What was found
MAIN CABIN FLOOR SUPPORT SUBSTRUCTURAL T ANGLE AT APPROX STA 951 IS GOUGED ON THE UPPER SURFACE AT APPROX LBL 20. REMOVED DAMAGE ORIG THICKNESS 0.075, REMOVED 0.012 REMAINING 0.063 AND REPAIRED IAW ECRA 5375-01024.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR SUPPORT SUBSTRUCTURAL T ANGLE AT APPROX STA 951 IS GOUGED ON THE UPPER SURFACE AT APPROX LBL 20. REMOVED DAMAGE ORIG THICKNESS 0.075, REMOVED 0.012 REMAINING 0.063 AND REPAIRED IAW ECRA 5375-01024.