What was found
DURING D-CHECK, FOUND PRESSURE PANEL SKIN IN NOSE WHEEL WELL CRACKED STA 83 AND LT CUSP LINE 5 INCHES IN LENGTH, RT CUSP LINE 2 PLACES STA 83. INSTALLED DOUBLER REPAIR IAW DAC SB53-187.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FOUND PRESSURE PANEL SKIN IN NOSE WHEEL WELL CRACKED STA 83 AND LT CUSP LINE 5 INCHES IN LENGTH, RT CUSP LINE 2 PLACES STA 83. INSTALLED DOUBLER REPAIR IAW DAC SB53-187.