What was found
SUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH.