What was found
During HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ventral door jamb. Repaired per EA 99-191325.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ventral door jamb. Repaired per EA 99-191325.