Mh-53e Helicopter Parts

(Page 209) End item NSN parts page 209 of 238
Part Number
NSN
NIIN
1299116+58 Diode Semiconductor Device
008469125
1299116-58 Diode Semiconductor Device
008469125
12BTX-S Tube Coupling Nut
008120924
12BTXS Tube Coupling Nut
008120924
12BUS Tube Coupling Nut
004602086
12C5-12RFJX Tube To Hose Straight Adapter
008815536
12C5BX-S-VITON Tube To Boss Elbow
010117736
12C5BXS Tube To Boss Elbow
010117736
12C5XS Tube To Boss Elbow
010117736
12ED2000 Composition Fixed Resistor
001468423
12F01270 Film Fixed Resistor
000046116
12F01820 Film Fixed Resistor
011771905
12F02370 Film Fixed Resistor
011771906
12F04640 Film Fixed Resistor
011772012
12F07680 Film Fixed Resistor
012001077
12F08660 Film Fixed Resistor
000052698
12F09760 Film Fixed Resistor
011850065
12F11820 Film Fixed Resistor
011751520
12F14640 Film Fixed Resistor
011850065
12F18250 Film Fixed Resistor
011069005
Page: 209 ...

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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