What was found
FUSELAGE FRAME HAD LEVEL 2 CORROSION AT LONGERON 30, STA 813. REPAIRED AREA IAW DC-9 SRM 53-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME HAD LEVEL 2 CORROSION AT LONGERON 30, STA 813. REPAIRED AREA IAW DC-9 SRM 53-03.