Mh-53e Helicopter Parts

(Page 103) End item NSN parts page 103 of 238
Part Number
NSN
NIIN
10119531 Packing Retainer
008082340
10119534 Packing Retainer
008142371
10119537 Packing Retainer
008204142
10119538 Packing Retainer
008218848
10119543 Packing Retainer
008357712
10119545 Packing Retainer
008391846
10119550 Packing Retainer
008507490
10119652 Packing Retainer
011174238
10119910 Sleeve Spacer
013581686
10119918 Sleeve Spacer
013582343
1011MF01816-103 Coupler Control Plate
013100524
1011MF01816-104 Coupler Control Plate
013100525
1011MF01816-105 Coupler Control Plate
013100526
1011MF01816-106 Coupler Control Plate
013100542
1012-8-4S Pipe To Tube Straight Adapter
004418700
10120-301-001 Tubeaxial Fan
002265872
10120154 Film Fixed Resistor
000040200
10120161 Composition Fixed Resistor
000052868
10120169 Film Fixed Resistor
000061288
10120243 Composition Fixed Resistor
001111692
Page: 103 ...

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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