What was found
CRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LT VERTICAL STABILIZER BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH CRJ-900 SRM 55-31-00-201-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LT VERTICAL STABILIZER BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH CRJ-900 SRM 55-31-00-201-001-A01.