What was found
DURING INSPECTION, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE 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, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE WAS REPLACED IAW SRM 51-40-02.