What was found
CRACK ON LT INTERNAL FUSELAGE LONGERON 4L BS 540. THE LONGERON WAS REPAIRED IAW. SRM. 53-02 FIG.18 (SHEET. 1), SRM. 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT INTERNAL FUSELAGE LONGERON 4L BS 540. THE LONGERON WAS REPAIRED IAW. SRM. 53-02 FIG.18 (SHEET. 1), SRM. 51-30-2, 51-30-5 AND 51-10-3 PAR 14, 21.