What was found
CRACK ON ANGLE TO ATTACH LT AFT ENGINE PYLON SUPPORT BULKHEAD, BS Y=1022 BETWEEN LONGERONS 6 TO 7L ALSO LONGERONS 16 TO 17L. ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-10-14, PAR. 21 AND 15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE TO ATTACH LT AFT ENGINE PYLON SUPPORT BULKHEAD, BS Y=1022 BETWEEN LONGERONS 6 TO 7L ALSO LONGERONS 16 TO 17L. ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-10-14, PAR. 21 AND 15.