Mh-53e Helicopter Parts

(Page 186) End item NSN parts page 186 of 238
Part Number
NSN
NIIN
119A2290-163 Electrical Insulation Sleeving
009441328
119A2290-165 Electrical Insulation Sleeving
007816826
119A2293-10 Electrical Wire
001288696
119B3-8 Nonmetallic Hose
002026927
119B3-8IN Nonmetallic Hose
002026927
11A Electrical Clip
007354393
11A13-S-41R Cotter Pin
002857161
11A8094 Fluid Passage Bolt
005167419
11A8617 Gasket
003589869
11A8887 Vent Valve
007264719
11AA1641 Clinch Self-locking Nut
006849765
11AF8A Lubrication Fitting
001720031
11B254121 Electrical Box Connector
005783643
11B254121-1 Electrical Box Connector
005783643
11BLH6 Fluid Passage Bolt
005167419
11BNC-50-7-2C Electrical Plug Connector
005778734
11BNC50-7-2C Electrical Plug Connector
005778734
11K10 Tube Elbow
001630236
11KP378 Machine Bolt
002264827
11KP842 Cotter Pin
002972444
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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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