Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Arkia A321 > Navigation > Flashcards

Navigation Flashcards

1
Q

What information may be available if the IR Rotary Selectors are set to ATT?

A
  • IR mode supplying only attitude and heading information, if the system loses its ability to navigate.
  • The heading must be entered through the CDU keyboard and has to be reset frequently (10min).
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

What are the 3 occasions when the ALIGN light will flash?

A
  • ALIGN fault
  • No present position entry after 10min
  • Different between position at shutdown and entered position exceeds 1 degree of latitude or longitude
  • If the aircraft moves during alignment (windy day).
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

When does the ON BAT light illuminate?

A

Comes on amber when one or more IRs is supplied only by the A/C battery. It also comes on for a few seconds at the beginning of the alignment, but not for a fast realignment.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

What should NOT be tested during APU start?

A

Compass, because of the location of the APU power on contractor in the cockpit the PAU start sequence may disturb the compass reading.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

When the ILS is tuned on an RMP, what information is NOT available?

A

When the flight crew uses an RMP t turn an ILS/DME, the PFDs do not display the DME distance.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

If both FMGS fail, how are navaids tuned?

A
  • RMP in the NAV backup mode, the crew can select radio communication systems as normal
  • Setting on RMP to NAV backup mode removes navaids tuning from both FMGCs.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Which NAVAIDS can be tuned from RMP1 & RMP2 and RMP3?

A

CAPT RMP: VOR1, ADF1
F/O RMP: VOR2, ADF2
Either RMP: both ILS
RMP3: not used for navaids tuning

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

What happens to GPWS warnings if the loudspeakers are turned off?

A

The audio volume of GPWS aural warning or cautions is not controlled by the loudspeaker volume knobs.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

When will TERR ON ND automatically switch on?

A

If an alert is generated (caution or warning) and TERR p/b switch ON ND is not selected, the terrain and the obstacles are automatically displayed, and the ON light of the TERRN p/b switch ON ND comes on.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

If TERR ON ND is indicating ON, what happens to the wether radar?

A

Weather radar image not displayed.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What produes the information on the ND when using EGPWS?

A

TAD

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

How is the information displayed in order to prevent confusion with weather radar?

A
  • The weather radar TILT is replaced by a blue TERR and the terrain display sweeps form the centre outward to both ND sides.
  • To differentiate between the terrain and the weather display, the terrain display sweeps form the centre outward to both sides of the ND.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

When should LDG FLAP 3 be selected ON?

A

Flap mode is inhibited when flaps config 3 is selected, in this case, LDG MEMO displays “flaps 3” instead of “config full”

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

When should FLAP MODE be selected OFF?

A

Flap mode (too low flaps mode 4) is inhibited, to avoid nuisance warning in case of landing with flaps setting reduced).

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

If the TERR function of EGPWS fails, or is selected OFF, what happens to GPWS?

A

Inhibits the TAD and TCF modes, and does not affect the basic GPWS mode 1-5. If OFF is selected the ECAM caution NAV GPWS TERR DET FAULT is displayed.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Apart from the EWD, where are TCAS failures displayed?

A

Flag on PFD and ND.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Which colours are displayed on the Vertical Speed Scale?

A

Red, green and normal (grey)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

What causes the pressure setting to pulse on the PFD?

A

When the selection made by the pilot is not correct. STD not selected above transition altitude in climb or STD still selected in approach below transition level or 2500’ radio height if transition level is not available.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

When is RA data displayed?

A
  • Lower than 2500’
  • Green DH+100’ < RA < dh +100’
    If no DHs has been entered, or if both FMGC fail, the radio height appears:
    Green: 400’ < RA < 2500’
    Amber: when RA is less or equal to 400’
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

What is displayed at the bottom corners of the ND?

A
  • NAVAIDS (ADF or VOR)
  • Shape and colour of the associated bearing pointer.
  • Identification or frequencies
  • DME distance
  • Mode of tuning
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

On the EFIS, where are ILS 1 and ILS 2 displayed?

A

ILS 1 information: PFD 1, ND 2

ILS 2 information: PFD 2, ND 1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

In the PLAN mode (ECP) what CANNOT be displayed on the ND?

A
  • Weather radar picture

- Data on NAVAIDS and associated pointers.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

If CHECK ATT appears on the PFD, what should you do?

A
  • Both PFDs display “check ATT” if there is a discrepancy of at least 5 degrees between the attitude valves, pitch and/or roll.
  • Crosscheck the three systems; switch the faulty side to number 3, on the switching panel.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

How long does an IRS alignment take?

