What was found
INSPECTION FOUND A 2 INCH CRACK IN ANGLE AT RT WHEEL WELL FORWARD OUTBOARD DOOR JAMB. THE CRACKED AREA WAS CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-70-12, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN ANGLE AT RT WHEEL WELL FORWARD OUTBOARD DOOR JAMB. THE CRACKED AREA WAS CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-70-12, FIGURE 1.