What was found
AT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE SHOWS CRACKS 1/4 INCH & 1/2 INCH AT STA. 660. REMOVED DAMAGED ANGLE IAW SRM 51-1-21 PAGE 1, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. REF: N/R 1431.
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 SHOWS CRACKS 1/4 INCH & 1/2 INCH AT STA. 660. REMOVED DAMAGED ANGLE IAW SRM 51-1-21 PAGE 1, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. REF: N/R 1431.