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CRJ Limitations > Abnormals > Flashcards

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

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2
Q

L/R REV UNLOCKED

A

Reverser has not been armed and is unlocked
Caution

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3
Q

L/R REV UNSAFE

A

Indicates reverser is unsafe to arm in Flight
Caution

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4
Q

AUTO PRESS

A

Automatic pressurization control is inoperative
Caution

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5
Q

ALT LIMITER

A

Indicates that altitude, limitation function is inoperative
Caution

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6
Q

OVBD COOL

A

Ground valve failed OPEN, in-flight
Caution

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7
Q

CONFIG AP

A

Indicates that the autopilot is engaged with the airplane configured for takeoff

Warning

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8
Q

L/R ENG BLEED

A

Indicates failure of high-pressure valve, pressure regulating shut off valve or controller
Caution

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9
Q

APU BLEED ON

A

Indicates APU bleed is selected above 25,000 feet
Caution

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10
Q

APU LCV OPEN (caution)

A

Indicates that APU load control valve failed to close when commanded to close
Caution

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11
Q

APU LCV CLOSED

A

Indicates that APU load control valve failed to open when commanded to open
Caution

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12
Q

ISOL FAIL

A

Indicates that bleed isolation shut off valve failed to attain selected position

Caution

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13
Q

ANTI ICE DUCT (warning)

A

Indicates a bleed air leak in the wing anti ice duct
Warning

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14
Q

L/R BLEED DUCT (warning)

A

Indicates a bleed air leak in the respective engine bleed ducting

Warning

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15
Q

ANTI ICE DUCT (caution)

A

Indicates bleed, shut down after bleed leak detected and system not selected off

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16
Q

L/R BLEED DUCT (caution)

A

Indicates respective bleed shut down after bleed leak detected and system has not been reconfigured

Caution

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17
Q

EMER PWR ONLY

A

Indicates that the ADG has deployed

Warning

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18
Q

AC BUS 1/2

A

Indicates that the associated bus is not powered

Caution

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19
Q

AC ESS BUS

A

Indicates that the AC essential bus is less than 90 V

Caution

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20
Q

AC SERV BUS

A

Indicates that AC bus 2 is powered and AC service bus is less than 90 V

Caution

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21
Q

AC 1/2 AUTOXFER

A

Indicates that the corresponding automatic bus transfer has failed

Caution

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22
Q

ADG FAIL

A

Indicates that the generator control unit has failed

Status msg

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23
Q

ADG AUTO FAIL

A

Indicates fault in the deploy control unit

Status msg

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24
Q

AP PITCH TRIM

A

Indicates that autopilot pitch trim has failed

Caution

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25
Q

YAW DAMPER

A

Indicates that yaw damping function has failed. The rudder system will then go to passive dampening

Caution

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26
Q

L/R XFER SOV

A

Indicates that the respective transfer shut off valve has failed

Caution

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27
Q

XFLOW PUMP (caution)

A

Indicates that the crossflow pump has failed

Caution

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28
Q

GRAV XFLOW FAIL (sts msg)

A

Indicates that the gravity cross flow shut off valve is not in selected position

Status msg

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29
Q

AUTO XFLOW INHIB

A

Indicates that powered cross flow is inhibited in automatic mode

Status msg

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30
Q

BULK FUEL TEMP

A

Indicates that fuel temperature and right wing tank is less than - 40 C

Caution

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31
Q

FUEL CH1/2 FAIL

A

indicates that fuel quantity gauging computer has failed

Caution

(Beide sind ausgefallen, bei nur einem ist es eine sts msg)

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32
Q

LOW FUEL

A
  • fuel quantity in either tank < 272 kg or
  • total quantity < 544 kg or
  • quantity in collector tank is low

Caution

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33
Q

FUEL QTY DEGRADED

A

Indicates an error in the attitude input to the fuel quantity gauging computer

Status msg

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34
Q

WING OVHT

A

Indicates that an overheat condition has been detected by at least one of the inboard wing skin temperature sensors

