Mh-53e Helicopter Parts

End item NSN parts
Filter By: Tapered Roller Bearings
page 1 of 1
Part Number
NSN
NIIN
073-5347 Tapered Roller Bearing
001005301
11205-05 Tapered Roller Bearing
006908923
12Z10600-12 Tapered Roller Bearing
002273280
1502592 Tapered Roller Bearing
006908923
1502692 Tapered Roller Bearing
006908923
151443 Tapered Roller Bearing
001005301
16392S Tapered Roller Bearing
001005301
22168-9U013 Tapered Roller Bearing
002273280
24780-24720 Tapered Roller Bearing
001005301
28299 Tapered Roller Bearing
001837550
3110001005301 Tapered Roller Bearing
001005301
3110001005951 Tapered Roller Bearing
001005951
3110006908923 Tapered Roller Bearing
006908923
33891-33821 Tapered Roller Bearing
001837550
3651552 Tapered Roller Bearing
001005951
3920/2984 Tapered Roller Bearing
001005951
3984-3920 Tapered Roller Bearing
001005951
411626-01R Tapered Roller Bearing
006908923
441295-187313 Tapered Roller Bearing
001020598
443748 Tapered Roller Bearing
001020598
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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