What was found
LOWER AFT CHORD ANGLE IS CRACKED AT 19, 22, 32, 37, 54 AND 59 FORM I/B END OF FLAP. REPAIR PER M/M 57/52/0 FIG 802.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER AFT CHORD ANGLE IS CRACKED AT 19, 22, 32, 37, 54 AND 59 FORM I/B END OF FLAP. REPAIR PER M/M 57/52/0 FIG 802.