What was found
UPPER HOIST POINT OF DORSAL FIN IS DAMAGED BY EROSION. SURFACE REPAIRED AS PER GUIDELINES OF SRM 51-77-11 PARA 3 A., USING PASTE ADHESIVE AS PER SRM 51-77-10 PARA 5 B (1) IAW. EA 6-5318-92211 AND RAS/DAHAM/4020086/2005 ISS A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER HOIST POINT OF DORSAL FIN IS DAMAGED BY EROSION. SURFACE REPAIRED AS PER GUIDELINES OF SRM 51-77-11 PARA 3 A., USING PASTE ADHESIVE AS PER SRM 51-77-10 PARA 5 B (1) IAW. EA 6-5318-92211 AND RAS/DAHAM/4020086/2005 ISS A.