Limitations Flashcards

1
Q

WIND LIMITS - Engine Start Max Crosswind

A

A320 - N/A

A321 - 45 kts

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2
Q

WIND LIMITS - Takeoff Crosswind (gusts included)

A

A320 - 38 kts

A321 - 35 kts

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3
Q

WIND LIMITS - Landing Crosswind (gusts included)

A

38 kts

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4
Q

WIND LIMITS - Takeoff & Landing Tailwind

A

10 kts

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5
Q

WIND LIMITS - Max Airfield Wind for Takeoff or Landing (ASA)

A

50 kts or gust factor of 20 kts

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6
Q

WIND LIMITS - Passenger Door Operation

A

65 kts

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7
Q

WIND LIMITS - Cargo Door Operation

A

40 kts
50 kts - If aircraft is positioned into the wind or door is on the leeward side
Must be closed before wind speed exceeds 65 kts

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8
Q

OPERATIONAL LIMITATIONS - Max operating altitude

A

39,000’

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9
Q

SEVERE TURBULENCE PENETRATION (ASA) A320

A

Below FL 200 - 250 kts

FL 200 and above - 275 kts/0.76 Mach

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10
Q

SEVERE TURBULENCE PENETRATION (ASA) A321

A

Below FL 200 - 275 kts

FL 200 and above - 305 kts/0.76 Mach

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11
Q

LANDING GEAR / TIRE SPEEDS (AFM)

Maximum speed with landing gear extended
VLE

A

280 kts / M 0.67

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12
Q

LANDING GEAR / TIRE SPEEDS (AFM)
Maximum speed at which the landing gear may be extended
(VLO extension)

A

250 kts

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13
Q

LANDING GEAR / TIRE SPEEDS (AFM)
Maximum speed at which the landing gear may be retracted
(VLO retraction)

A

220 kts

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14
Q

LANDING GEAR / TIRE SPEEDS (AFM)

Maximum tire ground speed

A

195 kts

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15
Q
GENERAL SPEEDS (FCOM) 
Max speed with Flight Deck window open
A

200 kts

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16
Q
GENERAL SPEEDS (FCOM)
Max speed when windshield wiper is in use
A

230 kts

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17
Q

AIR CONDITIONING WITH LP GROUND UNIT (FCOM)

Do not use LP Ground Conditioned Air while:

A

Packs Operating (avoids valve chatter)

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18
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

Min AP engagement on Takeoff

A

100 ft AGL or at least 5 seconds after liftoff

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19
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

Min height for AP use in approach with FINAL APP mode

A

250 ft AGL

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20
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

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

A

Applicable MDA/DH or 250 ft AGL whichever is higher

21
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

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.
22
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

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

A

160 ft AGL

23
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)
Min height for AP use during a CAT I ILS with CAT II or
CAT III DUAL/SINGLE displayed (ASA)

A

80 ft AGL

24
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

Min height for AP engagement after a manual Go-Around

A

100 ft AGL

25
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

Min height for AP Use in all other phases - A320

A

500 ft AGL

DES and OP DES mode is not permitted if FCU altitude set below MDA/MDH or (A320) 500
ft AGL, whichever is higher. (AFM/ASA)

26
Q

AUTOPILOT / AUTOTHRUST LIMITATIONS (AFM/ASA)

Min height for AP Use in all other phases - A321

A

900 ft AGL

DES and OP DES mode is not permitted if FCU altitude set below MDA/MDH or (A321) 900 ft AGL, whichever is higher. (AFM/ASA)

27
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Oil for Dispatch (ASA)

A

14 qts

28
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) Min Oil Temperature for Starting

A

-40°C

29
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Oil Temperature for Takeoff - A320

A

-10°C

30
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Oil Temperature for Takeoff - A321

A

19°C

31
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - 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.

32
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - 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.

33
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Cooling Period after Max Cycles

A

15 minutes

34
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Pause Between Start Attempts (Ground Start) - A320 (CFM 56-5B)

A

20 seconds

35
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Min Pause Between Start Attempts (Ground Start) - A321(LEAP 1A)

A

60 seconds

36
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Max N2 for Running Re-Engagement of Starter - A320

A

20%

37
Q

ENGINE LIMITATIONS (AFM/FCOM/ASA) - Max N2 for Running Re-Engagement of Starter - A321

A

63%

38
Q
ENGINE LIMITATIONS (AFM/FCOM/ASA) - Speed below which Max Reverse Thrust 
SHOULD NOT be used:
A

70 KIAS

39
Q

APU BLEED LIMITS (FCOM) - MAX Altitude for Dual Pack Ops:

A

15,000 ft

40
Q

APU BLEED LIMITS (FCOM) - MAX Altitude for Single Pack Ops:

A

22,500 ft

41
Q

APU BLEED LIMITS (FCOM) - MAX Altitude for ENG Start Assist:

A

20,000 ft

42
Q

APU BLEED LIMITS (FCOM) - MAX Altitude for APU Start during

EMERG ELEC CONFIG:

A

25,000 ft

43
Q

APU (AFM/FCOM) - After 3 motor Duty Cycles, Wait _________________________

A

60 minutes before attempting 3 more cycles

44
Q

FLIGHT CONTROLS - MAXIMUM ALTITUDES (AFM) - Slats and/or Flaps Extended…..

A

20,000 ft

45
Q

FUEL MANAGEMENT (AFM)

Takeoff on center tank is _______________________

A

prohibited.

46
Q

FUEL IMBALANCE (AFM/ASA)

Max Total Fuel Imbalance for Takeoff

A

800 lbs

47
Q
FUEL IMBALANCE (AFM/ASA) 
Max Total Fuel Imbalance In-Flight & Landing
A

1500 lbs

48
Q

LANDING GEAR, BRAKES

Maximum Brake Temperature for Takeoff

A

300°C