Mh-53e Helicopter Parts

(Page 148) End item NSN parts page 148 of 238
Part Number
NSN
NIIN
1081H09H44 Film Fixed Resistor
001585065
1081H10H17 Unitized Semiconductor Devices
012859902
1081H10H27 Film Fixed Resistor
003259097
1081H10H41 Film Fixed Resistor
000255988
1081H10H45 Film Fixed Resistor
007212385
1081H10H59 Film Fixed Resistor
002084407
1081H12H28 Film Fixed Resistor
000255988
1081H15H48 Film Fixed Resistor
007212385
10823 Recessed Washer
007755245
108307 Drain Cock
002769041
10833C Cable Assembly
010554844
108363-11 Loop Clamp
002907273
108402-33 Wire Wound Fixed Resistor
011427165
108406 Nonwire Wound Variable Resistor
010262141
108407 Composition Fixed Resistor
001114732
108457096002913 Electrical Receptacle Connector
012387768
108522 Composition Fixed Resistor
001168565
10855 Plain Tapered Pin
001873218
1085CP Sleeve Bearing Set
006628425
1085CPANDL Sleeve Bearing Set
006628425
Page: 148 ...

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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