Mh-53e Helicopter Parts

(Page 172) End item NSN parts page 172 of 238
Part Number
NSN
NIIN
114-6016 Vehicular Universal Joint Spider
008452875
114-6028 Vehicular Universal Joint Spider
008452875
114-6100 Vehicular Universal Joint Spider
008452875
114-6100A Vehicular Universal Joint Spider
008452875
114-6100AB Vehicular Universal Joint Spider
008452875
114-6113 Vehicular Universal Joint Spider
008452875
114-6141 Vehicular Universal Joint Spider
008452875
114-6143 Vehicular Universal Joint Spider
008452875
114-6143A Vehicular Universal Joint Spider
008452875
1140 ITEM 8 Bearing Ball
001151238
114004 Nonmetallic Grommet
002024004
114004ADX Nonmetallic Grommet
002024004
114019 Nonmetallic Grommet
002766098
114019ADX Nonmetallic Grommet
002766098
1142-1 Bearing Ball
001151238
1142-248 Screw Thread Insert
004713745
114277-7 Radio Frequency Interfere Filter
001194605
114277-7A Radio Frequency Interfere Filter
001194605
11431327 Incandescent Lamp
005426571
11437167-4 Electrical Wire
001288696
Page: 172 ...

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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