As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFING DAMAGE AT ONE POSITION AND CRACK WITH DEFORMATION AT ANOTHER LOCATION ON FIXED LEADING EDGE D-NOSE SKIN RT, BETWEEN TRACK 3 AND TRACK 4. REPAIR PERFORMED BY BLENDING OUT DAMAGES AT BOTH POSITIONS, REMOVING FASTENER OF HOLE IN AREA OF CRACK WITH ROTOTEST TO INSURE THE CRACK DOES NOT PROPAGATE FROM THE OTHER SIDE AWAY FROM THE SKIN EDGE, AREAS NDT INSPECTED, ALL IAW EA 6- 5740-92207 AND RAS/BAE/1001695/2005 ISSUE B.