Mh-53e Helicopter Parts

(Page 63) End item NSN parts page 63 of 238
Part Number
NSN
NIIN
0812-0074 Induct Wire Wound Fixed Resistor
009847704
0813-0050 Induct Wire Wound Fixed Resistor
000805899
081443-1 Tubeaxial Fan
002265872
0819-0019 Nonind Wire Wound Fixed Resistor
006421672
0822 011 23002 Electrical Insulation Sleeving
009038733
0826520 Diode Semiconductor Device
004218882
0826V030 Hexagon Head Cap Screw
002258507
0831040X5R0 471K Ceramic Dielectr Fixed Capacitor
008215215
0831040X5R0 471M Ceramic Dielectr Fixed Capacitor
008215215
0831SPN Electrical Plug Connector
005005183
084-10115-061 Transistor
009129008
084-20115-051 Transistor
009478263
084-20115-060 Transistor
009373768
084-20115-061 Transistor
009129008
084-20115-155 Transistor
001065179
084098 Push Switch
001118619
08484-60001 Radio Frequency Amplifier
012308661
08484-60031 Radio Frequency Amplifier
012308661
085100060 Plug-in Electronic Compon Socket
002229828
08551-5070 Electrical Dummy Load
008139111
Page: 63 ...

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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