Ch-53a/d/e Helicopter Parts

(Page 35) End item NSN parts page 35 of 66
Part Number
NSN
NIIN
369D02 Pitot-static Tube
005267852
36D423478G1 Electrical End Bell
011663874
37-00211-9 Electrical Wire
013139878
37-00212-9 Electrical Wire
013164050
370-0078-030 Electrical Contact
012961056
370-2139-00 Electrical Receptacle Connector
000608066
370-2139-000 Electrical Receptacle Connector
000608066
37025 Plastic Dielectr Fixed Capacitor
012463493
371-18C Machine Screw
000336173
371-8395-010 Electrical Plug Connector
008280581
372-1959-00 Voltmeter
007296723
372-2601-763 Electrical Contact
012274475
372-2628-025 Electrical Plug Connector Body
004784004
3722-501 Fluid Filter Element
002202417
373MS041G001 Fastener Assembly
008295678
3755P3 Pickoff Rotor
009413471
3762-0215 Externally Relieved Body Screw
007573235
37AA-0112-12-9 Electrical Wire
013164050
37AA-0112-14-9 Electrical Wire
013139878
Page: 35 ...

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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