What was found
LT WING UPPER TRAILING EDGE PANEL BETWEEN NR 5 AND 6 SPOILER LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R&R ANGLE IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING UPPER TRAILING EDGE PANEL BETWEEN NR 5 AND 6 SPOILER LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R&R ANGLE IAW SRM.