What was found
CRACK 0.656" ON ANGLE BELOW RT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS=153.5. DAMAGE WAS REMOVED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIG 3 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK 0.656" ON ANGLE BELOW RT VORTILON AND LOWER FLANGE, FRONT SPAR AT STA XRS=153.5. DAMAGE WAS REMOVED. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIG 3 AND 51-30-5.