What was found
CRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A.