Mh-53e Helicopter Parts

(Page 171) End item NSN parts page 171 of 238
Part Number
NSN
NIIN
113766 Serrated Lock Ring
002819224
1138 Fluid Filter Element
000198087
113849 Electrical Fuel Pump
006764957
113958 Nonmetallic Hose
002893306
114-0047 Induct Wire Wound Fixed Resistor
000803218
114-023-0001 Telephone Jack
001924789
114-066-1001 Electrical Conne Retaining Plate
001199020
114-109-0007 Electrical Plug Connector
005527699
114-242-0002 Electrical Plug Connector
000795458
114-242-002 Electrical Plug Connector
000795458
114-3-4X1-2 Pipe Bushing
002783167
114-367-0001 Electrical Plug Connector
008996869
114-560 Universal Joint Parts Kit
007024578
114-560R Universal Joint Parts Kit
007024578
114-6000 Vehicular Universal Joint Spider
008452875
114-60003 Vehicular Universal Joint Spider
008452875
114-6003 Vehicular Universal Joint Spider
008452875
114-6006 Vehicular Universal Joint Spider
008452875
114-6007A Vehicular Universal Joint Spider
008452875
114-6012 Vehicular Universal Joint Spider
008452875
Page: 171 ...

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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