Mh-53e Helicopter Parts

End item NSN parts
Filter By: Airframe Ball Bearings
page 1 of 1
Part Number
NSN
NIIN
10107325 Airframe Ball Bearing
000424807
10107371 Airframe Ball Bearing
002778348
11838508-1 Airframe Ball Bearing
006215240
1201578-101 Airframe Ball Bearing
000424807
15932 Airframe Ball Bearing
001060419
1775238 Airframe Ball Bearing
000420901
2147249 Airframe Ball Bearing
000424807
2910003 Airframe Ball Bearing
000424807
3103352 Airframe Ball Bearing
000424807
313352 Airframe Ball Bearing
000424807
38950-00903-103 Airframe Ball Bearing
001426571
38950-00906-104 Airframe Ball Bearing
011436742
3KSP4A20 Airframe Ball Bearing
000424807
538664-29 Airframe Ball Bearing
000420901
571-4801-1303062REVCPC3-8 Airframe Ball Bearing
000420901
578-4801-1572884RAPC227 Airframe Ball Bearing
000420901
8531007 Airframe Ball Bearing
000420901
A541DDE7751 Airframe Ball Bearing
001060419
AN202KP29B Airframe Ball Bearing
000420901
AS27642 Airframe Ball Bearing
000420901
Page:

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.

Jetzt vergleichen»
Klar | Verstecken