
002893418
000-8004-035 Film Fixed Resistor
004326366
000-8004-947 Electrical Connector Insert
001063803
000-8005-014 Electrical Contact
002568040
000-8006-108 Electrical Special Purpose Cable
010440855
000-8006-291 Electrical Power Cable
010429008
000-8006-353 Pipe To Boss Straight Adapter
010422960
000-8006-444 Electromagnetic Relay
000678582
000-8007-043 Electrical Contact
002568040
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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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