What was found
DURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER DORSAL FIN ATTACH ANGLE, 17 INCHES FROM AFT END. REPAIRED IAW SRM 53-05, FIG 23B, PAGE 205.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER DORSAL FIN ATTACH ANGLE, 17 INCHES FROM AFT END. REPAIRED IAW SRM 53-05, FIG 23B, PAGE 205.