What was found
TUL - FUSELAGE SKIN HAD VISUAL INDICATION OF CRACK EXTENDING FROM FASTENER AT STA 1380 ABOVE LONGERON 14L. STOP DRILLED CRACK INSTALLED 2024T3 DOUBLER PER 53-01 FIG 2. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - FUSELAGE SKIN HAD VISUAL INDICATION OF CRACK EXTENDING FROM FASTENER AT STA 1380 ABOVE LONGERON 14L. STOP DRILLED CRACK INSTALLED 2024T3 DOUBLER PER 53-01 FIG 2. (X)