What was found
FUSELAGE CENTER SECTION, CRACKED HOLE AT PICK UP ANGLE, C39-40 RT. REPAIR WAS PERFORMED BY OVERSIZING AND BUSHING INSTALLATION IAW EA 6-5315-103413 AND RAS/AS/0212/2006 ISSUE "A".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE CENTER SECTION, CRACKED HOLE AT PICK UP ANGLE, C39-40 RT. REPAIR WAS PERFORMED BY OVERSIZING AND BUSHING INSTALLATION IAW EA 6-5315-103413 AND RAS/AS/0212/2006 ISSUE "A".