What was found
(CAN) DURING INSPECTION PRIOR TO INSTALLATION OF SB218 KIT (REF AD95-13-02) TWO CRACKS WERE NOTED ON THE RT VERTICAL STAB SKIN AT FS 409.65 WL 5.10 AND 4.10. TH CRACK LENGTHS WERE 5/16 OF AN INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING INSPECTION PRIOR TO INSTALLATION OF SB218 KIT (REF AD95-13-02) TWO CRACKS WERE NOTED ON THE RT VERTICAL STAB SKIN AT FS 409.65 WL 5.10 AND 4.10. TH CRACK LENGTHS WERE 5/16 OF AN INCH.