Mh-53e Helicopter Parts

(Page 164) End item NSN parts page 164 of 238
Part Number
NSN
NIIN
1115202 Ignition Coil
003361702
111527 Metallic Hose Assembly
010199156
1115294 Ignition Coil
003361702
1115312 Nonmetallic Hose
005951089
11153149-1 S Electrical Insulation Sleeving
008283457
11153149-2 S Electrical Insulation Sleeving
009896238
11153149-3 Boot Protective
000049718
11153149-31 Boot Protective
000049718
11153257-21 Electrical Plug Connector
011077294
11153257-4 Electrical Plug Connector
011084485
11153883 Split Washer
008491984
1115405 Ignition Coil
003361702
1115407 Ignition Coil
003361702
11154550 Electrical Receptacle Connector
000516369
111564R91 Pressure Transmitter
009935546
11156744 Diode Semiconductor Device
008377065
11158-071 Plastic Dielectr Fixed Capacitor
006219456
1115836 Electromagnetic Relay
010389192
111598 Drain Cock
007204488
1116388 Engine Generator Regulator
011964882
Page: 164 ...

Helicopter, Mh-53e

Picture of Mh-53e 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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