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phenom 300 > Phenom 300 CAS Messages > Flashcards

Phenom 300 CAS Messages Flashcards

1
Q

DOOR EMER OPEN (red)

A

emergency door is open

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2
Q

DOOR PAX OPEN (red)

A

main door is open

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3
Q

DOOR BAG AFT OPEN (yellow)

A

aft baggage door is open

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4
Q

DOORBAG (LH) (RH) OPEN (yellow)

A

forward left/right baggage door is open

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5
Q

MFD FAULT (yellow)

A

failure of MFD

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6
Q

PFD 1 (2) FAULT (yellow)

A

failure of PFD 1 (2)

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7
Q

GTC 1 (2) FAULT (white)

A

failure of GTC 1 (2)

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8
Q

ELEC EMERGENCY (red)

A

DC main buses are de-energized and batteries are discharging in an electrical emergency

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9
Q

ELEC XFR FAIL (red)

A

automatic transfer to electrical emergency condition has failed

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10
Q

BATT 1 (2) OFF BUS (yellow)

A

associated battery is isolated from the electrical network

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11
Q

BATT DISCHARGE (yellow)

A

during a normal system operation, at least one battery is discharging

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12
Q

BATT EXCEEDANCE (yellow)

A

any battery voltage is above 29V

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13
Q

GEN 1 (2) OFF BUS (yellow)

A

generator failure or gen 1 and gen 2 switches are in the off position

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14
Q

GEN OVLD (yellow)

A

remaining generator current is above: 330A on ground and 390A in flight

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15
Q

GEN START FAULT (yellow)

A

generator start contactor failed in the closed position

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16
Q

DC BUS 1 (2) OFF (white)

A

associated DC bus is de-energized

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17
Q

ELEC SYS FAULT (white)

A

main DC channels are operating in parallel

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18
Q

EMER BUS OFF (white)

A

emergency bus is de-energized

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19
Q

GPU CONNECTED (white)

A

gpu connected to the airplane

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20
Q

SHED BUS OFF (white)

A

shed bus is de-energized

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21
Q

EMER LT NOT ARM (yellow)

A

emergency light switch is not in arm position

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22
Q

NO TO CONFIG (red)

A

airplane not in a valid takeoff configuration

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23
Q

AURAL WRN FAIL (yellow)

A

both aural warning channels are failed or off

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24
Q

PUSHER FAIL (yellow)

A

pusher is inoperative and aural warning is operative

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25
Q

PUSHER OFF (yellow)

A

pusher is disabled via cutout button

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26
Q

SWPS FAULT (yellow)

A

stall warning system activation angles are anticipated to conservative settings

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27
Q

SWPS UNTESTED (yellow)

A

stall warning and protection system pre-flight test has expired

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28
Q

TCAS FAIL (yellow)

A

TCAS failure

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29
Q

AURAL WARN FAULT (white)

A

one aural warning channel is failed or off

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30
Q

RALT FAIL (white)

A

radar altimeter is inoperative

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31
Q

FUEL 1 (2) LO LEVEL (yellow)

A

310 lbs of fuel remains in respective tank

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32
Q

FUEL 1 (2) LO PRES (yellow)

A

low pressure to associated engine while engine is running

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33
Q

FUEL 1 (2) SOV FAIL (yellow)

A

discrepancy between commanded and actual valve status

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34
Q

FUEL IMBALANCE (yellow)

A

imbalance between tanks greater than or equal to 220 lb. Remains until imbalance is reduced to 88 lb.

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35
Q

FUEL XFEED FAIL (yellow)

A

discrepancy between commanded and actual valve status

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36
Q

FUEL PUMP 1 (2) FAIL (yellow)

A

discrepancy between commanded and actual associated pump status or electric fuel pump failure

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37
Q

DOOR REFUEL OPEN (white)

A

refueling panel door is open

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38
Q

FUEL 1 (2) FEED FAULT (white)

A

indicates low pressure in primary fuel feed system activating DC pump

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39
Q

FUEL 1 (2) PSW FAIL (white)

A

failure in associated pressure switch

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40
Q

FUEL EQUAL (white)

A

fuel imbalance is less than 44 lb when xfeed is open

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41
Q

E1 (2) OIL LO PRES (red)

A

engine 1 (2) oil pressure low

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42
Q

E1 (2) CTRL FAULT (yellow)

A

pilot may be unable to modulate thrust or engine will respond slowly

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43
Q

E1 (2) FAIL (yellow)

A

engine 1 (2) shutdown has occurred without pilot command

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44
Q

E1 (2) FUEL IMP BYP (yellow)

