Ch-53a/d/e Helicopter Parts

(Page 28) End item NSN parts page 28 of 66
Part Number
NSN
NIIN
2B30-1A Current Transformer
009413184
2DHT50T800J Ceramic Dielectr Fixed Capacitor
009426766
2E122-106A Plastic Dielectr Fixed Capacitor
012463493
2J1M13G6-12 Immersion Thermocouple
008699356
2J1M13G6-7 Immersion Thermocouple
008699356
2J1M15G6-12 Immersion Thermocouple
008699356
2K4128-2 Electromagnetic Relay
004825283
2L509-E06-04 Pin-rivet
006372552
2LS509-T06-12 Pin-rivet
002057869
2LS509-T08-09 Pin-rivet
006164773
2N1167A Transistor
000458619
2N1285 Transistor
008091870
2N2228 Transistor
009249611
2N2229 Transistor
009249611
2N4137 Transistor
000976293
2N4429 Transistor
009989314
2N4429A Transistor
009989314
2N540A Transistor
005819888
2N550 Transistor
000882938
2VC1085-12 Aircraft Seat
000653215
Page: 28 ...

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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