Ch-53a/d/e Helicopter Parts

(Page 9) End item NSN parts page 9 of 66
Part Number
NSN
NIIN
10M200ZB2 Semiconductor Device Set
000876963
11-0499-1 Reflector
006235969
11-10008 Fluid Filter
000573834
11-11668-102 Fluid Filter
010264033
11-12057 Fluid Filter
000573834
11-138 O-ring
008006353
11-55-68 Motor-tachometer Generator
010918181
11-750-00-850 Diode Semiconductor Device
000113581
110-098-1C Tube To Boss Tee
007571945
110003-1 Cable Assembly
001248942
110541 Electronic Shielding Gasket
001030432
1105445-9 Diode Semiconductor Device
008560083
110552-01 Electrical Equipme Mounting Base
005646680
11059-1 Switch Actuator Arm
008246026
110700-1 Annular Ball Bearing
010159709
11072354 Electromagnetic Relay
009994901
1107W63 Aircraft Hydraulic Swivel Joint
009446704
1107W63-4 Aircraft Hydraulic Swivel Joint
009446704
11154559-8 Electrical Plug Connector
001392380
1118050-1 Generator Parts Kit
000730994
Page: 9 ...

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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