Mh-53e Helicopter Parts

End item NSN parts
Filter By: Annular Ball Bearings
page 1 of 3
Part Number
NSN
NIIN
0067916 Annular Ball Bearing
001448519
0067916-7 Annular Ball Bearing
001448519
00P00000-1524 Annular Ball Bearing
005543468
01-005184-203 Annular Ball Bearing
001089247
01-005184-205 Annular Ball Bearing
001091157
01-005184-305 Annular Ball Bearing
001448519
01-005248-330 Annular Ball Bearing
001089247
010 508 2 Annular Ball Bearing
005545396
0105082 Annular Ball Bearing
005545396
0105090 Annular Ball Bearing
001448519
012-21112-01 Annular Ball Bearing
001588265
022061700 Annular Ball Bearing
001448631
0301-BB1 Annular Ball Bearing
001448631
0301-BB1-001 Annular Ball Bearing
001448631
0385-5 Annular Ball Bearing
005290573
03963X Annular Ball Bearing
001448519
042979 Annular Ball Bearing
005545396
05012-0061 Annular Ball Bearing
007739554
051162 Annular Ball Bearing
001091157
058-4 Annular Ball Bearing
002274521
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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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