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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
Q

HYD FL LO (Amber)

A

Hydraulic reservoir fluid level below 55 cubic inches.

26
Q

IAC 1 CONFIG (Amber)

A

Integrated avionics computers 1 and 2 have mismatched configuration.

27
Q

IAC 2 CONFIG (Amber)

A

Integrated avionics computers 1 and 2 have mismatched configuration.

28
Q

IAC1 FAIL (Amber)

A

Integrated Avionics Computer 1 has failed.

29
Q

IAC2 FAIL (Amber)

A

Integrated Avionics Computer 2 has failed.

30
Q

IAC1 OVHT (Amber)

A

Integrated Avionics Computer 1 internal temperature is high and automatic shutdown is imminent.

31
Q

IAC 2 OVHT (Amber)

A

Integrated Avionics Computer 2 internal temperature is high and automatic shutdown is imminent.

32
Q

IAC XTALK (Amber)

A

Loss of communications between the integrated avionics computers.

33
Q

IRS FAIL (Amber)

A

Inertial Reference System has failed.

34
Q

OBOGS TEMP (Amber)

A

OBOGS Temperature is above 200 degrees F (93 degrees C).

35
Q

LPHT INOP (Amber)

A

Left pitot heater is not energised.

36
Q

RPHT INOP (Amber)

A

Right pitot heater is not energised.

37
Q

PMU STATUS (Amber)

A

Power Management Unit has detected and accommodated a fault in flight or WOW switch failure.

38
Q

TAD FAIL (Amber)

A

Rudder Trim Aid Device has failed.

39
Q

UFCP 1 FAIL (Amber)

A

The Up Front Control Panel in the front cockpit has failed.

40
Q

UFCP 2 FAIL (Amber)

A

The Up Front Control Panel in the rear cockpit has failed.

41
Q

XPDR FAIL (Amber)

A

The transponder has failed.

42
Q

IGN SEL (Green)

A

The ignition is on.

43
Q

M FUEL BAL (Green)

A

FUEL BAL switch is in MANUAL.

44
Q

ST READY (Green)

A

The throttle has been positioned for auto start.

45
Q

BOOST PUMP (Green)

A

The boost pump has been activated by switch, starter relay or low pressure switch.

46
Q

ANTI ICE (Green)

A

The PROBES ANTI-ICE switch is on.

47
Q

TAD OFF (Green)

A

Rudder Trim Aid Device is selected Off.

48
Q

TRIM OFF (Green)

A

The TRIM DISCONNECT switch had been activated,

49
Q

NWS ON (Green)

A

Nosewheel Steering is on.

50
Q

SPDBRK OUT (Green)

A

The speedbrake is extended or extending.

51
Q

RPT AFT (White)

A

The front cockpit MFDs are repeating IAC 2 or aft cockpit information.

52
Q

RPT FWD (White)

A

The rear cockpit MFSs are repeating IAC 1 or front cockpit information.

53
Q

RPT ERR (White)

A

Both cockpits have selected repeat mode on their UFCP at the same time.

54
Q

STATUS/BIT (White)

A

The Status/ Built-in Test page in the Flight Management System has updated or changed.

55
Q

ADC A INOP (White)

A

Internal failure of channel A of the Air Data Computer.

56
Q

ADC B INOP (White)

A

Internal failure of channel B of the Air Data Computer.

57
Q

EDM A INOP (White)

A

Internal failure of channel A of the Engine Data Manager.

58
Q

EDM B INOP (White)

A

Internal failure of channel B of the Engine Data Manager.

59
Q

LAMP TEST (White)

A

The lamp test switch is in the TEST position.

60
Q

IRS DEGD (White)

A

Inertial Reference System/ Global Positioning System hybrid operational mode is degraded.

Texan Emergencies (4 decks)

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