Mh-53e Helicopter Parts

(Page 219) End item NSN parts page 219 of 238
Part Number
NSN
NIIN
13156976-1 Magnetic Disk Cartridge
012818044
13160 Turnlock Fastener Receptacle
005054798
1317 Wire Braid
001918398
1318083 Tapered Roller Bearing Cup
001389994
1318084 Tapered Roller Cone And Rollers
001389993
13183-4 Nonwire Wound Variable Resistor
003595434
13183-7 Nonwire Wound Variable Resistor
001074881
131961-01 Transistor
006155186
131A3034 Light Lens
000801048
131A3049 Light Lens
008136642
131HA103 Tapered Roller Bearing Cup
001389994
132-92476 Reciprocating Compressor
013790752
1320 Lock Washer
006163554
13201 Pipe To Tube Elbow
002778269
13202 Pipe To Tube Straight Adapter
002891930
13202E0668-9 Light Lens
008136642
13205E3937-1 Pipe To Tube Straight Adapter
004418700
13205E4798 Liquid Quantity Indicator
009333600
13206E0449 Machine Bolt
002259087
13206E7432-46 Gate Valve
002689157
Page: 219 ...

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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