What was found
EXTERNAL FUSELAGE, STA 1422 LT SIDE. SKIN DENTED 4.0'' BELOW VERTICAL FIN Y=.080'' A=1.25'' A/Y = 15, REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, REF SRM 51-40-2, PG 1-6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERNAL FUSELAGE, STA 1422 LT SIDE. SKIN DENTED 4.0'' BELOW VERTICAL FIN Y=.080'' A=1.25'' A/Y = 15, REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, REF SRM 51-40-2, PG 1-6.