What was found
DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 69.55 3.5 INCHES BELOW L14L. REPAIRED IAW EA 98-197450.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 69.55 3.5 INCHES BELOW L14L. REPAIRED IAW EA 98-197450.