What was found
LT BS 1265 NR 1 HOLE FRAME WEB AND INNER STRUCTURE CRACKED. REPAIRED FRAME PER ENGINEERING CHANGE ORDER TASK CARD. SUSPECT PRESSURIZATION CYCLE FATIGUE DAMAGE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT BS 1265 NR 1 HOLE FRAME WEB AND INNER STRUCTURE CRACKED. REPAIRED FRAME PER ENGINEERING CHANGE ORDER TASK CARD. SUSPECT PRESSURIZATION CYCLE FATIGUE DAMAGE.