Mh-53e Helicopter Parts

(Page 231) End item NSN parts page 231 of 238
Part Number
NSN
NIIN
137031P90 Electrolytic Fixed Capacitor
009593300
13705E-048 Plate Self-locking Nut
007796689
1371 Connector Adapter
007167124
137104-8 Incandescent Lamp
000190878
137111PCM287 Lubrication Fitting
000481788
137137 Cotter Pin
000137137
137147 Fluid Filter Element
002380033
13715-02 Plate Self-locking Nut
007793601
137159-1 Clinch Self-locking Nut
009349973
13715E-62BC Plate Self-locking Nut
007789186
1371A Connector Adapter
007167124
137218 Cotter Pin
008499857
137228 Cotter Pin
000137228
13723 Plug-in Electronic Compon Socket
002323758
137244 Cotter Pin
002004545
137396 Tube Coupling Inverted Nut
002889390
137397 Tube Coupling Inverted Nut
000137397
137404 Pipe To Tube Straight Adapter
002891930
137405 Pipe To Tube Straight Adapter
005402612
137406 Pipe To Tube Straight Adapter
002784592
Page: 231 ...

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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