Mh-53e Helicopter Parts

(Page 19) End item NSN parts page 19 of 238
Part Number
NSN
NIIN
0117454T00 Turnlock Fastener Receptacle
005797825
012-068A008 Electrical Plug Connector Body
001484254
012-1004-000 Turnlock Fastener Stud
002828132
012-1004-004 Turnlock Fastener Stud
002828132
012-112982 Electrical Contact
012321671
012-112982-01 Electrical Contact
012321671
012-112983 Electrical Contact
008407204
012-112983-01 Electrical Contact
008407204
012-1194-00 Turnlock Fastener Lockspring
002853373
012-1194-000 Turnlock Fastener Lockspring
002853373
012-1867 O-ring
000684382
012-21112-01 Annular Ball Bearing
001588265
012-2171-000 Turnlock Fastener Receptacle
000369305
012-3366-00 Push On Nut
009425139
012-4931-190 Screw Thread Insert
010069404
012-597-324-000 Spur Gear
000106250
0120-002-601 Electrical Plug Connector
006860447
012119400 Turnlock Fastener Lockspring
002853373
012176R Radio Frequency Cable
008125034
0122-1 Lock Washer
006163554
Page: 19 ...

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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