Warning (aural)

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35
Q

WING A/I SNSR

A

Indicates failure of both channels of left or right outboard wing temperature sensors with wing anti-ice selected on

Caution

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36
Q

WING XBLEED

A

Indicates that the wing cross bleed valve has failed closed

Caution

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37
Q

L/R COWL A/I DUCT (warning)

A

Indicates that a bleed leak is detected in the cowl anti-ice duct

Warning

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38
Q

L/R COWL A/I OPEN

A

Indicates that respective cowl anti-ice valve failed to close when selected off

Caution

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39
Q

L/R COWL A/I

A

Indicates that the respective cowl anti-ice valve failed to open when selected on or valve position cannot be determined

Caution

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40
Q

L/R ENG TAT HEAT

A

Indicates that their respective T2 heater has failed

Caution

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41
Q

L/R COWL A/I DUCT sts msg

A

Indicates that respective cowl duct pressure is less than 3.12 PSI or greater than 53.1 PSI with battery bus powered

Status msg

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42
Q

L/R AOA HEAT

A

Indicates that respective angle of attack heater is off or has failed

Caution

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43
Q

L/R WSHLD HEAT

A

Indicates an overheat or a no heat condition at the respective windshield heater

Caution

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44
Q

ICE DET FAIL

A

Indicates both ice detector systems have failed

Caution

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45
Q

NOSE DOOR

A

Indicates that either nose landing gear door is not closed after gear is up

Warning (aural)

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46
Q

GEAR DISAGREE

A

Indicates that landing gear position does not agree with landing gear control handle position

Warning (aural)

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47
Q

L/R MLG FAULT (sts msg)

A

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

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48
Q

IB or OB BRAKE PRESS

A

Indicates that brake pressure of the respective system is less than 1800 psi and DC bus 2 is powered

Caution

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49
Q

PROX SYSTEM

A

Indicates loss of both PSEU channels

Caution

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50
Q

PROX SYS CHAN

A

Indicate loss of one PSEU channel or input/output of a critical system

Caution

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51
Q

WOW OUTPUT

A

Indicates that WOW output failed or disagrees with another critical output

Caution

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52
Q

WOW INPUT

A

Indicates that two or more WOW sensors disagree or have failed

Caution

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53
Q

MLG FAULT

A

Indicates PSEU has detected a fault in the main landing gear shuttle valve

Sts msg

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54
Q

HYD EDP 1A / 2A

A

Indicates that corresponding engine driven pump has a low pressure output (<1800 psi)

Caution

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55
Q

HYD 1/2 HI TEMP

A

Indicates that corresponding system has a fluid temperature of 96 C or greater

Caution

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56
Q

HYD 1/2 LO PRESS

A

Indicates that both EDP and AC motor pump have low pressure (<1800 psi)

Caution

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57
Q

HYD SOV 1/2 OPEN

A

Indicates that the respective shut off valve is open when the associated ENG FIRE pb switch has been pushed

Caution

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58
Q

HYD SOV 1/2 CLOSED

A

Indicates that the corresponding shut-off valve has been closed

Advisory green

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59
Q

L/R ENG SOV FAIL

A

Indicates that respective engine fuel shut off valve is not in commanded position

Caution

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60
Q

L/R ENG SOV OPEN

A

Indicates that respective engine fuel shut off valve is open and an engine fire is detected

Caution

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61
Q

L/R ENG SOV CLSD (caution)

A

Indicates that respective engine fuel shut off valve is closed and no engine fire is detected

Caution

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62
Q

L/R FUEL LO PRESS

A

Indicates that a low fuel pressure condition exists at the respective engine inlet

Caution

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63
Q

L/R FUEL LO TEMP

A

Indicates that fuel temperature is less than 4.3°C with respective engine running

Caution

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64
Q

L/R FUEL FILTER

A

Indicates that a bypass or impending bypass condition exists at respective filter

Caution

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65
Q

ENGINE OVERSPEED

A

Indicates that N1 or N2 has exceeded redline for more than four seconds

Warning

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66
Q

L/R ENG FLAMEOUT

A

Indicates flame out of respective engine, FADEC was not successful with relight and thrust lever not at shut off

Caution

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67
Q

L/R THROTTLE

A

Indicates failure of respective thrust lever. FADEC will maintain last power level setting until approach.

