VX Limitations &Recall (Memory) Items Flashcards

1
Q

Max Operating Altitude

A

39,000 ft

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2
Q

Engine Start Max Crosswind (gusts included)

A

A321 only

45 kts

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3
Q

Takeoff Crosswind (gusts included)

A

A320

38 kts

A321

35 kts

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4
Q

Landing Crosswind (gusts included)

A

A320/321

38 kts

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5
Q

Takeoff and Landing Tailwind

A

10 kts

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6
Q

Max Airfield Wind for Takeoff or Landing (ASA)

A

50 kts or gust factor of 20 kts

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7
Q

Passenger Door Operation

A

65 kts

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8
Q

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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9
Q

Cargo Doors must be closed before wind speed exceeds:

A

65 kts

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10
Q

Severe Turbulence Penetration (ASA)

A

A320

Below FL 200: 250 kts

FL 200 and above: 275 kts / 0.76 Mach

A321

Below FL 200: 275 kts

FL 200 and above: 305 kts / 0.76 Mach

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11
Q

Maximum speed with landing gear extended (VLE)

A

280 kts / M 0.67

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12
Q

Maximum speed at which the landing gear may be extended

(VLO - extension)

A

250 kts

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13
Q

Maximum speed at which the landing gear may be retracted

(VLO - Retraction)

A

220 kts

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14
Q

Maximum Tire Ground Speed (AFM)

A

195 kts

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15
Q

Max speed with Flight Deck window open

A

200 kts

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16
Q

Max speed when windshield wiper is in use

A

230 kts

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17
Q

Do not use LP Ground Conditioned Air while:

A

Packs Operating (avoids valve chatter)

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18
Q

Min AP Engagement on Takeoff

A

100 ft AGL or at least 5 seconds after liftoff

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19
Q

Min Height for AP Use in approach with FINAL APP mode

A

250 ft AGL

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20
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

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21
Q

Min Height for AP Use on a Circling Maneuver* (ASA)

A

1,000 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

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

A

160 ft AGL

23
Q

Min Height for AP Use during a CAT I ILS with CAT II or CAT III DUAL/SINGLE Displayed (ASA)

