Mh-53e Helicopter Parts

(Page 25) End item NSN parts page 25 of 238
Part Number
NSN
NIIN
018195 Wire Wound Fixed Resistor
004287487
01821211140002 Transistor
008280723
01828-00941 Electrical Insulation Sleeving
000631495
01845-1071 Tapered Roller Bearing Cup
001000359
01847-040 Hexagon Head Cap Screw
007813927
0187-3-4X1-2 Pipe Bushing
002783167
01877-3057 Pipe To Tube Tee
003190454
0188-2-3047 Wire Braid
005778452
01891852 Tapered Roller Cone And Rollers
006061841
019 771 Tapered Roller Cone And Rollers
007630259
019 772 Tapered Roller Cone And Rollers
009261379
019-00001-120 Drain Cock
002769041
019-00001-216 Matched Helical Gear Set
005918122
019-00001-354 Pipe Bushing
004956284
019-00001-374 Metal Tube Assembly
000202733
019-00001-375 Tube To Boss Straight Adapter
004466602
019-00001-54 Nonmetallic Hose
010252309
019-00003-9 Electrical Starter Engine Drive
010742030
019-00004-120 Drain Cock
002769041
019-00013-11 Tube To Boss Straight Adapter
009370229
Page: 25 ...

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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