Ch-53a/d/e Helicopter Parts

(Page 43) End item NSN parts page 43 of 66
Part Number
NSN
NIIN
5000X12 Pipe Coupling
011965217
5001696 Brake Backing Plate
001713498
50020-1 Electrical Equipment Rack
000639358
50020-1A Electrical Equipment Rack
000639358
50031642 Hexagon Self-locking Nut
007272809
50031763 Electromagnetic Relay
002581780
500403-4 Retaining Ring
002827127
500702-2595 Vaneaxial Fan
003361728
501344-1 Printed Circuit Board Holder
009841988
501D687M025PR Electrolytic Fixed Capacitor
011275576
502-2-62-431 Hose Clamp
009885290
503-4 Voltmeter
007296723
503-8 Needle Roller Bearing
002272980
503-8785-003 Arbitrary Scale Meter
000257110
504-7576-002 Hub Clamp
003229929
50400 Quick Release Pin
009280275
50401-14S Electrical Receptacle Connector
008401018
505-4369-004 Shock Electro Mount
000245391
505-9342-003 Electrical Dummy Load
005630342
5055109-1 Electrical Box Connector
011318057
Page: 43 ...

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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