What was found
FUSELAGE EXTERIOR ANGLE CRACKED 1 INCH AT STA 630 BETWEEN L31 AND L32R. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1-21 PG 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR ANGLE CRACKED 1 INCH AT STA 630 BETWEEN L31 AND L32R. REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-1-21 PG 7.