Crew Alert System

Question 1

Answer 1

BOLD FACE. - Engine chip detector indicates oil contamination

Question 2

Answer 2

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

Question 3

Answer 3

BOLD FACE. - Fuel pressure below 10 psi

Question 4

Answer 4

Generator inoperative

Question 5

Answer 5

BOLD FACE. OBOGS system failure

Question 6

Answer 6

Power management unit failure

Question 7

Answer 7

Generator bus inoperative

Question 8

Answer 8

Battery bus inoperative

Question 9

Answer 9

Cockpit overpressurization; pressure exceeds 3.9 to 4.0 psid

Question 10

Answer 10

Canopy unlocked/unsafe

Question 11

Answer 11

Engine data manager failed

Question 12

Answer 12

Air data computer failed

Question 13

Answer 13

Engine parameters have exceeded operating limitations

Question 14

Answer 14

Emergency hydraulic pressure at or below 2400 psi

Question 15

Answer 15

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

Question 16

Answer 16

Cockpit pressure altitude above 19,000 feet

Question 17

Answer 17

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

Question 18

Answer 18

Inertial reference system (IRS) has failed

Question 19

Answer 19

Integrated avionics computer 1 has failed

Question 20

Answer 20

Integrated avionics computer 2 has failed

Question 21

Answer 21

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

Question 22

Answer 22

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

Question 23

Answer 23

Left wing tank below 110 pounds usable fuel

Question 24

Answer 24

Right wing tank below 110 pounds usable fuel

Question 25

Answer 25

Fuel probe failure

Question 26

Answer 26

BOLD FACE. OBOGS temperature above 200 °F

Question 27

Answer 27

BUS TIE switch open, or bus tie inoperative

Question 28

Answer 28

Environmental duct or defog duct above 300 °F

Question 29

Answer 29

Rudder trim aid device failure

Question 30

Answer 30

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

Question 31

Answer 31

Left pitot heater is not energized

Question 32

Answer 32

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

Question 33

Answer 33

Right pitot heater is not energized

Question 34

Answer 34

Integrated avionics computers 1 and 2 have mismatched configuration

Question 35

Answer 35

Engine parameters are outside normal operating ranges

Question 36

Answer 36

Transponder failure or loss of communication

Question 37

Answer 37

Ignition on

Question 38

Answer 38

FUEL BAL switch in MANUAL position

Question 39

Answer 39

PCL positioned for auto start

Question 40

Answer 40

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

Question 41

Answer 41

PROBES ANTI-ICE switch on

Question 42

Answer 42

Rudder trim aid device selected off

Question 43

Answer 43

TRIM DISCONNECT switch activated

Question 44

Answer 44

Nose wheel steering is engaged/on

Question 45

Answer 45

Speed brake is extended or extending

Question 46

Answer 46

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

Question 47

Answer 47

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

Question 48

Answer 48

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

Question 49

Answer 49

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

Question 50

Answer 50

Internal failure of channel A of the ADC

Question 51

Answer 51

Internal failure of channel B of the ADC

Question 52

Answer 52

Internal failure of channel A of the EDM

Question 53

Answer 53

Internal failure of channel B of the EDM

Question 54

Answer 54

Condition indication for the lamp test switch in test position

Question 55

Answer 55

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