What was found
GSO - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEELWELL CEILING PRESSURE PANEL AT STA 277, RT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5310-03186. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEELWELL CEILING PRESSURE PANEL AT STA 277, RT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5310-03186. (X)