What was found
FUSELAGE SKIN IS CHAFED OUT OF LIMITS AT THE AFT END OF PANEL 192AR. DAMAGE IS ACCEPTABLE IAW MESABA EO S53288. REF: EAMS WORK ORDER 211770 TASK 1509.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN IS CHAFED OUT OF LIMITS AT THE AFT END OF PANEL 192AR. DAMAGE IS ACCEPTABLE IAW MESABA EO S53288. REF: EAMS WORK ORDER 211770 TASK 1509.