Mh-53e Helicopter Parts

(Page 105) End item NSN parts page 105 of 238
Part Number
NSN
NIIN
10121216 Hexagon Plain Nut
002532796
10121384 Clinch Self-locking Nut
004250402
10121534 Flat Washer
005956612
10121543 Hexagon Plain Nut
005968422
10121553 Lock Washer
006163554
10121559 Flat Washer
006168118
10121593 Clinch Self-locking Nut
006825993
10121604 Hexagon Self-locking Nut
007029649
10121610 Flat Washer
007215762
10121621 Plate Self-locking Nut
007287703
10121637 Spring Tension Washer
007534402
10121641 Plate Self-locking Nut
007614220
10121655 Plate Self-locking Nut
007646596
10121684 Plate Self-locking Nut
007789511
10121686 Plate Self-locking Nut
007793601
10121692 Plate Self-locking Nut
007796689
10121732 Hexagon Slotted Self-locking Nut
008161879
10121740 Flat Washer
008195413
10121845 Lock Washer
009340226
10121855 Clinch Self-locking Nut
009349973
Page: 105 ...

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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