Ch-53a/d/e Helicopter Parts

(Page 22) End item NSN parts page 22 of 66
Part Number
NSN
NIIN
2088468-4 Diode Semiconductor Device
000507309
2095K22-103 Paper Dielectric Fixed Capacitor
004688352
2095K22P103 Paper Dielectric Fixed Capacitor
004688352
20AS111-1 Connector Adapter
005390203
21228 Bearing Ball Retainer
012239591
21466 Rupturable Disk
004854294
21650 Mounting
006776046
216723 Electrical Conduit Coupling Nut
002803311
218-37691-3 Time Delay
006135527
21929 Motor Governor
005778156
21C1536-110 Quick Disconnect Coupling Half
009226247
22-800B5 Resistance Element
005721372
220-28502-101 Track Roller Ball Bearing
010354338
220312 Receiver Synchro
005048273
2226074-5 Plain Bearing Unit
012298310
2226074-6 Plain Bearing Unit
012298311
22300160 Chronograph Spring
007992965
224-312 Blind Rivet
008357334
224286-001 Electrical Receptacle Connector
001089996
2262764 Electromagnetic Relay
010625154
Page: 22 ...

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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