As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE, HEAT SHIELD NR 4 AND NR 5 NEED NDT REMAINING THICKNESS AND HFEC FOR CRACKS. ACCOMPLISHED HFEC AS REQUIRED ON AREAS AFTER BLENDING REF NDT MANUAL PART 6 51-00-06. NO CRACKS FOUND. ALSO PERFORMED ULTRASONIC REMAINING THICKNESS REF NDT MANUAL PART 4 51-00-10 PROCEDURE 2. NR 4 HEAT SHIELD REMAINING THICKNESS .39 INCH AND NR 5 REMAINING THICKNESS .048 INCH.