Ch-53a/d/e Helicopter Parts

(Page 25) End item NSN parts page 25 of 66
Part Number
NSN
NIIN
2504629-135 Electrical-electron Mounting Pad
009166189
251027-1 Aircraft Seat Cushion
011742000
251070-901 Bushing Assembly
004693431
25154236 Pressure Switch
011496864
2515546 Motional Pickup Transducer
004750284
251M15G6-12 Immersion Thermocouple
008699356
2561-180517-07103 Electrical Connector Backshell
012451950
257625-F2C Rotary Switch
009273483
2578884 Hexagon Slotted Plain Nut
001768102
2578885 Hexagon Slotted Plain Nut
001768100
258-2950 Electrical Conduit Coupling Nut
002803311
2587911 V Belt
004319117
259-2942-010 Rotary Switch
012758106
25A4 Thermal Resistor
000188965
26-50 Delay Line
009463855
260-290-1 Piston Housing
013273064
26029763 Diode Semiconductor Device
010266123
2603W70P001 Electrical Receptacle Connector
010783471
2603W90P001 Electrical Receptacle Connector
010783471
26076-1 Diode Semiconductor Device
007344620
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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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