Ch-53a/d/e Helicopter Parts

(Page 33) End item NSN parts page 33 of 66
Part Number
NSN
NIIN
334-1028-010 Plate Self-locking Nut
010124966
3385013-1 Blower Casing
004941157
34025-1 Dee Ring
009903186
340286 Clamp Bolt Assembly
000561231
34102EDN01D310 Direct Current Motor
006290967
34102H-CA-01 Direct Current Motor
006290967
3415-156PC Retaining Ring
008129828
3458AS101 Marine Navigational Light
011258331
3461169 Circuit Breaker
009418160
347-314-008 Electron Tube
006059192
34U-SS216 Sleeve Bearing
008195532
35-18049Z6 Dust And Moistur Protective Plug
008041252
352-0393-00 Transistor
000882938
35235VN10 Tube Fitting Clinch Sleeve
006181183
353-045-003 Electromagnetic Relay
009994901
353-2025-00 Semiconductor Device Set
008091898
353-2025-000 Semiconductor Device Set
008091898
353-2025-010 Semiconductor Device Set
008091898
353-2952-00 Diode Semiconductor Device
000641424
353-2952-000 Diode Semiconductor Device
000641424
Page: 33 ...

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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