What was found
INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD MIDFLAP LOWER TRAILING EDGE SKIN, 32 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD MIDFLAP LOWER TRAILING EDGE SKIN, 32 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1.