What was found
INSPECTION FOUND TWO EACH .125 INCH CRACKS IN NLG WHEEL WELL TOP CENTER PANEL AT BL 0, JUST FORWARD OF STA 294.5. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO EACH .125 INCH CRACKS IN NLG WHEEL WELL TOP CENTER PANEL AT BL 0, JUST FORWARD OF STA 294.5. THE CRACKS WERE STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.