Service difficulty report · Bearing

Difficulty date
December 16, 1995
Submitted
March 26, 2000
Operation
General aviation
Engine
Pwa PW126A
Part
Bearing
Condition
Failed
Location
Comp Nr 1
Stage of operation
CR
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

(CAN)AT 16,000 FEET THE PILOT REPORTED LOUD BANGS FROM #2 ENGINE AND THE AIRCRAFT BEGAN TO DESCEND. ALTHOUGH THE PROPELLER BEGAN AN AUTOFEATHER THE PILOT HAD TO SELECT MANUAL MODE TO COMPLETE THE SEQUENCE.GROUND INSPECTION REVEALS THE TORQUE SHAFT HANGING ABOUT 45 DEGREES THROUGH THE INLET CASE, BEING DETACHED AT ITS FORWARD END. THE CASING HAS A HOLE 5" X 5". ALL LAST STAGE PT BLADES ARE IN PLACE BUT THERE IS DAMAGE TO THE AIRFOILS. INITIAL INVESTIGATION LEADS TO THE FAILURE OF THE #1 BEARING AS THE PRIMARY CAUSE OF THE INCIDENT.