Mh-53e Helicopter Parts

(Page 29) End item NSN parts page 29 of 238
Part Number
NSN
NIIN
021.450505 Lock Washer
002240746
0210008-9 Tapered Roller Cone And Rollers
001003541
02100080 Transistor
009305325
0210009-7 Tapered Roller Bearing Cup
001000544
02105908-010 Tubeaxial Fan
000953831
02105908PC2 Tubeaxial Fan
000953831
0210723 Tapered Roller Bearing Cup
001000572
0211159 Tapered Roller Bearing Cup
001000542
0213-1-1074 Ferrule
008705350
021311-0001 Electrolytic Fixed Capacitor
011268439
02150-25 Hexagon Plain Nut
002686116
0215730 Incandescent Lamp
001558687
0219-0027-2 Electronic Tachometer
013789298
022-03836 Angle Valve
002894383
022061700 Annular Ball Bearing
001448631
0221 Electrical Box Connector
005783666
0225-0153 Ceramic Dielectr Fixed Capacitor
001139447
02261-0808 Hexagon Self-locking Nut
004780259
02263-0813 Alternator Assembly
001500038
022T-8-8 Pipe Tee
002635266
Page: 29 ...

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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