What was found
DURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C CHECK INSPECTION, RT FLAP SUPPORT FITTING CRACKED AT STA. XW 410.000. REMOVED AND REPLACED RT FLAP LINK SUPPORT AT STA XW 410.000 IAW DC8 MM 27-51-12 PAGES 201-204. REFER TO N/R FOR OPS CHECK.