Mh-53e Helicopter Parts

(Page 131) End item NSN parts page 131 of 238
Part Number
NSN
NIIN
10394005 Electrical Connector Cover
013044166
10394251-001 Diode Semiconductor Device
008548470
103950 Tapered Roller Cone And Rollers
001000233
10396036 Tube To Boss Straight Adapter
011564835
10396462 Machine Screw
009846216
10396471 Hexagon Head Cap Screw
007813927
10396524 Drive Screw
002535605
10396625 Hexagon Plain Nut
008807745
10396856 Machine Screw
009585450
10398 Transistor
001798478
10398674 Machine Screw
006140246
10399 Electrical Plug Connector
010476312
10399094 Incandescent Lamp
002994742
10399263 Electrical Connector Backshell
012281812
10399531 Hexagon Self-locking Nut
009591488
10399803 Flat Washer
011453153
103A3462 Breather
006403774
103S101 Tapered Roller Cone And Rollers
001003541
103S102 Tapered Roller Bearing Cup
001000544
104-0045-049 Film Fixed Resistor
001855432
Page: 131 ...

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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