Mh-53e Helicopter Parts

(Page 147) End item NSN parts page 147 of 238
Part Number
NSN
NIIN
108110-2 Compression Helical Spring
002010272
1081106P2 Compression Helical Spring
002010272
108111-1 Turnlock Fastener Stud
005432418
108111-2 Turnlock Fastener Stud
005432418
108114-1 Telephone Jack
001924789
108114GP1 Telephone Jack
001924789
10814 O-ring
011074956
1081A89G05 Angle Valve
002894383
1081H05H35 Film Fixed Resistor
004520764
1081H06H29 Film Fixed Resistor
007212385
1081H06H30 Film Fixed Resistor
001585065
1081H07H42 Film Fixed Resistor
001585065
1081H07H46 Unitized Semiconductor Devices
012859902
1081H08H41 Film Fixed Resistor
007212385
1081H08H42 Film Fixed Resistor
000255988
1081H08H43 Film Fixed Resistor
004520764
1081H09H16 Unitized Semiconductor Devices
012859902
1081H09H20 Film Fixed Resistor
000255988
1081H09H22 Film Fixed Resistor
002084407
1081H09H26 Film Fixed Resistor
003259097
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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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