Mh-53e Helicopter Parts

(Page 166) End item NSN parts page 166 of 238
Part Number
NSN
NIIN
111960 Spark Plug
009002876
1119832 Electrical Solenoid
008072408
1119832D Electrical Solenoid
008072408
1119843 Electrical Solenoid
008072408
1119848 Electrical Solenoid
008072408
111X01702X4000 Annular Ball Bearing
001089247
111X02003X0000 Annular Ball Bearing
005545396
111X02503X2000 Annular Ball Bearing
001448631
112 V Belt
005284287
112-0405 Film Fixed Resistor Network
010517994
112-05017 Fluid Passage Bolt
005167419
112-1051-017 Machine Screw
000593670
112-1055-009 Machine Screw
007808456
112-1055-026 Machine Screw
000572694
112-1055-047 Machine Screw
007815662
112-3769-1-1-2B Annular Ball Bearing
001448519
112-405 Film Fixed Resistor Network
010517994
11200107-1 Electrical Contact
011328789
11203A Tube Coupling Inverted Nut
000137397
11204-148 Composition Fixed Resistor
001219923
Page: 166 ...

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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