What was found
LOWER CHORD ANGLE CRACKED AT 55 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIGURE 802.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER CHORD ANGLE CRACKED AT 55 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIGURE 802.