Navigation Flashcards

1
Q

How is each ADIRU powered?

A

Normally 115V AC, and a backup 28V DC power source.

*when an ADIRU is selected to NAV, it is connected to battery to test backup power. ON BAT will illuminate for 5 seconds.

*ADIRU 1 receives power from AC Essential Bus (powered in emergency electrical configuration), while 2 and 3 are on main AC Buses.

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2
Q

How long will ADIRU 2 and 3 remain on battery if power cannot be restored to main AC buses?

A

5 minutes.
Then ADIRU 2 and 3 are disconnected from battery and remain unpowered.

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3
Q

How is a IRU fast alignment achieved?

A

Move mode selector to OFF and back to NAV within 5 seconds.

*IRU will determine if a fast alignment is possible and if not will automatically initiate a full alignment,

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4
Q

The managed speed for TAKEOFF phase is SRS (Speed Reference System). What does this equate to?

A

V2 plus 10kts for both engines running.

V2 for single engine (or current speed if it is higher but no more than V2 +15.
(magenta triangle indicates V2 in all cases).

The GO Around speed target is VAPP, or current speed if higher, limited to VLS +15 kt.

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5
Q

What is green dot speed?

A

The slowest speed the aircraft should fly in the clean configuration (with APPROACH phase activated and gear and flap retracted).

Engine-out operating speed in clean configuration.
Best lift-to-drag ratio speed.
Also corresponds to the final takeoff speed.

Below 15 000 ft AAL, equal to 1.5 × weight (metric tons) +110.
At or below 10 000 ft AAL, Green Dot speed is limited to a maximum of 250 kt.

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6
Q

What happens to MIX IRS if an IRS fails?

A

MIX position is not computed. Each FMGC uses it’s associated IRS position.

*IRS 3 is automatically substituted for a failure of 1 or 2.

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7
Q

When does FMGC position takeoff update occur?

A

When FLEX or TOGA thrust is set, FMGC position is automatically updated to the end of the entered runway.

*if an intersection takeoff is desired, a takeoff shift must be entered (only applicable to aircraft WITHOUT a functioning GPS)

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8
Q

Information from Multi-Mode Receiver 1 (MMR1) is sent to which displays?

A

CA’s PFD and FO’s ND.

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9
Q

What does a Multi-Mode Receiver (MMR) consist of?

A

ILS and GPS contained within one unit.

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