Mh-53e Helicopter Parts

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Filter By: Pipe To Boss Straight Adapters
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Part Number
NSN
NIIN
000-8006-353 Pipe To Boss Straight Adapter
010422960
0103-4-5C Pipe To Boss Straight Adapter
000013957
0136-13 Pipe To Boss Straight Adapter
001869495
0164-10 Pipe To Boss Straight Adapter
001969580
100564 Pipe To Boss Straight Adapter
011883184
10164-10 Pipe To Boss Straight Adapter
001969580
105P8 Pipe To Boss Straight Adapter
001969580
10639256-1 Pipe To Boss Straight Adapter
011883184
107A-942 Pipe To Boss Straight Adapter
011883184
15-58469 Pipe To Boss Straight Adapter
001969581
15145-1 Pipe To Boss Straight Adapter
001870844
2021-4-5C Pipe To Boss Straight Adapter
000013957
213692-6D Pipe To Boss Straight Adapter
001969580
213692-8D Pipe To Boss Straight Adapter
001969581
213706-9D Pipe To Boss Straight Adapter
001869495
2216-8-125 Pipe To Boss Straight Adapter
011883184
2216-8-12S Pipe To Boss Straight Adapter
011883184
3101259 Pipe To Boss Straight Adapter
002405904
3112151 Pipe To Boss Straight Adapter
001969581
33211AX Pipe To Boss Straight Adapter
010422960
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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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