As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
- CRACK - SKIN, R/H WING T/E NO.5 FLAP FAIRING (REPAIR). 1. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 PERFORM REPAIR AS BELOW STEP : REMOVE THE CRACK MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( DIA : 1", 32" FROM UPPER EDGE, 34.5" FROM T/E ). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 240 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. CONDITION CHECK IS SATISFACTORY.