What was found
EXTERIOR FUSELAGE REINFORCING ANGLE .5 INCH CRACK AT STA 761 LBL 22.0 (LOWER SECTION)REMOVED AND REPLACED CRACKED REINFORCING ANGLE PER SRM 51-1-20D PG 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERIOR FUSELAGE REINFORCING ANGLE .5 INCH CRACK AT STA 761 LBL 22.0 (LOWER SECTION)REMOVED AND REPLACED CRACKED REINFORCING ANGLE PER SRM 51-1-20D PG 21.