What was found
CRACK AT AFT END OF E&E COOLING EXHAUST PORT AT CENTER OF FUSELAGE. INSTALLED REPAIR PER EC/RA 5330-03806, STEPS 1-19. PLACED ON DIP FOR PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 12 MONTHS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK AT AFT END OF E&E COOLING EXHAUST PORT AT CENTER OF FUSELAGE. INSTALLED REPAIR PER EC/RA 5330-03806, STEPS 1-19. PLACED ON DIP FOR PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 12 MONTHS.