What was found
(AUS) INTERNAL SKIN REINFORCING STRAP LOCATED ON THE AFT SIDE OF FUSELAGE FRAME AT STA 1090 BETWEEN STRINGERS 26RT AND 27RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) INTERNAL SKIN REINFORCING STRAP LOCATED ON THE AFT SIDE OF FUSELAGE FRAME AT STA 1090 BETWEEN STRINGERS 26RT AND 27RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.