What was found
DURING COMPLIANCE OF A.D. 88-10-07, S.B. 27-246, A.S.B. 27-269 HAD CRACK INDICATION AT POINT J INBOARD SIDE RIGHT HAND FLAP LINK. REPLACED 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 OF A.D. 88-10-07, S.B. 27-246, A.S.B. 27-269 HAD CRACK INDICATION AT POINT J INBOARD SIDE RIGHT HAND FLAP LINK. REPLACED LINK IAW DC8 MM 27-51-4.