What was found
DURING CHECK-C MAINT, FOUND DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED ON RT SIDE AT STA 1097, APPROX 1.5 INCH LONG IN RADIUS. CRACK WAS STOP DRILLED AND CRACK CONTAINMENT VERIFIED BY NDT. ANGLE WAS REPAIRED PER SRM 53-05, FIG 23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, FOUND DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED ON RT SIDE AT STA 1097, APPROX 1.5 INCH LONG IN RADIUS. CRACK WAS STOP DRILLED AND CRACK CONTAINMENT VERIFIED BY NDT. ANGLE WAS REPAIRED PER SRM 53-05, FIG 23.