Phenom 300 CAS Messages

Question 1

Answer 1

The fire detection sensor senses fire/overheat in Engine 1 or Engine 2.

Question 2

Answer 2

The fire detection sensor for engine 1 or engine 2 is unable to detect fire/overheat condition (failed).

Question 3

Answer 3

Engine fire-extinguisher system has failed.

Question 4

Answer 4

Engine fire-extinguisher bottle has been discharged.

Question 5

Answer 5

Smoke Alarm in baggage area.

Question 6

Answer 6

Failure of both smoke detector sensors.

Question 7

Answer 7

Failure of one smoke detector sensor.

Question 8

Answer 8

Indicates loss of Hydraulic System; system pressure is below normal operational range.

Question 9

Answer 9

Hydraulic System fluid is over operating temperature range.

Question 10

Answer 10

Indicates the EDP 1 (2) Fire Shut Off Valve was commanded to close and did not close.

Question 11

Answer 11

Stall Protection not available. Stall warning operational.

Question 12

Answer 12

Indicates degradation of Hydraulic System available power. AFM note advises for hydraulic users actuation rates degraded.

Question 13

Answer 13

Low-level sensors indicate that 310 lbs of fuel remain in the respective tank.

Question 14

Answer 14

Indicates a low pressure to the associated engine while engine is running.

Question 15

Answer 15

Indicates a discrepancy between the commanded and actual valve status.

Question 16

Answer 16

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.

Question 17

Answer 17

Indicates a discrepancy between the commanded and the actual valve status.

Question 18

Answer 18

Refueling panel door is open and must be closed before takeoff.

Question 19

Answer 19

Indicates a low pressure in the primary fuel feed system activating the DC pump.

Question 20

Answer 20

Indicates a failure in the associated pressure switch.

Question 21

Answer 21

Lateral fuel quantities are balanced (difference less than 44 lbs) when XFEED is open.

Question 22

Answer 22

Indicates a discrepancy between the commanded and actual associated pump status or electric fuel pump failure.

Question 23

Answer 23

Engine 1 (2) has detected a fire condition.

Question 24

Answer 24

Engine 1 (2) message indicates that low oil pressure is detected on the engine.

Question 25

Answer 25

Pilot may be unable to modulate thrust or engine will respond slowly.

Question 26

Answer 26

Engine 1 (2) shutdown has occurred without pilot command.

Question 27

Answer 27

Fuel filter impending bypass.

Question 28

Answer 28

Dual thrust lever angle sensor failure.

Question 29

Answer 29

TT0 sensor heating failed or ice crystals detected.

Question 30

Answer 30

Takeoff data has not been successfully entered. This message is set while on ground only.

Question 31

Answer 31

Engine 1 (2) chip is detected.

Question 32

Answer 32

Avionics not receiving data from one FADEC channel.

Question 33

Answer 33

Engine oil filter impending bypass set.

Question 34

Answer 34

In-flight engine limit exceedance detected.

Question 35

Answer 35

No dispatch condition detected by FADEC.

Question 36

Answer 36

Oxygen cylinder pressure is below the accepted safety limit for dispatch, pressure sensor is failed, or the OXYGEN SUPPLY handle is pulled.

Question 37

Answer 37

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.”

Question 38

Answer 38

SUPPLY CONTROL knob not in PAX AUTO position.

Question 40

Answer 40

A discrepancy between the position of the LDG GEAR lever and at least one landing gear is detected.

Question 41

Answer 41

PARKING BRAKE is set and must be released prior to takeoff.

Question 42

Answer 42

Loss of the antiskid protection mode.

Question 43

Answer 43

Loss of wheel brakes on either the left or right landing gear.

Question 44

Answer 44

Emergency/parking brake accumulator pressure is low < 1640psi

Question 45

Answer 45

Indicates a failure condition in the WOW indication system.

Question 46

Answer 46

Indicates the emergency/parking brake actuated condition (not RELeased). Must be released before landing or takeoff.

Question 47

Answer 47

ADS 1(2) heater is failed or is OFF when it should be ON

Question 48

Answer 48

Indicates the EAI shutoff valve is closed when valve is commanded open or a EAI duct failure is detected.

Question 49

Answer 49

There is not enough thermal energy available for WHSAIS operation.

Question 50

Answer 50

Pilots switches the WHSAIS ON out of the icing envelope.

Question 51

Answer 51

There is a bleed hot air leakage at the WHSAIS pneumatic ducting.

Question 52

Answer 52

There is a component failure (AIV, pressure transducers, AMS Controller, other)

Question 53

Answer 53

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.

Question 54

Answer 54

Indiactes that the airplane is flying in icing conditions. the message is available only on airplanes with an ice detector (optional item).

Question 55

Answer 55

Pitot-Static probe heater is failed or is OFF when it should be ON.

Question 56

Answer 56

Associated windshield is overheated or heating system has failed.

Question 57

Answer 57

ADS heater manually activate on the ground.

Question 58

Answer 58

Engine anti-ice system valve failed when commanded to close.

Question 59

Answer 59

Engine anti-ice system is turned on and operating normally.

Question 60

Answer 60

Pilot activates the WINGSTAB toggle switch prior to takeoff.

Question 61

Answer 61

Indicates WHSAIS is operating.

Question 62

Answer 62

Ice detector failed. This message is available only on airplanes with ice detector (optional item).