What was found
C-CHECK - MAIN CARGO FLOOR PANELS CUSP EXTRUSION TO FRAME FITTING CRACKED 1 INCH STA 25.000 RT. REMOVED CRACKED FITTING. CLEANED, TREATED & PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21, 9, SRM 51-1-8B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK - MAIN CARGO FLOOR PANELS CUSP EXTRUSION TO FRAME FITTING CRACKED 1 INCH STA 25.000 RT. REMOVED CRACKED FITTING. CLEANED, TREATED & PRIMED AREA AND INSTALLED NEW FITTING IAW SRM 51-1-20D PAGE 21, 9, SRM 51-1-8B.