Mh-53e Helicopter Parts

(Page 77) End item NSN parts page 77 of 238
Part Number
NSN
NIIN
1/4 X 1/8 FF-B Pipe Reducer
006406330
1/4-30682-4 Tube To Hose Straight Adapter
005551152
1/8D X 2L Cotter Pin
002857161
10-00027-00 Mica Dielectric Fixed Capacitor
010493153
10-00080-00 Electrolytic Fixed Capacitor
008790123
10-00148-201 Film Fixed Resistor
004267133
10-00277-019 Composition Fixed Resistor
001311256
10-0055-9 Electric Lantern
005334960
10-05784 Plastic Dielectr Fixed Capacitor
008352710
10-05784-00 Plastic Dielectr Fixed Capacitor
008352710
10-10 Fixed Attenuator
007210255
10-10046-0A Transistor
001072571
10-10081-0A Transistor
009129008
10-101960-223 Electrical Connector Cover
011352059
10-104 Conductor Splice
005782281
10-120554-504 Paper Metallized Fixed Capacitor
001489365
10-125904-103 Plastic Dielectr Fixed Capacitor
008352710
10-128 Alternator Assembly
001500038
10-130P2 Light Lens
000787626
Page: 77 ...

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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