Ch-53a/d/e Helicopter Parts

End item NSN parts
Filter By: Airframe Ball Bearings
page 1 of 1
Part Number
NSN
NIIN
11838508-1 Airframe Ball Bearing
006215240
15932 Airframe Ball Bearing
001060419
38950-00903-103 Airframe Ball Bearing
001426571
38950-00906-104 Airframe Ball Bearing
011436742
A541DDE7751 Airframe Ball Bearing
001060419
B546DDFS160 Airframe Ball Bearing
006215240
B546ZZ Airframe Ball Bearing
006215240
MDW5A1173 Airframe Ball Bearing
001797564
MKP25BS-004M Airframe Ball Bearing
011436742
MKP25BSA1173 Airframe Ball Bearing
011436742
MKSP4 Airframe Ball Bearing
001426571
MKSP4A1173 Airframe Ball Bearing
001426571
MS27643-4R Airframe Ball Bearing
011246064
Page:

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.

Compare Now »
Clear | Hide