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Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
15 Cards in this Set
- Front
- Back
Auto Transfer
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Checked CP or FO
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L or R gen on
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After 2 second delay observe
Batt off Bus light on central Bus off light on Gen 1 and 2 off bus lights on Aux GEN 1 and 2 off bus lights on Transfer fail light on Emerg bus off light out indication that the battery is powering the embergency buses |
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Electrical emergecy switch
emerg |
L or R GEN off
Check that the system stays locked in Emergency transfer and annuciator lights remained unchanged |
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Electrical emergency switch
normal |
check all lights are out except the following
GEN 1 and GEN 2 off bus light on Aux Gen 1 and 2 off bus lights on |
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Back up battery test
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white on light on
standy horizon instrument back lighting on back up batt switch arm |
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Flight IDLE STOP cb
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checked by captain
check the captains left side console viewing window that the flight idle stop Circuit Breakers are not open |
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Crew oxygen masks
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checked by cp and fo
on audio control panel SPKR press Mask/boom switch mask adjust volume for oxygen flow test |
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on control wheel
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Hot mic/ptt switch hot mic
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Quick donning oxygen mask stowage box
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Regulator flow selector 100%
reset/test lever press and hold listen for oxygen flow through the speaker, and check that the flow indicator shows a yellow cross then turns black Emergency rotary knob Press the release Listen for oxygen flow through the speaker, and check that the flow indicator shows a yellow cross reset/test lever release mask/boom switch boom audio control panel as required |
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minimum oil temperature required to unfeather
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0 celcius
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Minimum oil temperature to feather
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10 celcius
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ice detector
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ice detector system test button press
single chime alert caution lights flash ice detection system inop light on ice condition light map on Deice light on MAP on This test will take 3 seconds. All lights going out at the end of the test sequence indicates a successful test |
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Rudder test
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checked by FO
This test must be completed with APU power and bleed air source for the hydraulic system reservoir. If APU is not available start the right engine as outlined in the Engine start check |
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Flap Bit
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Checked by first officer
BIT psush-button press single-chime alert on the suplementary flap panel, check the Control Fault caption comes on Flap and Advanced Sws legends flashing All light bars on the annuciator panel come on steady Flap position indicates below 0 degrees on flap totalizer Bit push-button release and press The Asymmetry caption illuminates on the suplementary flap panel RST push-butto press This restores automatic control |
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Ice protection monitor
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check Fo
Ice protection monitor switch test with 2 seconds single-chime alert INOP light on MONITOR panel on Deice light in map on Within 3 seconds All lights on the DE ICING pane on Within the next 2 seconds All lights on the DE-ICING panel OUT |