A

Completed alignment: 10 mins

Fast alignment: 30 sec

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

How is a rapid alignment done and when?

A
  • Turn off the 3 ADIRS then turn them back on within 5 seconds
  • When G/S > 5 knots
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

What should you do if there is a NAV ACCUR DOWNGRADE message?

A

Compare raw data from tuned navaids with FM computed data on ND or PROG.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

How can LAT/LONG be adjusted on the MCDU?

A
  • Slewing or overwriting, and then press the align IRS prompt. (INIT page)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

Wind Heading is displayed in true while the arrow displays in magnetic.

A

Why are the wind heading and arrow different?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

FO PFD, ND and lower ECAM

A

What does ADIRU 2 power?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

M inute: 1 minute to alignment countdown but still not alignedM easure: FROM airport is not current positionM emory: shutdown position different than present by 1 degree lat or longM otion: when tugged during alignment, will restart alignment process in 10 minutes

A

What are the 4 reasons fora IRS IN ALIGN memo?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

91 per axis per IR

A

How many Ring Laser Gyros are on board?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Baro Reference SelectorsADIRS Control and Display Unit (CDU)(MCDUs) Multifunction Control and Display Units

A

What are the pilot inputs to the ADIRS?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

GP-IRS position is accurate and used by FMS

A

What does GPS PRIMARY mean?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

FO angle of attackFO Total air temperatureFO pitot and static systemsUses 3 ADMs

A

What are the inputs for ADIRU 2?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

30 seconds, Switch all ADIRS knobs to NAV - OFF - NAV

A

How long does a fast realignment take and how do you accompl

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

Standby angle of attackCA Total air temperatureStandby pitot (1) and static (2) systemsUses 2 ADMs

A

What are the inputs for ADIRU 3?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

When APPR is pressed for an ILS approach or LOC is pressed for a LOC approach

A

When is the only time the aircraft is navigated by a ground

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

Through 2 Multi Mode Receivers (MMRs) which then send data to the ADIRUs. MMR1 =ADIRU1&3 MMR2=ADIRU2

A

How is GPS data calculated?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

On-side positionADIRU3 positionOff-side position

A

What is the MMR hierarchy?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

CA angle of attackCA Total air temperatureCA pitot and static systemsUses 3 ADMs

A

What are the inputs for ADIRU 1?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

91 per axis per IR

A

How many accelerometers are on board?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
42
Q

While in flight using MIX IRS position, FMS recalculates position based on DME/DME or VOR/DME and applies the BIAS to the FMS position. The MIX IRS position is never changed only the FMS position.

A

How is MIX IRS re-calibrated in-flight?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
43
Q

During takeoff, the FMS knows the location of the runway threshold and corrects the MIX IRS position when TOGO power is applied.

A

When GPS is lost and FMS is working off MIX IRS, what realig

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
44
Q

After alignment, the 3 independent IRs calculate present position. The FMS then take the average as the MIX IRS position.

A

When GPS is lost how is position information calculated?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
45
Q

(ADR) Air Data Reference :-Pitot/Static info(IR) Inertial Reference:-Gyro type info (attitude and heading)-position

A

What are the portions of the (ADIRUs) Air Data and Inertial

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
46
Q

Calculated hybrid position using GPS and IRS positionsIRS position only if GPS failsRadio NavigationInternal NAV Database

A

How does ADIRS calculate present position (PPOS)?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
47
Q

(EIS) Electronic Instrument System(FMS)Engine computersFlight Control computersWarning Computers

A

What systems use the ADIRS data?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
48
Q

CA PFD, ND and upper ECAM

A

What does ADIRU 1 power?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
49
Q

Airspeed trendAttitude Indicator and BEta Target (slip/skid)Instant VSIHeadingAll ND info (except TAS)G load meter

A

What does the IR (Inertial Reference) supply data to ?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
50
Q

AirspeedAltitudeBackup VSI (amber boarder around VSI)TASTotal Air Temp (TAT) and Saturated Air Temp (SAT)

A

What does the AD (Air Data) supply data to ?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
51
Q

3 separate (ADIRUs) Air Data and Inertial Reference Units

A

What does ADIRS consist of?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
52
Q

Terrain Awareness DisplayTerrain Clearance FloorRunway Field Clearance FloorTERR pb

A

What are the 3 enhanced features of the GPWS? What pb contro

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
53
Q

Basic simply looks at RA while enhanced looks and predicts terrain ahead.

