What was found
(CAN) WING STRUT WAS REMOVED TO INSPECT/REPAIR SLOPPY STRUT ATACHMENT CONDITION. UPON REMOVING STRUT ASSEMBLY, LUG FACES (FORWARD/AFT) FOUND CORRODED. REF. PSM 1-3-3 FIG 2-1 (DHC-3 REPAIR MANUAL).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) WING STRUT WAS REMOVED TO INSPECT/REPAIR SLOPPY STRUT ATACHMENT CONDITION. UPON REMOVING STRUT ASSEMBLY, LUG FACES (FORWARD/AFT) FOUND CORRODED. REF. PSM 1-3-3 FIG 2-1 (DHC-3 REPAIR MANUAL).