What was found
LEFT HORIZONTAL STABILIZER UPPER PANEL ATTACH CHORD ANGLE CRACKED IN RADIUS, 54" FROM WING TIP. REPLACED UPPER CHORD ANGLE IAW PRINT 183T1610 & SRM 51-40-03-0G.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HORIZONTAL STABILIZER UPPER PANEL ATTACH CHORD ANGLE CRACKED IN RADIUS, 54" FROM WING TIP. REPLACED UPPER CHORD ANGLE IAW PRINT 183T1610 & SRM 51-40-03-0G.