What was found
AT C CHECK, RT FLAP SCISSOR PANEL HAS DELAMINATED INNER UPPER AREA. REMOVED PANEL, REPAIRED, AND INSTALLED PANEL PER MM 27-50-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, RT FLAP SCISSOR PANEL HAS DELAMINATED INNER UPPER AREA. REMOVED PANEL, REPAIRED, AND INSTALLED PANEL PER MM 27-50-0.