Ch-53a/d/e Helicopter Parts

(Page 3) End item NSN parts page 3 of 66
Part Number
NSN
NIIN
006847795
046008-01 Fluid Filter
000573834
048853-2 Electrical Conductor Bushing
010907990
050-128-0000220 Electrical Plug Connector
000639010
050-266 Hexagon Plain Nut
008400530
05004-0009 Retaining Ring
002827127
0550F5-254 Thermal Resistor
008270728
055242 Fluid Filter Element
002202417
0568850 Radio Frequency Cable Assembly
000568850
06-140 Flat Washer
006328939
06-282-20C020 Sleeve Bearing
003219243
0619-1601 Blind Rivet
000051051
0659050182 Electrical Conduit Coupling Nut
002803311
071-45825 Fluid Filter Element
002202417
07A054-10HP Tube Fitting Clinch Sleeve
006181183
07D03 Regu Diaphragm Assembly
004491445
08TGSM1242 Motor-tachometer Generator
009127345
08TGSM1242-1 Motor-tachometer Generator
009127345
09-00733 Cable Assembly
013145651
095-9031-0103 Electrical Receptacle Connector
001187339
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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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