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Texan Emergencies > CAS Captions > Flashcards

CAS Captions Flashcards

1
Q

FIRE (Red)

A

Engine Fire or Bleed Air leak.

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2
Q

ADC FAIL (Red)

A

Air Data Computer has failed.

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3
Q

BATT BUS (Red)

A

Battery Bus has inoperative.

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4
Q

CANOPY (Red)

A

Canopy Unlocked/ Unsafe.

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5
Q

CHIP (Red)

A

Engine chip detector indicates oil contamination.

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6
Q

CHK ENG (Red)

A

Engine parameters have exceeded operation limitations.

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7
Q

CKPT PX (Red)

A

Cockpit Overpressurisation (3.9 to 4.0 PSI).

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8
Q

EDM FAIL (Red)

A

Engine Data Manager has failed.

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9
Q

FUEL PX (Red)

A

Fuel Pressure is below 10 PSI.

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10
Q

GEN (Red)

A

Generator inoperative.

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11
Q

GEN BUS (Red)

A

Generator Bus inoperative.

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12
Q

OBOGS FAIL (Red)

A

OBOGS system malfunction.

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13
Q

OIL PX (Red)

A

Oil pressure at/ below 40PSI, or oil pressure at 15 to 40 PSI for 5 seconds at Idle.

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14
Q

PMU FAIL (Red)

A

Power Management Unit has failed.

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15
Q

ADS-B FAIL (Amber)

A

Transponder indicates an Automatic Dependent Surveillance - Broadcast (ADS-B) Out function failure.

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16
Q

BUS TIE (Amber)

A

The Bus Tie switch is open, or the bus tie is inoperative.

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17
Q

CHK ENG (Amber)

A

Engine parameters outside normal operating ranges.

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18
Q

CKPT ALT (Amber)

A

Cockpit pressure altitude above 19,000ft.

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19
Q

DUCT TEMP (Amber)

A

Environmental/ Defog duct above 300 degrees F (148 degrees C).

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20
Q

EHYD PX LOW (Amber)

A

Emergency hydraulic pressure at/ below 2400 PSI.

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21
Q

FP FAIL (Amber)

A

Fuel probe malfunction.

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22
Q

FUEL BAL (Amber)

A

Fuel imbalance exceeds 30lb, or fuel probe or EDM fail.

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23
Q

L FUEL LO (Amber)

A

Left wing tank below 110lb usable fuel.

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24
Q

R FUEL LO (Amber)

A

Right wing tank below 110lb usable fuel.

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25
HYD FL LO (Amber)
Hydraulic reservoir fluid level below 55 cubic inches.
26
IAC 1 CONFIG (Amber)
Integrated avionics computers 1 and 2 have mismatched configuration.
27
IAC 2 CONFIG (Amber)
Integrated avionics computers 1 and 2 have mismatched configuration.
28
IAC1 FAIL (Amber)
Integrated Avionics Computer 1 has failed.
29
IAC2 FAIL (Amber)
Integrated Avionics Computer 2 has failed.
30
IAC1 OVHT (Amber)
Integrated Avionics Computer 1 internal temperature is high and automatic shutdown is imminent.
31
IAC 2 OVHT (Amber)
Integrated Avionics Computer 2 internal temperature is high and automatic shutdown is imminent.
32
IAC XTALK (Amber)
Loss of communications between the integrated avionics computers.
33
IRS FAIL (Amber)
Inertial Reference System has failed.
34
OBOGS TEMP (Amber)
OBOGS Temperature is above 200 degrees F (93 degrees C).
35
LPHT INOP (Amber)
Left pitot heater is not energised.
36
RPHT INOP (Amber)
Right pitot heater is not energised.
37
PMU STATUS (Amber)
Power Management Unit has detected and accommodated a fault in flight or WOW switch failure.
38
TAD FAIL (Amber)
Rudder Trim Aid Device has failed.
39
UFCP 1 FAIL (Amber)
The Up Front Control Panel in the front cockpit has failed.
40
UFCP 2 FAIL (Amber)
The Up Front Control Panel in the rear cockpit has failed.
41
XPDR FAIL (Amber)
The transponder has failed.
42
IGN SEL (Green)
The ignition is on.
43
M FUEL BAL (Green)
FUEL BAL switch is in MANUAL.
44
ST READY (Green)
The throttle has been positioned for auto start.
45
BOOST PUMP (Green)
The boost pump has been activated by switch, starter relay or low pressure switch.
46
ANTI ICE (Green)
The PROBES ANTI-ICE switch is on.
47
TAD OFF (Green)
Rudder Trim Aid Device is selected Off.
48
TRIM OFF (Green)
The TRIM DISCONNECT switch had been activated,
49
NWS ON (Green)
Nosewheel Steering is on.
50
SPDBRK OUT (Green)
The speedbrake is extended or extending.
51
RPT AFT (White)
The front cockpit MFDs are repeating IAC 2 or aft cockpit information.
52
RPT FWD (White)
The rear cockpit MFSs are repeating IAC 1 or front cockpit information.
53
RPT ERR (White)
Both cockpits have selected repeat mode on their UFCP at the same time.
54
STATUS/BIT (White)
The Status/ Built-in Test page in the Flight Management System has updated or changed.
55
ADC A INOP (White)
Internal failure of channel A of the Air Data Computer.
56
ADC B INOP (White)
Internal failure of channel B of the Air Data Computer.
57
EDM A INOP (White)
Internal failure of channel A of the Engine Data Manager.
58
EDM B INOP (White)
Internal failure of channel B of the Engine Data Manager.
59
LAMP TEST (White)
The lamp test switch is in the TEST position.
60
IRS DEGD (White)
Inertial Reference System/ Global Positioning System hybrid operational mode is degraded.

Texan Emergencies (4 decks)

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