As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAN - SUSPECT CRACK RIGHT DRAG ANGLE REPAIR PLATE AT LOWER END OF FIRST BANJO FITTING. AFTER NDT INSPECTION, CRACK CONFIRMED (1 INCH). CRACK STOP-DRILLED PER SRM 55-20-00, FIG 3. REPAIR PLATE REMOVED AND REPLACED PER SRM 55-20-00 FIG 3. (X)