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

CAS - Caution Messages Flashcards

1
Q

ACM BLEED LEAK

A

This message is displayed when a bleed leak is detected in the vicinity of the air cycle machine (ACM). The ACM will automatically turn off, emergency pressurization will automatically come on and the EMERGENCY PRESSURIZATION CAS message will be displayed. If the APU is running when the ACM BLEED LEAK CAS message occurs, the APU will shutdown automatically and will be unavailable for the remainder of the flight even if the ACM BLEED LEAK CAS message clears.

INHIBITS: LOPI, TOPI; DEBOUNCE: STANDARD

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2
Q

ACM O’TEMP

A

This message is displayed when an overtemperature of the ACM is detected. The ACM will automatically turn off, emergency pressurization will automatically come on and the EMERGENCY PRESSURIZATION CAS message will be displayed. Emergency pressurization will automatically turn off and the ACM will come back on after the ACM has cooled down.

INHIBITS: LOPI, TOPI; DEBOUNCE: STANDARD

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3
Q

ANTISKID FAIL

A

This message is displayed when an antiskid fault lasting for more than 1 second has been detected or if the antiskid system is turned off.

INHIBITS: TOPI, BFI; DEBOUNCE: 1 SECOND, WITH EXCEPTIONS

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4
Q

AOA HEAT FAIL L-R

A

This message is displayed when the ANTIICE PITOT/STATIC buttons are selected ON and current is not detected at the respective AOA probe. Affected side stall warning and low speed awareness may be unreliable in icing conditions.

INHIBITS: LOPI, TOPI; DEBOUNCE: 2 SECONDS

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5
Q

AOA/STALL WARN FAIL L-R

A

This message is displayed when the AOA and/or stick shaker function has failed. Affected side stick shaker, low speed awareness, and on-speed carat will be inoperative. If left AOA, the AOA indexer display will be inoperative.

INHIBITS: LOPI, TOPI, BFI; DEBOUNCE: 2 SECONDS

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6
Q

AP STAB TRIM INOP

A

This message is displayed when autopilot control of the horizontal stabilizer trim is inoperative.

INHIBITS: LOPI, TOPI, BFI; DEBOUNCE: 1 SECOND

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7
Q

APU FIRE DETECT FAIL

A

This message is displayed when the APU SYSTEM MASTER button is selected ON and the APU fire detect system is inoperative. The APU will not start and will automatically shut down if it is running.

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

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8
Q

APU ON

A

This message is displayed when the APU is running and altitude is greater than FL300. This message is only displayed on airplanes incorporating Epic Phase 5 software. This message is cyan when altitude is less than or equal to FL300.

INHIBITS: LOPI, TOPI; DEBOUNCE: STANDARD

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9
Q

ASCB BUS FAIL

A

This message is displayed when any line replaceable unit (LRU) detects an ASCB communication problem. Only the primary buses are checked in flight. The primary and backup buses are checked on the ground. Each LRU is inhibited from triggering the message when its respective bus power is off. Cross-side data may not be available.

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

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10
Q

BAGGAGE DOOR OPEN

A

This message is displayed when any baggage door sensor indicates the door is not fully closed, any of the four clasps are unlatched, or any one or more of the sensors are faulted.

INHIBITS: LOPI, TOPI, BFI
DEBOUNCE: 2 SECONDS

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11
Q

BATTERY O’CURRENT L-R

A

This message is displayed when the battery current is ≥ 200 amps (positive or negative).

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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12
Q

BATTERY OFF L-R

A

This message is displayed when the respective L BATT or R BATT button has been selected OFF.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS

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13
Q

BLEED AIR MONITOR FAIL

A

This message is displayed when one or both bleed air monitor cards have failed. If both cards have failed, the cabin altitude warning system will be inoperative.

INHIBITS: LOPI, TOPI
DEBOUNCE: 5 SECONDS

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14
Q

BLEED AIR O’TEMP L-R

A

This message is displayed when the bleed air temperature from the respective precooler has exceeded 293˚ C for more than 20 seconds or 316˚ C instantly.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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15
Q

BLEED SELECT NOT NORM L-R

A

This message indicates the bleed air selector is not in the normal position with the airplane on the ground.

