What was found
THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80 ; RII
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80 ; RII