What was found
DURING 4800/9600 HOUR STRUCTURAL INSP, DISCOVERED LONGERON AT FUSELAGE STA 127 LT SIDE CRACKED APPROX 3 INCHES. REMOVED DAMAGED LONGERON FRAME AT FUSELAGE STA 127 LT SIDE. NEW PART FABRICATED AND REPAIR INSTALLED IAW REPORT NR 8173-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 4800/9600 HOUR STRUCTURAL INSP, DISCOVERED LONGERON AT FUSELAGE STA 127 LT SIDE CRACKED APPROX 3 INCHES. REMOVED DAMAGED LONGERON FRAME AT FUSELAGE STA 127 LT SIDE. NEW PART FABRICATED AND REPAIR INSTALLED IAW REPORT NR 8173-1.