Ch-53a/d/e Helicopter Parts

End item NSN parts page 1 of 66
Part Number
NSN
NIIN
00-03005-022 Electrical Connector Backshell
014601701
00-05004-001 Motional Pickup Transducer
013853111
000-19663 Electrical Temperature Indicator
006033913
0017-0058 Light Transmitt Indicating Panel
011302959
0017-0076 Special Panel Assembly
013001603
0017-0084 Light Transmitt Indicating Panel
013060904
0017-0173 Light Transmitt Indicating Panel
011302954
002J-1-M-15-G006-12- Immersion Thermocouple
008699356
004-351-0 Aircraft Pneumatic Tire
009385964
008007-1 Electromagnetic Relay
010625154
009-1381-00 Vaneaxial Fan
005856016
009-1381-000 Vaneaxial Fan
005856016
009-1497-00 Vaneaxial Fan
005856016
0099517 Optoelectronic Display
010290612
01-91180-13 Indicator Light
014168427
0101238-01 Webbing Strap
006329608
010624-02 Blind Rivet
000051051
011074 Electromagnetic Relay
004825283
012-2876-00 Turnlock Fastener Stud
006804141
012-2876-000 Turnlock Fastener Stud
006804141
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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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