What was found
SKIN PANEL UNDER ANTI CHAFING PLATE FR 92 - FR 95 CRACKED AND IN SOME SMALL AREAS CORRODED STRUCTURE REPAIR IN ACCORDANCE WITH EA 6-5319-106511 AND RAS /DAHAM/4022481/2007 PERFORMED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN PANEL UNDER ANTI CHAFING PLATE FR 92 - FR 95 CRACKED AND IN SOME SMALL AREAS CORRODED STRUCTURE REPAIR IN ACCORDANCE WITH EA 6-5319-106511 AND RAS /DAHAM/4022481/2007 PERFORMED.