Mh-53e Helicopter Parts

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Filter By: Tube To Boss Straight Adapters
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Part Number
NSN
NIIN
019-00001-375 Tube To Boss Straight Adapter
004466602
019-00013-11 Tube To Boss Straight Adapter
009370229
058164-0502 Tube To Boss Straight Adapter
001257922
1-01264D6 Tube To Boss Straight Adapter
002776836
10-1948-28 Tube To Boss Straight Adapter
001257922
10178917 Tube To Boss Straight Adapter
002776836
102-0322 Tube To Boss Straight Adapter
002266772
10396036 Tube To Boss Straight Adapter
011564835
10503869 Tube To Boss Straight Adapter
011564835
10503899 Tube To Boss Straight Adapter
002266772
107A-0114 Tube To Boss Straight Adapter
011564835
107A114 Tube To Boss Straight Adapter
011564835
10F50X-B Tube To Boss Straight Adapter
006233889
10F5BXS Tube To Boss Straight Adapter
006233889
10F5X-S Tube To Boss Straight Adapter
006233889
10F6XS Tube To Boss Straight Adapter
006233889
12-1850-57 Tube To Boss Straight Adapter
001257922
16109583 Tube To Boss Straight Adapter
010199815
16541 Tube To Boss Straight Adapter
011564835
1834303PC4 Tube To Boss Straight Adapter
006233889
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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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