INHIBITS: LOPI, TOPI
DEBOUNCE: STANDARD

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16
Q

BUS TIE CLOSED

A

This message is displayed when the bus tie contactor between the emergency buses is closed.

INHIBITS: LOPI, TOPI
DEBOUNCE: 2 SECONDS

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17
Q

CABIN ALTITUDE

A

This message is displayed when the cabin altitude exceeds 8,500 feet due to failure of the pressurization system.

INHIBITS: LOPI, TOPI, BFI
DEBOUNCE: STANDARD

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18
Q

CABIN DOOR OPEN

A

This message is displayed when the cabin door switches indicate the door is in the open position, the inner handle is not secured, the locks are not engaged, or the monitor system operation has not been verified correct.

INHIBITS: LOPI, TOPI, BFI
DEBOUNCE: STANDARD

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19
Q

CAT2

A

The Category II approach mode criteria are not met, and Category II approach minimums are not authorized. This message is displayed when the RAD/BARO knob is set to RAD and minimums are less than 200 feet.

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20
Q

CHECK DU 1-2-3-4

A

The display unit wrap-around monitor has failed, and the affected display unit may present misleading information. DUs are numbered from left to right.

Inhibits: LOPI, TOPI, BFI
Debounce: 5 SECONDS

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21
Q

CONFIGURATION MISMATCH

A

A configuration monitor function detects that the software and/or hardware versions are not in a certified configuration. This message is displayed on the ground.

Inhibits: LOPI, TOPI, IN AIR
Debounce: 30 SECONDS

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22
Q

DC EMER BUS L-R

A

The respective emergency bus isolation relay is open, either due to DC generator overcurrent protection or pilot selection of the affected electrical L or R ELEC buttons to EMER. The affected R or L ELEC button will indicate amber EMER.

Inhibits: LOPI, TOPI
Debounce: 2 SECONDS

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23
Q

DC GEN O’CURRENT L-R-APU

A

The current for the respective generator is too high. This message is inhibited during engine start and for 2 minutes after start.

Inhibits: LOPI, TOPI
Debounce: 20 SECONDS

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24
Q

DC GEN OFF L-R-APU

A

A source of generator power is available, but the respective generator is not online. If the associated DC EMER BUS L-R CAS message is also displayed, an overcurrent condition was detected on the main bus or one of its extension buses.

