AUTO FLIGHT Flashcards

1
Q

On takeoff with SRS mode, minimum height for use of autopilot.

A

100 ft AGL

FMGS logic prevents the autopilot from engaging during the 5 s after liftoff.

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2
Q

Straight-in non precision approach, minimum height for use of autopilot.

A

Applicable MDA (MDH)

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3
Q

Straight-in LNAV VNAV approach, minimum height for use of autopilot.

A

Applicable DA

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4
Q

Circling approach, minimum height for use of autopilot.

A

Applicable circling minimums -100 ft.

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5
Q

ILS approach When

CAT2 or CAT3 is NOT displayed on the FMA, minimum height for use of autopilot.

A

160 ft AGL

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6
Q

PAR approach (Precision Approach Radar), minimum height for use of autopilot.

A

250 ft AGL.

Use AP and or FD , with HDG/V S or TRK/FPA.

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7
Q

Go-around (AP or FD engagement), minimum height for use of autopilot.

A

500 ft AGL

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8
Q

All other phases Not specified in Limitations, minimum height for use of autopilot

A

500 ft AGL

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9
Q

Use of AP or FD in OPEN DES or DES mode is not permitted in approach, unless …..

A

FCU altitude is set to, or above, MDA (MDH) or 500 ft, whichever is the highest.

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10
Q

AUTOTHRUST FUNCTION USE

A

Use of the autothrust is approved with, or without, AP FD in selected or managed mode.

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11
Q

FMGS lateral and vertical navigation has been certified, Except for:

A

ILS, LOC, LOC-BC, LDA, SDF and MLS

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12
Q

RNP accuracy with GPS PRIMARY, or radio updating, has been demonstrated ENROUTE to be:

A

With AP ON in NAV …………………….. 1 nm
With AP OFF and FD ON …………….. 1 nm
With AP OFF and FD OFF ……………..1.1 nm

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13
Q

RNP accuracy with GPS PRIMARY, or radio updating, has been demonstrated IN TERMINAL AREA to be:

A

With AP ON in NAV …………………….. 0.50 nm
With AP OFF and FD ON …………….. 0.51 nm
With AP OFF and FD OFF ……………. 0.51 nm

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14
Q

RNP accuracy with GPS PRIMARY, or radio updating, has been demonstrated IN APPROACH to be:

A

With AP ON in NAV …………………….. 0.3 nm
With AP OFF and FD ON …………….. 0.3 nm
With AP OFF and FD OFF ……………. Not Authorized

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15
Q

USE OF NAV AND FINAL APP MODES FOR NON-PRECISION APPROACH

A

VOR, VOR DME, NDB, NDB DME or RNAV (including GPS) approach.

Provided GPS PRIMARY is available.

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16
Q

FINAL APP mode guidance capability with GPS PRIMARY has been demonstrated down to …..

A

MDH DH (barometric) 250 ft.

17
Q

NAV mode may be used in the terminal area,

provided:

A

GPS PRIMARY is available,
or ‐ HIGH accuracy is displayed,
And the appropriate RNP is checked,
or ‐ NAVAID raw data is monitored.

18
Q

It is NOT permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV FPA. When…..

A

One engine is inoperative.

only FD use is permitted.

19
Q

CATEGORY II

Autopilot use

A

Minimum decision height………………………. 100 ft AGL
At least one autopilot must be engaged in APPR mode,
and CAT 2, CAT 3 SINGLE or CAT 3 DUAL on the FMA.
If automatic approach without autoland, autopilot
must be disengaged no later than 80 ft AGL.

20
Q

CATEGORY III FAIL PASSIVE (SINGLE)

Auto Pilot Use

A

Minimum decision height…………………………50 ft
At least one autopilot must be engaged in APPR mode,
and CAT 3 SINGLE or CAT 3 DUAL displayed on FMA.
A THR must be used in selected or managed speed.

21
Q

CATEGORY III FAIL OPERATIONAL (DUAL)

Auto Pilot Use

A

A THR must be used in selected or managed speed.
Alert height………………………………………………. 100 ft
CAT III with DH : Minimum decision height…… 25 ft
Minimum RVR…………………………………………… 75 m
2 autopilots must be engaged in APPR mode.

22
Q

Engien Out CAT II and CAT III fail passive autoland are only approved…

A

In configuration (3) and FULL,
and if engine-out procedures
are completed before reaching 1 000 ft.

23
Q

MAXIMUM WIND CONDITIONS FOR CAT II OR CAT III AUTOMATIC APPROACH LANDING AND ROLL OUT

A

Headwind……………………… 30 kt
Tailwind…………………………10 kt
Crosswind………………………20 kt
Crosswind MGO……………..15 kt

24
Q

CAT II and CAT III autoland are approved in FLAP CONF….

A

CONF 3 and CONF FULL

25
Q

Automatic landing is demonstrated:

A

‐ With CAT II and CAT III ILS beam.
‐ With slope angle within (-2.5 °, -3.15 °) range.
‐ At or below the maximum landing weight.
‐ For airport elevation at or below (6 500 ft.) (9 200 ft.)
‐ At approach speed (VAPP) = VLS + wind correction.
- min wind correction 5 kt, max wind correction 15 kt

26
Q

Automatic rollout performance has been approved on…..

A

Dry and wet runways,
but performance on snow-covered
or icy runways has NOT been demonstrated.

27
Q

ILS AUTOLAND
IN CAT I OR BETTER WEATHER CONDITIONS
Is possible on CAT I ILS when:

A

‐ The airline has checked that the ILS beam,
‐ The crew is aware that LOC or GS beam fluctuations,
‐ At least CAT2 capability is displayed on the FMA,
‐ Visual references at least for performed CAT I approach.