What was found
FOUND ON CV2 CHECK .25 INCH CRACKS IN SKIN AT FASTNER HOLES (4 PLACES) RT SIDE ABOVE FWD VERTICAL SPAR AND FWD OF PANEL 95012) FASTNERS LOOSE FWD OF PANEL 9501 REPAIR-1) REPAIR PER MM 54-30-0 PG801/FIG801 2).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ON CV2 CHECK .25 INCH CRACKS IN SKIN AT FASTNER HOLES (4 PLACES) RT SIDE ABOVE FWD VERTICAL SPAR AND FWD OF PANEL 95012) FASTNERS LOOSE FWD OF PANEL 9501 REPAIR-1) REPAIR PER MM 54-30-0 PG801/FIG801 2).