What was found
DURING C-CHECK, FOUND FORWARD FUSELAGE STRUCTURE JUST BELOW RADOME SUPPORT RODS, CRACKED LEFT AND RIGHT SIDE. ROUTED OUT CRACKED MATERIAL BLENDED, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND FORWARD FUSELAGE STRUCTURE JUST BELOW RADOME SUPPORT RODS, CRACKED LEFT AND RIGHT SIDE. ROUTED OUT CRACKED MATERIAL BLENDED, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0. (M)