What was found
DURING LINE CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1266 LT BELOW VERTICAL STABILIZER ATTACH ANGLE. REPAIRED PER EA 98-213119. (A)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING LINE CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1266 LT BELOW VERTICAL STABILIZER ATTACH ANGLE. REPAIRED PER EA 98-213119. (A)