Mh-53e Helicopter Parts

(Page 79) End item NSN parts page 79 of 238
Part Number
NSN
NIIN
10-305 Hexagon Head Cap Screw
002693240
10-33 Wire Rope Swaging Sleeve
001329163
10-349-2 Stud Terminal
000824890
10-350695-363 Electrical Connector Backshell
011839336
10-358860-1 Ignition Unit
000214946
10-36675-10S Electronic Shielding Gasket
005799513
10-386742 Hexagon Plain Nut
001768127
10-387650-1 Ignition Coil
001389494
10-40450-10S Electronic Shielding Gasket
005799513
10-40450-16S Electronic Shielding Gasket
007722223
10-40556 Electrical Contact
002593143
10-40557 Electrical Contact
004918194
10-407035-125 Electrical Contact
003780206
10-497015-133 Electrical Contact
001901887
10-504-2-03 Feedthru Terminal
007172907
10-51005 Hexagon Castellated Plain Nut
001671284
10-51643 Hexagon Castellated Plain Nut
005826058
10-52258-03 Blind Rivet
008828388
10-597817-351 Electrical Contact
008475535
10-601-2-05 Stud Terminal
000795760
Page: 79 ...

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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