Ch-53a/d/e Helicopter Parts

End item NSN parts
Filter By: Self-aligning Plain Bearings
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Part Number
NSN
NIIN
65106-11105 Self-aligning Plain Bearing
009487307
65106-11105SBS48ATC78 Self-aligning Plain Bearing
009487307
ADW16V Self-aligning Plain Bearing
011363573
AS14103 Self-aligning Plain Bearing
011363573
AS81820 Self-aligning Plain Bearing
011363573
AS81820-16 Self-aligning Plain Bearing
011363573
AS81820/1 Self-aligning Plain Bearing
011363573
DSB12-4001 Self-aligning Plain Bearing
010600423
KSBN24-10 Self-aligning Plain Bearing
009487307
KSBY10N7 Self-aligning Plain Bearing
009450618
KSSB16-15 Self-aligning Plain Bearing
009458422
KWDB16-37 Self-aligning Plain Bearing
011363573
MS14103-16 Self-aligning Plain Bearing
011363573
MS21230-14 Self-aligning Plain Bearing
002282851
SBS48ATC78 Self-aligning Plain Bearing
009487307
SBSH28ATC52 Self-aligning Plain Bearing
002282851
SBSH32ATC68Z Self-aligning Plain Bearing
011363573
SBSH32ATH68M Self-aligning Plain Bearing
011363573
WBS24ATC50Z Self-aligning Plain Bearing
010600423
WE1239D Self-aligning Plain Bearing
010600423
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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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