What was found
FUSELAGE DENTED AT BS 1620 STRINGER 19. MEASURED DENT REF SRM 53-00-01 A-Y=38.83 A=4.0 Y=.103. HFEC VERIFIED NO CRACK INDICATION REF UAL NDT P6 51-00-01. REMOVED DAMAGE, INSTALLED DOUBLER PER ECRA 5330-04278.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE DENTED AT BS 1620 STRINGER 19. MEASURED DENT REF SRM 53-00-01 A-Y=38.83 A=4.0 Y=.103. HFEC VERIFIED NO CRACK INDICATION REF UAL NDT P6 51-00-01. REMOVED DAMAGE, INSTALLED DOUBLER PER ECRA 5330-04278.