What was found
FUSELAGE BELLY SKIN IS CHAFED AT ACFT CTR LINE ROW OF RIVETS, BETWEEN FS 909 - 91, STRINGER 27, 3"" X .2"" X .010""-.015"". REPAIRED BELLY SKIN CHAFE IAW REO 670-53-00-290. ACTUAL DAMAGE FS 915 - 918. THIS IS A MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE BELLY SKIN IS CHAFED AT ACFT CTR LINE ROW OF RIVETS, BETWEEN FS 909 - 91, STRINGER 27, 3"" X .2"" X .010""-.015"". REPAIRED BELLY SKIN CHAFE IAW REO 670-53-00-290. ACTUAL DAMAGE FS 915 - 918. THIS IS A MAJOR REPAIR.