Mh-53e Helicopter Parts

(Page 134) End item NSN parts page 134 of 238
Part Number
NSN
NIIN
1046Z-247 Fluid Filter Element
010256853
1046Z247 Fluid Filter Element
010256853
1046Z467 Fluid Filter Element
011229517
1047096DC Cable Strain Relief Bushing
003516114
10472 Pipe To Tube Straight Adapter
005402612
104721 Nonwire Wound Variable Resistor
004812010
1047253-1 Shim
003332699
1047277-2 Annular Ball Bearing
006792598
1047293 Transmitter Synchro
005046032
10475-10 Tube Coupling Nut
000114627
10476-103 Quick Disconnect Terminal
009260085
10476-14 Pipe To Tube Straight Adapter
002784575
1047634P1 Diode Semiconductor Device
007613857
104790 Fluid Filter Element
002871912
1047909-1 Multiple Electron Tube Shield
008070273
1048-4-4S Tube To Boss Elbow
005852309
1048-8-6 Tube To Boss Elbow
008525581
1048G4 Cable Assembly
010554844
1049-050 Machine Screw
005432753
104917 Bearing Ball
001006150
Page: 134 ...

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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