A

What is the difference between the basic and enhanced GPWS f

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
54
Q

SYS pb

A

What pb turns the basic functions off?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
55
Q

When landing Flaps 3 instead of FULL. Disables the warning.However, will warn when not at Flaps 3

A

Why would you push the the LDG FLAP 3pb?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
56
Q

Plan Mode

A

What mode will not allow you to display Terrain on the ND?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
57
Q

60 seconds

A

You get a Terrain Caution, how long until impact?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
58
Q

30 seconds

A

You get a Terrain Caution, how long until impact?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
59
Q

<160NM

A

At what range will Terrain warnings and cautions be displaye

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
60
Q

System provides min altitudes at various ranges from airports, if airplane is lower than set min altitude you will get a “TOO LOW TERRAIN” alert

A

What is the Terrain Clearance Floor (TCF)?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
61
Q

The Runway Field Clearance Floor is for high altitude runways significantly higher than surrounding terrain.

A

What is the difference between the Terrain Clearance Floor a

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
62
Q

You have lost:Terrain DisplayTerrain Clearance FloorRunway Field Clearance Floor

A

What happens when you get a FAULT light on the TERR pb?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
63
Q

All basic GPWS functions are lost but Enhanced features remain

A

What happens when you get a FAULT light on the SYS pb?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
64
Q

There are two sweeps, an upper and a lower. The upper detects short range weather and the lower, long range weather.

A

Why is it a multiscan radar?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
65
Q

Doppler effect of moisture ahead of the aircraft allows the radar to predict windshear ahead.

A

How does the windshear warning system work?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
66
Q

Tilt knob

A

When MAN is selected how can the crew adjust radar tilt?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
67
Q

Ground Clutter Suppression, eliminates ground returns, allowing for lower tilt angles than normal.

A

What does the GCS mode do?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
68
Q

WX Weather onlyWX+T Weather + TurbulenceTURB Turbulence onlyMAP Ground Mapping

A

What are the 4 radar modes?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
69
Q

+8

A

When MULTISCAN switch is set to AUTO, what should the gain b

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
70
Q

The Tilt angle is reference to the horizon. So any pitch or roll will not affect the radar return.

A

When manually setting the tilt angle, what happens with when

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
71
Q

Predictive Wind Shear system

A

What is the PWS switch?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
72
Q

Turbulence, 40 NM

A

What does MAGENTA represent on the ND radar screen? What is

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
73
Q

Scan is 90 degrees until below 2300, then it is reduced to 60 degrees.Windshear is detected 30 degrees either side up to 5 NM. But range must be set to 10 NM for windshear to be displayed.

A

How is the radar scan changed during approach?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
74
Q

PWS switch…ONALT…below 1500Engine…runningTransponder…NOT in STBYRADAR does NOT have to be ON

A

What is the criteria for Predictive Windshear Alerts?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
75
Q

PWS…OFFSYS…OFFTransponder…STBY

A

How can you terminate radar emissions?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
76
Q

Below 50 AGLOn TO after passing 100 kts through 50 AGL

A

When are windshear alerts inhibited?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
77
Q

30-40 NM+/- 9900 feet

A

What is the range of detection?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
78
Q

Other - no threatProximate - no threat within 6NM and 1200’Traffic Advisory - Close but no collision (TCPA 40sec)Resolution Advisory - Collision Threat (TCPA 25sec)

A

What are the 4 types of traffic alerts?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
79
Q

SYS1 gets from ADR1SYS2 gets from ADR2

A

Where does the transponder gets ALT input from?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
80
Q

THRT TA or RA displayed only +/- 2700ALL all traffic +/- 2700ABV +9900(7000) / -2700BLW +2700 / -9900(-7000)

A

What does the Traffic Selector do?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
81
Q

TCAS selected to STBYBoth Transponders FAILBoth Radar Altimeters FAIL

A

When is a TCAS STBY memo displayed?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
82
Q

Corrective RA: climb/descendPreventative RA: No climb/descent required

A

What are the 2 types of RAs?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
83
Q

Ignore it or turn it off

A

What do you do with the FD during an RA?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
84
Q

If DMC1 fails, 2 auto replaces both ECAM, Capt. Lose PFD/ND.

A

What do you see if DMC 1, 2 or 3 fail?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
85
Q

Engine/Warning page replaces System/Status page on lower DU.

A

What happens if the UPPER ECAM screen fails?

