What was found
DURING D-CHECK, AFT FUS SKIN CRACKED AT LT PYLON UPPER ATTACH ANGLE, 1.5 INCH AT STA 991 UNDER LONGERON 15L. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 53-04, PG 279 FIG 46.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, AFT FUS SKIN CRACKED AT LT PYLON UPPER ATTACH ANGLE, 1.5 INCH AT STA 991 UNDER LONGERON 15L. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 53-04, PG 279 FIG 46.