Mh-53e Helicopter Parts

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Filter By: Electrical Connector Backshells
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Part Number
NSN
NIIN
013-004-001 Electrical Connector Backshell
012451950
076-006392-002 Electrical Connector Backshell
010144920
10-350695-363 Electrical Connector Backshell
011839336
1003293-05 Electrical Connector Backshell
010144920
10163553 Electrical Connector Backshell
011865611
10399263 Electrical Connector Backshell
012281812
1134662G1 Electrical Connector Backshell
007555793
12-14F05C3W Electrical Connector Backshell
013041954
1576AS667-10 Electrical Connector Backshell
014333235
1576AS940-2 Electrical Connector Backshell
013777601
1576AS940-3 Electrical Connector Backshell
013779551
165133P1 Electrical Connector Backshell
007555793
201M108-19-G Electrical Connector Backshell
011935995
201M114-19-A Electrical Connector Backshell
011842810
201M114-19A Electrical Connector Backshell
011842810
201M120-19B Electrical Connector Backshell
012281812
206138 Electrical Connector Backshell
010144920
206138-1 Electrical Connector Backshell
010144920
20745-8 Electrical Connector Backshell
007555793
229512B11W Electrical Connector Backshell
011527020
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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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