Mh-53e Helicopter Parts

End item NSN parts
Filter By: Self-aligning Plain Bearings
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Part Number
NSN
NIIN
03-001-0250 Self-aligning Plain Bearing
005285336
03-001-04 Self-aligning Plain Bearing
005285336
03-825-04 Self-aligning Plain Bearing
010069515
10-60545-107 Self-aligning Plain Bearing
011045989
10-60545-111S Self-aligning Plain Bearing
010069515
10107684 Self-aligning Plain Bearing
010069515
10159518 Self-aligning Plain Bearing
005285336
1417-526 Self-aligning Plain Bearing
010069515
2670406 Self-aligning Plain Bearing
010069515
2910231 Self-aligning Plain Bearing
010069515
76840-4 Self-aligning Plain Bearing
005285336
ADB4V Self-aligning Plain Bearing
010069515
ADW16V Self-aligning Plain Bearing
011363573
AS14101 Self-aligning Plain Bearing
010069515
AS14101-4 Self-aligning Plain Bearing
010069515
AS14103 Self-aligning Plain Bearing
011363573
AS14104 Self-aligning Plain Bearing
005285336
AS14104 Self-aligning Plain Bearing
011045989
AS14104-12 Self-aligning Plain Bearing
011045989
AS81820 Self-aligning Plain Bearing
005285336
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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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