Mh-53e Helicopter Parts

(Page 132) End item NSN parts page 132 of 238
Part Number
NSN
NIIN
104-0683 V Belt
000815436
104-1333 Film Fixed Resistor
011877374
104-1598 Quick Disconnect Terminal
009260085
104-1S12M Flat Washer
006858308
104-35816A Lock Washer
001941483
104-462 Unitized Semiconductor Devices
004688427
104-4641 Film Fixed Resistor
011772012
104-503-014 Diode Semiconductor Device
004218882
104-5111 Film Fixed Resistor
001420931
104.256-18 Incandescent Lamp
000131282
104.256-37 Incandescent Lamp
009418488
10401805 Paper Dielectric Fixed Capacitor
001296260
10402 Non Wire Wound Variable Resistor
009746426
10404N01P00 Pressure Indicator
005570215
10405343 Quick Disconnect Coupling Half
005401268
104076-42 Induct Wire Wound Fixed Resistor
002111319
104082 Tapered Roller Cone And Rollers
006061841
1040B9146-0001 Connector Adapter
003376770
1040B9146-1 Connector Adapter
003376770
104118279 Keyer Group Adapter
006148008
Page: 132 ...

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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