What was found
DURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 5 STIFFENER CLIP. REPAIRED IAW SRM 53-10-25.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING "H" CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD NR 5 STIFFENER CLIP. REPAIRED IAW SRM 53-10-25.