Narrative:

Air carrier flight zyyz departed toronto (yyz) at XA15 on jan/xa/99 en route to clt. About 40 mi from clt we started getting intermittent low oil pressure indications. I reviewed the procedures and informed ATC (ZTL) that we needed expeditious handling to clt. About 25 mi from clt the low oil pressure readings became constant (less than 25 psi) and a precautionary engine shutdown on the #2 engine was completed. I declared an emergency and the flight landed without incident. Cause: the aircraft (xyz) had had a hydraulic pump on the #2 engine replaced in ZZZ about 5 flight hours prior to this incident. The pump was installed poorly. A seal on the pump shaft had been nicked causing the engine to leak oil internally and vent it overboard. The aircraft uses general electric CF34-3b1 engines and none of our a&P's have had any training on this engine. Callback conversation with reporter revealed the following information: the reporter stated this right engine driven hydraulic pump shaft was installed 5 hours flight time prior to this failure. The reporter said there must be some installation problem when changing this seal because another failure he knew of was a damaged seal also. The reporter stated it was not a massive oil leak but just a steady dripping.

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Original NASA ASRS Text

Title: A CANADAIR CL65 IN DSCNT AT 11000 FT DECLARED AN EMER AND SHUT DOWN #2 ENG DUE TO LOW OIL PRESSURE WARNING AND INDICATION CAUSED BY THE LOSS OF OIL FROM A CUT SEAL ON THE ENG DRIVEN HYD PUMP DRIVE SHAFT.

Narrative: ACR FLT ZYYZ DEPARTED TORONTO (YYZ) AT XA15 ON JAN/XA/99 ENRTE TO CLT. ABOUT 40 MI FROM CLT WE STARTED GETTING INTERMITTENT LOW OIL PRESSURE INDICATIONS. I REVIEWED THE PROCS AND INFORMED ATC (ZTL) THAT WE NEEDED EXPEDITIOUS HANDLING TO CLT. ABOUT 25 MI FROM CLT THE LOW OIL PRESSURE READINGS BECAME CONSTANT (LESS THAN 25 PSI) AND A PRECAUTIONARY ENG SHUTDOWN ON THE #2 ENG WAS COMPLETED. I DECLARED AN EMER AND THE FLT LANDED WITHOUT INCIDENT. CAUSE: THE ACFT (XYZ) HAD HAD A HYD PUMP ON THE #2 ENG REPLACED IN ZZZ ABOUT 5 FLT HRS PRIOR TO THIS INCIDENT. THE PUMP WAS INSTALLED POORLY. A SEAL ON THE PUMP SHAFT HAD BEEN NICKED CAUSING THE ENG TO LEAK OIL INTERNALLY AND VENT IT OVERBOARD. THE ACFT USES GENERAL ELECTRIC CF34-3B1 ENGS AND NONE OF OUR A&P'S HAVE HAD ANY TRAINING ON THIS ENG. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THIS R ENG DRIVEN HYD PUMP SHAFT WAS INSTALLED 5 HRS FLT TIME PRIOR TO THIS FAILURE. THE RPTR SAID THERE MUST BE SOME INSTALLATION PROB WHEN CHANGING THIS SEAL BECAUSE ANOTHER FAILURE HE KNEW OF WAS A DAMAGED SEAL ALSO. THE RPTR STATED IT WAS NOT A MASSIVE OIL LEAK BUT JUST A STEADY DRIPPING.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.