What was found
PANEL 699AB IS CHAFED. BLENDED DAMAGE ON PANEL 699AB IAW SRM 51-12-00, MAX DAMAGE LOSS .015 MAT REMAINING .046 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 699AB IS CHAFED. BLENDED DAMAGE ON PANEL 699AB IAW SRM 51-12-00, MAX DAMAGE LOSS .015 MAT REMAINING .046 WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.