As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT AILERON WILL NOT TEST WITH SYSTEM 2 PRESSURE VERIFIED AT 2900 PSI. FOUND PCU OUTPUT LINK FOR SYSTEM 2 (INBOARD) BROKEN FORWARD OF AILERON ATTACH. REMOVED AND REPLACED OUTPUT LINK (P/N 27295-3) WITH SERVICEABLE (P/N 27295-5) IAW CANADAIR MM 27-14-15-400-801.