Mh-53e Helicopter Parts

(Page 120) End item NSN parts page 120 of 238
Part Number
NSN
NIIN
10173119 Screw Thread Insert
008644958
10173122 Screw Thread Insert
009909916
101740-023 Film Fixed Resistor Network
010829493
10175254 Electrical Insulation Sleeving
000523301
101754 O-ring
009247757
101760 Needle Roller Bearing
002274431
10176907 Electrical Contact
010357465
10177044 Lubrication Fitting
009725789
10178917 Tube To Boss Straight Adapter
002776836
10179171 Gaseou Pressure Equalizing Valve
010950017
10180302-1 Thrust Washer Bearing
009028470
10180331-028 Mica Dielectric Fixed Capacitor
010436897
10180383-2 Incandescent Lamp
004910402
101811 Turnlock Fastener Receptacle
008502240
10182358 Diode Semiconductor Device
011702173
10183637 Bearing Ball
002770119
101843 Film Fixed Resistor
001956377
101847 Electromagnetic Relay
010389192
10185959 Transistor
009443520
10185977 Radio Frequency Detector
008777148
Page: 120 ...

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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