What was found
CORROSION AT FUSELAGE FRAME AND FLOOR SUPPORT AREA STA 200, LONGERON 18 RIGHT AREA. REMOVED FLOOR PANEL AND J-CHANNEL AND RE-INSTALLED. ALL CORROSION WORK COMPLETED ON NON ROUTINE 0259 IAW DC-9 SRM 51-30-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AT FUSELAGE FRAME AND FLOOR SUPPORT AREA STA 200, LONGERON 18 RIGHT AREA. REMOVED FLOOR PANEL AND J-CHANNEL AND RE-INSTALLED. ALL CORROSION WORK COMPLETED ON NON ROUTINE 0259 IAW DC-9 SRM 51-30-1.