Mh-53e Helicopter Parts

(Page 47) End item NSN parts page 47 of 238
Part Number
NSN
NIIN
0550F5-254 Thermal Resistor
008270728
055242 Fluid Filter Element
002202417
0553-2029 Tube Coupling Inverted Nut
004346464
055DE18K Incandescent Lamp
001437432
0561C0029 Dust And Moisture Seal Boot
011415368
0568850 Radio Frequency Cable Assembly
000568850
057-616 Film Fixed Resistor
004267133
058-4 Annular Ball Bearing
002274521
058164-0502 Tube To Boss Straight Adapter
001257922
0584C28390-2 Pressure Switch
001212271
0584C28392-2 Di Compound Pressure-vacuum Gage
001326887
058526-01 Double Hexagon Self-locking Nut
000083696
059-20026-009 Mica Dielectric Fixed Capacitor
009268204
059-20027-004 Paper Dielectric Fixed Capacitor
001296260
059-20040-011 Electrolytic Fixed Capacitor
008790123
059609005 Radio Frequency Cable
008125034
05A111 Tapered Roller Cone And Rollers
001003541
05A112 Tapered Roller Cone And Rollers
006061841
05B0716G01 Connector Adapter
009514231
05C02484 Transistor
008149532
Page: 47 ...

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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