Mh-53e Helicopter Parts

(Page 165) End item NSN parts page 165 of 238
Part Number
NSN
NIIN
1116405 Engine Generator Regulator
011964882
111677-0071 Paper Dielectric Fixed Capacitor
006550159
1117-15-0119 Feedthru Terminal
007269778
1117-5999 Glass Dielectric Fixed Capacitor
001371031
1117080 Engine Accessory Generator
010976213
11171-29-92G Pressure Transmitter
009935546
111748-011 Tube Tee
009927988
11176177-1 S Electrical Insulation Sleeving
001461122
11176486 Electrical Plug Connector
009310412
1117734 Engine Accessory Generator
010976213
11177546-3 Tube Nipple
007816089
1117772 Engine Accessory Generator
010976213
1118 Lock Washer
005146674
1118-87-2 Electrical Cable Nipple
005031440
1118301-5 Electrolytic Fixed Capacitor
011194333
11186798 Electronic Shielding Gasket
005799513
1119 Weighing Scale
005144117
11190 Tube Coupling Inverted Nut
000137397
111923 Tapered Roller Bearing Cup
001000359
111945 Transistor
009790108
Page: 165 ...

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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