What was found
CRACK OF 0.937 ON ANGLE BELOW LT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS 153.5 REF. NRC (T0 266025). VORTILON ANGLE WAS REPAIRED IAW SRM 57-01 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK OF 0.937 ON ANGLE BELOW LT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS 153.5 REF. NRC (T0 266025). VORTILON ANGLE WAS REPAIRED IAW SRM 57-01 FIG 3.