What was found
FUSELAGE FRAME FS X 216.00, STR. 24P, CORROSION BETWEEN CLEAT AND STR. 24P. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME FS X 216.00, STR. 24P, CORROSION BETWEEN CLEAT AND STR. 24P. CORROSION BEYOND MANUFACTURES LIMITS, PART REPLACEMENT REQUIRED.