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41 Cards in this Set
- Front
- Back
- 3rd side (hint)
Magenta colours on the mini ND indicate what? |
PF has selected FMS1 on FGCP |
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The amber SINGLE SRC indicates? |
That the AP is working with one source (ADC failure) |
What has failed? |
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The yellow ADC2 on the PFD indicates? |
ADC1 is failed and information is now from ADC2 |
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Normal (non icing) flight conditions. To safely retract flap from 15° to 0°... |
... Speed must be above the white bug |
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DU5 has failed... |
... Automatic reconfiguration is preformed by the system. Other views can be displayed via the FO switching PFD/EWD/MFD push button |
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What has failed? |
AHRS |
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In flight... |
... DC bus 2 has failed |
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In case of a dual DC generator loss... |
... An automatic switching allows some batteries to supply some DC buses |
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Assuming normal operation in flight, when are the DC EMER and DC ESS buses connected to DC bus 1 and/or DC bus 2 |
Always through the BAT CHG contractors and the respective HOT EMER or HOT MAIN BAT bus |
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In flight with OEI, which indication would be displayed on the shutdown engines DC GEN pushbutton? |
Amber FAULT if push button is depressed (in) |
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With batteries only, AC bus 1 and AC bus 2 are: |
Never supplied |
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With batteries only, AC bus 1 and AC bus 2 are: |
Never supplied |
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With all four aircraft generator push buttons in, and EXT PWR supplying both ACW and DC, which light should be illuminated in all four generator pushbuttons? |
Amber FAULT |
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The UND/V light illuminates amber when: |
DC STBY bus voltage is less than 19.5 volts |
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With the engines shut down and the BAT switch ON: |
Allows EXT PWR operation or a reduced DC supply |
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When the DC starter/generator is functioning as a started during a battery start: |
It is electrically supplied from the HOT MAIN BAT bus |
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In the event of thermal runaway of the MAIN BAT the MAIN BAT CHG FAULT light illuminates (BAT CHG contactor opens) and: |
The MAIN BAT supplies the HOT MAIN BAT bus and DC ESS bus is transferred to DC bus 1 |
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Illumination of one emergency power indicator (arrow)in flight shows: |
The supply of DC ESS or DC EMER bus from the corresponding HOT BAT bus |
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What is the finunction of the OVRD position for the BAT toggle switch? |
Overrides all automatic operation to ensure that the buses are supplied by their respective battery |
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With the STBY bus OVRD push button set to OVRD, where will the DC STBY bus and AC STBY bus (via INV 1) be supplied from? |
The HOT EMER BAT bus |
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From where is the DC GND HDLG bus powered? |
HOT MAIN BAT bus or DC SVCE bus |
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With the aircraft on the ground, BAT switch is OFF and the EXT PWR AVAIL light illuminated, what must be done to fully power the DC electrical system? |
Place the BAT switch to ON and after the self test process is complete press the EXT PWR push button. |
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Following an inverter failure, the INV light illuminates and: |
The associated AC bus is supplied by the other inverter. |
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In the event that both DC bus 1 and DC bus 2 are lost, INV 1 will be supplied automatically by the HOT MAIN BAT bus or: |
By the HOT EMER BAT bus on the OVRD configuration, or if the TRU if selected on. |
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With the DC BTC pb selected to NORM, when will the flow bar illuminate? |
Only during EXT PWR, Hotel mode or single gender operation |
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With only the BAT switch ON, which battery powers the DC STBY bus? |
The main battery |
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With only the BAT switch ON, which battery powers the DC STBY bus? |
The main battery |
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If the number 1 inverter fails: |
The AC bus 1 BUS OFF light will illuminate for 10 seconds, and then extinguish and the INV FAULT light illuminates |
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During the start sequence on the ground, the cross start system: |
Uses the MAIN BAT and opposite DC GEN |
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Turning on the TRU... |
Supplies four buses without a time limitation |
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ACW GEN 1 has failed |
The BTC has closed automatically |
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ACW BUS 2 has failed... |
TRU is lost |
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When ACW SVCE bus is shed, what indications are given? |
SHED amber light on attendant panel ACW SVCE bus push button |
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Can the ACW SVCE bus be powered exclusively by an external AC supply? |
Yes, but the flight attendant panel ACW GND SVCE bus push button must be selected on |
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Can the ACW SVCE bus be powered exclusively by an external AC supply? |
Yes, but the flight attendant panel ACW GND SVCE bus push button must be selected on |
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To climb from the cockpit through the emergency hatch... |
... Steps are available |
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The oxygen supply is... |
... Available for flight crew and passengers |
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With the N/100% rocker on the flight crew oxygen mask set to N the mask will deliver: |
A diluted oxygen flow only |
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To obtain a correct pressure indication of the pressure gauge located on the overhead panel: |
Electrical power (DC ESS Bus) is required |
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What provision is made to allow entry into the forward baggage compartment from the cockpit when oxygen is required? |
The supply hose on the observers mask is long enough for the purpose |
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When the emergency selector on the flight crew oxygen mask is rotated on the direction of the arrow the mask will deliver: |
A continuous flow of 100% oxygen |
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