Phenom 300 CAS Messages Flashcards
The fire detection sensor senses fire/overheat in Engine 1 or Engine 2.
The fire detection sensor for engine 1 or engine 2 is unable to detect fire/overheat condition (failed).
Engine fire-extinguisher system has failed.
Engine fire-extinguisher bottle has been discharged.
Smoke Alarm in baggage area.
Failure of both smoke detector sensors.
Failure of one smoke detector sensor.
Indicates loss of Hydraulic System; system pressure is below normal operational range.
Hydraulic System fluid is over operating temperature range.
Indicates the EDP 1 (2) Fire Shut Off Valve was commanded to close and did not close.
Stall Protection not available. Stall warning operational.
Indicates degradation of Hydraulic System available power. AFM note advises for hydraulic users actuation rates degraded.
Low-level sensors indicate that 310 lbs of fuel remain in the respective tank.
Indicates a low pressure to the associated engine while engine is running.
Indicates a discrepancy between the commanded and actual valve status.
Indicates an imbalance of fuel between the two tanks greater than or equal to 220 lbs. It remains displayed until the imbalance is reduced to 132 lbs.
Indicates a discrepancy between the commanded and the actual valve status.
Refueling panel door is open and must be closed before takeoff.
Indicates a low pressure in the primary fuel feed system activating the DC pump.
Indicates a failure in the associated pressure switch.
Lateral fuel quantities are balanced (difference less than 44 lbs) when XFEED is open.
Indicates a discrepancy between the commanded and actual associated pump status or electric fuel pump failure.
Engine 1 (2) has detected a fire condition.
Engine 1 (2) message indicates that low oil pressure is detected on the engine.
Pilot may be unable to modulate thrust or engine will respond slowly.
Engine 1 (2) shutdown has occurred without pilot command.
Fuel filter impending bypass.
Dual thrust lever angle sensor failure.
TT0 sensor heating failed or ice crystals detected.
Takeoff data has not been successfully entered. This message is set while on ground only.
Engine 1 (2) chip is detected.
Avionics not receiving data from one FADEC channel.
Engine oil filter impending bypass set.
In-flight engine limit exceedance detected.
No dispatch condition detected by FADEC.
Oxygen cylinder pressure is below the accepted safety limit for dispatch, pressure sensor is failed, or the OXYGEN SUPPLY handle is pulled.
Passenger masks not deployed in a cabin depressurization condition. “This message will be available only if the rigid door between cockpit and passenger cabin door is installed.”
SUPPLY CONTROL knob not in PAX AUTO position.
A discrepancy between the position of the LDG GEAR lever and at least one landing gear is detected.
PARKING BRAKE is set and must be released prior to takeoff.
Loss of the antiskid protection mode.
Loss of wheel brakes on either the left or right landing gear.
Emergency/parking brake accumulator pressure is low < 1640psi
Indicates a failure condition in the WOW indication system.
Indicates the emergency/parking brake actuated condition (not RELeased). Must be released before landing or takeoff.
ADS 1(2) heater is failed or is OFF when it should be ON
Indicates the EAI shutoff valve is closed when valve is commanded open or a EAI duct failure is detected.
There is not enough thermal energy available for WHSAIS operation.
Pilots switches the WHSAIS ON out of the icing envelope.
There is a bleed hot air leakage at the WHSAIS pneumatic ducting.
There is a component failure (AIV, pressure transducers, AMS Controller, other)
Pilot switches the WHSAIS ON outside the icing envelope or the aircraft is in single bleed configuration OR pilot switches the WHSAIS ON above 15,000 feet inside icing envelope.
Indiactes that the airplane is flying in icing conditions. the message is available only on airplanes with an ice detector (optional item).
Pitot-Static probe heater is failed or is OFF when it should be ON.
Associated windshield is overheated or heating system has failed.
ADS heater manually activate on the ground.
Engine anti-ice system valve failed when commanded to close.
Engine anti-ice system is turned on and operating normally.
Pilot activates the WINGSTAB toggle switch prior to takeoff.
Indicates WHSAIS is operating.
Ice detector failed. This message is available only on airplanes with ice detector (optional item).