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
86
Q

ECAN/ND XFR, to display the E/W on a ND.Push and hold the related system page P/B on ECAM control panel for 3 mins max to show on ND.

A

What should you do if both ECAM Screens fail?

87
Q

PFD/ND XFR.If a PFDU fails, the system auto transfers the PFD image to the NDU.

A

What happens if the Capt’s LEFT EFIS screen fails? How can the ND be displayed?

88
Q

Automatic call of the relevant system page on the S/D. the affected parameter pulses green. None aural.

A

What happens when an ADVISORY is triggered?

89
Q

Caution (amber) on E/WD without procedure.No chime. Crew awareness, 1 system redundancy.E.g. CPC is level 1.

A

What indications follow a level 1 caution?

90
Q

Master cautions (steady, amber)Caution message on E/WD.Auto call of the relevant system page on the S/D.E.g. engine failure

A

What indications follow a level 2 caution?

91
Q

Master WARN light flashing (red).Warning message (red) on E/WD.Call of system page on the S/D.Continue, repetitive chime, sound or voiceE.g. engine fire.

A

What indications follow a level 3 warning?

92
Q

Independent: affects an isolated system without degrading the others, e.g. a pump.Primary: cost the aircraft the use of other systems, e.g. an engine.Secondary: loss of systems result of a primary failure, e.g. hydraulics.

A

What is meant by Independent, Primary, or Secondary failures?

93
Q

The information has overflowed off the screen.Press the clear button to scroll down.

A

What does a downward pointing arrow at the bottom or the EWD or STS S.D. signify?

94
Q

Avoid alerting crew during high workload.T/O: phases 3-5 (1st ENG T/O til 1500’RA or 2’ after T/O).LDG: phases 7-8 (800’ til 80kts).

A

What is the meaning of: T/O (or LAND) INHIBIT (magenta memo)? When are they displayed?

95
Q

Below 2000’RA until 80kts after touchdown.

A

When does the LDG MEMO appear on the EWD?

96
Q

2mins after 2nd engine start, orAt least 1 engine running when T/O config button pressed.Disappears at T/O thrust application.Won’t warn the crew if only 1 engine started for T/O til T/O thrust selected.

A

When does the T/O MEMO appear on the EWD?

97
Q

[ADV] shown on bottom half of screenan advisory message appears on the upper part of the EWD associated key on the ECAM control panel lights up.

A

With one ECAM screen failed, how is an ADV shown?

98
Q

Wheel page appears.

A

What happens to the SD when the Gear is extended on Finals?

99
Q

The APU page appears, until RMP>75% for >10secs or switched off.

A

During APU start, what happens to the SD?

100
Q

Sidestick >3degrees in pitch or roll, rudder >22degrees.

A

What causes the FLT CTLS SD to appear automatically on taxy-out?

101
Q

1st ENG T/O power.

A

What causes the ENG SD to be Auto-called on T/O?

102
Q

When slats are extended during descends unless the page is empty.

A

When is the STS S.D. automatically called (other than during an ECAM drill)?

103
Q

Light up until cleared or pressed again.

A

What happens on the ECP (ECAM Control Panel) if a system is manually called?

104
Q

All warning, caution messages and status pages that have been suppressed by the activation of the CLR P/B.All the alerts that are still active but inhibits in the whole active flight phases, if there are no suppressed, it shows NORMAL for 5secs.

A

Pressing the RCL button, for LESS than 3 seconds, does what?

105
Q

EWD displays caution messages that were suppressed by the EMER CANC (cancel all cautions but no all warning cannot be cancelled, e.g. OVSPD.

A

Pressing the RCL button, for MORE than 3 seconds, does what?

106
Q

Display the status pageShows ‘normal’ for 5 seconds.

A

What happens if the STS button is pressed on a fully serviceable aircraft?

107
Q

Test that triggers a warning if the aircraft is not in T/O config.

A

What is the effect of pressing the T/O CONFIG button?

108
Q

The SD successively displays all the system page at 1 second intervalsAll button is powered with separate with power.

A

How does the ALL button work?

109
Q

Up to 3mins by pushing and holding the system page P/B (simulates button stuck), even holding longer, disappears after 3mins.

A

In single ECAM screen operation, how can a S.D. be displayed? And for how long?

110
Q

To suppress spurious all master cautions + some warnings.

A

When should the EMER CANX button be used?

111
Q

RED: immediate actionAMBER: be aware, but no immediate actionGREEN: normalBLUE: normal operation of a system used temporarilyWHITE: abnormal P/B position, test or maintenance information.

