Mh-53e Helicopter Parts

(Page 199) End item NSN parts page 199 of 238
Part Number
NSN
NIIN
124-3705 Fluid Filter Element
002871912
124-4322651 PC 104 Cotter Pin
002857161
124-4322652 PC 99 Cotter Pin
002857161
124-4365530 PC Cotter Pin
002857161
124-4365530 PC 31 Cotter Pin
002857161
124-4366739 PC 120 Cotter Pin
002857161
124-5589896 PC 95 Cotter Pin
002857161
124-5589897 PC 89 Cotter Pin
002857161
124-6293626 PC 96 Cotter Pin
002857161
124-6938645 PART 299 Hexagon Head Cap Screw
007247224
124-7121005 PC 59 Cotter Pin
002857161
124-7121006 PC 60 Cotter Pin
002857161
1240 Cable Strain Relief Bushing
001078198
1240-0154 Electrical Contact
010357465
124008B0144C305 Nonmetallic Hose Assembly
013991881
1240230H91 Engine Water Pump Parts Kit
012376299
124027-4CR0136 Tube Fitting Flared Sleeve
005552901
1240388H1 Fluid Filter Element
012808419
1240520H91 Engine Water Pump Parts Kit
012376299
Page: 199 ...

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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