What was found
AFT UPPER FUSELAGE AFT BULKHEAD LOWER LEFT ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 53-40-00 FIG 6 VOL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT UPPER FUSELAGE AFT BULKHEAD LOWER LEFT ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 53-40-00 FIG 6 VOL 1.