Mh-53e Helicopter Parts

(Page 189) End item NSN parts page 189 of 238
Part Number
NSN
NIIN
12-Z-7001-2422 Lug Terminal
002430409
12-Z-7001-2507 Lug Terminal
001152678
12-Z-7001-2512 Lug Terminal
001150775
12-Z-7001-2513 Lug Terminal
001150776
120 Electrical Plug Connector
000164054
120-075-1 Plug-in Electronic Compon Socket
003911930
120-199 Plug-in Electronic Compon Socket
002229828
120-25 Plug-in Electronic Compon Socket
002229828
120-70E500 Non Wire Wound Variable Resistor
010489167
120-AA Pipe Coupling
004153172
1200-0019 Plug-in Electronic Compon Socket
002229828
1200-0473 Plug-in Electronic Compon Socket
004814141
1200-9STCD Retaining Ring
000813470
120014 Thrust Roller Bearing
001170763
12003578 Turnlock Fastener Stud
002828132
120050-1-10PCT3W Induct Wire Wound Fixed Resistor
000455422
120050-10-5PCT Induct Wire Wound Fixed Resistor
000455422
12007167 Standoff Insulator
001421840
1200A-4 Stud Terminal
000824890
1200S27-10 Induct Wire Wound Fixed Resistor
009936985
Page: 189 ...

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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