What was found
DURING OP16, FOUND FS 1038 REAR ENGINE MOUNT WEB, TOP FWD END OF INTERCOSTAL IS CRACKED IN THE WEB RADIUS 13 INCHES FROM THE FUSELAGE. INSTALLED DOUBLER TOP FORWARD END OF THE INTERCOSTAL PER SRM 54-01 FIG 2 PG 7. OP16 05-15-00 MCI.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP16, FOUND FS 1038 REAR ENGINE MOUNT WEB, TOP FWD END OF INTERCOSTAL IS CRACKED IN THE WEB RADIUS 13 INCHES FROM THE FUSELAGE. INSTALLED DOUBLER TOP FORWARD END OF THE INTERCOSTAL PER SRM 54-01 FIG 2 PG 7. OP16 05-15-00 MCI.