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Cessna CE-680 Sovereign PTM Questions (Rev 5.0) > CAS - Advisory Messages > Flashcards

CAS - Advisory Messages Flashcards

1
Q

AC BEARING L-R

A

This message indicates impending alternator bearing failure. Maintenance is required within 20 hours of the message being posted.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS, WITH EXCEPTIONS

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2
Q

AHRS BASIC L-R

A

This message indicates that the respective AHRS has lost air data information and has entered a reversionary mode, which may result in degradation in pitch and roll accuracy in certain flight conditions.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS

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3
Q

ANTI-ICE ON ALL

A

This message is displayed when all anti-ice is selected ON.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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4
Q

ANTI-ICE ON ENGINE/STAB

A

This message is displayed when engine/stab anti-ice is selected ON and either wing anti-ice is selected OFF. This message is not displayed when the ANTI-ICE ON ALL CAS message is displayed.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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5
Q

AP FAIL A-B

A

This message indicates the autopilot has failed. A loss of the guidance panel, aileron servo, or elevator servo will also cause the message to be displayed. The AFCS will automatically select the other side if it is available.

INHIBITS: LOPI, TOPI, BFI
DEBOUNCE: 1 SECOND

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6
Q

APU ON

A

This message is displayed when the APU is running and altitude is less than or equal to FL300. This message is amber if altitude is greater than FL300.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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7
Q

AUX HYDRAULIC PUMP

A

This message indicates that the HYDRAULIC PUMP AUX button has been selected ON. When the use of the pump is not required, the buttons should be selected OFF to conserve pump life.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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8
Q

BAGGAGE HEAT FAIL

A

This message is displayed in flight if the baggage heat shutoff valve fails to open to provide heat to the baggage compartment.

INHIBITS: LOPI, TOPI
DEBOUNCE: 5 SECONDS

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9
Q

BATTERY OFF L-R

A

This message indicates the respective battery (L or R BATT button) has been selected OFF in response to a battery overtemperature condition and the battery overtemperature still exists.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS

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10
Q

BLEED SELECT NOT NORM

A

This message is displayed when an engine bleed air source is selected to other than normal position in the air.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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11
Q

BUS TIE CLOSED

A

This message is displayed when the bus tie contactor between the emergency buses is closed. To accommodate in-flight engine or APU starts, selected cases start out cyan and change to amber after 5 minutes when an electrical source is active on both sides.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS

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12
Q

CABIN ALTITUDE

A

This message indicates the cabin altitude is above 8,000 feet and the pressurization controller is set for the high elevation airfield mode. This message will be amber if the cabin altitude is above 9,650 feet for more than 30 minutes. This message will be red if the cabin altitude is above 14,500 feet while operating in the high elevation airfield mode.

INHIBITS: LOPI, TOPI, BFI
DEBOUNCE: STANDARD

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13
Q

ENG ANTI-ICE COLD L-R

A

ON GROUND: This message is displayed cyan when the respective engine anti-ice is selected ON and the inlet lip surface is cold (below 60˚ C). This message should clear within 2.5 minutes of selecting the button ON; otherwise the message will turn amber. IN FLIGHT: This message is displayed cyan if the inlet lip surface is cold (below 60˚ C) due to automatic shutoff from an engine anti-ice overheat condition.

INHIBITS: LOPI, TOPI, ESDI
DEBOUNCE: STANDARD

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14
Q

ENGINE DISPATCH LIMIT L-R

A

This message is displayed when the respective engine FADEC has detected a condition that will require a logbook entry and maintenance within 125 hours of the message being posted. This message is inhibited in flight. Pressing the EVENT MARKER on the pilot’s lower left panel will record additional information to assist maintenance.

Inhibits: LOPI, TOPI, IN AIR; Debounce: STANDARD

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15
Q

ENGINE SHUTDOWN L-R

A

This message is displayed when the engine throttle has shutdown the respective engine or when a below idle recovery is in progress. The message clears after completion of the engine start sequence.

Inhibits: NONE; Debounce: STANDARD

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16
Q

FDR FAIL

A

This message indicates the flight data recorder has failed.

Inhibits: LOPI, TOPI, BFI; Debounce: 7 SECONDS

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17
Q

FIRE BOTTLE LOW BAG-APU

A

This message indicates the rapid discharge baggage compartment/APU fire bottle pressure is low because the bottle has discharged. The baggage heat valve will close and the APU will shut down automatically. The APU will be inhibited from starting.

Inhibits: LOPI, TOPI; Debounce: 2 SECONDS

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18
Q

FIRE BOTTLE LOW BAGGAGE

A

This message indicates the metered discharge baggage compartment fire bottle pressure is low because the bottle has discharged. The baggage heat valve will close.

Inhibits: LOPI, TOPI; Debounce: 2 SECONDS

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19
Q

FUEL BOOST PUMP ON L-R

A

This message is displayed when the fuel pump is on in normal operation (i.e., FUEL BOOST L or R button selected ON by the crew, or automatically comes on during an engine start).

Inhibits: LOPI, TOPI, EDSI; Debounce: STANDARD

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20
Q

FUEL CROSS FEED

A

This message is displayed when the fuel crossfeed valve is open and fuel is flowing from the tank with more fuel. This message will be amber when fuel is flowing from the tank with less fuel.

Inhibits: LOPI, TOPI; Debounce: STANDARD

21
Q

FUEL FW SHUTOFF L-R

A

This message is displayed when the fuel firewall shutoff valve is fully closed.

