Ch-53a/d/e Helicopter Parts

(Page 26) End item NSN parts page 26 of 66
Part Number
NSN
NIIN
261177 Packing Retainer
011174238
261832-145 Hi-set Marker
004693435
261836-901 Actuator Hub Assembly
004693436
261865-901 Gear Assembly
004693440
261867-001 Indica Switch Wiper
004693441
261893-901 Plate Assembly
004693437
261915 Pointer Assembly
004725177
261953-167 Meter Panel
007165248
262657-1 Electrical-electron Mounting Pad
009166189
2633157 Refueling Valve Adapter
001183602
264-0812-000 Cartridge Fuse
009994861
2640W10-004 Electr Receptacle Connector Body
004687447
2643206-3 Wire Rope Swaging Sleeve
011325671
265056-901 Bracket Assembly
007165246
2667567-1 Electrical Plug Connector
000639010
269-2158-000 Rotary Switch Section
000342340
269-2159-00 Rotary Switch Section
000342338
269-2159-000 Rotary Switch Section
000342338
26927 Electromagnetic Relay
002581780
26SM12AE Electromagnetic Relay
000594814
Page: 26 ...

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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