What was found
AT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE CRACKED 1/4 INCH AT STA. 920. PERFORMED STOP DRILL IAW SRM 53-2-0, FABRICATED AND INSTALLED ANGLE IAW SRM 53-2-0. REF: N/R 1437.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE CRACKED 1/4 INCH AT STA. 920. PERFORMED STOP DRILL IAW SRM 53-2-0, FABRICATED AND INSTALLED ANGLE IAW SRM 53-2-0. REF: N/R 1437.