Narrative:

Aircraft arrived with the following log engine #2 stall ECAM engine now normal; accomplish full borescope of compressor. Report all findings; pay attention to stages 3 and 6. Reference amm 72-00-00 and mt 72-025. I opened and closed the thrust reverser and engine fan cowls. Lubed the vsv. Borescope was accomplished on third and sixth stages per the tsm. I found water in the burner pressure sensor tube. After purging the water from tubes; the aircraft was taken out for a power assurance run with no faults found.

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Original NASA ASRS Text

Title: AN A319 HAD A #2 COMPRESSOR STALL. TECHNICIAN ACCOMPLISHED ALL ENGINEERING ORDERS EXCEPT ENTIRE BORESCOPE; ONLY THIRD AND SIXTH STAGE BORESCOPED. FOUND WATER IN THE BURNER PRESSURE SENSOR LINE. ENG OP OK ON RUN.

Narrative: ACFT ARRIVED WITH THE FOLLOWING LOG ENG #2 STALL ECAM ENG NOW NORMAL; ACCOMPLISH FULL BORESCOPE OF COMPRESSOR. RPT ALL FINDINGS; PAY ATTN TO STAGES 3 AND 6. REF AMM 72-00-00 AND MT 72-025. I OPENED AND CLOSED THE THRUST REVERSER AND ENG FAN COWLS. LUBED THE VSV. BORESCOPE WAS ACCOMPLISHED ON THIRD AND SIXTH STAGES PER THE TSM. I FOUND WATER IN THE BURNER PRESSURE SENSOR TUBE. AFTER PURGING THE WATER FROM TUBES; THE ACFT WAS TAKEN OUT FOR A PWR ASSURANCE RUN WITH NO FAULTS FOUND.

Data retrieved from NASA's ASRS site as of January 2009 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.