What was found
AT C-CHECK, LT FAIRING PANEL FRAME TO FUSELAGE AT LONGERON APPROX STA 1000 HAS FORMED ANGLE CRACKED AT LOWER SURFACE. STOP DRILLED END OF CRACK, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-21, 1 X 1 X 3.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LT FAIRING PANEL FRAME TO FUSELAGE AT LONGERON APPROX STA 1000 HAS FORMED ANGLE CRACKED AT LOWER SURFACE. STOP DRILLED END OF CRACK, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-21, 1 X 1 X 3.5.