Mh-53e Helicopter Parts

(Page 169) End item NSN parts page 169 of 238
Part Number
NSN
NIIN
113-016-220 Electrical Wire
001819773
113-953ID1 Nonmetallic Hose
000670454
113-957ID1 Nonmetallic Hose
004509156
113-958 Nonmetallic Hose
002893306
113003 Nonmetallic Grommet
005432902
113003ADX Nonmetallic Grommet
005432902
113019 Nonmetallic Grommet
002766090
113019ADX Nonmetallic Grommet
002766090
113025 Nonmetallic Grommet
002708890
113033 Annular Ball Bearing
005165699
1130389G30 Electrical Insulation Sleeving
000523301
1130389G35 Electrical Insulation Sleeving
000523297
1130389G40 Electrical Insulation Sleeving
000896041
1130389G47 Electrical Insulation Sleeving
008222775
1130389G50 Electrical Insulation Sleeving
009596336
1130389G56 Electrical Insulation Sleeving
009441328
1130389G61 Electrical Insulation Sleeving
007816826
11304 Lug Terminal
001133142
113059-01 Nonmetallic Grommet
002764205
1130620G17 Turnlock Fastener Stud
000056302
Page: 169 ...

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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