Abnormals Flashcards
1
Q
L/ R REV DEPLOYED
A
If the reverser has not been commanded to deploy and is not stowed and locked
warning
2
Q
L/R REV UNLOCKED
A
Reverser has not been armed and is unlocked
Caution
3
Q
L/R REV UNSAFE
A
Indicates reverser is unsafe to arm in Flight
Caution
4
Q
AUTO PRESS
A
Automatic pressurization control is inoperative
Caution
5
Q
ALT LIMITER
A
Indicates that altitude, limitation function is inoperative
Caution
6
Q
OVBD COOL
A
Ground valve failed OPEN, in-flight
Caution
7
Q
CONFIG AP
A
Indicates that the autopilot is engaged with the airplane configured for takeoff
Warning
8
Q
L/R ENG BLEED
A
Indicates failure of high-pressure valve, pressure regulating shut off valve or controller
Caution
9
Q
APU BLEED ON
A
Indicates APU bleed is selected above 25,000 feet
Caution
10
Q
APU LCV OPEN (caution)
A
Indicates that APU load control valve failed to close when commanded to close
Caution
11
Q
APU LCV CLOSED
A
Indicates that APU load control valve failed to open when commanded to open
Caution
12
Q
ISOL FAIL
A
Indicates that bleed isolation shut off valve failed to attain selected position
Caution
13
Q
ANTI ICE DUCT (warning)
A
Indicates a bleed air leak in the wing anti ice duct
Warning
14
Q
L/R BLEED DUCT (warning)
A
Indicates a bleed air leak in the respective engine bleed ducting
Warning
15
Q
ANTI ICE DUCT (caution)
A
Indicates bleed, shut down after bleed leak detected and system not selected off
16
Q
L/R BLEED DUCT (caution)
A
Indicates respective bleed shut down after bleed leak detected and system has not been reconfigured
Caution
17
Q
EMER PWR ONLY
A
Indicates that the ADG has deployed
Warning
18
Q
AC BUS 1/2
A
Indicates that the associated bus is not powered
Caution
19
Q
AC ESS BUS
A
Indicates that the AC essential bus is less than 90 V
Caution
20
Q
AC SERV BUS
A
Indicates that AC bus 2 is powered and AC service bus is less than 90 V
Caution
21
Q
AC 1/2 AUTOXFER
A
Indicates that the corresponding automatic bus transfer has failed
Caution
22
Q
ADG FAIL
A
Indicates that the generator control unit has failed
Status msg
23
Q
ADG AUTO FAIL
A
Indicates fault in the deploy control unit
Status msg
24
Q
AP PITCH TRIM
A
Indicates that autopilot pitch trim has failed
Caution
25
YAW DAMPER
Indicates that yaw damping function has failed. The rudder system will then go to passive dampening
Caution
26
L/R XFER SOV
Indicates that the respective transfer shut off valve has failed
Caution
27
XFLOW PUMP (caution)
Indicates that the crossflow pump has failed
Caution
28
GRAV XFLOW FAIL (sts msg)
Indicates that the gravity cross flow shut off valve is not in selected position
Status msg
29
AUTO XFLOW INHIB
Indicates that powered cross flow is inhibited in automatic mode
Status msg
30
BULK FUEL TEMP
Indicates that fuel temperature and right wing tank is less than - 40 C
Caution
31
FUEL CH1/2 FAIL
indicates that fuel quantity gauging computer has failed
Caution
(Beide sind ausgefallen, bei nur einem ist es eine sts msg)
32
LOW FUEL
- fuel quantity in either tank < 272 kg or
- total quantity < 544 kg or
- quantity in collector tank is low
Caution
33
FUEL QTY DEGRADED
Indicates an error in the attitude input to the fuel quantity gauging computer
Status msg
34
WING OVHT
Indicates that an overheat condition has been detected by at least one of the inboard wing skin temperature sensors
Warning (aural)
35
WING A/I SNSR
Indicates failure of both channels of left or right outboard wing temperature sensors with wing anti-ice selected on
Caution
36
WING XBLEED
