Mh-53e Helicopter Parts

(Page 163) End item NSN parts page 163 of 238
Part Number
NSN
NIIN
1113253 Electrical Engine Starter
011350091
1113253IMP Electrical Engine Starter
011350091
1113256 Electrical Engine Starter
011212577
1113277 Electrical Engine Starter
011924469
1113594 Electrical Engine Starter
011924469
11138-005 Electrical Special Purpose Cable
011033078
11141-0046 Non Wire Wound Variable Resistor
002717421
111417-12D-0350 Nonmetallic Hose Assembly
002298838
11142-130 Electrolytic Fixed Capacitor
011194323
1114223 Electrical Solenoid
008536024
11143-035 Electrolytic Fixed Capacitor
011194307
1114536 Electromagnetic Relay
007359542
111456-14 Glass Dielectric Fixed Capacitor
001317444
111460-01 Induct Wire Wound Fixed Resistor
010971613
1115082 Ignition Coil
003361702
1115087 Ignition Coil
003361702
11151-34 Pipe To Tube Elbow
002871766
1115161 Ignition Coil
003361702
1115182 Ignition Coil
003361702
11152 Pipe Bushing
002783167
Page: 163 ...

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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