What was found
DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1418 BTW LONGERON 1 AND 2RT WITH 0.562" LENGTH. CRACK AREA ON FUSELAGE WAS CUT OUT AND FILLER, DOUBLER INSTALLED IAW ERA 497385-14 REV ORIG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1418 BTW LONGERON 1 AND 2RT WITH 0.562" LENGTH. CRACK AREA ON FUSELAGE WAS CUT OUT AND FILLER, DOUBLER INSTALLED IAW ERA 497385-14 REV ORIG.