What was found
DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 400+10, STR 17R. REPAIRED SKIN PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED SPV CHECK, FOUND RT FUSELAGE WINDOW SKIN UPPER FORWARD CORNER CRACKED AT BS 400+10, STR 17R. REPAIRED SKIN PER SRM.