Ch-53a/d/e Helicopter Parts

(Page 45) End item NSN parts page 45 of 66
Part Number
NSN
NIIN
52-028-125-0937 Spring Pin
002347456
52-028-125-0938 Spring Pin
002347456
52-41682 Branched Wiring Harness
010624001
5213-08002-212 Sponson Assembly Fairing
012382473
522-8945-003 Cable Assembly
007047933
52511-230ADL Serrated Lock Ring
002184927
525148-2 Guide Pin Mount
008532926
528-4SS Tube To Hose Elbow
007280520
528907-6 Externally Relieved Body Screw
009489815
52B10726-3 End Chain Link
012560470
52LHA3022-02 Plate Self-locking Nut
005848164
5300320-1 Direct Current Motor
012405586
5301-03043-106 Quick Disconnect Coupling Half
000573072
53026-1 Cable Assembly
001248942
530311-1 Electrical Receptacle Connector
001089996
5305002642685 Shoulder Screw
002642685
531012-1 Electrical Clip
000651833
531021-681 Thermal Resistor
000411310
5315005769877 Headless Straight Pin
005769877
5315008561206 Spring Pin
005760599
Page: 45 ...

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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