What was found
INSPECTION FOUND TWO .0625 INCH CRACKS AT RIVETS IN LT FUSELAGE FORWARD NOSE SECTION EXTERIOR SKIN, STA 695. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5330-02413 AND DOUGLAS DRAWING SR09530239.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO .0625 INCH CRACKS AT RIVETS IN LT FUSELAGE FORWARD NOSE SECTION EXTERIOR SKIN, STA 695. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5330-02413 AND DOUGLAS DRAWING SR09530239.