What was found
LEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.