What was found
PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT, Q5, TOP SKIN - CORE BOND, 3 INCH X 3 INCH AREA, DEBONDED. LT IB AFT FLAP, UPPER OB T/E. REMOVED DAMAGE, INSTALLED CORE, DOUBLER IAW TR 57-53-01A, EA 79082, SRM 51-70-10.