Mh-53e Helicopter Parts

(Page 106) End item NSN parts page 106 of 238
Part Number
NSN
NIIN
10121867 Hexagon Self-locking Nut
009471380
10121923 Hexagon Castellated Plain Nut
009901350
10122063 Recessed Washer
010573114
10122082 Clinch Self-locking Nut
010741495
10122106 Flat Washer
010885813
10122112 Clinch Self-locking Nut
010904865
10122181 Flat Washer
013048733
10122211 Flat Washer
013384121
10122225 Flat Washer
013522752
10122236 Flat Washer
013529588
10122274 Flat Washer
013824522
10122276 Flat Washer
013854499
10122278 Flat Washer
013861519
10122284 Flat Washer
013958986
10122432 Annular Ball Bearing
007739554
10122542 Spring Pin
000589747
10122543 Spring Pin
000589771
10122545 Spring Pin
000589782
10122556 Headed Straight Pin
000801940
10122561 Headed Straight Pin
000817876
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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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