Crew Alert System Flashcards by Philip Wheat | Brainscape

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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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Q

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Left wing tank below 110 pounds usable fuel

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Right wing tank below 110 pounds usable fuel

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Fuel probe failure

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BOLD FACE. OBOGS temperature above 200 °F

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BUS TIE switch open, or bus tie inoperative

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Environmental duct or defog duct above 300 °F

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Rudder trim aid device failure

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

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Left pitot heater is not energized

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

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Right pitot heater is not energized

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Integrated avionics computers 1 and 2 have mismatched configuration

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Engine parameters are outside normal operating ranges

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Transponder failure or loss of communication

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Ignition on

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FUEL BAL switch in MANUAL position

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PCL positioned for auto start

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

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PROBES ANTI-ICE switch on

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Rudder trim aid device selected off

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TRIM DISCONNECT switch activated

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Nose wheel steering is engaged/on

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Speed brake is extended or extending

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

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

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

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

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Internal failure of channel A of the ADC

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Internal failure of channel B of the ADC

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Internal failure of channel A of the EDM

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Internal failure of channel B of the EDM

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Condition indication for the lamp test switch in test position

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