Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
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. |