Mh-53e Helicopter Parts

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Filter By: Pipe To Hose Straight Adapters
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Part Number
NSN
NIIN
10874976 Pipe To Hose Straight Adapter
007225194
12-12 160143CA Pipe To Hose Straight Adapter
005682200
13620P11 Pipe To Hose Straight Adapter
002258596
141-16612 Pipe To Hose Straight Adapter
005682200
16-16 160143C Pipe To Hose Straight Adapter
002258596
171SB0286000 Pipe To Hose Straight Adapter
007225194
171SB286 Pipe To Hose Straight Adapter
007225194
171SL785 Pipe To Hose Straight Adapter
002258596
19159P11 Pipe To Hose Straight Adapter
005682200
1947217-3 Pipe To Hose Straight Adapter
007225194
20130-16-16 Pipe To Hose Straight Adapter
002258596
212-2012-62 Pipe To Hose Straight Adapter
007225194
220-3 Pipe To Hose Straight Adapter
007225194
244326 R91 Pipe To Hose Straight Adapter
007225194
30182-4-6B Pipe To Hose Straight Adapter
007225194
327-12-12S Pipe To Hose Straight Adapter
005682200
327-16 Pipe To Hose Straight Adapter
002258596
327-16-16 Pipe To Hose Straight Adapter
002258596
42516N116 Pipe To Hose Straight Adapter
002258596
453-0003-2 Pipe To Hose Straight Adapter
007225194
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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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