Mh-53e Helicopter Parts

(Page 156) End item NSN parts page 156 of 238
Part Number
NSN
NIIN
11-10-104Y Annular Ball Bearing
001448519
11-100-0250 Retaining Ring
008042026
11-106118 O-ring
005421586
11-10967-00 Diode Semiconductor Device
004654405
11-15369-00 U Semiconductor Device Rectifier
010705243
11-16477-00 Diode Semiconductor Device
009116104
010624733
11-238 O-ring
002913077
11-290-10-124 Metallic Shielded Cable Ferrule
005496220
11-300-C Nonmetallic Grommet
002764205
11-3757 Incandescent Lamp
009418488
11-38B Electrical Box Connector
007076229
11-50 Electrical Box Connector
005783666
11-55-68 Motor-tachometer Generator
010918181
11-590-990-00 Diode Semiconductor Device
001926262
11-591-930-00 Transistor
008405316
11-702 Electrical Plug Connector
000670032
11-9525 Electrical Power Cable
002448152
11-952S Electrical Power Cable
002448152
110-0005-039 Film Fixed Resistor
004267133
Page: 156 ...

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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