Indicates that the wing cross bleed valve has failed closed
Caution
37
L/R COWL A/I DUCT (warning)
Indicates that a bleed leak is detected in the cowl anti-ice duct
Warning
38
L/R COWL A/I OPEN
Indicates that respective cowl anti-ice valve failed to close when selected off
Caution
39
L/R COWL A/I
Indicates that the respective cowl anti-ice valve failed to open when selected on or valve position cannot be determined
Caution
40
L/R ENG TAT HEAT
Indicates that their respective T2 heater has failed
Caution
41
L/R COWL A/I DUCT sts msg
Indicates that respective cowl duct pressure is less than 3.12 PSI or greater than 53.1 PSI with battery bus powered
Status msg
42
L/R AOA HEAT
Indicates that respective angle of attack heater is off or has failed
Caution
43
L/R WSHLD HEAT
Indicates an overheat or a no heat condition at the respective windshield heater
Caution
44
ICE DET FAIL
Indicates both ice detector systems have failed
Caution
45
NOSE DOOR
Indicates that either nose landing gear door is not closed after gear is up
Warning (aural)
46
GEAR DISAGREE
Indicates that landing gear position does not agree with landing gear control handle position
Warning (aural)
47
L/R MLG FAULT (sts msg)
Indicates that left or right actuator shuttle valve or the pressure switch have failed in the closed (MLG downlocked) or open (MLG uplocked) position
Sts msg
48
IB or OB BRAKE PRESS
Indicates that brake pressure of the respective system is less than 1800 psi and DC bus 2 is powered
Caution
49
PROX SYSTEM
Indicates loss of both PSEU channels
Caution
50
PROX SYS CHAN
Indicate loss of one PSEU channel or input/output of a critical system
Caution
51
WOW OUTPUT
Indicates that WOW output failed or disagrees with another critical output
Caution
52
WOW INPUT
Indicates that two or more WOW sensors disagree or have failed
Caution
53
MLG FAULT
Indicates PSEU has detected a fault in the main landing gear shuttle valve
Sts msg
54
HYD EDP 1A / 2A
Indicates that corresponding engine driven pump has a low pressure output (<1800 psi)
Caution
55
HYD 1/2 HI TEMP
Indicates that corresponding system has a fluid temperature of 96 C or greater
Caution
56
HYD 1/2 LO PRESS
Indicates that both EDP and AC motor pump have low pressure (<1800 psi)
Caution
57
HYD SOV 1/2 OPEN
Indicates that the respective shut off valve is open when the associated ENG FIRE pb switch has been pushed
Caution
58
HYD SOV 1/2 CLOSED
Indicates that the corresponding shut-off valve has been closed
Advisory green
59
L/R ENG SOV FAIL
Indicates that respective engine fuel shut off valve is not in commanded position
Caution
60
L/R ENG SOV OPEN
Indicates that respective engine fuel shut off valve is open and an engine fire is detected
Caution
61
L/R ENG SOV CLSD (caution)
Indicates that respective engine fuel shut off valve is closed and no engine fire is detected
Caution
62
L/R FUEL LO PRESS
Indicates that a low fuel pressure condition exists at the respective engine inlet
Caution
63
L/R FUEL LO TEMP
Indicates that fuel temperature is less than 4.3°C with respective engine running
Caution
64
L/R FUEL FILTER
Indicates that a bypass or impending bypass condition exists at respective filter
Caution
65
ENGINE OVERSPEED
Indicates that N1 or N2 has exceeded redline for more than four seconds
Warning
66
L/R ENG FLAMEOUT
Indicates flame out of respective engine, FADEC was not successful with relight and thrust lever not at shut off
Caution
67
L/R THROTTLE
Indicates failure of respective thrust lever. FADEC will maintain last power level setting until approach.