Inhibits: LOPI, TOPI, BFI
Debounce: 2 SECONDS

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25
DU 1-2-3-4 O’TEMP
The respective display unit detects an overtemperature and will shut down due to the overtemperature. ## Footnote Inhibits: LOPI, TOPI Debounce: 2 SECONDS
26
DUCT O’TEMP CABIN
The cabin duct temperature exceeds 149˚ C. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
27
DUCT O’TEMP COCKPIT
The cockpit duct temperature exceeds 149˚ C. ## Footnote Inhibits: LOPI, TOPI Debounce: STANDARD
28
EMERGENCY EXIT OPEN
An emergency exit door sensor indicates that the emergency exit door is unlatched or the door sensor is faulted. ## Footnote Inhibits: LOPI, TOPI, BFI Debounce: 2 SECONDS
29
EMERGENCY PRESSURIZATION
This message is displayed when emergency pressurization is active. It is automatically turned on during ACM overtemperature, ACM bleed leak, or cabin altitude greater than 14,500 feet. ## Footnote Inhibits: LOPI, TOPI; Debounce: 0.5 seconds
30
ENG ANTI-ICE COLD L-R on the ground
This message is displayed when the preflight check has failed, the stator anti-ice valve is not open, or the surface has not achieved adequate temperature for anti-icing. ## Footnote If present after a satisfactory preflight check, the surface is cold and can be cleared by waiting for it to warm up. Inhibits: LOPI, TOPI; Debounce: Standard
31
ENG ANTI-ICE COLD L-R in flight
This message is displayed when an undertemperature condition of the engine inlet is detected or the engine stator anti-ice valve has not opened fully. ## Footnote Inhibited for 2.5 minutes after turning the system on. Inhibits: LOPI, TOPI, ESDI; Debounce: Standard
32
ENG ANTI-ICE O’TEMP L-R
This message is displayed when an overtemperature condition of the engine inlet is detected. The system automatically closes the respective engine anti-ice shut off valve. ## Footnote Overtemperature monitoring is active at all times. Inhibits: LOPI, TOPI; Debounce: Standard
33
ENG FIRE BOTTLE LOW 1-2
This message is displayed when the respective engine fire bottle pressure is low. ## Footnote Inhibits: LOPI, TOPI; Debounce: 5 seconds
34
ENG FIRE DETECT FAIL L-R
This message indicates the affected engine fire detection system is inoperative. ## Footnote Inhibits: LOPI, TOPI; Debounce: 2 seconds, with exceptions
35
ENGINE CHIP DETECT L-R
This message is displayed when metal chips have been detected in the engine oil by the electronic magnetic chip detector switch. ## Footnote Inhibits: LOPI, TOPI, ESDI; Debounce: 5 seconds
36
ENGINE CONTROL FAULT L-R
This message is displayed when the redundancy of the engine control systems is reduced due to FADEC detecting an internal fault or sensor miscompare. ## Footnote Inhibits: LOPI, TOPI, BFI, EFI; Debounce: 1 second
37
FD MODE OFF
This message is displayed when the AFCS has dropped the selected modes and reverted to basic pitch and roll modes. ## Footnote Inhibits: LOPI, TOPI, ON GROUND; Debounce: Standard
38
FLAPS FAIL
This message is displayed when the flaps have failed. The amber FLAPS RESET light will illuminate and the flap position indicator will be amber. ## Footnote Flap position may not match flap handle. Inhibits: LOPI, TOPI, BFI; Debounce: 1 second
39
FMS 1-2 GPS MISCOMPARE
This message is displayed when the FMS calculated position does not agree with the GNSS sensor position. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 6 SECONDS
40
FUEL BOOST PUMP ON L-R
This message is displayed when the pump is activated by the low pressure switch. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
41
FUEL CROSS FEED
This message is displayed when the crossfeed valve is open and flow is in the wrong direction with an imbalance more than 60 pounds. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
42
FUEL CROSS FEED TRANSIT
This message is displayed when the cross feed valve is neither fully open nor closed. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
43
FUEL FILTER BYPASS L-R
This message is displayed when there is an impending bypass of the fuel filter due to fuel contamination. ## Footnote INHIBITS: LOPI, TOPI, ESDI DEBOUNCE: 2 SECONDS
44
FUEL FW S/O TRANSIT L-R
This message is displayed when the fuel firewall shutoff valve is neither fully open nor closed. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 2 SECONDS
45
FUEL LEVEL LOW L-R
This message is displayed when the affected tank fuel quantity is less than 540 ± 60 pounds. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 90 SECONDS, WITH EXCEPTIONS
46
FUEL MOTIVE VLV FAIL L-R
