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2021 Alaska Airbus > Limitations / Memory (Recall) Items > Flashcards

Limitations / Memory (Recall) Items Flashcards

1
Q

Maximum Operating Altitude

A

39,000ft

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2
Q

Engine Start Max Crosswind - A321

A

45 kts

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3
Q

Takeoff Crosswind (gusts included) - A320

A

38 kts

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4
Q

Takeoff Crosswind (gusts included) - A321

A

35 kts

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5
Q

Landing Crosswind (gusts included)

A

38 kts

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6
Q

Takeoff & Landing Tailwind

A

10 kts

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7
Q

Max Airfield Wind for Takeoff or Landing (ASA)

A

50 kts or gust factor of 20 kts

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8
Q

Wind

Passenger Door Operation

A

65 kts

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9
Q

Wind

Cargo Door Operation*

A

40 kts

*50 kts
If aircraft is positioned into the wind
or door is on the leeward side

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10
Q

Cargo doors must be closed before the wind speed

exceeds…

A

65 kts

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11
Q

SEVERE TURBULENCE PENETRATION (ASA)

A320

A

Below FL200:
250 kts

Above FL200:
275kts/0.76 Mach

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12
Q

SEVERE TURBULENCE PENETRATION (ASA)

A321

A

Below FL200:
275 kts

Above FL200:
305 kts/0.76 Mach

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13
Q

Maximum speed with landing gear extended (VLE)

A

280 kts / M 0.67

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14
Q

Maximum speed at which the landing gear may be extended

VLO extension

A

250 kts

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15
Q

Maximum speed at which the landing gear may be retracted

VLO retraction

A

220 kts

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16
Q

Maximum tire ground speed (AFM)

A

195 kts

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17
Q

Max speed with Flight Deck window open

A

200 kts

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18
Q

Max speed when windshield wiper is in use

A

230 kts

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19
Q

Do not use LP Ground Conditioned Air while…

A

Packs Operating (avoids valve chatter)

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20
Q

Min AP engagement on Takeoff

A

100 ft AGL or

at least 5 seconds after liftoff

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21
Q

Min height for AP use in approach with FINAL APP mode

A

250 ft AGL

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22
Q

Min height for AP use in approach with V/S or FPA mode (ASA)

A

Applicable MDA/DH or 250 ft

whichever is higher

23
Q

Min height for AP use on a Circling Maneuver* (ASA)

A

1000 ft AGL or Circling MDA(H),
whichever is higher

  • Alaska Airlines only conducts circling maneuvers (not circling approaches) in VMC weather conditions. The Flight Crew must conduct the maneuver within the circling area while maintaining required visual reference at all times.
24
Q

Min height for AP use during ILS when CAT I is displayed on FMA

A

160 ft AGL

25
Q

Min height for AP use during a CAT I ILS with CAT II or

CAT III DUAL/SINGLE displayed (ASA)

A

80 ft AGL

26
Q

Min height for AP engagement after a manual Go-Around

A

100 ft AGL

27
Q

Min height for AP Use in all other phases

A320

A

500 ft AGL

28
Q

Min height for AP Use in all other phases

A321

A

900 ft AGL

29
Q

Min Oil Quantity for Dispatch (ASA)

A

14 qts

30
Q

Min Oil Temperature for Starting

A

-40°C

31
Q

Min Oil Temperature for Takeoff

A320

A

-10°C

32
Q

Min Oil Temperature for Takeoff

A321

A

19°C

33
Q

Max Number of Consecutive Start Cycles

A320

A

4*

  • A standard auto-start cycle for the Leap1A and CFM56-B engines may consist of up to 3 start
    attempts.
34
Q

Max Number of Consecutive Start Cycles

A321

A

3*

  • A standard auto-start cycle for the Leap1A and CFM56-B engines may consist of up to 3 start
    attempts.
35
Q

Min Cooling Period after Max Engine Start Cycles

A

15 Minutes

36
Q

Min Pause Between Engine Start Attempts (Ground Start)

A320

A

20 Seconds

37
Q

Min Pause Between Engine Start Attempts (Ground Start)

A321

A

60 Seconds

38
Q

Max N2 for Running Re-Engagement of Starter

A320

A

20%

39
Q

Max N2 for Running Re-Engagement of Starter

A321

A

63%

40
Q

Speed below which Max Reverse Thrust

SHOULD NOT be used

A

70 KIAS

41
Q

APU

After 3 motor Duty Cycles:

A

Wait 60 minutes before attempting 3 more cycles

42
Q

Maximum Altitude

Slats and/or Flaps Extended

A

20,000 ft

43
Q

FUEL MANAGEMENT (AFM)

Center Tank

A

Takeoff on center tank is prohibited.

44
Q

Max Total Fuel Imbalance for Takeoff

A

800 lbs

NOTE: The above limitations are the most restrictive (rounded) Airbus A320/321 fuel imbalance values. Anytime either of these values is reached or is about to be reached, the table below must be referenced for actual values applicable to the specific fuel configuration and phase of flight.

45
Q

Max Total Fuel Imbalance In-Flight & Landing

A

1500 lbs

NOTE: The above limitations are the most restrictive (rounded) Airbus A320/321 fuel imbalance values. Anytime either of these values is reached or is about to be reached, the table below must be referenced for actual values applicable to the specific fuel configuration and phase of flight.

46
Q

Maximum Brake Temperature for Takeoff

A

300°C

47
Q

Max Altitude for APU Start during

EMERG ELEC CONFIG

A

25,000 ft

48
Q

Max Altitude for APU Bleed Dual Pack Ops

A

15,000 ft

49
Q

Max Altitude for APU Bleed Single Pack Ops

A

22,500 ft

50
Q

Max Altitude for APU Bleed Engine Start Assist

A

20,000 ft

51
Q

Unreliable Speed Indication
- or -
ADR CHECK PROC

A

1 AP ………………………………………………………….. OFF
2 A/THR……………………………………………………… OFF
3 FD………………………………………………………….. OFF
4 Pitch / Thrust………………………………………………Set
If climb required or safety of flight is a concern:
Below THRUST RED ALT …………………… 15°/TOGA
Above THRUST RED ALT & Below 10,000 ft….10°/CLB
Above THRUST RED ALT & Above 10,000 ft……5°/CLB

52
Q

Emergency Descent

A

1 Crew Oxygen Masks……………………………………….On
2 Crew Communications……………………………. Establish

53
Q

Engine Failure Driftdown –

Unable to Maintain Altitude

A

1 Thrust Levers ……………………………………………. MCT
2 A/THR ……………………………………………………… OFF

54
Q

Loss of Braking

A 
If no braking:
1 Reverse…………………………MAX
2 Brake Pedals………………..Release
3 Antiskid…………………………OFF
4 Brake Pedals…………………Press
5 Max Brake Pressure……..1000 psi
If still no braking:
6 Parking Brake……………….Use

2021 Alaska Airbus (1 decks)

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