Phenom 300 CAS Messages Flashcards
(129 cards)
1
Q
DOOR EMER OPEN (red)
A
emergency door is open
2
Q
DOOR PAX OPEN (red)
A
main door is open
3
Q
DOOR BAG AFT OPEN (yellow)
A
aft baggage door is open
4
Q
DOORBAG (LH) (RH) OPEN (yellow)
A
forward left/right baggage door is open
5
Q
MFD FAULT (yellow)
A
failure of MFD
6
Q
PFD 1 (2) FAULT (yellow)
A
failure of PFD 1 (2)
7
Q
GTC 1 (2) FAULT (white)
A
failure of GTC 1 (2)
8
Q
ELEC EMERGENCY (red)
A
DC main buses are de-energized and batteries are discharging in an electrical emergency
9
Q
ELEC XFR FAIL (red)
A
automatic transfer to electrical emergency condition has failed
10
Q
BATT 1 (2) OFF BUS (yellow)
A
associated battery is isolated from the electrical network
11
Q
BATT DISCHARGE (yellow)
A
during a normal system operation, at least one battery is discharging
12
Q
BATT EXCEEDANCE (yellow)
A
any battery voltage is above 29V
13
Q
GEN 1 (2) OFF BUS (yellow)
A
generator failure or gen 1 and gen 2 switches are in the off position
14
Q
GEN OVLD (yellow)
A
remaining generator current is above: 330A on ground and 390A in flight
15
Q
GEN START FAULT (yellow)
A
generator start contactor failed in the closed position
16
Q
DC BUS 1 (2) OFF (white)
A
associated DC bus is de-energized
17
Q
ELEC SYS FAULT (white)
A
main DC channels are operating in parallel
18
Q
EMER BUS OFF (white)
A
emergency bus is de-energized
19
Q
GPU CONNECTED (white)
A
gpu connected to the airplane
20
Q
SHED BUS OFF (white)
A
shed bus is de-energized
21
Q
EMER LT NOT ARM (yellow)
A
emergency light switch is not in arm position
22
Q
NO TO CONFIG (red)
A
airplane not in a valid takeoff configuration
23
Q
AURAL WRN FAIL (yellow)
A
both aural warning channels are failed or off
24
Q
PUSHER FAIL (yellow)
A
pusher is inoperative and aural warning is operative
25
PUSHER OFF (yellow)
pusher is disabled via cutout button
26
SWPS FAULT (yellow)
stall warning system activation angles are anticipated to conservative settings
27
SWPS UNTESTED (yellow)
stall warning and protection system pre-flight test has expired
28
TCAS FAIL (yellow)
TCAS failure
29
AURAL WARN FAULT (white)
one aural warning channel is failed or off
30
RALT FAIL (white)
radar altimeter is inoperative
31
FUEL 1 (2) LO LEVEL (yellow)
310 lbs of fuel remains in respective tank
32
FUEL 1 (2) LO PRES (yellow)
low pressure to associated engine while engine is running
33
FUEL 1 (2) SOV FAIL (yellow)
discrepancy between commanded and actual valve status
34
FUEL IMBALANCE (yellow)
imbalance between tanks greater than or equal to 220 lb. Remains until imbalance is reduced to 88 lb.