Caution

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68
Q

L/R ENG SRG CLSD

A

Indicates that respective operability bleed valve has failed closed

Caution

69
Q

L/R ENG SRG OPEN

A

Indicates that respective of probability bleed valve has failed open

Caution

70
Q

L/R FADEC OVHT

A

Indicates possible erroneous, information or loss of an engine

Caution

71
Q

L/R PACK AUTOFAIL

A

Indicates failure of respective pack in automatic mode and system is not in manual mode

Caution

72
Q

L/R PACK TEMP

A

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
Q

L/R PACK

A

Indicates failure of respective pack in automatic and manual modes

Caution

74
Q

L/R PACK FAULT

A

Indicates a fault in respective pack

Status msg

75
Q

L/R RARV FAULT (sts msg)

A

Indicates that the L/R RARV has failed in the open or toward the CLSD position

Status msg

76
Q

OVBD COOL (on ground)

A

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
Q

OVBD COOL FAIL

A

Indicates overboard exhaust shut off valve has failed closed with the airplane on the ground and the passenger door unlatched

Status msg

78
Q

AUTO PRESS

A

Indicates that automatic pressurization control is inoperative

Caution

79
Q

EMER DEPRESS

A

Indicates that EMER DEPRESS switch has been selected on

Caution

80
Q

ALT LIMITER

A

Indicates that altitude limitation function is inoperative

Caution

81
Q

OVBD COOL (in flight)

A

Ground valve failed OPEN in flight

Caution

82
Q

CABIN ALT WARN HI

A

Indicates that landing elevation has been set > 8000 ft

Green/white je nach Flugzeug

83
Q

AUTO PRESS 1/2 FAIL

A

Indicates that respective cabin pressure controller is inoperative

Status msg

84
Q

AUTO PRS 1/2 FAIL

A

Indicates loss of active channel in manual mode

Status msg

85
Q

OUTFLOW VLV OPEN

A

Indicates outflow valve in full open position

Status msg

86
Q

CPAM FAIL

A

Indicates failure of cabin pressure control panel indication system

Status msg

87
Q

ANTI-ICE LOOP

A

Indicates loss of both wing anti-ice leak detection loops during power up test (on ground only)

Caution

88
Q

L/R COWL LOOP

A

Indicates loss of both left or right cowl bleed air leak detection loops during power up test (on ground only)

Caution

89
Q

L/R BLEED LOOP

A

Indicates loss of both left or right engine bleed air leak detection loops during power up test

Caution

90
Q

DUCT MON FAULT

A

Indicates a loss of redundancy in bleed leak detection system

Caution

91
Q

APU DOOR OPEN (caution)

A

Indicates that APU door failed to close after APU shutdown

Caution

92
Q

APU IN BITE

A

Indicates air inlet door not in position with PWR FUEL selected on

Status msg

93
Q

APU OVERSPEED

A

Indicates that APU overspeed condition exists. APU shuts down automatically.

Warning (aural)

94
Q

APU OVERTEMP

A

Indicates that EGT overtemperature shutdown limit exceeded. APU shuts down automatically on the ground.

Warning (aural)

95
Q

APU ECU FAIL

A

Indicates that no data is received from the ECU with PWR FUEL selected on

Caution

96
Q

APU FAULT (caution)

A

Indicates a fault requiring the APU to be shutdown. APU shuts down automatically on the ground.

