What was found
LEFT ENGINE AFT STRUT FAIRING STIFFENER I/B BOLTS LOOSE WITH ELONGATED HOLES IN STIFFENER. STIFFENER LOCATED UNDER FWD END OF PANEL 434BL. / COMPLIED WITH EA 1-754-2497
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT ENGINE AFT STRUT FAIRING STIFFENER I/B BOLTS LOOSE WITH ELONGATED HOLES IN STIFFENER. STIFFENER LOCATED UNDER FWD END OF PANEL 434BL. / COMPLIED WITH EA 1-754-2497