What was found
WEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB201.