As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
: FUSELAGE SKIN BETWEEN STA 246 AND STA 266.5 AND BETWEEN STR 25L AND STR 28L: DURING CONVERSION AT IAI, SHOP FOUND AN EXISTING REPAIR IN FUSELAGE SKIN AT STA 250, S-26L, COMMON TO LAP SPLICE AND 4 INCHES AWAY FROM BUTT SPLICE. EXISTING REPAIR SIZE: 6.0” X 4.0”.