What was found
DURING COMPLIANCE OF AD 88-10-07, ASB A27-269, FOUND THE RIGHT FLAP DRIVE LINK CRACKED AT POINT-J USING ULTRASONIC METHOD OF INSPECTION. REPLACED RIGHT FLAP DRIVE LINK IAW DC8 MM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING COMPLIANCE OF AD 88-10-07, ASB A27-269, FOUND THE RIGHT FLAP DRIVE LINK CRACKED AT POINT-J USING ULTRASONIC METHOD OF INSPECTION. REPLACED RIGHT FLAP DRIVE LINK IAW DC8 MM.