Mh-53e Helicopter Parts

(Page 11) End item NSN parts page 11 of 238
Part Number
NSN
NIIN
0067916 Annular Ball Bearing
001448519
0067916-7 Annular Ball Bearing
001448519
007-00078-0001 Transistor
009373768
007-00137-0000 Thyristor Semiconductor Device
001063698
007-00151-0000 Transistor
002462449
007-0078-01 Transistor
009373768
007-01157-0008 Electrical Contact
001634081
007-0119-00 Transistor
001798478
007-0137-00 Thyristor Semiconductor Device
001063698
007-0151-00 Transistor
002462449
007-0153-00 Transistor
001240117
007-05011-0000 Diode Semiconductor Device
009042020
007-06016-0000 Diode Semiconductor Device
009244587
007-06047-0000 Diode Semiconductor Device
004654405
007-1091-20 Electrical Contact
002568040
007-1091-23 Electrical Contact
010879279
007-1091-25 Electrical Contact
007641923
007-4012401-03 Incandescent Lamp
009273180
007-5011-00 Diode Semiconductor Device
009042020
007-5011-14 Diode Semiconductor Device
003656459
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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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