What was found
INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 575 BETWEEN S42L AND S43L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 575 BETWEEN S42L AND S43L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 2.