What was found
LEFT WING TO FUSELAGE UPPER ATTACH ANGLE CRACKED, BETWEEN FRAMES 48 & 49. REPAIRED IAW SRM 53-23-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TO FUSELAGE UPPER ATTACH ANGLE CRACKED, BETWEEN FRAMES 48 & 49. REPAIRED IAW SRM 53-23-12.