What was found
COCKPIT TEMP CONTROL GOES FULL HOT & FULL COLD, AUTO REGULATION INOPERATIVE. PERFORMED TEMP CONTROL SYS ADJUSTMENT AND TEST, SYS FUNCTIONS NORMAL IAW AMM 21-61-00/501.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COCKPIT TEMP CONTROL GOES FULL HOT & FULL COLD, AUTO REGULATION INOPERATIVE. PERFORMED TEMP CONTROL SYS ADJUSTMENT AND TEST, SYS FUNCTIONS NORMAL IAW AMM 21-61-00/501.