Mh-53e Helicopter Parts

(Page 153) End item NSN parts page 153 of 238
Part Number
NSN
NIIN
10F50X-B Tube To Boss Straight Adapter
006233889
10F5BXS Tube To Boss Straight Adapter
006233889
10F5X-S Tube To Boss Straight Adapter
006233889
10F6XS Tube To Boss Straight Adapter
006233889
10H-J4 Glow Lamp
000142870
10HJ4 Glow Lamp
000142870
10KP192 Hexagon Head Cap Screw
007247219
10M200ZB2 Semiconductor Device Set
000876963
10M33Z5 Diode Semiconductor Device
004844605
10M4156 Test Lead
001751431
10M4161 Connector Adapter
000539454
10M56-1870 Film Fixed Resistor
004820732
10M56-8870 Film Fixed Resistor
003339543
10P1553 Incandescent Lamp
008362079
10P1701 Incandescent Lamp
008362079
10P49 Pipe To Tube Elbow
006401051
10R8V Fluid Filter Element
002871912
10SD2642 Fluid Passage Bolt
005167419
10SS-D15 Ceramic Dielectr Fixed Capacitor
011273762
10TCUT47 Ceramic Dielectr Fixed Capacitor
008215215
Page: 153 ...

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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