What was found
DURING SHOP INSPECTION, FOUND NR 2 AFT FLAP PANEL L/E HAD WEAR DAMAGE AT 40 INCHES FROM O/B END. REPAIRED PER SRM 57-53-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, FOUND NR 2 AFT FLAP PANEL L/E HAD WEAR DAMAGE AT 40 INCHES FROM O/B END. REPAIRED PER SRM 57-53-4.