This message is displayed when crossfeed is selected and the opposite side motive flow pressure failed to drop. ## Footnote INHIBITS: LOPI, TOPI, ESDI DEBOUNCE: 10 SECONDS
47
FUEL PRESSURE LOW L-R
This message is displayed when the fuel supplied to the engine is low. ## Footnote INHIBITS: LOPI, TOPI, BFI, ESDI DEBOUNCE: 1 SECOND, WITH EXCEPTIONS
48
GPS 1-2 INACTIVE
This message is displayed when one or both GNSS sensors become inactive. FMS position will continue to be computed from the remaining GNSS sensor, DME/DME, VOR/DME or optional IRS information. ## Footnote INHIBITS: LOPI, TOPI, BFI, ESDI; DEBOUNCE: 6 SECONDS
49
GROUND IDLE L-R
This message is displayed when the FADEC is in ground mode when the airplane is actually in the air. ## Footnote INHIBITS: TOPI, ESDI, ON GROUND; DEBOUNCE: STANDARD
50
HYDRAULIC PRESSURE HIGH
This message indicates excessive hydraulic system pressure. ## Footnote INHIBITS: LOPI, TOPI; DEBOUNCE: 10 SECONDS
51
HYDRAULIC PRESSURE LOW L-R
This message is displayed when one or both hydraulic pumps are not operating due to failure or crew selection. Hydraulically powered systems will operate normally if only one side’s pressure is low. ## Footnote INHIBITS: TOPI; DEBOUNCE: 3 SECONDS
52
HYDRAULIC VOLUME LOW
This message is displayed when the hydraulic reservoir volume is less than 120 cubic inches. ## Footnote INHIBITS: TOPI; DEBOUNCE: 1 SECOND
53
INBD WING A/I COLD L-R on ground
This message is displayed when either the preflight check has failed or the surface has not achieved adequate temperature for anti-icing. If this message is present after a satisfactory preflight check, then the surface is cold and can be cleared by continuing to wait for the surface to warm up. ## Footnote INHIBITS: LOPI, TOPI; DEBOUNCE: STANDARD
54
INBD WING A/I COLD L-R in flight
This message is displayed when an undertemperature condition of the inboard wing is detected. The inboard wing is considered part of engine anti-ice protection and is turned on with the ANTI-ICE ENGINE/STAB buttons. This message is inhibited for 2.5 minutes after turning the system on to allow the surface to achieve adequate temperature for anti-icing. ## Footnote INHIBITS: LOPI, TOPI; DEBOUNCE: STANDARD
55
IRS FAIL L-R
This message is displayed when the IRS has detected an internal failure. The red ATT and HDG messages may also be displayed on the affected side PFD and MFD. This message is only displayed if the optional IRS is installed. ## Footnote INHIBITS: LOPI; DEBOUNCE: STANDARD
56
IRS NOT READY
This message is displayed on the ground only when there is excessive motion of the airplane before IRS alignment is complete. This message is only displayed if the optional IRS is installed. ## Footnote INHIBITS: IN AIR; DEBOUNCE: STANDARD
57
IRS POSITION FAULT
This message is displayed when the IRS position is not entered (FME position not initialized) or there is an IRS alignment fault. This message is only displayed if the optional IRS is installed. ## Footnote INHIBITS: NONE; DEBOUNCE: STANDARD
58
LAVATORY DOOR
This message is displayed when the lavatory doors in the aft cabin are not latched open in the taxi, takeoff, approach, or landing configurations. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
59
MACH TRIM FAIL
This message is displayed when the Mach trim system has failed. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 5 SECONDS
60
MAU 1-2-3-4 FAIL
This message is displayed when the system detects a loss of ASCB traffic from the affected MAU or a loss of selected functions within the MAU. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 2 SECONDS
61
MAU 1-2-3-4 O’TEMP
This message is displayed when the main MAU power supply detects an overheat situation and is about to shut down. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
62
MONITOR WARNING FAIL L-R
This message is displayed when the monitor warn function in either MAU 1 or MAU 4, the aural function in MAU 2 or MAU 3, or the comparison monitor function in MAU 1 or MAU 4 has failed. This indicates a loss in redundancy only. If both monitor warning functions in MAU 1 and MAU 4 fail, the CAS message display will be lost (red “X” in CAS display area). ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 7 SECONDS
63
NOSE DOOR OPEN L-R
This message is displayed when either of the two lower latch assemblies on the respective nose door is not secured. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
64
OIL LEVEL LOW L-R
