What was found
FUSELAGE SKIN CHAFED AT BS 2704-2705 BL 0 INSIDE APU COMPARTMENT. REMOVED DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED IAW DWG 53301313-1 AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CHAFED AT BS 2704-2705 BL 0 INSIDE APU COMPARTMENT. REMOVED DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED IAW DWG 53301313-1 AND SRM 51-40-02.