What was found
CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1562/1582 AND STRINGER S-24L / S-25L, AT THE VACUUM OUTLET NOZZLE.(<P ><SPAN>FUSELAGE SKIN REPAIRED / PER SRM 53-60-01-2R-3 REPAIR 3. SEE RAM FORM N662GT-20-02.</SPAN></P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN STA 1562/1582 AND STRINGER S-24L / S-25L, AT THE VACUUM OUTLET NOZZLE.(<P ><SPAN>FUSELAGE SKIN REPAIRED / PER SRM 53-60-01-2R-3 REPAIR 3. SEE RAM FORM N662GT-20-02.</SPAN></P>)