Mh-53e Helicopter Parts

(Page 17) End item NSN parts page 17 of 238
Part Number
NSN
NIIN
010104.012 Lamp Ballast
014157902
010105163 Composition Fixed Resistor
001048374
010106 Ball Socket Seat
003835001
0101238-01 Webbing Strap
006329608
010164-009 Ceramic Dielectr Fixed Capacitor
008047566
0102-6-2 Pipe Reducer
008730110
0102-9001 Muffler- Protective Cap Assembly
004381551
0102164 Transistor
000681985
010235018 Film Fixed Resistor
004817871
010235121 Film Fixed Resistor
001514664
010235125 Film Fixed Resistor
004337039
0103-16-16 Pipe To Tube Straight Adapter
007182621
0103-20-20 Pipe To Tube Straight Adapter
002028470
0103-4-5C Pipe To Boss Straight Adapter
000013957
0103-8-6C Pipe To Tube Straight Adapter
000798814
0104-02-12 O-ring
002500221
0105037 Tapered Roller Cone And Rollers
006061841
0105082 Annular Ball Bearing
005545396
0105090 Annular Ball Bearing
001448519
01054 Film Fixed Resistor
002524003
Page: 17 ...

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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