What was found
AFT FUSELAGE INT FOUND CRACK ON TEE CAP VERTICAL STIFFENER. REPAIRED AREA IAW SRM 53-00-01, FIG 19, VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE INT FOUND CRACK ON TEE CAP VERTICAL STIFFENER. REPAIRED AREA IAW SRM 53-00-01, FIG 19, VOL I.