Limitations

Question 1

NAV mode may be used in the terminal area, provided:

Answer 1

• GPS PRIMARY
  or
• The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed
  or
• FMS navigation is cross-checked with NAVAID raw data

Question 2

Runway Slope (mean)

Answer 2

+/-2%

Question 3

Max crosswind for start

Answer 3

35kts

Question 4

Max operating altitude with slats and/or flaps extended is

Answer 4

20,000ft

Question 5

Minimum Height For Use Of Autopilot

Take off with SRS

Answer 5

100 ft AGL.
Note: Takeoff with SRS mode - An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.

Question 6

Minimum Height For Use Of Autopilot

ILS approach when CAT 2 or CAT 3 is not displayed on the FMA

Answer 6

160 ft AGL

Question 7

Minimum Height For Use Of Autopilot

Straight-in non-precision approach

Answer 7

Applicable Minimum

Question 8

Maximum wind for passenger door operation

Answer 8

65kts

Question 9

Takeoff and GA (TOGA and FLEX)

Thrust Setting/EGT Limits

Answer 9

Takeoff and GA (TOGA and FLEX)
319 and 320 / 321 / NEO

635 °C / 650 °C / 1,083°C

5 min (10 min engine failure.)

Question 10

Maximum brake temperature for takeoff (brake fans (if installed) off)

Answer 10

300 C

Question 11

RunwayAltitude

Answer 11

9,200ft

Question 12

NominalRunwayWidth

Answer 12

45m(148ft)

Question 13

VLE

Answer 13

280kts (M .67)

Question 14

Oil Temperature (CEO)

Answer 14

Starting
-40 °C

Above Idle
-10°C

Question 15

APU Starter

Answer 15

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

Question 16

Minimum Height For Use Of Autopilot

UseoftheAPorFDinOPENDESor DES mode is not permitted in approach, unless the FCU altitude is set at or above:

Answer 16

Highest of:

Minimums or 500 ft (A319/A320) Minimum or 900 ft (A321)

Question 17

Fuel Temp

Answer 17

For JET A only, if TAT reaches -34C , monitor on FUEL SD page that fuel temperature remains higher than -36C

Question 18

Reverser Limits

Answer 18

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.

Question 19

VLO (extension)

Answer 19

250kts (M .60)

Question 20

Cabin Pressure
• Maxpositivedifferentialpressure
• Maxnegativedifferentialpressure

Answer 20

9. 0psi

- 1.0psi

Question 21

Max Landing (320)

Answer 21

145,505lb

Question 22

Max Landing (657-687)

Answer 22

171,519lb

Question 23

MCT

Thrust Setting/EGT Limits

Answer 23

MCT
CEO / NEO

610 °C / 1,043°C

Question 24

Max Taxi speed (A320CEO)

Answer 24

When the taxi weight is higher than 67,550lbs (76,000kg): Caution: Do not exceed a taxi speed of 20 kt during a turn.

Question 25

Non-Precision Approaches with Engine-Out (319 and 657-668, 670, 671)

Answer 25

``` 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. ```

Question 26

Minimum Height For Use Of Autopilot Circling Approach

Answer 26

100 feet below Applicable Circling Minimums

Question 27

Max Landing (502-536)

Answer 27

137,788 lb

Question 28

Minimum Oil Pressure (901-905)

Answer 28

65 PSI

Question 29

Max Alt for landing gear extended

Answer 29

25,000ft

Question 30

VLO (retraction)

Answer 30

220kts (M .54)

Question 31

Fuel Imbalance, Inner tanks when one is full

Answer 31

TO / Flight&Landing 319 and 320s: (At TO / Flight and Landing) 1,102 / 3306 321: 882 / 2910

Question 32

Minimum Height For Use Of Autopilot All other phases

Answer 32

500 ft AGL (A319/A320) 900 ft AGL (A321)

Question 33

Maximum Certified Altitude

Answer 33

FL398

Question 34

Max speed for Windshield Wipers

Answer 34

230kts

Question 35

STARTING (On Ground and Inflight) | Thrust Setting/EGT Limits

Answer 35

STARTING CEO / NEO 635 °C / 1,083°C

Question 36

Wingspans

Answer 36

Non-Sharklet 111feet,10inches Sharklet 117feet,5inches

Question 37

Maximum demonstrated crosswind

Answer 37

38kts (gust included)

Question 38

Reduced Thrust Takeoff Limits

Answer 38

FLEX takeoff is not permitted on contaminated runways

Question 39

Max crosswind with CAT II and III

Answer 39

Crosswind: 15 kts

Question 40

Max tire speed

Answer 40

195 kts

Question 41

APU With HP Ground Unit

Answer 41

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

Question 42

Starter Limitations

Answer 42

ALL CEO / NEO: One Cycle = 1 / 2 consecutive start attempts (CEO)Man start, 2 mins max start / 5 mins crack For Ground Starts (auto or man), between cycle pause: 15 s / 35 s After 3 cycles or 5 / 15 min continuous cranking (or cumulated NEO) Cooling Period = 30 min / 15 min Do not start, when N2 is above 10% GND, 18 % FLT / 20%

Question 43

Tailstrike Pitch Attitudes

Answer 43

L/G Struts Compressed 319 - 13.9 degrees 320 - 11.7 degrees 321 - 9.7 degrees

Question 44

Max tailwind for: Takeoff Landing

Answer 44

Takeoff - 15kts | Landing - 10kts

Question 45

APU Bleed use with Air Start Unit

Answer 45

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

Question 46

Packs use with the LP Air Conditioning Unit

Answer 46

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

Question 47

What is the reduced usable fuel capacity of the Center Tank on 697 and 698 (Invicta-FRS system)

Answer 47

reduced usable capacity of up to 42.9 gallons

Question 48

ELAC Functions

Answer 48

Normal Elevators Normal Ailerons Normal Pitch and Roll Alternate Pitch Direct Pitch and Roll Abnormal Attitude Aileron Droop Autopilot orders

Question 49

SEC Functions

Answer 49

Normal Roll Alternate Pitch Direct Pitch and Roll Abnormal Attitude Speed Brakes

Question 50

FAC Functions

Answer 50

Rudder Limitations Turn Coordination Rudder Dampening Rudder Trim Aircraft envelope Windshear Low Energy Warning