What was found
DURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81& STRINGER 8R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81& STRINGER 8R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.