What was found
DURING M-CHECK, FOUND CRACK IN LONGERON 4L AT BS 200. REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-3, SRM 51-20-0, SRM 53-13-2 FIG 3, SRM 53-02 FIGURE 18 AND PROCESS STANDARD 900-5-1 NR4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M-CHECK, FOUND CRACK IN LONGERON 4L AT BS 200. REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-3, SRM 51-20-0, SRM 53-13-2 FIG 3, SRM 53-02 FIGURE 18 AND PROCESS STANDARD 900-5-1 NR4.