What was found
*LH V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK) RO 2/14/2020 CRACK CONFIRMED WITH NDT, COMPLIED WITH V. STAB DRAG ANGLE REPAIR REF CRJ 900 SRM. COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
*LH V/STAB TO FUSELAGE ATTACHMENT DRAG ANGLE POSSIBLE CRACK. MARKED (C-CHECK) RO 2/14/2020 CRACK CONFIRMED WITH NDT, COMPLIED WITH V. STAB DRAG ANGLE REPAIR REF CRJ 900 SRM. COMPLETED FORM M-337. SEE CONTINUATION CARD FOR DETAILS.