Ch-53a/d/e Helicopter Parts

(Page 52) End item NSN parts page 52 of 66
Part Number
NSN
NIIN
618733-117 O-ring
001051122
619006-7 Transistor
000976293
62002ZNJLT10 Annular Ball Bearing
005165318
62002ZNRJC3 Annular Ball Bearing
005165318
6200ZZNCE1BT2 Annular Ball Bearing
005165318
620482-3 Electrical Equipme Mounting Base
005646680
6214-2-3 Valve Disk
009092767
622937-2 Cursor Adjust Assem
001346210
62508 Electrical Contact Brush Holder
013162229
626-001-9119 Retaining Ring
008129828
6260 Hydraulic Mo Cylinder Block Unit
001362424
62988 Packing Retainer
012242336
62A5A43-9 Electrical Receptacle Connector
008401018
63-0505 Rotor And Shaft Assembl Impeller
009416376
63-0989 Semiconductor Devic
008741123
6316 Transformer Assembly
004693093
6324 Compression Helical Spring
011608053
632C6-12BR Insert
000235928
641-3549-001 Rotating Shaft Eye Bracket
011148426
64104-11045-105 Sleeve Spacer
011255299
Page: 52 ...

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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