Ch-53a/d/e Helicopter Parts

(Page 53) End item NSN parts page 53 of 66
Part Number
NSN
NIIN
64111-07303-102 Sleeve Bushing Half
004838490
64161-07026-101 Rudder Blade Root Fairing Cap
011351512
642007-1 Electron Tube Shield
001793148
64207-09043-101 Lock Pin Fitting
011396881
64207-09046-041 Platform Hinge Assembly
011396882
6434-2-6 Conductor Bus
005578906
64356-04049-102 Oil Monitor
011358830
64357-07022-102 Round Plain Nut
011481706
644594 Hexagon Plain Nut
008400530
6455-61243-105 Circuit Breaker
009418160
6465-62314-101 Solenoid Valve
004843760
647-2756-001 Electronic Components Assembly
011213795
647SP1 Composition Fixed Resistor
000619550
649311-000 Knob
005198056
65-0151-1 Indicator Light
009398609
65-3621-5 Electronic Shielding Gasket
009027407
6500C2 Watch Gauge Torque
008005361
65010-00100 Plate Spacer
001107194
650574-62 Electrical Conduit Coupling Nut
002803311
65072-15001-016 Helicopter Rotor Parts Kit
012155502
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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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