Caution
68
L/R ENG SRG CLSD
Indicates that respective operability bleed valve has failed closed
Caution
69
L/R ENG SRG OPEN
Indicates that respective of probability bleed valve has failed open
Caution
70
L/R FADEC OVHT
Indicates possible erroneous, information or loss of an engine
Caution
71
L/R PACK AUTOFAIL
Indicates failure of respective pack in automatic mode and system is not in manual mode
Caution
72
L/R PACK TEMP
Indicates a high (>85) or low (<5) outlet temperature when in manual mode or PACK INLET TEMP is high or PACK COMPRESSOR DISCHARGE TEMP is high
Caution
73
L/R PACK
Indicates failure of respective pack in automatic and manual modes
Caution
74
L/R PACK FAULT
Indicates a fault in respective pack
Status msg
75
L/R RARV FAULT (sts msg)
Indicates that the L/R RARV has failed in the open or toward the CLSD position
Status msg
76
OVBD COOL (on ground)
Indicates overboard exhaust shut off valve, not closed with passenger door and service door closed. The airplane will not pressurize to normal levels if valve has failed open.
Caution
77
OVBD COOL FAIL
Indicates overboard exhaust shut off valve has failed closed with the airplane on the ground and the passenger door unlatched
Status msg
78
AUTO PRESS
Indicates that automatic pressurization control is inoperative
Caution
79
EMER DEPRESS
Indicates that EMER DEPRESS switch has been selected on
Caution
80
ALT LIMITER
Indicates that altitude limitation function is inoperative
Caution
81
OVBD COOL (in flight)
Ground valve failed OPEN in flight
Caution
82
CABIN ALT WARN HI
Indicates that landing elevation has been set > 8000 ft
Green/white je nach Flugzeug
83
AUTO PRESS 1/2 FAIL
Indicates that respective cabin pressure controller is inoperative
Status msg
84
AUTO PRS 1/2 FAIL
Indicates loss of active channel in manual mode
Status msg
85
OUTFLOW VLV OPEN
Indicates outflow valve in full open position
Status msg
86
CPAM FAIL
Indicates failure of cabin pressure control panel indication system
Status msg
87
ANTI-ICE LOOP
Indicates loss of both wing anti-ice leak detection loops during power up test (on ground only)
Caution
88
L/R COWL LOOP
Indicates loss of both left or right cowl bleed air leak detection loops during power up test (on ground only)
Caution
89
L/R BLEED LOOP
Indicates loss of both left or right engine bleed air leak detection loops during power up test
Caution
90
DUCT MON FAULT
Indicates a loss of redundancy in bleed leak detection system
Caution
91
APU DOOR OPEN (caution)
Indicates that APU door failed to close after APU shutdown
Caution
92
APU IN BITE
Indicates air inlet door not in position with PWR FUEL selected on
Status msg
93
APU OVERSPEED
Indicates that APU overspeed condition exists. APU shuts down automatically.
Warning (aural)
94
APU OVERTEMP
Indicates that EGT overtemperature shutdown limit exceeded. APU shuts down automatically on the ground.
Warning (aural)
95
APU ECU FAIL
Indicates that no data is received from the ECU with PWR FUEL selected on
Caution
96
APU FAULT (caution)
Indicates a fault requiring the APU to be shutdown. APU shuts down automatically on the ground.