This message is displayed when the oil quantity is too low for an engine start with the airplane on level ground. This message is displayed only on the ground with engines not running. The OIL LEVEL LOW L-R CAS message is displayed if the oil level low sensor is failed. ## Footnote INHIBITS: TOPI, ESDI, IN AIR DEBOUNCE: 5 SECONDS, WITH EXCEPTIONS
65
PARKING BRAKE LOW PRESSURE
This message is displayed when the parking brake handle is not stowed and the pressure switch indicates less than 1850 PSI. This message is only displayed on the ground. ## Footnote INHIBITS: LOPI, TOPI, IN AIR DEBOUNCE: STANDARD
66
PARKING BRAKE ON
This message is displayed when the PARK BRAKE handle is not stowed. On the ground, if the PARK BRAKE handle is not stowed and adequate brake pressure is applied, the cyan message is displayed. The cyan message turns amber once a throttle is above the CRU detent. The amber message is displayed in the air. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
67
PITCH/ROLL DISCONNECT
This message is displayed when the PITCH/ROLL RECONNECT handle has been pulled up to stowed incorrectly. If a single axis has been reconnected, the message will remain displayed. The autopilot will disengaged and will not re-engage. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 2 SECONDS
68
PITOT/STATIC COLD L-R-STBY
This message is displayed when either ANTI-ICE PITOT/STATIC button is ON and no current is flowing to the probe or static port, when either switch is OFF and a throttle is in the TO detent, or either switch is OFF and the airplane is airborne. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS, WITH EXCEPTIONS
69
PRESS SOURCE NOT NORM
This message is displayed when the PRESS SOURCE selector is not in the normal position and emergency pressurization is not active. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
70
PRIMARY STAB TRIM FAIL
This message is displayed on the ground until a satisfactory preflight check of the primary stabilizer trim system has been accomplished and in flight if the primary stabilizer trim system has failed. The autopilot will be inoperative. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: STANDARD
71
RAT HEAT FAIL L-R
This message is displayed when current is not detected at one or both of the respective RAT probes with the ANTI-ICE ENGINE/STAB button ON. If in icing conditions, the FADECs will automatically compensate RAT information. ## Footnote INHIBITS: LOPI, TOPI, ESDI, BFI DEBOUNCE: 2 SECONDS
72
REMOTE CB TRIPPED
This message is displayed when a circuit breaker in the aft J-box has tripped. These circuit breakers cannot be accessed by the crew. ## Footnote INHIBITS: LOPI, TOPI, ESDI, BFI DEBOUNCE: STANDARD
73
RETRIM L-R WING DOWN
This message is displayed when the autopilot is detecting a lateral mistrim as indicated by a sustained aileron servo current. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
74
RETRIM NOSE UP-DOWN
This message indicates the autopilot is detecting a longitudinal mistrim as indicated by a sustained elevator servo current. This message may be momentarily displayed during aggressive acceleration, deceleration, or configuration changes. If the trim in motion aural alert is present, the message will extinguish as trim is adjusted. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
75
ROLL SYSTEM CONTROL FAULT
This message is displayed when the roll system module detects a fault in the aileron ratio changer. Lateral control force will vary depending on what position the aileron ratio changer failed at. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 3 SECONDS
76
RUDDER BIAS FAULT
This message is displayed when a failure of the variable rudder bias system is detected. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 3 SECONDS
77
SECONDARY STAB TRIM FAIL
This message is displayed when the secondary trim is commanded and there is no resulting stabilizer position feedback or the resulting stabilizer position feedback is in the wrong direction. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
78
SPEED BRAKES
Displayed if a sensor or hydraulic system failure is detected or when the airplane is below 500 feet radio altitude with speedbrakes deployed and steep approach mode not selected. ## Footnote Inhibits: TOPI, Debounce: 5 seconds
79
STAB ANTI-ICE COLD L-R on the ground
Displayed when either the preflight check has failed or the surface has not achieved adequate temperature for anti-icing. If present after a satisfactory preflight check, the surface is cold and can be cleared by waiting for it to warm up. ## Footnote Inhibits: LOPI, TOPI, Debounce: Standard
80
STAB ANTI-ICE COLD L-R in flight
