What was found
PRESSURIZATION WOULD NOT REACH MAX DIFFERENTIAL. REPLACED ELECTRONIC CONTROLLER AND OUTFLOW VALVE, OPS CHECKED SYSTEM SATISFACTORY.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PRESSURIZATION WOULD NOT REACH MAX DIFFERENTIAL. REPLACED ELECTRONIC CONTROLLER AND OUTFLOW VALVE, OPS CHECKED SYSTEM SATISFACTORY.