As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IDENTIFIED CRACK AT FASTENER HOLE CAUSED BY A SHORT EDGE DISTANCE AT BS 1112 FRAME. TRIM OUT THE DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED FILLER OF 056 INCH 7075-T6, FABRICATED AND INSTALLED 063 INCH REPAIR STRAP, CLEANED AND TREATED ALL EXPOSED AREAS IAW ECO 3202, 8110-3 APPROVAL RECEIVED. AIRCRAFT RETURNED TO SERVICE. (M)