What was found
INSPECTION FOUND A 1.2 INCH CRACK IN SKIN AT FORWARD LT SIDE OF STA 1485 CANTED FRAME BELOW YAW DAMPENER ACTUATOR, LONGERON 10L. THE SKIN PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.2 INCH CRACK IN SKIN AT FORWARD LT SIDE OF STA 1485 CANTED FRAME BELOW YAW DAMPENER ACTUATOR, LONGERON 10L. THE SKIN PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.