Caution
97
APU ALT LIMIT
Indicates that surge control valve has failed, APU operation limited to <= 17000 ft
Status msg
98
APU FAULT (Status)
Indicates loss of redundancy in sensors, impending filter bypass or fuel valve has failed open
Status msg
99
APU START
Indicates that starter motor is engaged
Status msg
100
APU PUMP
Indicates that APU pump has failed
(Die Fuel pump)
Caution
101
L/R FUEL PUMP
Indicates that the respective engine boost pump has failed
Caution
102
L/R MAIN EJECTOR
Indicates that low fuel pressure condition exists at respective ejector with engine running
Caution
103
L/R SCAV EJECTOR
Indicates that low fuel pressure condition exists at respective ejector with engine running or a high fuel pressure condition exists at respective ejector with engine not running
Caution
104
FUEL IMBALANCE
Indicates that fuel imbalance greater than 363 kg detected by the fuel computer
Caution
105
APU SOV FAIL
Indicates that APU shutoff valve is not in commanded position
Caution
106
APU SOV OPEN (caution)
Indicates that APU shutoff valve is open with APU ready to load and an APU fire is detected
Caution
107
L/R ENG SOV CLSD (advisory)
Indicates that respective engine fuel shutoff valve is closed and an engine fire is detected
Advisory (green)
108
APU SOV OPEN (status msg)
Indicates that APU shutoff valve is open with APU not ready to load and no APU fire detected
Status msg
109
PAX DR OUT HNDL
Indicates that the passenger door outer handle is not stowed
Caution
110
PAX DR LATCH
Indicates that the passenger door is not latched
Caution
111
PASSENGER DOOR
Indicates that the passenger door is unsafe
Warning (aural)
112
APU GEN OFF
Indicates that APU generator is off and APU is ready to load
Caution
113
IDG 1/2
Indicates that IDG has low oil pressure or high oil temperature
Caution
114
APU GEN OVLD
Indicates that generator control unit has detected a load of greater than 40kVA
Caution
115
GEN 1/2 OVLD
Indicates that generator control unit has detected a load of greater than 40 kVA
Caution
116
AC 1/2 AUTOXFER OFF
Indicates that the corresponding automatic bus transfer has been selected off
Status msg
117
AC ESS ALTN
Indicates that AC essential bus is being fed from AC bus 2
Status msg
118
APU BATT OFF / MAIN BATT OFF
Indicates that APU or main battery is not available
Caution
119
DC BUS 1/2
Indicates that the corresponding DC bus is not powered with either AC bus 1/2 on line
Caution
120
DC EMER BUS
Indicates that emergency bus is not powered
Caution
121
DC ESS BUS
Indicates that essential bus is not powered in flight or essential bus is not powered on ground with either AC essential bus or APU generator in line
Caution
122
DC SERV BUS
Indicates that service bus is not powered with either DC bus 2 powered or DC SERVICE selected on and APU voltage >= 18 V
Caution
123
BATTERY BUS
Indicates that battery bus is not powered
Caution
124
DC CROSS/ MAIN/ ESS TIE CLOSED
Indicates that the corresponding bus tie is closed
Status msg
125
ESS TRU 2 XFER
Indicates that essential TRU 2 is powered by AC essential bus
Status msg
126
APU/MAIN BATT CHGR
Indicates that the corresponding battery is overheating or not charging
Status msg
127
TRU 1(2) FAIL
Indicates that TRU 1(2) voltage is <18V with AC bus 1(2) on line or main tie is closed with TRU 1(2) load <3,7 amps
Status msg
128
ESS TRU 1 FAIL
Indicates that essential TRU 1 voltage is <18V with AC essential bus on line or essential tie is closed with essential TRU 1 load <3,7 amps
Status msg
129
ESS TRU 2 FAIL
Indicates that essential TRU 2 voltage is <18V with AC bus 2 on line or essential TRU 2 is powered by AC essential bus or
essential tie is closed with essential TRU 2 load <3,7 amps
Status msg
130
TRU FAN FAIL
Indicates that any of 4 TRU fans have failed
Status msg
131
FIRE SYSTEM FAULT
Indicates a loss of all ARINC communication to the FIDEEX system
Caution
Aeronautical Radio Incorporated
132
L/R ENG SQB (caution)
Indicates that left or right squibs of both bottles have failed or have fired
