What was found
LEFT AFT FUSELAGE AFT DRAG ANGLE CRACKED. INSTALLED NEW L/H AFT FUSELAGE AFT DRAG ANGLE IAW CRJ700 SRM 51-42-10-001-001-A01, 51-42-21-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AFT FUSELAGE AFT DRAG ANGLE CRACKED. INSTALLED NEW L/H AFT FUSELAGE AFT DRAG ANGLE IAW CRJ700 SRM 51-42-10-001-001-A01, 51-42-21-001-A01.