Ch-53a/d/e Helicopter Parts

(Page 24) End item NSN parts page 24 of 66
Part Number
NSN
NIIN
239B0006-1 Cable Assembly
001096133
23P106-3 Electrical Plug Connector
012757271
24-SJ-12X12 Pipe Coupling
011965217
241-0775-010 Band Suppression Filter
012495906
2440032-8 Electrical Plug Connector
000639010
24466-8 Needle Roller Bearing
002272980
2447443-1 Annular Ball Bearing
010159709
2465-010-W5T0-102P Ceramic Dielectr Fixed Capacitor
008841653
2465-010W5T0102P Ceramic Dielectr Fixed Capacitor
008841653
2465-019-X7T0-102P Ceramic Dielectr Fixed Capacitor
008841653
2470264 Ring
005331720
2482-009-W5R0-501M Ceramic Dielectr Fixed Capacitor
001132462
2482-009W5R0-501M Ceramic Dielectr Fixed Capacitor
001132462
2482-022-W5R0-501M Ceramic Dielectr Fixed Capacitor
001132462
2487-1 Capacitor-resistor
001538462
24SJ-12 Pipe Coupling
011965217
25-0929-173 Light Transmitt Indicating Panel
011683167
25-0929-265 Light Transmitt Indicating Panel
011690191
25-0929-311 Light Transmitt Indicating Panel
011687772
2504-600 Electric Temperature Transmitter
012196319
Page: 24 ...

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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