Mh-53e Helicopter Parts

(Page 188) End item NSN parts page 188 of 238
Part Number
NSN
NIIN
12-14F05C3W Electrical Connector Backshell
013041954
12-178-2890 Dust And Moisture Protective Cap
004878119
12-1850-57 Tube To Boss Straight Adapter
001257922
12-200010 Transistor
004368953
12-200030 Diode Semiconductor Device
004446607
12-260-72 Turnlock Fastener Receptacle
005054798
12-50 Electrical Box Connector
005783643
12-517-00-000 Hexagon Self-locking Nut
007029649
12-5X1500N275 V Belt
000815436
12-712114-71 Film Fixed Resistor
011659847
12-712123-71 Film Fixed Resistor
011771906
12-712138-30 Film Fixed Resistor
011845235
12-712146-41 Film Fixed Resistor
011772012
12-712156-22 Film Fixed Resistor
011877463
12-712182-51 Film Fixed Resistor
002739720
12-740-00-031 Turnlock Fastener Stud
005432418
12-749418-08 Plug-in Electronic Compon Socket
010689359
12-749425-03 Electromagnetic Relay
007873068
12-8 130140BA Pipe Bushing
002783167
12-910-00-100 Flat Washer
007215762
Page: 188 ...

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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