Crew Alert System Flashcards by Philip Wheat

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BOLD FACE. - Engine chip detector indicates oil contamination

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BOLD FACE. - Oil pressure below 40 psi above idle, below 15 psi at idle, or oil pressure between 15-40 psi at idle for 5 seconds or more

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BOLD FACE. - Fuel pressure below 10 psi

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Generator inoperative

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BOLD FACE. OBOGS system failure

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Power management unit failure

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Generator bus inoperative

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Battery bus inoperative

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Cockpit overpressurization; pressure exceeds 3.9 to 4.0 psid

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Canopy unlocked/unsafe

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Engine data manager failed

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Air data computer failed

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Engine parameters have exceeded operating limitations

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Emergency hydraulic pressure at or below 2400 psi

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Hydraulic reservoir fluid level below 55 cubic inches (1qt)

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Cockpit pressure altitude above 19,000 feet

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BOLD FACE. Oil pressure between 15-40 psi at idle or if oil pressure drops below 40 and 90 psi, above idle power for 10 seconds or more

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Inertial reference system (IRS) has failed

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Integrated avionics computer 1 has failed

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Integrated avionics computer 2 has failed

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Up front control panel (UFCP) in front cockpit has failed

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Up front control panel (UFCP) in aft cockpit has failed

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Left wing tank below 110 pounds usable fuel

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Right wing tank below 110 pounds usable fuel

Fuel probe failure

BOLD FACE. OBOGS temperature above 200 °F

BUS TIE switch open, or bus tie inoperative

Environmental duct or defog duct above 300 °F

Rudder trim aid device failure

Fuel imbalance exceeds 30 pounds, or fuel probe or EDM fail

Left pitot heater is not energized

PMU has detected and accomodated a fault in-flight or WOW switch failure

Right pitot heater is not energized

Integrated avionics computers 1 and 2 have mismatched configuration

Engine parameters are outside normal operating ranges

Transponder failure or loss of communication

Ignition on

FUEL BAL switch in MANUAL position

PCL positioned for auto start

BOOST PUMP selected by switch, starter relay, or low pressure switch

PROBES ANTI-ICE switch on

Rudder trim aid device selected off

TRIM DISCONNECT switch activated

Nose wheel steering is engaged/on

Speed brake is extended or extending

Front cockpit multifunction displays (MFD) are repeating IAC2 or aft cockpit MFD information

Aft cockpit multifunction displays (MFD) are repeating IAC1 or front cockpit MFD information

Repeated information has defaulted to last selected configuration because cockpit REPEAT switch positions are conflicted

Status/built in test (BIT) page in flight management system (FMS) information has updated or changed

Internal failure of channel A of the ADC

Internal failure of channel B of the ADC

Internal failure of channel A of the EDM

Internal failure of channel B of the EDM

Condition indication for the lamp test switch in test position

GPS hybrid operational mode is in initialization, acquisition or altitude/clock aiding mode