Mh-53e Helicopter Parts

End item NSN parts page 1 of 131
Part Number
NSN
NIIN
0 451 104 063 Fluid Filter Element
010585455
0 986 450 713 Fluid Filter Element
011924622
0-1459-1 Lug Terminal
001567196
0-40450-16S Electronic Shielding Gasket
007722223
0-80 UNF-3AX1/16 Setscrew
004625407
0.62518UNF3BT1G 405NSA/BEB Hexagon Self-locking Nut
000509372
000-0000-003 Diode Semiconductor Device
001704430
000-44859 Machine Bolt
002264827
000-60-8017-03-1 Electrical Contact
000796624
000-60-8017-03-13 Electrical Contact
000796624
000-60-8017-0313 Electrical Contact
000796624
000-8002-312 Electromagnetic Relay
000678582
000-8002-337 Incandescent Lamp
004910402
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
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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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