What was found
(CAN) DURING ROUTINE INSPECTION A CRACK WAS FOUND ALONG THE INSIDE WELD OF THE PRIMARY INLET HEADER (AMS 4015)REF: HAM STD CMM 21-51-50
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING ROUTINE INSPECTION A CRACK WAS FOUND ALONG THE INSIDE WELD OF THE PRIMARY INLET HEADER (AMS 4015)REF: HAM STD CMM 21-51-50