Mh-53e Helicopter Parts

(Page 99) End item NSN parts page 99 of 238
Part Number
NSN
NIIN
10112416 Loop Clamp
011212862
10112490 Loop Clamp
011259077
10112500 Loop Clamp
011268906
10112580 Loop Clamp
011313132
101130-2 Knob
009084394
10113095 Dust And Moistur Protective Plug
012820812
10114169 Machine Bolt
001357233
10114198 Machine Bolt
001822056
10114549 Machine Screw
008177590
10114586 Machine Screw
008242023
10114591 Machine Screw
008242029
10114606 Machine Screw
008393437
10114610 Machine Screw
008409275
10114617 Machine Screw
008420240
10114699 Machine Screw
009296421
10114700 Machine Screw
009296457
10114708 Externally Relieved Body Screw
009390485
10114718 Machine Screw
009430898
10114727 Machine Screw
009572383
10114742 Machine Screw
009583409
Page: 99 ...

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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