What was found
LH, AFT VERTICAL DRAG ANGLE CRACKED. INSTALLED DRAG ANGLE ON LH AFT VERTICAL STAB TO FUSELAGE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01 PN AV67-21186-003.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LH, AFT VERTICAL DRAG ANGLE CRACKED. INSTALLED DRAG ANGLE ON LH AFT VERTICAL STAB TO FUSELAGE IAW CRJ 900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01 PN AV67-21186-003.