Caution

97
Q

APU ALT LIMIT

A

Indicates that surge control valve has failed, APU operation limited to <= 17000 ft

Status msg

98
Q

APU FAULT (Status)

A

Indicates loss of redundancy in sensors, impending filter bypass or fuel valve has failed open

Status msg

99
Q

APU START

A

Indicates that starter motor is engaged

Status msg

100
Q

APU PUMP

A

Indicates that APU pump has failed
(Die Fuel pump)

Caution

101
Q

L/R FUEL PUMP

A

Indicates that the respective engine boost pump has failed

Caution

102
Q

L/R MAIN EJECTOR

A

Indicates that low fuel pressure condition exists at respective ejector with engine running

Caution

103
Q

L/R SCAV EJECTOR

A

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
Q

FUEL IMBALANCE

A

Indicates that fuel imbalance greater than 363 kg detected by the fuel computer

Caution

105
Q

APU SOV FAIL

A

Indicates that APU shutoff valve is not in commanded position

Caution

106
Q

APU SOV OPEN (caution)

A

Indicates that APU shutoff valve is open with APU ready to load and an APU fire is detected

Caution

107
Q

L/R ENG SOV CLSD (advisory)

A

Indicates that respective engine fuel shutoff valve is closed and an engine fire is detected

Advisory (green)

108
Q

APU SOV OPEN (status msg)

A

Indicates that APU shutoff valve is open with APU not ready to load and no APU fire detected

Status msg

109
Q

PAX DR OUT HNDL

A

Indicates that the passenger door outer handle is not stowed

Caution

110
Q

PAX DR LATCH

A

Indicates that the passenger door is not latched

Caution

111
Q

PASSENGER DOOR

A

Indicates that the passenger door is unsafe

Warning (aural)

112
Q

APU GEN OFF

A

Indicates that APU generator is off and APU is ready to load

Caution

113
Q

IDG 1/2

A

Indicates that IDG has low oil pressure or high oil temperature

Caution

114
Q

APU GEN OVLD

A

Indicates that generator control unit has detected a load of greater than 40kVA

Caution

115
Q

GEN 1/2 OVLD

A

Indicates that generator control unit has detected a load of greater than 40 kVA

Caution

116
Q

AC 1/2 AUTOXFER OFF

A

Indicates that the corresponding automatic bus transfer has been selected off

Status msg

117
Q

AC ESS ALTN

A

Indicates that AC essential bus is being fed from AC bus 2

Status msg

118
Q

APU BATT OFF / MAIN BATT OFF

A

Indicates that APU or main battery is not available

Caution

119
Q

DC BUS 1/2

A

Indicates that the corresponding DC bus is not powered with either AC bus 1/2 on line

Caution

120
Q

DC EMER BUS

A

Indicates that emergency bus is not powered

Caution

121
Q

DC ESS BUS

A

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
Q

DC SERV BUS

A

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
Q

BATTERY BUS

A

Indicates that battery bus is not powered

Caution

124
Q

DC CROSS/ MAIN/ ESS TIE CLOSED

A

Indicates that the corresponding bus tie is closed

Status msg

125
Q

ESS TRU 2 XFER

A

Indicates that essential TRU 2 is powered by AC essential bus

Status msg

126
Q

APU/MAIN BATT CHGR

A

Indicates that the corresponding battery is overheating or not charging

Status msg

127
Q

TRU 1(2) FAIL

A

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
Q

ESS TRU 1 FAIL

A

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
Q

ESS TRU 2 FAIL

A

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
Q

TRU FAN FAIL

A

Indicates that any of 4 TRU fans have failed

Status msg

131
Q

FIRE SYSTEM FAULT

A

Indicates a loss of all ARINC communication to the FIDEEX system

Caution

Aeronautical Radio Incorporated

132
Q

L/R ENG SQB (caution)

