What was found
DURING ROUTINE MAINTENANCE, FOUND A 2 INCH CRACK ON LEFT WING FLAP FITTING, STA 220 INBOARD SIDE. REMOVED AND REPLACED FLAP SUPPORT FITTING IAW DOUGLAS MM, CHAPTER 27-27-7 AND ACCOMPLISHED FLAP RIG CHECK IAW CHAPTER 27-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE MAINTENANCE, FOUND A 2 INCH CRACK ON LEFT WING FLAP FITTING, STA 220 INBOARD SIDE. REMOVED AND REPLACED FLAP SUPPORT FITTING IAW DOUGLAS MM, CHAPTER 27-27-7 AND ACCOMPLISHED FLAP RIG CHECK IAW CHAPTER 27-30-0.