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|
Attributes | |
ACN | 414764 |
Time | |
Date | 199809 |
Day | Thu |
Local Time Of Day | 0001 To 0600 |
Place | |
Locale Reference | airport : zzz |
State Reference | US |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B737-300 |
Operating Under FAR Part | Part 121 |
Navigation In Use | Other Other |
Flight Phase | other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 414764 |
Person 2 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 414595 |
Events | |
Anomaly | aircraft equipment problem : critical non adherence : far non adherence : published procedure |
Independent Detector | other other : unspecified |
Resolutory Action | other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
On sep/xa/98 I performed air carrier cfm-56 engine job card #xyz-abc (fan blade lubrication) on engine yxzy with another mechanic. It was reported to me by the company that on engine change run (test) this engine had a vibration. The cause of the vibration was out of sequence blades. Line maintenance removed and reinstalled blades and this corrected the problem and aircraft was returned to service. I remember checking blade sequence on reinstallation of fan blades, but must have inadvertently crossed blades. To correct this situation, I should have rechked blade sequence. Also a better mapping system and blade identify system should be put into the routine job card with a separate sign off block for blade sequencing.
Original NASA ASRS Text
Title: A B737-300 ENG DISPLAYED EXCESSIVE VIBRATION ON ENG CHANGE TEST RUN CAUSED BY THE FAN BLADES BEING INCORRECTLY INSTALLED BY THE ENG SHOP.
Narrative: ON SEP/XA/98 I PERFORMED ACR CFM-56 ENG JOB CARD #XYZ-ABC (FAN BLADE LUBRICATION) ON ENG YXZY WITH ANOTHER MECH. IT WAS RPTED TO ME BY THE COMPANY THAT ON ENG CHANGE RUN (TEST) THIS ENG HAD A VIBRATION. THE CAUSE OF THE VIBRATION WAS OUT OF SEQUENCE BLADES. LINE MAINT REMOVED AND REINSTALLED BLADES AND THIS CORRECTED THE PROB AND ACFT WAS RETURNED TO SVC. I REMEMBER CHKING BLADE SEQUENCE ON REINSTALLATION OF FAN BLADES, BUT MUST HAVE INADVERTENTLY CROSSED BLADES. TO CORRECT THIS SIT, I SHOULD HAVE RECHKED BLADE SEQUENCE. ALSO A BETTER MAPPING SYS AND BLADE IDENT SYS SHOULD BE PUT INTO THE ROUTINE JOB CARD WITH A SEPARATE SIGN OFF BLOCK FOR BLADE SEQUENCING.
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.