What was found
CRACK FOUND ON VERTICAL STAB LH AFT DRAG ANGLE AT VS67.5% REAR SPAR DATUM REMOVED AND REPLACED IMPACT ANGLE IAW CRJ900 SRMS 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON VERTICAL STAB LH AFT DRAG ANGLE AT VS67.5% REAR SPAR DATUM REMOVED AND REPLACED IMPACT ANGLE IAW CRJ900 SRMS 51-40-11-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01.