What was found
TWO CRACKS FOUND AT L/E OF LT STABILIZER UPPER SKIN PANEL, AT CLOSING RIB AREA STA XE = 28.426, XFS = 86.616. CRACKS ARE APPROX .25 INCH AND 2.0 INCH IN LENGTH. REPAIRED AS PER EO 8-5510-7-3312 PART 4 AND SRM 55-20-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO CRACKS FOUND AT L/E OF LT STABILIZER UPPER SKIN PANEL, AT CLOSING RIB AREA STA XE = 28.426, XFS = 86.616. CRACKS ARE APPROX .25 INCH AND 2.0 INCH IN LENGTH. REPAIRED AS PER EO 8-5510-7-3312 PART 4 AND SRM 55-20-00.