What was found
FUSELAGE FRAME STRAP WAS CHAFED AT BS 859.5, STRINGER 18L. R & R THE FRAME STRAP IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME STRAP WAS CHAFED AT BS 859.5, STRINGER 18L. R & R THE FRAME STRAP IAW SRM 51-40-02-0G-0.