What was found
DAMAGE FOUND ON THE DORSAL FIN SKIN, FWD OF ACCESS PANEL, AT FASTENER HOLES BY BSS 52. REMOVED THE DAMAGE AND REPAIRED IAW SRM 55-30-05, FIG 20, SHEET 3. AND APPLIED PROTECTIVE COATINGS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DAMAGE FOUND ON THE DORSAL FIN SKIN, FWD OF ACCESS PANEL, AT FASTENER HOLES BY BSS 52. REMOVED THE DAMAGE AND REPAIRED IAW SRM 55-30-05, FIG 20, SHEET 3. AND APPLIED PROTECTIVE COATINGS.