What was found
FUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN, 1 INCH CRACK. UNDER ENGINE INLET FWD END OF CAVITY THROUGH ACCESS PANELS 9521 AND 9522, ON FUSELAGE.