What was found
DURING C-04 CHECK IN TPE, CRACK .55 INCH FOUND ON UPPER HORIZONTAL DECK OF FORWARD AFT FUSELAGE COMPARTMENT AT EMPENNAGE STA Y=2015, X=-14, Z=+61. INSTALLED REPAIR PER MD-11 SRM VOL.I 53-00-01 REV.38 FIG.10
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-04 CHECK IN TPE, CRACK .55 INCH FOUND ON UPPER HORIZONTAL DECK OF FORWARD AFT FUSELAGE COMPARTMENT AT EMPENNAGE STA Y=2015, X=-14, Z=+61. INSTALLED REPAIR PER MD-11 SRM VOL.I 53-00-01 REV.38 FIG.10