Mh-53e Helicopter Parts

(Page 42) End item NSN parts page 42 of 238
Part Number
NSN
NIIN
043960 Fluid Filter Element
001365066
044-233 Nonwire Wound Variable Resistor
005523480
044052D Electrical Contact
010242004
0441B0195 Turnlock Fastener Receptacle
005054798
0441B0210 Turnlock Fastener Receptacle
000369305
0442321 Pipe To Tube Straight Adapter
005402612
0442322 Pipe To Tube Straight Adapter
002784592
04440041-002 Transistor
004335809
0445370009 Transistor
004368953
044621 Stud Terminal
005390511
0448040000 Transistor
001072571
044828-2 Time Totalizing Meter
010051885
0451203228 Fluid Filter Element
012808419
045147 Breather
006403774
045434-01 Sediment Strainer Element
008936402
045523-0003 Electrical Receptacle Connector
008831977
04610002-009 Incandescent Lamp
009267603
046153-0001 Diode Semiconductor Device
008366667
046154-0001 Diode Semiconductor Device
008653448
046433 Push Switch
001118619
Page: 42 ...

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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