A

What do the various colours signify on the pushbutton switches on the overhead panel?

112
Q

IRS DME/DME.

A

How does the FMGC compute radio position?

113
Q

Yes.

A

Can you turn the ADR OFF and still have the IR?

114
Q

The crew can use the MCDU to override the FMGCs automatic selection and tuning of navaids and select a specific navaid for visual display.

A

How does the manual tuning work?

115
Q

The aircraft has two independent GPS receivers. Each GPS receiver is integrated in a modular avionic unit called MMR (Multi Mode Receiver) GPS 1 receiver in MMR1 nas GPS 2 receiver in MMR2.

A

How many GPS receivers are installed?

116
Q

The GPWS is embedded in the T2CAS system (Terrain and Traffic Collision Avoidance system) and generates aural and visual warnings between radio altitudes 10 and 2450ft.

A

When is the Ground Proximity Warning System (GPWS) active?

117
Q

It is possible to carry out a rapid alignment by turning off all three ADIRS momentarily.

A

During a turnaround you notice that there is a residual ground speed on both ND’s. How do you correct this?

118
Q

All modes except PLAN.

A

The weather radar image can be displayed on which modes of the ND?

119
Q

If both FMGCs fail the flight crew can use the Radio Management Panels RMP 1 and 2 on the pedestal for back up tuning. The CAPT RMP controls VOR 1 and ADF 1 the F/O RMP controls VOR 2 and ADF 2.

A

How does the BACK UP TUNING work?

120
Q

Each ADIRU is divided in two parts either of which can work separately in case of failure in the other: The ADR part which supplies barometric altitude airspeed mach angle of attack temperature and overspeed warnings. The IR part which supplies attitude flight pathvector track heading accelerations angular rates ground speed and aircraft position.

A

How many parts does each Air Data and Inertial Reference System (ADIRS) have?

121
Q

Approximately 10 minutes.

A

With the DATA selector set to HDG the time remaining until the completed IRS alignment is displayed on the control display. How long does is normally take?

122
Q

At takeoff alerts are inhibited above 100 knots and up to 50 feet. During landing alerts are inhibited below 50 feet.

A

When are windshear alerts inhibited?

123
Q

Attitude airspeed and mach altitude barometric pressure LS function and bugs.

A

What kind of information is displayed on the Integrated Standby Instrument System (ISIS)?

124
Q

The ADIRS supplies temperature anemometric barometric and inertial parameters.

A

What kind of information are supplied by the Air Data and Inertial Reference System (ADIRS)?

125
Q

ILS1 on the PFD and ILS2 on the ND (if selected).

A

An ILS approach is being carried out. Which ILS information is currently provided to the captain?

126
Q

The system scans the airspace within a range of 5 NM ahead of the aircraft for windshears. Below 1500 feet when the system detects a windshear depending on the range selected on teh ND a warning caution or advisory message appears on the ND. Predictive windshear warnings and cautions are associated with an aural warning.

A

How does the Predictive Windshear System (PWS) operate?

127
Q

If one GPS receiver fails the three ADIRU‘s automatically select the only operative GPS receiver.

A

What occurs in case of one GPS failure?

128
Q

The PWS operates when the PWS switch is in AUTO position (even if the weather radar is OFF) and the aircraft is below 2300 feet AGL and ATC is switched to ON or AUTO or XPdR or XPNDR position (depending on the ATC panel) and either engine is running.

A

When does the Predictive Windshear System (PWS) operate?

129
Q

Mode 1 - Excessive rate of decentMode 2 -Excessive terrain closure rateMode 3 -Altitude loss after takeoff or go-aroundMode 4 -Unsafe terrain clearance when nor in landing configurationMode 5 -Too far below glideslope

A

What are the basic functions of the Ground Proximity Warning System (GPWS)?

130
Q

OFF:All basic GPWS alerts (Mode 1 to 5) are inhibited.FAULT LT:This amber light comes on, along with an ECAM caution, if the basic GPWS mode 1 to 5 malfunction.

A

SYS pb
(GPWS panel)

  • OFF
  • FAULT Light
131
Q

OFF: Glideslope mode (mode 5) is inhibited.

A

G / S MODE pb
(GPWS panel)

  • OFF
132
Q

OFF:Flap mode (“TOO LOW FLAPS” mode 4) is inhibited. (To avoid nuisance warning in case of landing with flaps setting reduced).