Displayed when an undertemperature condition of the horizontal stabilizer exists. Inhibited for 2.5 minutes after turning the system on. ## Footnote Inhibits: LOPI, TOPI, Debounce: Standard
81
STAB ANTI-ICE O'TEMP L-R
Displayed when an overtemperature condition of the respective horizontal stabilizer is detected. The system automatically closes the respective anti-ice shutoff valve. ## Footnote Inhibits: LOPI, TOPI, Debounce: Standard
82
STAB ANTI-ICE O'TEMP L-R
After the surface has cooled, the system will automatically restore normal operation. Overtemperature monitoring is active at all times. | An overtemperature indication with the system off indicates a failure of
83
STAB BLEED LEAK
Displayed when a bleed leak in the horizontal stabilizer anti-ice bleed air supply system is detected. The stabilizer anti-ice valves close automatically. ## Footnote Inhibits: LOPI, TOPI, Debounce: Standard
84
STAB TRIM MONITOR WARNING
Displayed when a degradation of the no-back brake in the stabilizer actuator is detected. ## Footnote Inhibits: LOPI, TOPI, Debounce: 0.25 seconds
85
SUPPLY BLEED LEAK L-R
Displayed when a bleed leak to the ECS supply or wing and stabilizer anti-ice system is detected. ## Footnote Inhibits: LOPI, TOPI, Debounce: Standard
86
T/R ARMED L-R
Displayed when the respective thrust reverser is armed in flight. ## Footnote Inhibits: TOPI, BFI, On Ground, Debounce: Standard
87
T/R UNLOCK L-R
Displayed when two or more of the four locks are sensed to be unlocked on the respective thrust reverser in flight. ## Footnote Inhibits: TOPI, On Ground, Debounce: Standard
88
TAILCONE DOOR OPEN
This message is displayed when the tailcone door is open as detected by a switch on the forward edge of the door panel. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 2 SECONDS
89
TCAS FAIL
This message is displayed in the TCAS window on the MFD when TCAS has failed due to an internal fault or a failure of one or more of the components required for TCAS operation. ## Footnote INHIBITS: NONE DEBOUNCE: STANDARD
90
WINDSHIELD HEAT INOP L-R
This message is displayed when the windshield heat has failed. The windshield temperature controller has detected a fault and has shut off the windshield heat. ## Footnote INHIBITS: LOPI, TOPI, ESDI, BFI DEBOUNCE: 5 SECONDS, WITH EXCEPTIONS
91
WINDSHIELD OVERTEMP L-R
This message is displayed when the windshield controller has detected an overheat situation which could result in damage. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 5 SECONDS, WITH EXCEPTIONS
92
WING A/I CROSSFLOW OPEN
This message is displayed when the wing anti-ice crossflow valve has failed to fully close. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 5 SECONDS
93
WING ANTI-ICE COLD L-R ON GROUND
This message is displayed when either the preflight check has failed or the surface has not achieved adequate temperature for anti-icing. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
94
WING ANTI-ICE COLD L-R IN FLIGHT
This message is displayed when an undertemperature condition of the outboard wing is detected. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: STANDARD
95
WING ANTI-ICE O’TEMP L-R
This message is displayed when an overtemperature condition of either the inboard or outboard section of the respective wing is detected. ## Footnote INHIBITS: LOPI, TOPI DEBOUNCE: 5 SECONDS
96
WING BLEED LEAK L-R
This message is displayed when a bleed leak in the inboard or outboard wing anti-ice supply line is detected. If wing anti-ice can be verified to be off (buttons, N2, ITT), this message may be a monitor failure. | The associated wing anti-ice valve closes automatically when the WING BL ## Footnote The associated wing anti-ice valve closes automatically when the WING BLEED LEAK L-R CAS message is displayed. The valve will stay closed after the sensor cools. The WING ANTI-ICE COLD CAS message is displayed if the WING BLEED LEAK monitor is active. INHIBITS: LOPI, TOPI DEBOUNCE: 5 SECONDS
97
WOW MISCOMPARE
This message is displayed when the weight-on-wheels module has detected a miscompare between the squat switches or the MAU has detected a miscompare between weight-on-wheels modules. ## Footnote INHIBITS: LOPI, TOPI, BFI DEBOUNCE: 2 SECONDS
98
XPDR STBY
This message is displayed when the airplane is in the air and the TCAS/Transponder is selected to STBY. This message is only displayed on airplanes incorporating Epic Phase 5 software. ## Footnote INHIBITS: LOPI, TOPI, ON GROUND DEBOUNCE: 8 SECONDS

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

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