A

fuel filter impending bypass

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45
Q

E1 (2) TLA FAIL (yellow)

A

dual thrust lever angle sensor fail

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46
Q

E1 (2) TT0 HTR FAIL (yellow)

A

TT0 sensor heating failed

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47
Q

E1 (2) TT0 PROBE ICE (yellow)

A

heating is turned off because of ice crystal formation on E1 (2) TT0 sensor probe

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48
Q

ENG NO TO DATA (yellow)

A

takeoff data not entered successfully

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49
Q

E1 (2) CHIP DETECTED (white)

A

E1 (2) chip is detected

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50
Q

E1 (2) FADEC FAULT (white)

A

Avionics not receiving data from one FADEC channel

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51
Q

E1 (2) OIL IMP BYP (white)

A

engine oil filter impending bypass

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52
Q

E1 (2) FIRE (red)

A

engine 1 (2) has detected a fire condition

53
Q

BAG SMK (red)

A

smoke detected in baggage compartment

54
Q

E1 (2) FIRE DET FAIL (yellow)

A

engine fire detection system has failed

55
Q

E1 (2) FIREX FAIL (yellow)

A

engine fire extinguisher system has failed

56
Q

BAG SMK FAIL (yellow)

A

both baggage compartment smoke sensors have failed

57
Q

ENG FIREX DISCH (white)

A

engine fire extinguisher bottle has been discharged

58
Q

BAG SMK FAULT (white)

A

one baggage compartment smoke sensor has failed

59
Q

AMS CTRL FAIL (yellow)

A

both AMS controller channels have failed. no bleed air temperature and pressure control is performed

60
Q

BLEED 1 (2) FAIL (yellow)

A

a bleed failure has been detected. bleed is no longer available

61
Q

BLEED 1 (2) LEAK (yellow)

A

leakage detected in associated bleed line

62
Q

BLEED 1 (2) OVERPRES (yellow)

A

there is a bleed air overpressure condition at the LH or RH bleed manifold

63
Q

EBAY LEAK (yellow)

A

a bleed hot air leaks is detected in loop 8

64
Q

AMS CTRL FAULT (yellow)

A

A channel has failed in the AMS controller

65
Q

BLEED 1 (2) OFF (white)

A

associated PRSOV is closed

66
Q

XBLEED FAIL (white)

A

cross bleed failure has been detected. Not responding to automatic or manual input commands

67
Q

XBLEED SW OFF (white)

A

XBLEED switch is in off position

68
Q

ADS 1 (2) HTR FAIL (yellow)

A

associated heater is off or failed

69
Q

A-1 E1 (2) FAIL (yellow)

A

nacelle anti-ice valve is closed when commanded to open, or an engine anti-ice duct failure is detected

70
Q

A-I LO CAPACITY (yellow)

A

there is not enough thermal energy available for WHSAIS operation

71
Q

A-I WINGSTAB INHB (yellow)

A

pilot commands the WINGSTAB switch on outside the WHSAIS operational envelope when below 30000 ft

72
Q

A-I WINGSTAB LEAK (yellow)

A

there is a bleed hot air leakage on the WHSAIS pneumatic ducting

73
Q

A-I WINGSTAB FAIL (yellow)

A

a WINGSTAB anti-ice system failure has been detected

74
Q

ICE CONDITION (yellow)

A

ice detector has detected the aircraft is in icing conditions

75
Q

STBY HTR FAIL (yellow)

A

ADS STBY heater is off or failed

76
Q

WSHLD 1 (2) HTR FAIL (yellow)

A

associated windshield is overheated or heating system is failed

77
Q

ADS HTR SW ON (white)

A

ADS probe knob is on

78
Q

A-I E1 (2) FAULT (white)

A

engine anti-ice system valve failed when commanded to close

79
Q

A-I E1 (2) ON (white)

A

engine anti-ice system is turned on and operating normally

80
Q

A-I WINGSTAB ARM (white)

A

pilot commands the WINGSTAB ON prior to takeoff or above 30000 ft

81
Q

A-I WINGSTAB ON (white)

A

WINGSTAB anti-ice system is turned on and operating normally

82
Q

ICE DET FAIL (white)

A

ice detector is failed

83
Q

DUCT 1 (2) OVERTEMP (yellow)

A

an overheat condition has been detected at the associated bleed line

84
Q

EBAY OVHT (yellow)

A

the electronic bay temperature is above 70 C

85
Q

ECS 1 (2) VALVE FAIL (yellow)

A

associated FCSOV is failed

86
Q

ECS 1 (2) OFF (white)

