Mh-53e Helicopter Parts

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Filter By: Bearing Balls
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Part Number
NSN
NIIN
0000453578 Bearing Ball
001006158
0000453632 Bearing Ball
001151238
000381-5 Bearing Ball
001151238
00381-5 Bearing Ball
001151238
0114-1 Bearing Ball
001006147
0114-4 Bearing Ball
001006150
025-4S Bearing Ball
001006147
048-0284 Bearing Ball
001519213
0625SS Bearing Ball
000442269
0912738 Bearing Ball
001006150
1-16 Bearing Ball
001006150
1-8BALL Bearing Ball
001006147
100-6-1427-1 Bearing Ball
001837537
10045027 Bearing Ball
000442269
10107352 Bearing Ball
001837537
10107361 Bearing Ball
002274718
10183637 Bearing Ball
002770119
1024 Bearing Ball
001006150
10390419 Bearing Ball
001006147
104223-000 Bearing Ball
000442269
Page:

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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