What was found
FUSELAGE FRAME TO SKIN CLIP WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AT STA 1562 AND BL 0 BETWEEN STRINGERS 38L AND 38R. THE (P/N 140T2102-23) SKIN CLIP WAS REPLACED PER SRM 51-10-00 AND DWG 146T1223.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME TO SKIN CLIP WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AT STA 1562 AND BL 0 BETWEEN STRINGERS 38L AND 38R. THE (P/N 140T2102-23) SKIN CLIP WAS REPLACED PER SRM 51-10-00 AND DWG 146T1223.