What was found
DRIVE LINK FITTING STIFFENER ANGLE CRACKED, LEFT WING, FLAP STATION 3.00. REPAIRED IAW DC8 SRM 53-8-1 AND 51-1-20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DRIVE LINK FITTING STIFFENER ANGLE CRACKED, LEFT WING, FLAP STATION 3.00. REPAIRED IAW DC8 SRM 53-8-1 AND 51-1-20.