Mh-53e Helicopter Parts

(Page 173) End item NSN parts page 173 of 238
Part Number
NSN
NIIN
11437862-4 Electrical Compone Tiedown Strap
009376691
11439297-1 Electronic Shielding Gasket
005799513
114445 Annular Ball Bearing
000196390
11450 Electromagnetic Relay
011026488
11450701-1 Electrical Plug Connector
008129240
1146016 Vehicular Universal Joint Spider
008452875
114605 Lock Washer
005146674
1146166AB Vehicular Universal Joint Spider
008452875
114627 Tube Coupling Nut
000114627
114628 Tube-hose Fit Compression Sleeve
011937390
114629 Pipe To Tube Straight Adapter
002704613
11464608-3 Electrical Textile Sleeving
011684246
11466598-17 Radio Frequency Coil
011044465
1147 Cable Strain Relief Bushing
003516114
1147 BLACK (SR-5P-4) Cable Strain Relief Bushing
003516114
114724PC740 Pipe Bushing
002783167
114730PC740 Pipe Bushing
002783167
114733 U Semiconductor Device Rectifier
010471412
114796 Pipe To Tube Straight Adapter
002704613
Page: 173 ...

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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