What was found
THE .020 S/STEEL OVERLAY FROM PREVIOUS REPAIR DATED NOV. 88 CRACKED AND PYLON WALL CRACKED 1/8" PAST PREVIOUS STOP DRILL HOLE. STOP DRILL NEW CRACK AND OVERLAID WITH .032 S/STEEL AS PER NEW REPAIR IN 8110-23551 DATED 25 MAY 1995.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE .020 S/STEEL OVERLAY FROM PREVIOUS REPAIR DATED NOV. 88 CRACKED AND PYLON WALL CRACKED 1/8" PAST PREVIOUS STOP DRILL HOLE. STOP DRILL NEW CRACK AND OVERLAID WITH .032 S/STEEL AS PER NEW REPAIR IN 8110-23551 DATED 25 MAY 1995.