Ch-53a/d/e Helicopter Parts

(Page 18) End item NSN parts page 18 of 66
Part Number
NSN
NIIN
173438-901 Jewel Assembly
004693459
175-7008SS Plain Tapered Pin
001873218
17541-3 Electrical Connector Cable Clamp
004440249
17541-3-ZZ Electrical Connector Cable Clamp
004440249
176448 Annular Ball Bearing
000943418
176497 Cylindrical Roller Bearing
000974461
176512 Ball Retainer
001573750
176521 Winch Brake Cover
000299034
176530 Bearing Retaining Plate
001737550
176532 Winch Assembly Cover Bracket
000299051
176556 Sleeve Bushing
001590934
176558 Sleeve Bushing
001639361
177642 Annular Ball Bearing
001677914
177870-001 Indicator Base
009257636
177871-901 Plate Assembly
009257617
178356 Friction Lining
001622925
178C4115-P3 Externally Relieved Body Screw
012789001
1790-1030G1 Seat-crystal
000906903
1794AS1030 Rotary Switch
013739822
179678-1 Solid State Relay
004604476
Page: 18 ...

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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