Ch-53a/d/e Helicopter Parts

(Page 50) End item NSN parts page 50 of 66
Part Number
NSN
NIIN
59/44-12-9 Electrical Wire
013164050
59/44-14-9 Electrical Wire
013139878
5900087-3 Vent Plug
000742617
5904044 Motor Stator
012395712
590528-3 Diode Semiconductor Device
003718400
592575-4 Conductor Splice
001772683
597324 Spur Gear
000106250
597325 Spur Gear
000106251
597986 Ceramic Diele Variable Capacitor
008796715
59917 Directional Con Sleeve And Slide
008383420
5L4541-004-19 Electrical Receptacle Connector
006606189
5LV4541-004-19 Electrical Receptacle Connector
006606189
5M948E12-10PSR Electrical Plug Connector
001652514
5S7-5 Turnlock Fastener Stud
006527289
5S7-6 Turnlock Fastener Stud
006804141
5T848 Transformer Assembly
004693093
6-40NF3X5-16LG Socket Head Cap Screw
002862083
6-40UNF3X5-16 Socket Head Cap Screw
002862083
6-535512-2 Electrical Receptacle Connector
010783471
6-85930-4 Electrical Receptacle Connector
010783471
Page: 50 ...

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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