Mh-53e Helicopter Parts

End item NSN parts
Filter By: Rod End Ball Bearings
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Part Number
NSN
NIIN
ABR4M-1009W Rod End Ball Bearing
012295251
ABR4M-1009W(L) Rod End Ball Bearing
012295251
ABR4M-1009W(P) Rod End Ball Bearing
012295251
ABR4M-100W(P) Rod End Ball Bearing
012295251
ABR4M-8G Rod End Ball Bearing
007272694
ABR4M-8WG Rod End Ball Bearing
007272694
AS21151 Rod End Ball Bearing
002323329
BACB10A446 Rod End Ball Bearing
007272694
BACB10AD5 Rod End Ball Bearing
007272694
BACB10AD5K Rod End Ball Bearing
007272694
GB525L4B Rod End Ball Bearing
007272694
HHRE-4-MS-6-1 Rod End Ball Bearing
007272694
MS21151-11 Rod End Ball Bearing
002323329
MS21151-11G Rod End Ball Bearing
002323329
RAP4M6-3A2462 Rod End Ball Bearing
012295251
REP4M6-4 Rod End Ball Bearing
007272694
REP4M6-4FS210 Rod End Ball Bearing
007272694
REP4M6-4FS210C1 Rod End Ball Bearing
007272694
REP4M6-4FS428 Rod End Ball Bearing
007272694
REP5M7 Rod End Ball Bearing
002323329
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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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