Mh-53e Helicopter Parts

(Page 36) End item NSN parts page 36 of 238
Part Number
NSN
NIIN
0312225208 Fluid Filter Element
010585455
0314020 Cartridge Fuse
002809539
031634-3 Incandescent Lamp
009418488
031L7E Pipe To Tube Straight Adapter
002784574
031LTE Pipe To Tube Straight Adapter
002784574
032-00403-1 Retaining Ring
007815874
0325504 Tapered Roller Bearing Cup
001000380
03267650 Electrolytic Fixed Capacitor
008790123
033-3612 Power Supply
000547794
0330-0029 Electrical Cable Nipple
005031440
0332-0500 Pressure Switch
005034884
033278 Transistor
004826753
0333 5356 Hexagon Head Cap Screw
000712514
03348 Digital Display Indicator
010045648
0335138 Composition Fixed Resistor
001468423
033581-0003 Electrical Box Connector
002961669
033581-0004 Electrical Box Connector
002807763
0340-0164 Electrical-electron Mounting Pad
009089666
0340-0453 Electrical-electron Mounting Pad
011997462
0340-1130-01-0 Nonmetallic Hose
010748373
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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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