35
FUEL XFEED FAIL (yellow)
discrepancy between commanded and actual valve status
36
FUEL PUMP 1 (2) FAIL (yellow)
discrepancy between commanded and actual associated pump status or electric fuel pump failure
37
DOOR REFUEL OPEN (white)
refueling panel door is open
38
FUEL 1 (2) FEED FAULT (white)
indicates low pressure in primary fuel feed system activating DC pump
39
FUEL 1 (2) PSW FAIL (white)
failure in associated pressure switch
40
FUEL EQUAL (white)
fuel imbalance is less than 44 lb when xfeed is open
41
E1 (2) OIL LO PRES (red)
engine 1 (2) oil pressure low
42
E1 (2) CTRL FAULT (yellow)
pilot may be unable to modulate thrust or engine will respond slowly
43
E1 (2) FAIL (yellow)
engine 1 (2) shutdown has occurred without pilot command
44
E1 (2) FUEL IMP BYP (yellow)
fuel filter impending bypass
45
E1 (2) TLA FAIL (yellow)
dual thrust lever angle sensor fail
46
E1 (2) TT0 HTR FAIL (yellow)
TT0 sensor heating failed
47
E1 (2) TT0 PROBE ICE (yellow)
heating is turned off because of ice crystal formation on E1 (2) TT0 sensor probe
48
ENG NO TO DATA (yellow)
takeoff data not entered successfully
49
E1 (2) CHIP DETECTED (white)
E1 (2) chip is detected
50
E1 (2) FADEC FAULT (white)
Avionics not receiving data from one FADEC channel
51
E1 (2) OIL IMP BYP (white)
engine oil filter impending bypass
52
E1 (2) FIRE (red)
engine 1 (2) has detected a fire condition
53
BAG SMK (red)
smoke detected in baggage compartment
54
E1 (2) FIRE DET FAIL (yellow)
engine fire detection system has failed
55
E1 (2) FIREX FAIL (yellow)
engine fire extinguisher system has failed
56
BAG SMK FAIL (yellow)
both baggage compartment smoke sensors have failed
57
ENG FIREX DISCH (white)
engine fire extinguisher bottle has been discharged
58
BAG SMK FAULT (white)
one baggage compartment smoke sensor has failed
59
AMS CTRL FAIL (yellow)
both AMS controller channels have failed. no bleed air temperature and pressure control is performed
60
BLEED 1 (2) FAIL (yellow)
a bleed failure has been detected. bleed is no longer available
61
BLEED 1 (2) LEAK (yellow)
leakage detected in associated bleed line
62
BLEED 1 (2) OVERPRES (yellow)
there is a bleed air overpressure condition at the LH or RH bleed manifold
63
EBAY LEAK (yellow)
a bleed hot air leaks is detected in loop 8
64
AMS CTRL FAULT (yellow)
A channel has failed in the AMS controller
65
BLEED 1 (2) OFF (white)
associated PRSOV is closed
66
XBLEED FAIL (white)
cross bleed failure has been detected. Not responding to automatic or manual input commands
67
XBLEED SW OFF (white)
XBLEED switch is in off position
68
ADS 1 (2) HTR FAIL (yellow)
associated heater is off or failed
69
A-1 E1 (2) FAIL (yellow)
nacelle anti-ice valve is closed when commanded to open, or an engine anti-ice duct failure is detected
70
A-I LO CAPACITY (yellow)
there is not enough thermal energy available for WHSAIS operation
71
A-I WINGSTAB INHB (yellow)
pilot commands the WINGSTAB switch on outside the WHSAIS operational envelope when below 30000 ft
72
A-I WINGSTAB LEAK (yellow)
there is a bleed hot air leakage on the WHSAIS pneumatic ducting
73
A-I WINGSTAB FAIL (yellow)
a WINGSTAB anti-ice system failure has been detected
74
ICE CONDITION (yellow)
ice detector has detected the aircraft is in icing conditions
75
STBY HTR FAIL (yellow)
ADS STBY heater is off or failed
76
WSHLD 1 (2) HTR FAIL (yellow)
associated windshield is overheated or heating system is failed
77
ADS HTR SW ON (white)
ADS probe knob is on
78
A-I E1 (2) FAULT (white)
engine anti-ice system valve failed when commanded to close
79
A-I E1 (2) ON (white)
engine anti-ice system is turned on and operating normally
80
A-I WINGSTAB ARM (white)
pilot commands the WINGSTAB ON prior to takeoff or above 30000 ft
81
A-I WINGSTAB ON (white)
WINGSTAB anti-ice system is turned on and operating normally
82
