Limitations - LIM-22 Auto Flight Flashcards

1
Q

052- Automatic Approach, Landing and Roll Out:

ILS CAT II:

Decision Height

LIM-22-20

A

Minimum Decision Height

— 100 Ft AGL

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2
Q

053- Automatic Approach, Landing and Roll Out:

ILS CAT II:

Manual Landing

LIM-22-20

A

Automatic Approach Without Autoland, the Autopilot Must Be Disengaged Before

— 80 Ft AGL

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3
Q

054- Automatic Approach, Landing and Roll Out:

ILS CAT II:

Maximum Wind

LIM-22-20

A

Head wind : 40 Kt

Cross wind : 25 Kt

Tail wind : 10 Kt

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4
Q

055- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Passive (Single):

Decision Height

LIM-22-20

A

Minimum Decision Height

— 50 Ft AGL

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5
Q

056- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Passive (Single):

Auto-Thrust (A/THR)

LIM-22-20

A

A/THR Must Be Used in Selected or Managed Speed

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6
Q

057- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Operational (Dual):

Alert height

LIM-22-20

A

Alert Height

— 100 Ft RAD ALT

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7
Q

058- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Operational (Dual):

Auto-Thrust (A/THR)

LIM-22-20

A

A/THR Must Be Used in Selected or Managed Speed

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8
Q

059- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Operational (Dual):

CAT III with DH (A320)

LIM-22-20

A

Minimum Decision Height

— 25 Ft AGL

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9
Q

060- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Operational (Dual):

CAT III with DH (A321)

LIM-22-20

A

Minimum Decision Height

— 22 Ft AGL

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10
Q

061- Automatic Approach, Landing and Roll Out:

ILS CAT III Fail Operational (Dual):

Min. RVR

LIM-22-20

A

Minimum Runway Visual Range

— 75 M

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11
Q

062- Automatic Approach, Landing and Roll Out:

Engine Out:

CAT II and CAT III Fail Passive A320

LIM-22-20

A

Autoland are Only Approved in

— Config FULL,

N-1 Procedures Completed Before 1000 Ft AGL on APP

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12
Q

063- Automatic Approach, Landing and Roll Out:

Engine Out:

CAT II and CAT III Fail Passive A321

LIM-22-20

A

Autoland are Only Approved in

— Config 3 & FULL,

N-1 Procedures Completed Before 1000 Ft AGL on APP

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13
Q

064- Automatic Approach, Landing and Roll Out:

Maximum Wind Conditions for CAT II or CAT III

Automatic Approach Landing And Roll Out

LIM-22-20

A

Head wind : 30 Kt

Cross wind : 20 Kt

Tail wind : 10 Kt

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14
Q

065- Automatic Approach, Landing and Roll Out:

Maximum Reported Wind LIM-22-20

A

* Wind Limitation is Based On:

— Surface Wind Reported by ATC.

* If Wind on ND Exceeds the Autoland Limitations and the

Tower Reports a Wind within Limitations

— The autopilot can remain engaged.

* If the Tower Reports a Wind Beyond Limitations

— Only CAT I Approach WITHOUT Autoland

can be done

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15
Q

067- Automatic Approach, Landing and Roll Out:

Automatic Landing:

Demonstrated with…

B-HTD to B-HTF

LIM-22-20

A
  • CONF 3 and CONF FULL
  • With CAT II and CAT III ILS Beam
  • With Slope Angle within (-2.5°, -3.15°) Range
  • ≤ Maximum Landing Weight
  • Airport elevation ≤ 2500 Ft
  • At Approach Speed (VAPP) = VLS + Wind Correction.

Min Corr +5 Kt, Max Corr +15 Kt

  • Automatic Rollout Approved on:

Dry and Wet RWY,

  • Not Been Demonstrated on Snow-Covered or Icy RWY
  • For Automatic Rollout (N-1) or One REV Inop, the Use

of the Thrust Reverser is Limited to IDLE with a Max

X-Wind of 15 Kt

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16
Q

068- Automatic Approach, Landing and Roll Out:

Automatic Landing:

Demonstrated with…

B-HTJ to B-HTK

LIM-22-20

A
  • CONF 3 and CONF FULL
  • With CAT II and CAT III ILS Beam
  • With Slope Angle within (-2.5°, -3.15°) Range
  • ≤ Maximum Landing Weight
  • Airport elevation ≤ 5750 Ft
  • At Approach Speed (VAPP) = VLS + Wind Correction.

Min Corr +5 Kt, Max Corr +15 Kt

  • Automatic Rollout Approved on:

Dry and Wet RWY,

  • Not Been Demonstrated on Snow-Covered or Icy RWY
  • For Automatic Rollout (N-1) or One REV Inop, the Use

of the Thrust Reverser is Limited to IDLE with a Max

X-Wind of 15 Kt

17
Q

069- Automatic Approach, Landing and Roll Out:

ILS Automatic Landing in CAT I or Better Weather Conditions:

Conditions Required

LIM-22-20

A
  • The Airline has Checked the ILS Beam Quality
  • Awareness that LOC/GS Beam Fluctuations Might Occur
  • At least CAT 2 Capability is Displayed on the FMA
  • CAT 2/3 Procedures are Used
  • Visual References are Obtained at MDA for CAT I

If Not –> GO Around is Initiated