What was found
CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE PREVIOUS REPAIR BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. PREVIOUS REPAIR ON LH VERTICAL AFT DRAG ANGLE WAS REPLACED PER 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 ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE PREVIOUS REPAIR BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. PREVIOUS REPAIR ON LH VERTICAL AFT DRAG ANGLE WAS REPLACED PER CRJ 900 SRM 55-31-00-201-001-A01