24
Q

Min Height for AP Engagement after a manual Go Around

A

100 ft AGL

25
Min Height for AP Use in All Other Phases
**A320** 500 ft AGL **A321** 900 ft AGL
26
Min Oil Temperature for Starting
**A320/321** - 40°C
27
Min Oil Temperature for Takeoff
**A320** - 10°C **A321** 19°C
28
Max Number of Consecutive Start Cycles
**A320** 4\* **A321** 3\* \* A standard auto-start cycle for the Leap 1A and CFM56-5B engine may consist of up to 3 start attempts
29
Min Cooling Period After Max Cycles
15 min
30
Min Pause Between Start Attempts (Ground Start)
**A320** 20 sec **A321** 60 sec
31
Max N2 for Running Re-Engagement of Starter
**A320** 20% **A321** 63%
32
Speed below which Max Reverse Thrust SHOULD NOT be Used
70 KIAS
33
APU Bleed Limit Max Altitude for Dual Pack Ops
15,000 ft
34
APU Bleed Limit Max Altitude for Single Pack Ops
22,500 ft
35
APU Bleed Limit Max Altitude for ENG Start Assist
20,000 ft
36
APU Bleed Limit Max Altitude for APU Start during EMER ELEC CONFIG
25,000 ft
37
After 3 (APU starter) motor Duty Cycles
Wait 60 min before attempting 3 more cycles
38
Max Altitude Slats and/or Flaps Extended
20,000 ft
39
Fuel Management Limitation (Takeoff)
Takeoff on center tank is prohibited
40
Max Total Fuel Imbalance for Takeoff
800 lbs\* \* The above limitations are the most restrictive (rounded) Airbus A320/A321 fuel imbalance values. Anytime either of these values is reached or is about to be reached, the table in the FUEL IMBALANCE (AFM/ASA) section of the LIMITATIONS in the FH must be referenced for actual values applicable to the specific fuel configuration and phase of flight.
41
Max Total Fuel Imbalance In-flight & Landing
1,500 lbs\* \* The above limitations are the most restrictive (rounded) Airbus A320/A321 fuel imbalance values. Anytime either of these values is reached or is about to be reached, the table in the FUEL IMBALANCE (AFM/ASA) section of the LIMITATIONS in the FH must be referenced for actual values applicable to the specific fuel configuration and phase of flight.
42
Maximum Brake Temperature for Takeoff
300°C
43
Emergency Descent
CREW OXY MASKS...............................................................ON CREW COMMUNICATIONS...........................ESTABLISH "QRC Emergency Descent"
44
Loss of Braking
1 **If** Autobrake is selected: Brake Pedals..............................................PRESS 2 **If** no braking available: Reverse........................................................FULL Brake Pedals...............................................Release A/SKID & N/W STRG ................................OFF Brake Pedals ..............................................Press Max Brake Pressure Available ...............1000 psi 3**If** still no braking: Parking Brake............Short Successive Applications Refer to QRC
45
Engine Failure Driftdown - Unable to Maintain Altitude
1 THR LEVERS........................................................MCT 2 A/THR.....................................................................OFF "QRC Engine Failure Driftdown - Unable to Maintain Altitude"
46
Unreliable Speed Indication or ADR CHECK PROC
## Footnote **1 AP....................................................................................................OFF** **2 A/THR............................................................................................OFF** **3 FDs..................................................................................................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 **"QRC Unreliable Speed Indication"**
47
EGPWS Alert ## Footnote For any EGPWS warning/caution for terrain/obstacles during night or IMC conditions. Either pilot calls "**GPWS**."
**Pilot Flying:** Simultaneously: AP............................................................................Off Pitch..................................................................Pull Up Pull to full backstick and maintain in that position. Thrust Levers...................................................TOGA Speed Brakes..................................Check Retracted Bank..........................................Wings level or adjust Do Not Change Configuration (Slats/Flaps, Gear) Until Clear of Obstacle.
48
STALL RECOVERY ## Footnote **As soon as stall is recognized, either pilot calls out, "Stall."**
Nose Down Pitch Control..............................................Apply Bank.........................................................................Wings Level **When Out of Stall (no longer stall indications):** Thrust....................................Increase Smoothly as Needed SPEEDBRAKES.............................................Check Retracted **When the aircraft has recovered sufficient energy:** Flight Path.................................................Recover Smoothly If in clean configuration and below 20,000 ft, call, **"Flaps 1"**
49
STALL WARNING AT LIFT-OFF PF/PM call out, "**Stall at Liftoff."**
Simultaneously: Thrust.................................................TOGA Pitch........................................................15° Bank..................................WINGS LEVEL
50
TCAS WARNING At TCAS alert, either pilot calls, **"TCAS"**
AP.................................................................................... Off FDs...................................................................................Off V/S .....................Adjust Pitch, maintain green, avoid red ATC.............................................................................Notify
51
WINDSHEAR At alert or pilot direction, either pilot calls out, **"Windshear."**
**Before V1:** ## Footnote \*TAKEOFF....................................................................REJECT Reject the takeoff if there are significant variations in airspeed and in airspeed trend below the indicated V1, and there is sufficient runway remaining to stop the aircraft. If windshear occurs during the takeoff roll, the aircraft may reach V1 later (or sooner) than expected **After V1:** THR Levers..........................................................................TOGA Reaching VR........................................................................Rotate SRS Orders.........................................................................Follow **Airborne, Initial Climb or Landing:** THR Levers.............................................TOGA (set or confirm) AP (If engaged).............................................................Keep On SRS Orders........................................................................Follow Do not change configuration (slats/flaps, gear) until out of windshear. Closely monitor flight path and speed. Recover smoothly to normal climb out of windshear.
52
WINDSHEAR AHEAD At alert, either pilot calls out "**Windshear Ahead**."
**During the Takeoff Run:** \*Takeoff............................................................Reject **When Airborne:** \*THR Levers....................................................TOGA AP (If engaged)..........................................Keep On SRS Orders.....................................................Follow **Landing:** Go-Around...................................................Perform AP (If engaged)...........................................Keep On