What was found
FRAME 54.1-54.2, STR 39-41 LT EXT FUSELAGE SKIN CRACKED. REMOVED AND REPLACED REINFORCEMENT DOUBLER (16R539H0126) PER DWG 16R539H0111, SHEET 2 IAW DWG 74626/99-04 PC.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 54.1-54.2, STR 39-41 LT EXT FUSELAGE SKIN CRACKED. REMOVED AND REPLACED REINFORCEMENT DOUBLER (16R539H0126) PER DWG 16R539H0111, SHEET 2 IAW DWG 74626/99-04 PC.