What was found
AT SCHEDULED INSPECTION DISCOVERED A 1.5 INCH CRACK ON THE LT WING BELLY SKIN RUNNING LATERALLY AT FS 303.25 X BL30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL MM 53-90-18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT SCHEDULED INSPECTION DISCOVERED A 1.5 INCH CRACK ON THE LT WING BELLY SKIN RUNNING LATERALLY AT FS 303.25 X BL30.62. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURAL MM 53-90-18.