Ch-53a/d/e Helicopter Parts

(Page 48) End item NSN parts page 48 of 66
Part Number
NSN
NIIN
549840-1 Power Transformer
000103005
54H19650 Aircraft Safety Belt
005166542
55-0912-5 Transistor
012157183
55-1037-1R0AJ01 Electrolytic Fixed Capacitor
012166385
55-38 Motor-tachometer Generator
009127345
550390 Solenoid Valve
009257511
554453PC4 Retaining Ring
002827127
55A0112-12-9 Electrical Wire
013164050
55A0112-14-9 Electrical Wire
013139878
55A0812-24-9 Electrical Wire
012004527
5611 Band Suppression Filter
012495906
56415400050 Flat Spring
004556792
5663 Unloading Sleeve
001017790
5666 Seal Plate
001017791
5669 Needle Roller Bearing
001027568
5670 Needle Roller Bearing
001018553
5673K70G700 Bearing And Pivot
008598607
5673K70G701 Bearing And Pivot S
008598703
5679 Cam Assembly Trunion
001017832
568-1-29942-000 Rotor And Shaft Assembl Impeller
009416376
Page: 48 ...

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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