Mh-53e Helicopter Parts

(Page 100) End item NSN parts page 100 of 238
Part Number
NSN
NIIN
10114750 Tapping Screw
009591086
10114752 Machine Screw
009592345
10114756 Socket Head Cap Screw
009640077
10114768 Socket Head Cap Screw
009836659
10114780 Machine Screw
009846222
10114792 Machine Screw
009889106
10114798 Machine Screw
009909220
10114902 Socket Head Cap Screw
010457585
10115 Transistor
004974280
10115543 Machine Screw
011739465
10116114-01 Electrical Contact
010357465
10116563 Assembled Washer Plain Nut
001265753
10116564 Assembled Washer Plain Nut
001265754
10116599 Recessed Washer
001658391
10116635 Flat Washer
001834362
10116667 Hexagon Plain Nut
001991028
10117035 O-ring
000039157
10117075 O-ring
002500235
10117083 O-ring
002917295
10117242 Vent Plug
000742617
Page: 100 ...

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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