What was found
T-CAP AT FR 15 Y-1959 HAS CORROSION. REMOVED CORROSION PER SRM 53-12-15, MATERIAL LOSS AT FASTENER HOLE 100%, BEYOND LIMITS PER SRM 53-12-15. REMOVED AND REPLACED T-CAP, FR12 TO FR17, -Y1959 PER SRM 51-40-20 AND DWG A536-12213.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
T-CAP AT FR 15 Y-1959 HAS CORROSION. REMOVED CORROSION PER SRM 53-12-15, MATERIAL LOSS AT FASTENER HOLE 100%, BEYOND LIMITS PER SRM 53-12-15. REMOVED AND REPLACED T-CAP, FR12 TO FR17, -Y1959 PER SRM 51-40-20 AND DWG A536-12213.