Ch-53a/d/e Helicopter Parts

(Page 17) End item NSN parts page 17 of 66
Part Number
NSN
NIIN
15932 Airframe Ball Bearing
001060419
16 Externally Relieved Body Screw
007573235
160024-200 Governor Housing Assembly
001047381
1601-0619 Blind Rivet
000051051
16315 Voltmeter
007296723
1637705-184 Paper Dielectric Fixed Capacitor
004099324
163B2 Electrical Temperature Indicator
006033913
163B202D Electrical Temperature Indicator
006033913
163B2C Electrical Temperature Indicator
006033913
163B2D Electrical Temperature Indicator
006033913
163W0-2DCMA IAW 476-0257 Arbitrary Scale Meter
000257110
1650H37-007 Seal Retainer
000493732
16610171-006 Sleeve Spacer
001217871
169071 Transformer Assembly
004693093
1693-0619 Blind Rivet
000051051
16BS100C3 Valve Fitting
009639501
16BS100C5 Valve Ball
009639500
16D10 Regulator Plunger
000701730
172793 Aircraft Mounted Winch Cover
000299044
172B4344P1 Transf Tube Adapter
011851972
Page: 17 ...

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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