Mh-53e Helicopter Parts

(Page 12) End item NSN parts page 12 of 238
Part Number
NSN
NIIN
007-5067-02 Diode Semiconductor Device
011879137
007-59-F-3 Pipe To Tube Straight Adapter
005402612
007-6016-00 Diode Semiconductor Device
009244587
007-6017-00 Diode Semiconductor Device
009124907
007-6047-00 Diode Semiconductor Device
004654405
007-675249 Tapered Roller Bearing Cup
001000572
007-T-0078-01 Transistor
009373768
007002700 Transistor
001798478
007002900 Transistor
004368953
007003000 Transistor
001072571
007003400 Transistor
008836389
007003600 Thyristor Semiconductor Device
001063698
007003700 Transistor
001188433
00705 Flat Washer
006858308
0070977Q00 Cable Assembly
010554844
0071513816 Electromagnetic Relay
010389192
00719-F-2 Pipe Reducer
008730110
0073-2147 Incandescent Lamp
009267603
0073-768P1 Electrical Compone Tiedown Strap
009376691
0074452 Incandescent Lamp
000193093
Page: 12 ...

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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