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
Min height for AP use during a CAT I ILS with CAT II or | CAT III DUAL/SINGLE displayed (ASA)
80 ft AGL
26
Min height for AP engagement after a manual Go-Around
100 ft AGL
27
Min height for AP Use in all other phases | A320
500 ft AGL
28
Min height for AP Use in all other phases | A321
900 ft AGL
29
Min Oil Quantity for Dispatch (ASA)
14 qts
30
Min Oil Temperature for Starting
-40°C
31
Min Oil Temperature for Takeoff | A320
-10°C
32
Min Oil Temperature for Takeoff | A321
19°C
33
Max Number of Consecutive Start Cycles | A320
4* * A standard auto-start cycle for the Leap1A and CFM56-B engines may consist of up to 3 start attempts.
34
Max Number of Consecutive Start Cycles | A321
3* * A standard auto-start cycle for the Leap1A and CFM56-B engines may consist of up to 3 start attempts.
35
Min Cooling Period after Max Engine Start Cycles
15 Minutes
36
Min Pause Between Engine Start Attempts (Ground Start) | A320
20 Seconds
37
Min Pause Between Engine Start Attempts (Ground Start) | A321
60 Seconds
38
Max N2 for Running Re-Engagement of Starter | A320
20%
39
Max N2 for Running Re-Engagement of Starter | A321
63%
40
Speed below which Max Reverse Thrust | SHOULD NOT be used
70 KIAS
41
APU After 3 motor Duty Cycles:
Wait 60 minutes before attempting 3 more cycles
42
Maximum Altitude Slats and/or Flaps Extended
20,000 ft
43
FUEL MANAGEMENT (AFM) Center Tank
Takeoff on center tank is prohibited.
44
Max Total Fuel Imbalance for Takeoff
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
Max Total Fuel Imbalance In-Flight & Landing
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
Maximum Brake Temperature for Takeoff
300°C
47
Max Altitude for APU Start during | EMERG ELEC CONFIG
25,000 ft
48
Max Altitude for APU Bleed Dual Pack Ops
15,000 ft
49
Max Altitude for APU Bleed Single Pack Ops
22,500 ft
50
Max Altitude for APU Bleed Engine Start Assist
20,000 ft
51
Unreliable Speed Indication - or - ADR CHECK PROC
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
Emergency Descent
1 Crew Oxygen Masks..............................................On 2 Crew Communications.................................. Establish
53
Engine Failure Driftdown – | Unable to Maintain Altitude
1 Thrust Levers .................................................... MCT 2 A/THR ............................................................... OFF
54
Loss of Braking
``` 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 ```