What was found
FUSELAGE INTERCOSTAL WEB UPPER ANGLE CRACKED FROM BODY BS 660 TO 680, BUTTLINE 0. CRACK 14 INCHES. REPLACED ANGLE PER SRM 53-00-51-2R AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERCOSTAL WEB UPPER ANGLE CRACKED FROM BODY BS 660 TO 680, BUTTLINE 0. CRACK 14 INCHES. REPLACED ANGLE PER SRM 53-00-51-2R AND 51-40-02.