What was found
INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AFT OF RADOME AT 12 O'CLOCK POSITION. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AFT OF RADOME AT 12 O'CLOCK POSITION. THE SKIN PANEL WAS REMOVED AND A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.