Mh-53e Helicopter Parts

(Page 5) End item NSN parts page 5 of 238
Part Number
NSN
NIIN
0007-00119-0000 Transistor
001798478
00076-0238 Engine Accessory Generator
001643243
000952T Transmission Cover
009197240
0009830600V Fluid Filter Element
010585455
001-30162 Tapered Roller Bearing Cup
001000572
0010106 Ball Socket Seat
003835001
001179 Electrical Wire
008397432
001198 Tube Elbow
002546447
001198-1 Tube Elbow
002546447
001366 Pre Wire Wound Variable Resistor
012325593
0014772 Hexagon Head Cap Screw
000712074
00154-0645-01 Electromagnetic Relay
005081815
00154-0645-1 Electromagnetic Relay
005081815
0015972-001 Cable Assembly
012266023
0017-0058 Light Transmitt Indicating Panel
011302959
0017-0084 Light Transmitt Indicating Panel
013060904
00171-0110 Electrical Solenoid
008536024
00173-12 O-ring
000684382
001787 Composition Fixed Resistor
004935249
0017930-01 Electrical Plug Connector Body
012290918
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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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