Ch-53a/d/e Helicopter Parts

(Page 60) End item NSN parts page 60 of 66
Part Number
NSN
NIIN
65251-08219-041 Landing Gear Torque Arm Assembly
011266160
65251-08261-041 La End Cap Assembly
001598124
65254-02012-101 Boot Plug
000279144
65254-02037-041 Handle Assembly
010109706
65254-03014-101 Uplock Release Arm
000517893
65255-02022-101 Sealing Washer
008645783
65255-02038-101 Sleeve Bushing
009465318
65255-02102-103 Drag Strut Piston Housing
000580680
65257-07031-041 Tail Sk Bumper Assembly
004509972
65261-08015-041 Landing Gear Torque Arm Assembly
011266160
65261-08031-101 Liquid Quantity Indicator
011266232
65261-08064-101 Main Landing Gear Middle Cap
011266037
65265-02026-101 Landing Gear Axle
011507064
653-12003-101 Flange To Tube Straight Adapter
011232948
65301-01052-101 Lever Stop
011302832
65301-03078-102 Fuel Valve Roller
000609546
65301-03079-101 Fuel Valve Plate
000166050
65301-12048-041 Cockpit Controls Bracket
002258320
65302-12017-043 Strut Support Hinge
000279415
65302-12022-041 Strut Assemblyxpanel
009156648
Page: 60

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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