What was found
AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON STIFFENER ABOVE. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 2 SHT 2 VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON STIFFENER ABOVE. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 2 SHT 2 VOL I.