What was found
TAIL COMPT 60 L17R HAS 2.5 IN CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND INSTALLED L17R STA 1771 IAW SRM'S 53-2-2 FIG10, 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL COMPT 60 L17R HAS 2.5 IN CRACK AT END FITTING STA 1771 (LWR SURFACE OF UPPER LEG). REMOVED FABRICATED AND INSTALLED L17R STA 1771 IAW SRM'S 53-2-2 FIG10, 51-1-21, 51-1-20D, 51-3-0 AND DWG 5649327.