Mh-53e Helicopter Parts

(Page 109) End item NSN parts page 109 of 238
Part Number
NSN
NIIN
10124972 Machine Screw
000889158
10124980 Machine Screw
000943430
10125010 Machine Screw
001515795
10125041 Machine Screw
001829411
10125069 Machine Screw
002349629
10125070 Socket Head Cap Screw
002359883
10125277 Machine Screw
004033502
10125282 Machine Screw
004110681
10125294 Machine Screw
004388682
10125306 Machine Screw
004552507
10125307 Machine Screw
004552508
10125312 Machine Screw
004591147
10125361 Electr Receptacle Connector Body
002261743
101254301FC1 Film Fixed Resistor
002084786
10125431 Instrument Screw
006937770
10125447 Setscrew
007245813
10125487 Machine Screw
007808456
10125488 Machine Screw
007815662
10125494 Socket Head Cap Screw
007885487
10125514 Machine Screw
008132791
Page: 109 ...

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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