A

FLAP MODE pb
(GPWS panel)

  • OFF
133
Q

ON:Flap mode is inhibited when FLAPS CONF 3 is selected (to avoid nuisance warning in case of landing in CONF 3). In this case, LDG MEMO displays FLAPS … 3 instead of “CONF… FULL.”

A

LDG FLAP 3 pb
(GPWS panel)

  • OFF
134
Q

OFF: Inhibits the Terrain Awareness Display (TAD) and Terrain Clearance Floor (TCF) modes. Does not affect basic modes.If OFF is selected the ECAM caution NAV GPWS TERR DET FAULT is displayed.FAULT LT:TAD or TCF mode fails. The terrain is not shown on the ND. The basic GPWS mode 1 to 5 are still operative if the SYS pb OFF or FAULT lights are not illuminated.

A

TERR pb
(GPWS panel)

  • OFF
  • FAULT Light
135
Q

PULL UP:Comes on red + specific voice alert when the second boundary of Mode 1 is penetrated, or when Mode 2, or any TAD or TCF alert is activated.GPWS:Comes on amber + specific voice warning when any other mode is activated.

A

PULL UP - GPWS pb
(Instrument panel)

  • PULL UP Light
  • GPWS Light
136
Q

ON:The terrain is displayed on the ND, if the:- TERR pb is selected ON, and- TERR FAULT light is not on.The ON light comes on.OFF:The terrain data is not displayed on the ND.

A

TERR ON ND pb
(Instrument panel)

  • ON
  • OFF
137
Q

OFF:The ADIRU is not energized. ADR and IR data are not available.NAV:Supplies full inertial data to aircraft systems.ATT: IR mode supplies only attitude and heading information, if the system loses its ability to navigate. The heading must be entered through the CDU keyboard and has to be reset frequently (about every 10 minutes).

A 
IR 1(2)(3) Mode Rotary Selector
(ADIR Panel)
  • OFF
  • NAV
  • ATT
138
Q

FAULT:With an ECAM caution when a fault affects the respective IR.Steady: the respective IR is lost.Flashing: the attitude and heading information may be recovered in ATT mode.ALIGN:Steady: the respective IR is operating normally in align mode.Flashing IR alignment fault:1. no present position entry after 10 min2. difference between IR positions3. difference between position at shutdown and entered position exceeds 1° of latitude or longitude.4. movement during alignmentExtinguished: Alignment has been completed.

A 
IR 1 (2) (3) LT
(ADIR Panel)
  • FAULT Light
  • ALIGN Light
139
Q

Comes on amber when one or more IRs is supplied only by the a/c battery. It also comes on for a few sec at the beginning of the alignment, but not for a fast realignment.

A

ON BAT LT

ADIR Panel

140
Q

This knob selects the information to be displayed in the ADIRS display window.TEST: The ENT and CLR buttons on the keyboard come on, and the display shows all 8’s.TK/GS: The display shows true track and ground speed.PPOS: The display shows present latitude and longitudeWIND: The display shows true wind direction and speed.HDG: The display shows true heading and the minutes remaining until alignment iscompleted.STS: The display shows an action code.

A

DATA selector knob

ADIR Panel

141
Q

OFF:The CDU display is not energized. ADIRS are still energized if the associated IR mode rotary selectors are not at OFF.1.2.3:System selected for data display.

A

SYS selector knob
(ADIR Panel)

  • OFF
  • 1.2.3
142
Q

OFF:Air data output disconnected.FAULT:This amber light comes on with an ECAM caution, if a fault is detected in the air data reference part.

A 
ADR 1 (2) (3) pb (momentary action)
(ADIR Panel)
  • OFF
  • FAULT Light
143
Q
  • Mode 1: Excessive descent rate (“Sink Rate”)- Mode 2: Excessive terrain closure (“Terrain, Terrain”)- Mode 3: Altitude loss after takeoff (“Don’t Sink”)- Mode 4: Unsafe terrain clearance (“Too Low Flaps”, “Too Low Gear”)- Mode 5: Excessive GS deviation (“Glideslope”)
A

What are the GPWS modes?

144
Q
  • Flight Guidance- Flight Management
A

What are the functions of the Flight Management Guidance Computers?

145
Q
  • Managed Guidance- Selected Guidance
A

What are the 2 modes of flight guidance?

146
Q

Long-term lateral, vertical and speed profiles as determined by the FMGS

A

What is the Managed mode of flight guidance used for?

147
Q

Temporary lateral, vertical and speed commands as selected with the FCU

A

What is the Selected mode of flight guidance used for?

