What was found
WHILE REMOVING LH I/B FOREFLAP, THE LEADING EDGE WAS DAMAGED NEAR O/B HINGE FITTING. 1.INSTALLED L/H WING INBD FORE FLAP TOP PANELS I.A.W SRM 51-40-02-0G REV 100 AND AMM 20-51-01-912-008 REV 110 . 2. JOB COMPLETED. REVIEW COMPELTED
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE REMOVING LH I/B FOREFLAP, THE LEADING EDGE WAS DAMAGED NEAR O/B HINGE FITTING. 1.INSTALLED L/H WING INBD FORE FLAP TOP PANELS I.A.W SRM 51-40-02-0G REV 100 AND AMM 20-51-01-912-008 REV 110 . 2. JOB COMPLETED. REVIEW COMPELTED