What was found
DURING COMPLIANCE WITH AD 88-10-07, FOUND FLAP DRIVE LINK CRACKED AT POINT J. REPLACED FLAP DRIVE LINK IAW DC8 MM 27-51-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING COMPLIANCE WITH AD 88-10-07, FOUND FLAP DRIVE LINK CRACKED AT POINT J. REPLACED FLAP DRIVE LINK IAW DC8 MM 27-51-4.