Mh-53e Helicopter Parts

(Page 37) End item NSN parts page 37 of 238
Part Number
NSN
NIIN
034222-010 Incandescent Lamp
008015941
03541 Pipe Bushing
001930869
035580 Tapered Roller Cone And Rollers
001003541
035738-0003 Light Lens
000801048
0358-08 Metallic Shielded Cable Ferrule
005496220
035911 Headless Straight Pin
009391146
0360-0001 Lug Terminal
001567196
0360MTG9 Adjustable Resistor
002801609
036100052 Telephone Jack
001924789
0362-0129 Quick Disconnect Terminal
009489686
0362-0366 Quick Disconnect Terminal
009260085
0362972 Fluid Filter Element
002380033
037-0013-01 Incandescent Lamp
001680411
037-004400-001 Transmission Line Coupler
013438721
037-243 Diode Semiconductor Device
007285309
037-425 Electrolytic Fixed Capacitor
009593298
0370-1103 Knob
001780676
037422-0156 Electrical Receptacle Connector
001235821
037547021 Electrical Receptacle Connector
000683546
0377338 Nonwire Wound Variable Resistor
003595434
Page: 37 ...

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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