Mh-53e Helicopter Parts

(Page 50) End item NSN parts page 50 of 238
Part Number
NSN
NIIN
0627885 Transistor
010169906
063-74695-203 Electrical Power Cable
002950851
0632707 Intake Air Cleane Filter Element
008421878
0632707-6 Intake Air Cleane Filter Element
008421878
063274629 Electron Tube
000824139
0635-11 Incandescent Lamp
009273180
0635-19 Incandescent Lamp
000802012
0635-2 Incandescent Lamp
005426571
063T-4-4 Tube Tee
006185382
064302010 Diode Semiconductor Device
005430490
0647809 Fluid Filter Element
000748627
064792-2 Dust And Moisture Protective Cap
004878119
0647996 Annular Ball Bearing
005555210
0647996-8 Annular Ball Bearing
005555210
065-001756-012 Electrical Insulation Sleeving
009441328
065-001756-013 Electrical Insulation Sleeving
007816826
065-001756-024 Electrical Insulation Sleeving
008222775
065-001756-048 Electrical Insulation Sleeving
000523301
065-001756-049 Electrical Insulation Sleeving
000523297
065-001756-050 Electrical Insulation Sleeving
000896041
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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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