Mh-53e Helicopter Parts

(Page 104) End item NSN parts page 104 of 238
Part Number
NSN
NIIN
10120263 Film Fixed Resistor
001129104
10120295 Composition Fixed Resistor
001311256
10120296 Film Fixed Resistor
001315807
10120312 Film Fixed Resistor
001374511
10120316 Film Fixed Resistor
001374824
10120353 Film Fixed Resistor
001392146
10120365 Film Fixed Resistor
001392470
10120370 Composition Fixed Resistor
001406155
10120411 Film Fixed Resistor
001514675
10120416 Film Fixed Resistor
001530178
10120423 Composition Fixed Resistor
001534896
10120426 Composition Fixed Resistor
001560435
10120435 Film Fixed Resistor
001636958
10120442 Film Fixed Resistor
001670625
10120478 Film Fixed Resistor
001855432
10120552 Film Fixed Resistor
002334515
10120600 Composition Fixed Resistor
002478724
10120682 Film Fixed Resistor
002893418
10120751 Film Fixed Resistor
003339543
10121181 O-ring
011604327
Page: 104 ...

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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