Ch-53a/d/e Helicopter Parts

End item NSN parts
Filter By: Sleeve Bearings
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Part Number
NSN
NIIN
06-282-20C020 Sleeve Bearing
003219243
10056040 Sleeve Bearing
008195532
103-0109-020 Sleeve Bearing
013548269
10772 Sleeve Bearing
008195532
117-21-20-020 Sleeve Bearing
003219243
122-2020C020 Sleeve Bearing
003219243
124-1553927 Sleeve Bearing
006861011
124-1553927 PART NO. 96 Sleeve Bearing
006861011
124-1553929 PART NO. 35 Sleeve Bearing
006861011
12Z10003-366 Sleeve Bearing
006861011
14312-13 Sleeve Bearing
014215392
14312-14 Sleeve Bearing
014215393
1560CH37-253-3 Sleeve Bearing
007872420
309-0804-00 Sleeve Bearing
008195532
309-0804-000 Sleeve Bearing
008195532
3120-686-1011 Sleeve Bearing
006861011
3120006861011 Sleeve Bearing
006861011
34U-SS216 Sleeve Bearing
008195532
65362-05021-102 Sleeve Bearing
010077690
8L1FF Sleeve Bearing
008195532
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Helicopter, Ch-53a/d/e

Picture of Ch-53a/d/e 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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