Mh-53e Helicopter Parts

(Page 48) End item NSN parts page 48 of 238
Part Number
NSN
NIIN
05D00007 Transistor
001629773
06-01-30-651 Transistor
001065179
06-11-0214-01 Packing Retainer
005437089
06-25 Annular Ball Bearing
005545396
06-282-20C020 Sleeve Bearing
003219243
06-463-106 Directional Control Linear Valve
014357705
06-50 Digital Display Indicator
010034223
06-L50-X1058B Digital Display Indicator
010034223
06-L50-X2424 Digital Display Indicator
010034223
060-03905-063 Composition Fixed Resistor
002521050
060-086 Incandescent Lamp
005426571
060-382 Incandescent Lamp
001680411
0600700 Tapered Roller Cone And Rollers
001003541
0600800 Tapered Roller Bearing Cup
001000544
0601-0350-0002 Air Duct Hose
005641413
060115B Tube-hose Fit Compression Sleeve
011937390
0601B0003-4 Spring Tension Washer
009542353
060202BA4-2 Pipe To Tube Elbow
002871766
0603-6-4 Tube Reducer
007068711
0604-6 Drain Cock
002769041
Page: 48 ...

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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