Ch-53a/d/e Helicopter Parts

(Page 37) End item NSN parts page 37 of 66
Part Number
NSN
NIIN
3M117-304 Blind Rivet
003251240
3M117-312 Blind Rivet
008357334
3S2791GB200AD26C Electromagnetic Relay
008508421
3SAE2062A2 Electromagnetic Relay
008508421
3VX450-3 V Belt
004319117
3WC1073-52 Aircraft Seat
006313415
4-00528-002 Plain Tapered Pin
001873218
40 Telephone Plug
000272390
40-0025-13 Aircraft Navigational Light
009533460
40-702-13 Connector Adapter
005390203
4004C5-5-10 Bearing Roller Set
006301293
400638-0029 Incandescent Lamp
013406497
4011SS Loop Clamp
005841550
4016567-14 Electrical Receptacle Connector
010783471
40196-3 Power Supply
001644217
4039-0000 Solid State Relay
004604476
40522 Transformer Assembly
004693093
41-0940-1 Lampholder
001027416
410-0520-010 Electromagnetic Relay
010326282
4115W12G701 Shim Set
004218427
Page: 37 ...

Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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