What was found
CRACKED LT AFT DRAG ANGLE BETWEEN UNION OF FUSELAGE AND VERTICAL STABILIZER. 67.5% REAR SPAR DATUM. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED LT AFT DRAG ANGLE BETWEEN UNION OF FUSELAGE AND VERTICAL STABILIZER. 67.5% REAR SPAR DATUM. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.