What was found
FUSELAGE FRAME CHAFED AT BS 2701 BL 0 INSIDE APU COMPARTMENT. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-11, FIG. 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME CHAFED AT BS 2701 BL 0 INSIDE APU COMPARTMENT. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-11, FIG. 1.