What was found
DURING L CHECK FOUND CRACK, 39 INCHS O/B OF FUSELAGE SPAR CAP ON RIGHT WING UPPER SURFACE. REPAIRED PER EA 67-175083.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING L CHECK FOUND CRACK, 39 INCHS O/B OF FUSELAGE SPAR CAP ON RIGHT WING UPPER SURFACE. REPAIRED PER EA 67-175083.