Mh-53e Helicopter Parts

(Page 115) End item NSN parts page 115 of 238
Part Number
NSN
NIIN
10138322 Induct Wire Wound Fixed Resistor
011779465
10138448 Dust And Moisture Seal Boot
011315036
10138454 Wire Braid
001705274
10138625 Ceramic Dielectr Fixed Capacitor
012046063
10138679 Electrolytic Fixed Capacitor
011194332
10138693 Electrolytic Fixed Capacitor
012836890
10138734 Electrical Cap
010793462
10138805 Electrical Plug Connector
011907609
10138827 Electrical Plug Connector
006247660
10138880 Electrical Receptacle Connector
010559236
10138881 Electrical Receptacle Connector
010134473
10139364 Electrical-electron Mounting Pad
001400366
10139369 Electrical Contact
001901887
10139436 Electrical-electron Mounting Pad
010406371
10139485 Heat Sink-insulator
011220470
10139874 Wire Braid
001949841
10139884 Radio Frequency Cable
005422773
10139897 Electrical Wire
009686566
1014-0020 Electrolytic Fixed Capacitor
011196166
1014261D00 Pre Wire Wound Variable Resistor
012325593
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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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