VX Limitations &Recall (Memory) Items Flashcards Preview

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Flashcards in VX Limitations &Recall (Memory) Items Deck (52)
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1
Q

Max Operating Altitude

A

39,000 ft

2
Q

Engine Start Max Crosswind (gusts included)

A

A321 only

45 kts

3
Q

Takeoff Crosswind (gusts included)

A

A320

38 kts

A321

35 kts

4
Q

Landing Crosswind (gusts included)

A

A320/321

38 kts

5
Q

Takeoff and Landing Tailwind

A

10 kts

6
Q

Max Airfield Wind for Takeoff or Landing (ASA)

A

50 kts or gust factor of 20 kts

7
Q

Passenger Door Operation

A

65 kts

8
Q

Cargo Door Operation

A

40 kts

(50 kts if aircraft is positioned into the wind or door is on the leeward side)

9
Q

Cargo Doors must be closed before wind speed exceeds:

A

65 kts

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

11
Q

Maximum speed with landing gear extended (VLE)

A

280 kts / M 0.67

12
Q

Maximum speed at which the landing gear may be extended

(VLO - extension)

A

250 kts

13
Q

Maximum speed at which the landing gear may be retracted

(VLO - Retraction)

A

220 kts

14
Q

Maximum Tire Ground Speed (AFM)

A

195 kts

15
Q

Max speed with Flight Deck window open

A

200 kts

16
Q

Max speed when windshield wiper is in use

A

230 kts

17
Q

Do not use LP Ground Conditioned Air while:

A

Packs Operating (avoids valve chatter)

18
Q

Min AP Engagement on Takeoff

A

100 ft AGL or at least 5 seconds after liftoff

19
Q

Min Height for AP Use in approach with FINAL APP mode

A

250 ft AGL

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

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)

A

80 ft AGL

24
Q

Min Height for AP Engagement after a manual Go Around

A

100 ft AGL

25
Q

Min Height for AP Use in All Other Phases

A

A320

500 ft AGL

A321

900 ft AGL

26
Q

Min Oil Temperature for Starting

A

A320/321

  • 40°C
27
Q

Min Oil Temperature for Takeoff

A

A320

  • 10°C

A321

19°C

28
Q

Max Number of Consecutive Start Cycles

A

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
Q

Min Cooling Period After Max Cycles

A

15 min

30
Q

Min Pause Between Start Attempts (Ground Start)

A

A320

20 sec

A321

60 sec

31
Q

Max N2 for Running Re-Engagement of Starter

A

A320

20%

A321

63%

32
Q

Speed below which Max Reverse Thrust

SHOULD NOT be Used

A

70 KIAS

33
Q

APU Bleed Limit

Max Altitude for Dual Pack Ops

A

15,000 ft

34
Q

APU Bleed Limit

Max Altitude for Single Pack Ops

A

22,500 ft

35
Q

APU Bleed Limit

Max Altitude for ENG Start Assist

A

20,000 ft

36
Q

APU Bleed Limit

Max Altitude for APU Start during EMER ELEC CONFIG

A

25,000 ft

37
Q

After 3 (APU starter) motor Duty Cycles

A

Wait 60 min before attempting 3 more cycles

38
Q

Max Altitude Slats and/or Flaps Extended

A

20,000 ft

39
Q

Fuel Management Limitation (Takeoff)

A

Takeoff on center tank is prohibited

40
Q

Max Total Fuel Imbalance for Takeoff

A

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
Q

Max Total Fuel Imbalance In-flight & Landing

A

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
Q

Maximum Brake Temperature for Takeoff

A

300°C

43
Q

Emergency Descent

A

CREW OXY MASKS………………………………………………………ON

CREW COMMUNICATIONS………………………ESTABLISH

“QRC Emergency Descent”

44
Q

Loss of Braking

A

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

3If still no braking:

Parking Brake…………Short Successive Applications

Refer to QRC

45
Q

Engine Failure Driftdown -

Unable to Maintain Altitude

A

1 THR LEVERS………………………………………………..MCT

2 A/THR……………………………………………………………OFF

“QRC Engine Failure Driftdown - Unable to Maintain Altitude”

46
Q

Unreliable Speed Indication

or

ADR CHECK PROC

A

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
Q

EGPWS Alert

For any EGPWS warning/caution for terrain/obstacles during night or IMC conditions. Either pilot calls “GPWS.”

A

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
Q

STALL RECOVERY

As soon as stall is recognized, either pilot calls out, “Stall.”

A

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
Q

STALL WARNING AT LIFT-OFF

PF/PM call out, “Stall at Liftoff.”

A

Simultaneously:

Thrust………………………………………….TOGA

Pitch………………………………………………..15°

Bank…………………………….WINGS LEVEL

50
Q

TCAS WARNING

At TCAS alert, either pilot calls, “TCAS”

A

AP………………………………………………………………………… Off

FDs………………………………………………………………………..Off

V/S …………………Adjust Pitch, maintain green, avoid red

ATC…………………………………………………………………..Notify

51
Q

WINDSHEAR

At alert or pilot direction, either pilot calls out, “Windshear.”

A

Before V1:

*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
Q

WINDSHEAR AHEAD

At alert, either pilot calls out “Windshear Ahead.”

A

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