Narrative:

Aircraft arrived with #1 engine C1 blades shingled. Removed front and rear spinner cones and un-shingled blades. Inspected mid spans and blade root area -- no damage found. Re-installed spinner cones per maintenance manual. I was just informed this afternoon of the requirement for a full blade inspection within 50 cycles. I was unaware of this requirement and did not create a deferred item to accomplish this task (my thinking was that the visual inspection accomplished at the time was acceptable).

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Original NASA ASRS Text

Title: A B737-400 ARRIVED WITH THE L FAN BLADES SHINGLED. REMOVED FRONT AND REAR SPINNER AND UN-SHINGLED BLADES. FAILED TO MAKE DEFERRED ITEM FOR 50 HR INSPECTION.

Narrative: ACFT ARRIVED WITH #1 ENG C1 BLADES SHINGLED. REMOVED FRONT AND REAR SPINNER CONES AND UN-SHINGLED BLADES. INSPECTED MID SPANS AND BLADE ROOT AREA -- NO DAMAGE FOUND. RE-INSTALLED SPINNER CONES PER MAINT MANUAL. I WAS JUST INFORMED THIS AFTERNOON OF THE REQUIREMENT FOR A FULL BLADE INSPECTION WITHIN 50 CYCLES. I WAS UNAWARE OF THIS REQUIREMENT AND DID NOT CREATE A DEFERRED ITEM TO ACCOMPLISH THIS TASK (MY THINKING WAS THAT THE VISUAL INSPECTION ACCOMPLISHED AT THE TIME WAS ACCEPTABLE).

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.