What was found
INSPECTION FOUND A 1 INCH CRACK IN CEILING WEB OF LT WHEEL WELL AT BS 663, LBL 32. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN CEILING WEB OF LT WHEEL WELL AT BS 663, LBL 32. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 203.