What was found
LEFT FORWARD FUSELAGE SKIN CUTOUT FOR L1 DOOR, GUST LOCK IS CHAFED AT APPROXIMATELY STA 125, L15L. BLENDED OUT DAMAGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PAN IAW SRM 53-30-01 AND DWG 5911402, REV AD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FORWARD FUSELAGE SKIN CUTOUT FOR L1 DOOR, GUST LOCK IS CHAFED AT APPROXIMATELY STA 125, L15L. BLENDED OUT DAMAGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PAN IAW SRM 53-30-01 AND DWG 5911402, REV AD.