Mh-53e Helicopter Parts

(Page 110) End item NSN parts page 110 of 238
Part Number
NSN
NIIN
10125759 Blind Rivet
012311349
10125974-110 Electrical Conne Cover And Guard
013040457
10125974-111 Electrical Connector Cover
013044166
10125DAP Electrical-electron Mounting Pad
001400366
10125N Electrical-electron Mounting Pad
001400366
10127365 Induct Wire Wound Fixed Resistor
011170555
10127549 Film Fixed Resistor
011707738
10127618 Film Fixed Resistor
011772014
10127857 Film Fixed Resistor
012868945
10128125 Paper Dielectric Fixed Capacitor
008375109
10128136 Plastic Dielectr Fixed Capacitor
010174120
10128267 Ceramic Dielectr Fixed Capacitor
012485659
10128615 Incandescent Lamp
003724841
10128858 Electrical Conne Cover And Guard
013040457
10129112 Electrical Contact
010879279
10129220 Electrical Dummy Load
011450138
10129255 Cartridge Fuse
005774716
10129305 S Electrical Insulation Sleeving
000680790
10129325 Electrical Connector Jackscrew
012829858
10129329 Incandescent Lamp
008179803
Page: 110 ...

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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