148
Q

Selected Guidance has priority

A

Does Selected or Managed Guidance have priority?

149
Q

FMGS Managed Guidance is in use

A

What do dashes in the FCU display windows along with the adjacent white dot indicate?

150
Q

Pull the appropriate selector knob

A

How is Selected Guidance engage?

151
Q
  • 2 FMGCs- 2 MCDUs- 1 FCU- 2 FACs
A

What are the main components of the FMGS?

152
Q

Navigation database

A

What type of database is periodically updated in the FMGS?

153
Q

Dual mode, with one FMGS as master and the other FMGS as slave

A

What is the normal operational mode of the FMGS?

154
Q
  • If one autopilot is engaged, the respective FMGS is master- If both autopilots are engaged, FMGS 1 will be the master
A

How does autopilot selection influence master FMGS logic?

155
Q

An FMGS has failed and both NDs must be set to the same mode and range (Single Mode)

A

If an amber SELECT OFFSIDE RNG/MODE message is displayed on the ND what action should the crew take?

156
Q
  • Permits short term interface between the pilot and FMGS- Allows temporary modification of any flight parameter (HDG, SPD, ALT, V/S)- Used to select operations modes of the autopilots, flight directors, and A/THR system
A

What is the function of the Flight Control Unit?

157
Q

The pressurization system uses the FMGS data to construct an optimized pressurization schedule

A

The LDG ELEV selector in the AUTO position does what?

158
Q

The pressurization system uses the FMGS data to construct an optimized pressurization schedule

A

The LDG ELEV selector in the AUTO position does what?

159
Q

The pressurization system uses the FMGS data to construct an optimized pressurization schedule

A

The LDG ELEV selector in the AUTO position does what?

160
Q
  • Independent (MCDU scratchpad displays - INDEPENDENT OPERATION)- Single (ND displays - SELECT OFFSIDE RNG/MODE)- Dual (Normal)
A

What are the 3 modes of FMGC operation?

161
Q

A hybrid IRS/GPS position

A

What input does each FMGC use for position determination?

162
Q
  • NO. RMP now control the VOR/ILS receivers- NAV key on RMP 3 has no effect- Normal radio communication is still available
A

If the NAV key is selected on either RMP, can the FMGC still auto tun navaids?

163
Q
  • Magenta: Managed speed computed by the FMGC- Blue: Selected speed on the FCU
A

What is the difference between the magenta and blue target airspeeds?

164
Q

The aircraft has descended below the MDA/DH entered into the FMGC

A

What does it mean when the altitude digits change from green to amber?

165
Q

FMGC database

A

From what source does the pressurization system obtain landing elevation?

166
Q

The crew has limited ability to create pilot stored navigational data

A

Can the crew modify data in the navigation database?

167
Q

On the Aircraft Status page

A

How do you determine the validity of the navigation database?

168
Q
  • Large: Pilot entries and modifiable data- Small: Default/computed non-modifiable data
A

What is the difference between the large and small fonts utilized in the MCDU?

169
Q

An entry is mandatory

A

What do amber box prompts on the MCDU indicate?

170
Q
  • After the LS pushbutton is pressed - green light- ILS frequency and course on PFD- ILS identifier once identified- LOC and GS scales displayed on PFD
A

After you input the destination and ILS information into the MCDU, what do you check for?

171
Q

-Insert the Lat/Long on the MCDU INIT page-Then press Align IRS

A

How do you normally enter Present Position into the IR?

172
Q

When takeoff begins at a runway intersection

A

When would a Takeoff Shift be entered on the PERF TO page?

173
Q

NAV mode will be lost and the HDG/TRK mode engages

A

What occurs when managed NAV mode is engaged and the aircraft flies into the flight plan discontinuity?

174
Q
  • Rose ILS- Rose VOR- Rose NAV- ARC- PLAN
A

What displays or modes are available on the ND?

175
Q

ROSE NAV and 80 NM range

A

If mode range data fails what should you expect to see on the ND?

176
Q
  • ILS- Blue LOC and GS in FMA- RNAV- APP NAV and FINAL
A

After pressing the APPR button, what do you check for?

177
Q

No, they are separate bulbs

A

Are the NAV 1 and 2 positions connected to a single bulb?

178
Q

Ensure that each ADIRU has the ability to revert to the batteries by observing the BAT light illuminating for several seconds.

A

When you turn the mode selectors to NAV, what are you looking for on the panel?

