As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(UT) THICKNESS MEASUREMENT INSPECTION WAS ACCOMPLISHED ON LONGERON STA Y=1002 AND STA Y=1005. ORIGINAL THICKNESS WAS 0.080 INCHES AND REMAINING THICKNESS IS 0.058 INCHES. THEREFOR AREA IS OUT LIMITS IAW SRM 53- 00-00-1A AT AFT CARGO COMPARMENT. CORROSION LEVEL 2. LONGERON 29L REPAIRED IAW SRM 53-00-05-2R PROCEDURE 3 FIG. 201.