What was found
DURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALLED NEW ATTACH ANGLE PER SRM 51-30-02, 51-30-05, & MO 72R22 & ARA 17951.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALLED NEW ATTACH ANGLE PER SRM 51-30-02, 51-30-05, & MO 72R22 & ARA 17951.