A

Indicates that left or right squibs of both bottles have failed or have fired

Caution

133
Q

L/R FIRE FAIL

A

Indicates a failure of the respective engine detection system

Caution

134
Q

ENG BTL 1/2 LO

A

Indicates that respective bottle has discharged

Caution

135
Q

L/R ENG SQ (status msg)

A

Indicates that one left or right squib has failed or has fired

Status msg

136
Q

APU SQB

A

Indicates that APU bottle squib has failed or fired

Caution

137
Q

APU FIRE FAIL

A

Indicates a failure of the APU detection system

Caution

138
Q

APU BTL LO

A

Indicates that APU bottle has discharged

Caution

139
Q

FWD/AFT CARGO SQB 1/2

A

Indicates that the forward or aft cargo bottle squib 1/2 has failed or fired

Caution

140
Q

FWD/AFT CARGO DET

A

Indicates a failure of the fwd or aft cargo detection system

Caution

141
Q

CARGO BTL LO

A

Indicates that one or both cargo bottle(s) have discharged

Caution

142
Q

SPOILERONS ROLL

A

Indicates that roll disconnect has been selected and either no or both roll priorities have been selected

Caution

143
Q

PLT/CPLT ROLL CMD

A

Indicates that pilot or copilot roll authority has been selected

Advisory (green)

144
Q

FLUTTER DAMPER

A

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
Q

RUD LIMITER

A

Indicates loss of rudder limiter function

Caution

146
Q

RUD LIMIT FAULT

A

Indicates loss of redundancy in rudder limiter

Status msg

147
Q

ELEVATOR SPLIT

A

Indicates that left and right elevator surface mismatch exceeds 6° (below 250 kt) or 3° (above 250 kt)

Caution

148
Q

PITCH FEEL

A

Indicates a failure of the pitch feel system

Caution

149
Q

PITCH FEEL FAULT

A

Indicates a loss or redundancy in the pitch feel system (one actuator failed)

Status msg

150
Q

STALL FAIL

A

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
Q

STAB TRIM

A

Indicates that both channels of the control unit are disengaged or have failed

Caution

152
Q

STAB TRIM LIMIT

A

Indicates that stabilizer trim is at or greater than 14 trim units

Caution

153
Q

MACH TRIM

A

Indicates that Mach trim is not engaged or has failed in both channels

Caution

154
Q

STAB FAULT

A

Indicates loss of redundancy in stabilizer trim control

Status msg

155
Q

SPLR/STAB FAULT

A

Indicates a fault in the spoiler and stabilizer control unit

Status msg

156
Q

SSCU 1/2 FAULT

A

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
Q

FLAPS FAIL (caution)

A

Indicates that both Flap channels have failed

Caution

158
Q

SLATS FAIL

A

Indicates that both Slat channels have failed

Caution

159
Q

SLAT FAULT

A

Indicates that left or right slat disconnect sensor has detected a mismatch (one detects open)

Status msg

160
Q

FLAP FAULT (sts msg)

A

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
Q

SLATS/FLAPS HALFSPEED

A

Indicates that one channel of the respective system has failed or system is operating on ADG power

Status msg

162
Q

IB/OB FLT SPLRS

A

Indicates a loss of proportional lift dumping capability for respective multi function spoilers

Caution

163
Q

IB/OB GND SPLRS

A

Indicates that respective ground spoilers are inoperative

Caution

164
Q

IB/OB SPOILERONS

A

Indicates loss of roll assist capability for respective multi function spoilers

Caution

165
Q

FLT SPLR DEPLOY (caution)

A

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
Q

GND SPLR DEPLOY

A

Indicates that a ground spoiler is deployed and airplane is not on the ground

Caution

167
Q

GLD NOT ARMED

A

Indicates that ground lift dumping is not armed and airplane is either in approach or takeoff configuration

Caution

168
Q

GLD UNSAFE

A

Indicates that ground lift dumping mode is unsafe (possible inadvertent deployment of spoilers due to failure if two or more input sensors)

Caution

CRJ Limitations (5 decks)

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