What was found
ON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER TITANIUM STRAP AT FRAME 23, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 1896-1, REV A, DATED 2-7-97.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER TITANIUM STRAP AT FRAME 23, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 1896-1, REV A, DATED 2-7-97.