Inhibits: LOPI, TOPI; Debounce: STANDARD

22
Q

GROUND PROX FAIL

A

This message indicates the TAWS computer has detected a fault or a required airplane system input has been lost. All TAWS functions will be inoperative and the annunciations will be inhibited. If the TAWS FLAP OVERRIDE CAS message is also displayed and the airspeed is over 250 KIAS, verify TAWS FLAP OVRD is selected OFF.

Inhibits: LOPI, TOPI, BFI; Debounce: 2 SECONDS

23
Q

INBD WING A/I COLD L-R on the ground

A

Displayed cyan when the inboard wing anti-ice is ON and the surface is cold (below 18˚ C). It should clear within 2.5 minutes; otherwise, it turns amber.

24
Q

INBD WING A/I COLD L-R

A

Displayed cyan if the surface is cold (below 18˚ C) due to automatic shutoff from a wing anti-ice overheat condition or a wing bleed leak condition.

25
IRS ALIGNING L-R
Displayed when the IRS is aligning. Only shown if the optional IRS is installed.
26
NO TAKEOFF
Displayed on the ground if any no takeoff items are active. It turns red when throttles are advanced. Crews should refer to the NO TAKEOFF window on the MFD.
27
OIL FILTER BYPASS L-R
Displayed when the pressure across the oil filter is large due to debris contamination. Active when oil temperature is greater than -38˚ C.
28
OIL LEVEL LOW L-R
Displayed when a fault occurs in the oil level low sensor. If engine oil level is low, it will be amber. Only displayed on the ground.
29
PARKING BRAKE ON
Displayed when the parking brake is on and brake pressure is adequate. It will be amber when a throttle is advanced on the ground or in the air.
30
PHONE CALL
Indicates that there is an incoming phone call to the airplane.
31
PITOT/STATIC COLD L-R-STBY
Displayed on the ground with the ANTI-ICE PITOT/STATIC buttons OFF. Will be amber in flight or on the ground when a throttle is advanced.
32
RAAS FAIL
Displayed when the optional runway awareness advisory system (RAAS) is enabled but the function is inoperative.
33
RAAS INHIB
This message is displayed when the optional RAAS is enabled but advisories are inhibited because TAWS MUTE is selected ON.
34
RAAS NOT AVAIL
This message is displayed when the optional RAAS is enabled but the system either has no position information or the airplane is at an airport that has not been validated.
35
SELCAL VHF 1-2 HF 1-2
This message is displayed when the SELCAL system receives a VHF or HF radio transmission with the airplane specific tone sequence. ## Footnote Inhibits: LOPI, TOPI Debounce: 2 SECONDS
36
STAB ANTI-ICE COLD L-R on the ground
This message is displayed cyan when the respective stabilizer anti-ice is selected ON and the surface is cold (below 10˚ C). This message should clear within 2.5 minutes of selecting the button ON; otherwise the message will turn amber.
37
STAB ANTI-ICE COLD L-R in flight
This message is displayed cyan if the surface is cold (below 10˚ C) due to automatic shutoff from a stabilizer anti-ice overheat condition or a stabilizer bleed leak condition. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
38
STEEP APPROACH MODE
This message is displayed when the steep approach mode has been selected ON. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
39
TAWS AUDIO INHIB
This message is displayed when the TAWS MUTE is selected ON. The windshear (mode 7) function remains active. ## Footnote Inhibits: LOPI, TOPI Debounce: 2 SECONDS
40
TAWS FLAP OVERRIDE
This message is displayed when the TAWS FLAP OVRD is selected ON. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
41
TAWS GLIDESLOPE CANCEL
This message is displayed when TAWS G/S CANCEL is selected ON. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
42
TERRAIN FAIL
This message is displayed when the TAWS is unable to display terrain and obstacles or provide enhanced mode alert warnings. Basic TAWS (modes 1-6) and windshear (Mode 7) remain active. ## Footnote Inhibits: LOPI, TOPI, BFI Debounce: STANDARD
43
TERRAIN INHIBITED
This message is displayed when the TAWS TERR INHIB is selected ON. Basic TAWS (Modes 1-6) and windshear (Mode 7) remain active. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
44
WINDSHEAR FAIL
This message is displayed when the windshear warning system computer has detected a fault or a required airplane system input has been lost. All windshear warning and caution functions will be inoperative and the annunciations will be inhibited. ## Footnote Inhibits: LOPI, TOPI, BFI Debounce: 2 SECONDS
45
WING A/I CROSSFLOW OPEN
This message is displayed when the ANTIICE WING/STAB XFLOW button has been selected to XFLOW and the wing crossflow valve is open. It will be amber if the valve is not fully closed and the ANTIICE WING/STAB XFLOW button is selected to OFF. ## Footnote Inhibits: LOPI, TOPI; Debounce: 5 seconds
46
WING ANTI-ICE COLD L-R on ground
This message is displayed cyan when the respective outboard wing anti-ice (ANTI-ICE WING L-R button) is selected ON and the surface is cold (below 16˚ C). It should clear within 2.5 minutes of selecting the button ON; otherwise, it will turn amber. ## Footnote Inhibits: LOPI, TOPI; Debounce: Standard
47
WING ANTI-ICE COLD L-R in flight
This message is displayed cyan if the surface is cold (below 16˚ C) due to automatic shutoff from a wing anti-ice overheat condition or a wing bleed leak condition. ## Footnote Inhibits: LOPI, TOPI; Debounce: Standard
48
YD FAIL A-B indicate?
This message indicates the respective yaw damper system has failed. A loss of the guidance panel or rudder servo will also cause the message to be displayed. The AFCS will automatically select the other side if it is available. ## Footnote Inhibits: LOPI, TOPI, BFI; Debounce: 1 second

Cessna CE-680 Sovereign PTM Questions (Rev 5.0) (4 decks)

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