Mh-53e Helicopter Parts

(Page 66) End item NSN parts page 66 of 238
Part Number
NSN
NIIN
09101896 Tapered Roller Bearing Cup
001000380
0910240 Pipe To Tube Elbow
002871766
0910240-1 Pipe To Tube Elbow
002871766
0910302-9 Cotter Pin
008499857
0910943-0 Pipe To Tube Straight Adapter
002784574
0911201-2 Woodruff Key
006165531
0911435 Tube-hose Fit Compression Sleeve
011937390
0911437 Tube Coupling Nut
000114627
0912738 Bearing Ball
001006150
0913526 Tube Coupling Inverted Nut
002889390
0913526-0 Tube Coupling Inverted Nut
002889390
0913535 Pipe To Tube Straight Adapter
005402612
0913535-1 Pipe To Tube Straight Adapter
005402612
0913536 Tube Coupling Inverted Nut
000137397
09136664-9 Pipe To Tube Straight Adapter
002891930
0913888 Pipe To Tube Elbow
002216215
0913888-4 Pipe To Tube Elbow
002216215
0914094 Pipe To Tube Elbow
002778269
0914094-8 Pipe To Tube Elbow
002778269
0915661 Pipe To Tube Elbow
006401051
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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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