What was found
WHILE ACCELERATING BETWEEN 200 AND 250 PITCH FELL FAIL CAS MESSAGE ILLUMINATED. REMOVED ACTUATOR AND INSTALLED COMPLETED PITCH FEEL SYS FUNCTIONAL TEST, FOUND NORMAL. WORK DONE IAW MM CHAPTER 27-30-00 AND 27-33-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE ACCELERATING BETWEEN 200 AND 250 PITCH FELL FAIL CAS MESSAGE ILLUMINATED. REMOVED ACTUATOR AND INSTALLED COMPLETED PITCH FEEL SYS FUNCTIONAL TEST, FOUND NORMAL. WORK DONE IAW MM CHAPTER 27-30-00 AND 27-33-00.