What was found
PIT - BC6/BRIDGE - MAJOR REPAIR - BLENDED AREA OF FUSELAGE SKIN FOUND OUT OF LIMITS AT FR25 + 5 INCHES, S39L. REPAIRED FUSELAGE SKIN AT FR25 + 5 INCHES, S39L IAW A319 SRM 53-21-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - BC6/BRIDGE - MAJOR REPAIR - BLENDED AREA OF FUSELAGE SKIN FOUND OUT OF LIMITS AT FR25 + 5 INCHES, S39L. REPAIRED FUSELAGE SKIN AT FR25 + 5 INCHES, S39L IAW A319 SRM 53-21-11.