Mh-53e Helicopter Parts

(Page 137) End item NSN parts page 137 of 238
Part Number
NSN
NIIN
10510553 Pump Piston Assembly
001049293
10510557 Hydraulic Mo Cylinder Block Unit
001362424
10510559 Compression Helical Spring
011608053
10510833 Coupling Retainer
009090001
10511269 Electrical Insulation Sleeving
007670511
10511273 Dust And Moistur Protective Plug
008170912
105122 Electrolytic Fixed Capacitor
008790123
1051237 Hexagon Head Cap Screw
007247220
10513438 Stud Terminal
005390511
10516333 Paper Dielectric Fixed Capacitor
006550159
10524-18 Pipe Nipple
001961471
10524-29 Pipe Nipple
001961472
105256 Pipe To Tube Straight Adapter
002028470
105262 Check Valve
006040668
1053 Nonmetallic Grommet
002764205
105300 Lubrication Fitting
001720031
10531906-1 Nonwire Wound Variable Resistor
005811403
10532545 Film Fixed Resistor
007213705
10532701 Film Fixed Resistor
002403016
10534500 Extractor Post Fuseholder
000181450
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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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