A

associated FCSOV is closed

87
Q

RAM AIR FAIL (white)

A

forward emergency ram air valve has failed closed

88
Q

CAB ALTITUDE HI (red)

A

cabin altitude is equal to or higher than 10000 ft in normal mode

89
Q

CAB DELTA-P FAIL (yellow)

A

cabin differential pressure is higher than 9.5 psid or lower than -0.3 psid

90
Q

PRESN AUTO FAIL (yellow)

A

loss of automatic mode

91
Q

HYD HI TEMP (yellow)

A

hydraulic system temperature is higher than the normal operating range

92
Q

HYD LO PRES (yellow)

A

hydraulic system pressure is lower than the normal operating range

93
Q

HYD SOV 1 (2) FAIL (yellow)

A

fire shutoff valve fails to close

94
Q

HYD SYS FAULT (white)

A

degradation for hydraulic system available power

95
Q

LG LEVER DISAG (red)

A

discrepancy between position of LDG GEAR lever and at least one landing gear

96
Q

ANTI-SKID FAIL (yellow)

A

loss of anti-skid protection

97
Q

BRK FAIL (yellow)

A

loss of when brake on either the left or right landing gear

98
Q

EMER BRK LO PRES (yellow)

A

emergency/paring brake accumulator pressure is low

99
Q

LG WOW SYS FAIL (yellow)

A

indicates a failure condition in the WOW indication system

100
Q

PARK BRK NOT REL (yellow)

A

emergency/parking brake actuated condition in fight

101
Q

FLAP FAIL (yellow)

A

flap control system is inoperative or there is a jam preventing movement

102
Q

GND SPLR FAIL (yellow)

A

loss of ground spoiler function

103
Q

PTRIM BKP FAIL (yellow)

A

pitch trim backup function no longer available

104
Q

PTRIM NML FAIL (yellow)

A

pitch trim normal function no longer available

105
Q

RUD OVERBOOST (yellow)

A

spring loaded rudder booster uncommanded actuation

106
Q

STEEP FAIL (yellow)

A

steep approach mode required data was lost during steep approach

107
Q

FLAP NOT AVAIL (white)

A

flaps not available

108
Q

PTRIM LO RATE (white)

A

pitch trim is being actuated a low rate

109
Q

PTRIM SW 1 (2) FAIL (white)

A

associated control wheel pitch trim switch is inoperative

110
Q

RUD BOOST FAIL (white)

A

loss of spring loaded rudder booster force assistance in case of thrust asymmetry

111
Q

SPDBRK SW DISAG (white)

A

speed brake switch position disagrees with spoiler surface position

112
Q

SPOILER FAULT (white)

A

loss of roll spoiler and/or speed brake functions

113
Q

STEEP NOT AVAIL (white)

A

steep approach mode is not available

114
Q

AP FAIL (yellow)

A

autopilot function is no longer operative

115
Q

AP PITCH MISTRIM (yellow)

A

airplane is mistrimmed in pitch axis when AP is engaged

116
Q

AP ROLL MISTRIM (yellow)

A

airplane is mistrimmed in roll axis when AP is engaged

117
Q

AUTO PTRIM FAIL (yellow)

A

any failure that is restricted to the proper automatic pitch trim operation, which does not affect the proper operation of the other pitch trim functions

118
Q

YD FAIL (yellow)

A

yaw damper function is no longer operative

119
Q

YD MISTRIM (yellow)

A

airplane is mis-trimmed in yaw axis when YD is engaged

120
Q

VENTRAL RUD FAIL (white)

A

ventral rudder control damping mode is not available

121
Q

ADS 1 (2) FAIL (yellow)

A

associated ADS is off or has failed

122
Q

AHRS 1 (2) FAIL (yellow)

A

total loss of AHRS 1 (2)

123
Q

ADS 1 (2) SLIP FAIL (white)

A

ADS 1 (2) side-slip compensation is off

124
Q

AHRS 1 (2) FAULT (white)

A

failure of AHRS 1 (2)
may have lost some internal redundancy
performance may be degraded
magnetic heading may be unavailable

125
Q

NAV 1 (2) FAIL (white)

A

a failure has been detected in the NAV 1 (2) receiver

126
Q

XPDR 1 (2) FAIL (white)

A

XPDR 1 (2) is failed

127
Q

OXY lO PRES (yellow)

A

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

128
Q

PAX OXY NO PRES (yellow)

A

passenger masks not deployed in a cabin depressurization condition

129
Q

OXY SW NOT AUTO (white)

A

SUPPLY CONTROL knob not in PAX AUTO position

phenom 300 (6 decks)

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