What was found
LEFT NACELLE STRUT AFT TORQUE BOX AREA I/B INTERIOR VERTICAL STIFFENER AFT OF ACCESS PANEL 436 AR @ APPROX NAC 254 HAS MARKED CRACK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT NACELLE STRUT AFT TORQUE BOX AREA I/B INTERIOR VERTICAL STIFFENER AFT OF ACCESS PANEL 436 AR @ APPROX NAC 254 HAS MARKED CRACK.