Mh-53e Helicopter Parts

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Filter By: Pipe To Tube Straight Adapters
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Part Number
NSN
NIIN
00205-0246 Pipe To Tube Straight Adapter
004418700
002177T Pipe To Tube Straight Adapter
005402612
00646210 Pipe To Tube Straight Adapter
007182621
007-59-F-3 Pipe To Tube Straight Adapter
005402612
0103-16-16 Pipe To Tube Straight Adapter
007182621
0103-20-20 Pipe To Tube Straight Adapter
002028470
0103-8-6C Pipe To Tube Straight Adapter
000798814
031L7E Pipe To Tube Straight Adapter
002784574
031LTE Pipe To Tube Straight Adapter
002784574
0431537 Pipe To Tube Straight Adapter
002891930
0442321 Pipe To Tube Straight Adapter
005402612
0442322 Pipe To Tube Straight Adapter
002784592
07-59F2 Pipe To Tube Straight Adapter
002891930
07-59F3 Pipe To Tube Straight Adapter
005402612
07-620564 Pipe To Tube Straight Adapter
005402612
07-851618 Pipe To Tube Straight Adapter
005402612
0910943-0 Pipe To Tube Straight Adapter
002784574
0913535 Pipe To Tube Straight Adapter
005402612
0913535-1 Pipe To Tube Straight Adapter
005402612
09136664-9 Pipe To Tube Straight Adapter
002891930
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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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