What was found
CENTER FUSELAGE ONE LT, AFT STEP ANGLE CRACKED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE ONE LT, AFT STEP ANGLE CRACKED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.