What was found
DURING 2C INSPECTION, TASK 5320-244-02I FOUND WING TO FUSELAGE FAIRING ATTACH ANGLE PART NR 120-31657-002 CRACKED. REPAIRED ANGLE IAW APPROVED AERO-DESIGN REPORT 1226-3 REV A 2-18-95.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 2C INSPECTION, TASK 5320-244-02I FOUND WING TO FUSELAGE FAIRING ATTACH ANGLE PART NR 120-31657-002 CRACKED. REPAIRED ANGLE IAW APPROVED AERO-DESIGN REPORT 1226-3 REV A 2-18-95.