What was found
LT WING I/B FOREFLAP I/B PANEL FOUND SKIN DISBONDED AT CORROSION REWORK LOCATION 2 BY 10 INCHES. HOT BOND REPAIRED PER SRM 51-40-06 FIG 17 AND FIG 17A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING I/B FOREFLAP I/B PANEL FOUND SKIN DISBONDED AT CORROSION REWORK LOCATION 2 BY 10 INCHES. HOT BOND REPAIRED PER SRM 51-40-06 FIG 17 AND FIG 17A.