What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE FS 1143 CANTED FRAME FORWARD OF THE INTERIOR TAILCONE RELEASE HANDLE. REPAIRED PER XEA X9-53-88.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE FS 1143 CANTED FRAME FORWARD OF THE INTERIOR TAILCONE RELEASE HANDLE. REPAIRED PER XEA X9-53-88.