179
Q

-No present position entered within 10 minutes of NAV selection.-Difference of 1 Degree Lat/Long between shutdown and entered position-IR alignment fault

A

What does a flashing white ALIGN light mean?

180
Q

Attitude and Heading may be recovered in ATT mode (you have lost the navigation portion)

A

What does a flashing illumination of the amber IR “FAULT” light indicate?

181
Q

Attitude and Navigation information.

A

What would be missing on the Captain’s PFD if IR 1 failed or was turned off?

182
Q

Selecting CAPT 3 on the EIS switching panel ATT/HDG selector

A

What action would recover the attitude and navigation information?

183
Q

INIT B

A

Where do you enter the Zero Fuel Weight?

184
Q

At ranges of 40 NM or less

A

When is WX/TURB mode available?

185
Q
  • Weather Avoidance- Turbulence Detection- Terrain Mapping- Predictive Windshear Detection
A

What capabilities does the RADAR system have?

186
Q

Yes, if the Windshear switch is in AUTO

A

Does predictive windshear detection work when the RADAR system is switched OFF?

187
Q

1

A

How many RADAR systems are installed?

188
Q

Below 2500’ AGL

A

When is Radio Height displayed on PFD?

189
Q
  • Captain’s PFD- F/O’s ND
A

Information from ILS receiver 1 is displayed where?

190
Q

Flashes amber when APPR mode is armed and the LS display is not selected

A

What would a flashing amber ILS indicate on the bottom of the PFD?

191
Q

Airspeed and Altitude information

A

With the loss of ADR 1 what would be lost on the Captain’s PFD?

192
Q

Up to 5 NM ahead of the aircraft when the aircraft is below 1500’ AGL

A

What is the scanned area of the predictive windshear detection feature?

193
Q
  • When on the ground above 100knots until reaching 50’ AGL- When landing below 50’ AGL
A

When are predictive windshear alerts inhibited?

194
Q
  • Engine out operating speed in clean configuration- Appears when the aircraft is in the clean configuration- Corresponds to the best lift-to-drag ratio
A

What is Green Dot speed?

195
Q

Arms, engages, or disengages the LOC mode

A

What is the function of the LOC pushbutton?

196
Q
  • At or below 20,000 ft equal to 2 x weight in metric tons (2204.6 lbs) + 85- Above 20,000 ft add 1 kt for each 1000’(FCOM 3.04.10)
A

How is Green Dot speed computed?

197
Q
  • Mode selector in PLAN- TERR selected ON
A

What would prevent the weather display on the ND?

198
Q

-Select Position Monitor page. Verify position deviation is <15 Knots. (FCOM 3.03.25)

A

Describe a post flight ADIRU accuracy check.

199
Q

-Flight Path Vector-Airplane Position-Track-Heading-Attitude-Acceleration-Ground Speed

A

What information is provided by the “IR” units?

200
Q

The respective IR is in the Align mode.

A

What does a steady white ALIGN light indicate?

201
Q

Alignment has been completed.

A

What does it mean when the IR lights are extinguished?

202
Q

Turn the IR mode selectors OFF momentarily (not more than 5 seconds) and then back on.

A

How do you fast align an IR?

203
Q

The respective IR has a fault.

A

What does steady illumination of the amber IR “FAULT” light indicate?

204
Q

A fault is detected in the Air Data Reference portion.

A

What does the amber ADR “FAULT” light indicate?

205
Q

Yes

A

Does turning the IR to OFF also turn off the ADR?

206
Q

Yes

A

Can you turn the ADR OFF and still have the IR?

207
Q

Input Heading (ex. 180.0) on the IR panel every 10 minutes

A

What information must be input when the IR is in ATT?

208
Q

Selecting CAPT 3 on the EIS switching panel AIR DATA selector

A

What would restore the lost altitude and airspeed information?

209
Q

Both NDs and the DDRMI

A

Where is VOR data displayed?

210
Q
  • Based on a calculated groundspeed at the runway- Protects against actual groundspeed dropping below this calculated groundspeed
A

What is Ground Speed Mini?

211
Q

Inhibits all EGPWS warning except TERR system

A

Pressing the SYS pushbutton does what?

212
Q

Any failure of GPWS mode 1-5

A

What does an amber “FAULT” light in the SYS pushbutton indicate on the GPWS panel?

213
Q

No

A

If the TERR mode failed, does it affect the basic GPWS?

214
Q

No

A

Does a “FAULT” light on the SYS pushbutton affect the TERRAIN mode?

Arkia A321 (23 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions