Ch-53a/d/e Helicopter Parts

(Page 64) End item NSN parts page 64 of 66
Part Number
NSN
NIIN
65380-03107-041 Aircraft Spool Assembly
000429814
65380-03108-101 Spool Support
000429818
65391-11664-102 Sediment Strainer Element
011265993
65391-11699-104 Sediment Strainer Element
011259074
65400-11123-041 Bell Crank
009389610
65402-02101-042 Canceller Assembly
009413407
65402-02131-043 Bracket Assembly
009413408
65403-02625-041 Toe Brake Lever Assembly
008941566
65403-02625-042 Toe Brake Lever Assembly
008941545
65407-05018-041 Load Cell Fork Assembly
004805963
65407-05037-101 Plate Spacer
004182649
65407-06007-041 Roller Guar Fitting
004722664
65407-06024-041 Towhook Centering Arm
004722666
65407-06081-101 Block Fitting
004722661
65407-10003 Cargo Guard Roller
004713627
65407-10003-041 Cargo Guard Roller
004713627
65410-03110-118 Recessed Washer
011248025
65414-03107-109 Limiter Assembly Stop
011293603
65415-11251-042 Bell Crank Support
011302806
65415-11401-044 Bell Crank Support
011302810
Page: 64

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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