Ch-53a/d/e Helicopter Parts

(Page 8) End item NSN parts page 8 of 66
Part Number
NSN
NIIN
10646-0-6 Time Delay
006135527
1064868G2 Cartridge Fuse
000454211
10658187 Electromagnetic Relay
002581780
106A0001-2 Electromagnetic Relay
008660803
106D5008-1 Indicator Panel
007771704
107026-9 Flat Washer
006328939
1075394-7 Plastic Dielectr Fixed Capacitor
012602205
10772 Sleeve Bearing
008195532
108 Voltmeter
007296723
1081H37H36 Thermal Resistor
004438864
10855 Plain Tapered Pin
001873218
10876 Governor Housing Assembly
001047381
10886307 Extension Helical Spring
008277077
10921647 Retaining Ring
008129828
109250-1 Electric Motor Cover
012178825
1092683P5 Machine Screw
000388558
109605-5 Flat Washer
006328939
109608-2 Turnlock Fastener Stud
006804141
109608-3 Turnlock Fastener Stud
006527289
10A200B2 Semiconductor Device Set
000876963
Page: 8 ...

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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