Mh-53e Helicopter Parts

(Page 52) End item NSN parts page 52 of 238
Part Number
NSN
NIIN
0690-1831 Composition Fixed Resistor
001368338
0690-3341 Composition Fixed Resistor
002478724
06918-5H1 Ball Bearing Unit
001169034
0693-1041 Composition Fixed Resistor
007598896
0693-1211 Composition Fixed Resistor
004723470
0693-1231 Composition Fixed Resistor
001605945
0693-1531 Composition Fixed Resistor
000052867
0693-2231 Composition Fixed Resistor
001406155
0693-2241 Composition Fixed Resistor
004224129
0693-3901 Composition Fixed Resistor
001560435
0693-3931 Composition Fixed Resistor
000052868
0698-0077 Film Fixed Resistor
004320434
0698-0079 Film Fixed Resistor
007583407
0698-0305 Composition Fixed Resistor
001111692
0698-3132 Film Fixed Resistor
002848262
0698-3150 Film Fixed Resistor
007583407
0698-3212 Film Fixed Resistor
001923882
0698-3226 Film Fixed Resistor
004320426
0698-3258 Film Fixed Resistor
002585882
0698-3348 Film Fixed Resistor
007584453
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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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