Ch-53a/d/e Helicopter Parts

(Page 46) End item NSN parts page 46 of 66
Part Number
NSN
NIIN
531710-1 Electromagnetic Relay
001018569
531900-1 Transistor
001037410
532226-1 Electronic Shielding Gasket
001030432
532245-2 Diode Semiconductor Device
004974091
5331720 Ring
005331720
535733-1 Diode Semiconductor Device
004329264
5360008277077 Extension Helical Spring
008277077
537842 Receiver Synchro
005048273
538079-17 Induct Wire Wound Fixed Resistor
002617373
5380W10P002 Motor-tachometer Generator
010918181
5380W10P007 Motor-tachometer Generator
010918181
5388-01 Terminal Plate Assembly
009445746
5389-01 End Cover Assembly
009437869
539D10100 Seat Rubbing Strip
007805373
539D10100-5 Seat Rubbing Strip
007805373
53A106-1 Alternating Current Motor
008693353
53A556 Alternating Current Motor
008693353
54111-1 Fluid Filter
009480526
541615-1 Sleeve Bushing
009022291
54230031 Motor-tachometer Generator
009004143
Page: 46 ...

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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