Mh-53e Helicopter Parts

(Page 13) End item NSN parts page 13 of 238
Part Number
NSN
NIIN
0074452-4 Incandescent Lamp
000193093
007614631 Diode Semiconductor Device
007614631
00762-F-8 Pipe To Tube Elbow
002216215
00763414 Electrical Receptacle Connector
002593329
007813927 Hexagon Head Cap Screw
007813927
007887764 Fluid Filter Element
000748627
007890384 Cam Actuated Fuel Pump
009081269
007K0078-01 Transistor
009373768
007K5011-00 Diode Semiconductor Device
009042020
007K6017-00 Diode Semiconductor Device
009124907
007K6045-00 Diode Semiconductor Device
004654405
008 O-ring
005805937
008-90004-40 Lubrication Fitting
001720031
008001-3 Electrical Connector Cover
000042054
00801-2372 Fluid Passage Bolt
005167419
008457T Vent Valve
007264719
00871-2297-0001 Transistor
001041402
009-00473-9 Electrical Connec Polarizing Key
009989281
009-1627-00 Vaneaxial Fan
000431981
009-1627-000 Vaneaxial Fan
000431981
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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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