Mh-53e Helicopter Parts

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Filter By: Tube To Hose Straight Adapters
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Part Number
NSN
NIIN
000-002-430 Tube To Hose Straight Adapter
010878886
000-8002-430 Tube To Hose Straight Adapter
010878886
05189294 Tube To Hose Straight Adapter
004462584
1-2 8-20630-1 Tube To Hose Straight Adapter
009520038
1-2 8-21230-1 Tube To Hose Straight Adapter
008843920
1-4-4-30682-4 Tube To Hose Straight Adapter
005551152
1/4-30682-4 Tube To Hose Straight Adapter
005551152
10004-404 Tube To Hose Straight Adapter
005551152
10004B404 Tube To Hose Straight Adapter
005551152
10004B604 Tube To Hose Straight Adapter
005551152
1000650 Tube To Hose Straight Adapter
010878886
10008B408 Tube To Hose Straight Adapter
005422807
1001277-0404 Tube To Hose Straight Adapter
010878886
1001277-1212 Tube To Hose Straight Adapter
008815536
1001277-16 Tube To Hose Straight Adapter
009291107
100534 Tube To Hose Straight Adapter
008815536
100798R91 Tube To Hose Straight Adapter
008815536
1008080-0000 Tube To Hose Straight Adapter
005422807
1008080-0808 Tube To Hose Straight Adapter
005422807
100958 Tube To Hose Straight Adapter
010878886
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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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