What was found
LT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING I/B MIDFLAP T/E WEDGE IS DELAMINATED AT 20 FROM I/B END, UPPER AND LOWER SURFACE. *S/D* FOUND CORROSION ON T/E WEDGE SPAR TO BE OUT OF LIMITS. REMOVED AND REPLACED MIDFLAP IAW FED-EX M/M 27-51-3.