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63 Cards in this Set

  • Front
  • Back
A319/A320/A321 Wingspan
111 feet, 10 inches
A320S/A321S Wingspan
117 feet, 5 inches
A319 Max Landing Weight
137,788 lbs
A320 Max Landing Weight
145,505 lbs
A320S Max Landing Weight
145,505 lbs
A321 Max Landing Weight
171,519 lbs
A321S Max Landing Weight
171,519 lbs
Max Certified Altitude
FL398
Runway Slope
+/- 2%
Max Runway Altitude
9,200 ft
Nominal Runway Width
148 ft (A319/A320/A321S - 98 ft with "Operations on Narrow Runways" procedure)
Max Demonstrated Crosswind
38 knots (gust included)
Max Tailwind - Takeoff
15 knots
Max Tailwind - Landing
10 knots
Max Wind for PAX Door Operation
65 knots
Max Gear Extended Speed
280 knots/M.67
Max Gear Extension Speed
250 knots
Max Gear Retraction Speed
220 knots
Max Altitude Gear May Be Extended
25,000 ft
Max Wiper Speed
230 knots
Max Taxi Speed
>167,550 lbs: 20 knots in a turn
Air Conditioning with LP Ground Unit
Do not use conditioned air simultaneously from PACKs and LP ground unit (to avoid chattering of non-return valves).
Air Conditioning with HP Ground Unit
Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage.
Max Positive Differential Pressure
8.6 PSI
Max Negative Differential Pressure
-1.0 PSI
Min Height for AP - Takeoff with SRS Mode
100 ft AGL
Min Height for AP - Straight-in NPA
Applicable Minimum
Min Height for AP - Circling Approach
Applicable Circling Minimum - 100 ft
Min Height for AP - ILS w/o CAT 2 or 3 Displayed
160 ft AGL
Min Height for AP - Go-Around
100 ft AGL
Min Height for AP - All Other Phases
500 ft AGL (A319/A320)
900 ft AGL (A321)
Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above:
Highest of:
Minimum or 500 ft (A319/A320)
Minimum or 900 ft (A321)
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY is available, or
- HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
- NAVAID raw data is monitored
A319/A321: If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:
FINAL APP
NAV V/S
NAV/FPA
*Only FD use is permitted.
Max Altitude for Flaps and/or Slats
20,000 ft
Max Fuel Imbalance - Takeoff (A320S)
Inner tanks: Full: 1,102 lbs
Max Fuel Imbalance - In Flight and at Landing (A320S)
Inner tanks: Full: 3,306 lbs
Max Fuel Imbalance - In Flight or at Landing (A321)
Inner tanks: Full: 2,910 lbs
Max Fuel Imbalance - Takeoff (A321S)
Inner tanks: Full: 882 lbs
Min Fuel for Takeoff
3,307 lbs
Max Brake Temp for Takeoff (fans off)
300 C
APU Starter Cycles
After 3 starter motor duty cycles, wait 60 minutes before attempting 3 more cycles.
Max Altitude for APU Bleed with 2 PACKs
15,000 ft
Max Altitude for APU Bleed with 1 PACK
20,000 ft
Max Altitude for APU Start on Battery Power
25,000 ft
Max Altitude for APU Start (on A/C power) and Operation
FL 410
EGT Limit for Starting
635 C
EGT Limit for TOGA (A319/A320)
635 C (5 min/10 min for single engine)
EGT Limit for TOGA (A321)
650 C (5 min/10 min for single engine)
EGT Limit for MCT
610 C
Min Engine Oil Temp for Starting
-40 C
Min Engine Oil Temp Prior to Exceeding Idle
-10 C
Min Engine Oil Quantity
11 qts + ~.3qt/hr
Engine Starter
3 consecutive cycles:
- 2 cycles of 2 minutes each,
- 3rd cycle of 1 minute
Pause 15 seconds between attempts

Cooling period: 30 minutes after 3 start attempts or 4 minutes of continuous cranking

No running engagement of the starter, when N2 is above 10% on ground or 18% in flight.
Min Speed for Max Reverse Thrust
70 knots
Max reverse should not be used when (A319/A320):
Airspeed indication starts to fluctuate.
Reduced thrust takeoff is not permitted:
On contaminated runways.
Max Crosswind for Engine Start
35 knots
EGPWS Alert
Simultaneously:
1. AP - OFF
2. Pitch - Full backstick and maintain
3. Thrust levers - TOGA
4. Speed brakes - Check retracted
5. Bank - Wings level or adjust

- Best climb performance is obtained when close to wings level
- For terrain and obstacle alerts, if the crew concludes that turning is the safest way of action, a turning maneuver can be initiated.

Emergency Descent

1. Crew O2 masks - On


2. Emergency descent - Announce


- "Attention, take the first available seat and prepare to put on your oxygen mask."


3. Signs - On


4. Emergency descent - Initiate


- Descend with the autopilot engaged:


- Turn the ALT selector knob and pull


- Turn the HDG selector knob and pull


- Adjust the target SPD/MACH


*Expedite mode is also permitted


5. Thrust levers (if A/THR not engaged) - Idle


- If A/THR is engaged, check that THR IDLE is on FMA


- If A/THR is not engaged, thrust levers idle


6. SPD BRK - Full


- Extension of the speedbrakes will significantly increase VLS.


- To avoid autopilot disconnection and automatic retraction of the speedbrakes, due to possible activation of the angle of attack protection, allow the speed to increase before starting to use speedbrakes.

Loss of Braking

If No Braking Available:


1. Reverse - Max


2. Brake pedals - Release


- Brake pedals should be released when the A/SKID & NW STRG sw is switched OFF, since the pedal force or displacement produces more braking action in alternate mode than in normal mode.


3. A/SKID & NW STRG - Off


- Braking system reverts to alternate mode.


4. Brake pedals - Press


- Apply brakes with care, since initial pedal force or displacement produces more braking action in alternate mode than in normal mode.


5. Max brake pressure - 1,000 PSI


- Monitor brake pressure or BRAKES PRESS indicator. Limit brake pressure to approximately 1,000 PSI and at low ground speed, adjust brake pressure as required.


If still no Braking:


6. Parking brake - Short and successive applications


- Use short successive parking brake applications to stop the aircraft. Brake onset asymmetry may be felt at each parking brake application. If possible, delay the use of parking brake until low speed, to reduce the risk of tire burst and lateral control difficulties.

TCAS RA

1. AP - Off


2. Both FDs - Off


3. Vertical speed - Adjust


- Respond promptly and smoothly to an RA by adjusting or maintaining the pitch, as required, to reach the green area and/or avoid the red area of the vertical speed scale.


- Avoid excessive maneuvers while aiming to keep the vertical speed just outside the red area or the VSI, and within the green area. If necessary, use the full speed range between Va max and Vmax.


4. ATC - Notify



*Respect stall, GPWS or windshear warning.

Unreliable Speed Indication

If the safe conduct of flight is impacted:


1. AP/FD - Off


2. A/THR - Off


3. Pitch/Thrust:


- Below THRUST RED ALT - 15/TOGA


- Above THRUST RED ALT and below FL100 - 10/CLB


- Above THRUST RED ALT and Above FL100 - 5/CLB


4. Flaps (Config 0,1,2,3) - Maintain


5. Flaps (Config full) - Select config 3 and maintain


6. Speedbrakes - Check retracted


7. L/G - Up



*When at or above MSA or circuit altitude, level off for troubleshooting.