What was found
LEFT WING OUTBOARD MIDFLAP TRAILING EDGE COVE PANEL CRACKED AT MIDPOINT. REMOVED DAMAGED PANEL AND CORE, FABRICATED CORE, FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-09 AND 51-40-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OUTBOARD MIDFLAP TRAILING EDGE COVE PANEL CRACKED AT MIDPOINT. REMOVED DAMAGED PANEL AND CORE, FABRICATED CORE, FILLER AND DOUBLERS AND INSTALLED IAW SRM 51-40-09 AND 51-40-12.