Caution
133
L/R FIRE FAIL
Indicates a failure of the respective engine detection system
Caution
134
ENG BTL 1/2 LO
Indicates that respective bottle has discharged
Caution
135
L/R ENG SQ (status msg)
Indicates that one left or right squib has failed or has fired
Status msg
136
APU SQB
Indicates that APU bottle squib has failed or fired
Caution
137
APU FIRE FAIL
Indicates a failure of the APU detection system
Caution
138
APU BTL LO
Indicates that APU bottle has discharged
Caution
139
FWD/AFT CARGO SQB 1/2
Indicates that the forward or aft cargo bottle squib 1/2 has failed or fired
Caution
140
FWD/AFT CARGO DET
Indicates a failure of the fwd or aft cargo detection system
Caution
141
CARGO BTL LO
Indicates that one or both cargo bottle(s) have discharged
Caution
142
SPOILERONS ROLL
Indicates that roll disconnect has been selected and either no or both roll priorities have been selected
Caution
143
PLT/CPLT ROLL CMD
Indicates that pilot or copilot roll authority has been selected
Advisory (green)
144
FLUTTER DAMPER
Indicates that low fluid level is detected in a flutter damper, refer to flight control synoptic page for the affected flutter damper
Status msg
145
RUD LIMITER
Indicates loss of rudder limiter function
Caution
146
RUD LIMIT FAULT
Indicates loss of redundancy in rudder limiter
Status msg
147
ELEVATOR SPLIT
Indicates that left and right elevator surface mismatch exceeds 6° (below 250 kt) or 3° (above 250 kt)
Caution
148
PITCH FEEL
Indicates a failure of the pitch feel system
Caution
149
PITCH FEEL FAULT
Indicates a loss or redundancy in the pitch feel system (one actuator failed)
Status msg
150
STALL FAIL
Indicates that the pusher is deactivated or
has failed
or
one channel of the stall protection computer has failed
or
the angel of attack sensor has failed
Caution
151
STAB TRIM
Indicates that both channels of the control unit are disengaged or have failed
Caution
152
STAB TRIM LIMIT
Indicates that stabilizer trim is at or greater than 14 trim units
Caution
153
MACH TRIM
Indicates that Mach trim is not engaged or has failed in both channels
Caution
154
STAB FAULT
Indicates loss of redundancy in stabilizer trim control
Status msg
155
SPLR/STAB FAULT
Indicates a fault in the spoiler and stabilizer control unit
Status msg
156
SSCU 1/2 FAULT
Indicates that one of two spoiler and stabilizer control modules has failed or is not powered
Status msg
If 1+2 fault do the SPOST again as it was probably interrupted
157
FLAPS FAIL (caution)
Indicates that both Flap channels have failed
Caution
158
SLATS FAIL
Indicates that both Slat channels have failed
Caution
159
SLAT FAULT
Indicates that left or right slat disconnect sensor has detected a mismatch (one detects open)
Status msg
160
FLAP FAULT (sts msg)
Indicates that emergency flap switch has failed, loss of cross channel talk, flap skew detection or sensor failure or any flap actuator fault
Status msg
161
SLATS/FLAPS HALFSPEED
Indicates that one channel of the respective system has failed or system is operating on ADG power
Status msg
162
IB/OB FLT SPLRS
Indicates a loss of proportional lift dumping capability for respective multi function spoilers
Caution
163
IB/OB GND SPLRS
Indicates that respective ground spoilers are inoperative
Caution
164
IB/OB SPOILERONS
Indicates loss of roll assist capability for respective multi function spoilers
Caution
165
FLT SPLR DEPLOY (caution)
Indicates that any flight spoiler is deployed > 3° or the flight spoiler handle out the 0 position with the airplane in go around or RA < 800 ft
Caution
166
GND SPLR DEPLOY
Indicates that a ground spoiler is deployed and airplane is not on the ground
Caution
167
GLD NOT ARMED
Indicates that ground lift dumping is not armed and airplane is either in approach or takeoff configuration
Caution
168
GLD UNSAFE
Indicates that ground lift dumping mode is unsafe (possible inadvertent deployment of spoilers due to failure if two or more input sensors)
Caution