ICE DET FAIL (white)
ice detector is failed
83
DUCT 1 (2) OVERTEMP (yellow)
an overheat condition has been detected at the associated bleed line
84
EBAY OVHT (yellow)
the electronic bay temperature is above 70 C
85
ECS 1 (2) VALVE FAIL (yellow)
associated FCSOV is failed
86
ECS 1 (2) OFF (white)
associated FCSOV is closed
87
RAM AIR FAIL (white)
forward emergency ram air valve has failed closed
88
CAB ALTITUDE HI (red)
cabin altitude is equal to or higher than 10000 ft in normal mode
89
CAB DELTA-P FAIL (yellow)
cabin differential pressure is higher than 9.5 psid or lower than -0.3 psid
90
PRESN AUTO FAIL (yellow)
loss of automatic mode
91
HYD HI TEMP (yellow)
hydraulic system temperature is higher than the normal operating range
92
HYD LO PRES (yellow)
hydraulic system pressure is lower than the normal operating range
93
HYD SOV 1 (2) FAIL (yellow)
fire shutoff valve fails to close
94
HYD SYS FAULT (white)
degradation for hydraulic system available power
95
LG LEVER DISAG (red)
discrepancy between position of LDG GEAR lever and at least one landing gear
96
ANTI-SKID FAIL (yellow)
loss of anti-skid protection
97
BRK FAIL (yellow)
loss of when brake on either the left or right landing gear
98
EMER BRK LO PRES (yellow)
emergency/paring brake accumulator pressure is low
99
LG WOW SYS FAIL (yellow)
indicates a failure condition in the WOW indication system
100
PARK BRK NOT REL (yellow)
emergency/parking brake actuated condition in fight
101
FLAP FAIL (yellow)
flap control system is inoperative or there is a jam preventing movement
102
GND SPLR FAIL (yellow)
loss of ground spoiler function
103
PTRIM BKP FAIL (yellow)
pitch trim backup function no longer available
104
PTRIM NML FAIL (yellow)
pitch trim normal function no longer available
105
RUD OVERBOOST (yellow)
spring loaded rudder booster uncommanded actuation
106
STEEP FAIL (yellow)
steep approach mode required data was lost during steep approach
107
FLAP NOT AVAIL (white)
flaps not available
108
PTRIM LO RATE (white)
pitch trim is being actuated a low rate
109
PTRIM SW 1 (2) FAIL (white)
associated control wheel pitch trim switch is inoperative
110
RUD BOOST FAIL (white)
loss of spring loaded rudder booster force assistance in case of thrust asymmetry
111
SPDBRK SW DISAG (white)
speed brake switch position disagrees with spoiler surface position
112
SPOILER FAULT (white)
loss of roll spoiler and/or speed brake functions
113
STEEP NOT AVAIL (white)
steep approach mode is not available
114
AP FAIL (yellow)
autopilot function is no longer operative
115
AP PITCH MISTRIM (yellow)
airplane is mistrimmed in pitch axis when AP is engaged
116
AP ROLL MISTRIM (yellow)
airplane is mistrimmed in roll axis when AP is engaged
117
AUTO PTRIM FAIL (yellow)
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
YD FAIL (yellow)
yaw damper function is no longer operative
119
YD MISTRIM (yellow)
airplane is mis-trimmed in yaw axis when YD is engaged
120
VENTRAL RUD FAIL (white)
ventral rudder control damping mode is not available
121
ADS 1 (2) FAIL (yellow)
associated ADS is off or has failed
122
AHRS 1 (2) FAIL (yellow)
total loss of AHRS 1 (2)
123
ADS 1 (2) SLIP FAIL (white)
ADS 1 (2) side-slip compensation is off
124
AHRS 1 (2) FAULT (white)
failure of AHRS 1 (2)
may have lost some internal redundancy
performance may be degraded
magnetic heading may be unavailable
125
NAV 1 (2) FAIL (white)
a failure has been detected in the NAV 1 (2) receiver
126
XPDR 1 (2) FAIL (white)
XPDR 1 (2) is failed
127
OXY lO PRES (yellow)
oxygen cylinder pressure is below the accepted safety limit for dispatch, pressure sensor is failed, or the OXYGEN SUPPLY handle is pulled
128
PAX OXY NO PRES (yellow)
passenger masks not deployed in a cabin depressurization condition
129
OXY SW NOT AUTO (white)
SUPPLY CONTROL knob not in PAX AUTO position
