What was found
DURING PERIODIC CHECK, FOUND TWO CRACKS IN NOSE WHEEL WELL PRESSURE PANEL AT FS 110, INBOARD OF CUSP AT ATTACH FITTING. INSTALLED DOUBLER AND FITTINGS PER EA 99-11976.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING PERIODIC CHECK, FOUND TWO CRACKS IN NOSE WHEEL WELL PRESSURE PANEL AT FS 110, INBOARD OF CUSP AT ATTACH FITTING. INSTALLED DOUBLER AND FITTINGS PER EA 99-11976.