What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .5 INCH LONG CRACKS IN THE FUSELAGE SKIN AND A PYLON ATTACH ANGLE AT A COMMON FASTENER HOLE. REPAIRED BOTH PER EA 99-102923.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .5 INCH LONG CRACKS IN THE FUSELAGE SKIN AND A PYLON ATTACH ANGLE AT A COMMON FASTENER HOLE. REPAIRED BOTH PER EA 99-102923.