Limitations

Question 1

Wingspans A319, A320

Answer 1

111’ 10”

Question 2

Wingspans Sharklet (A320, A321)

Answer 2

117’ 5”

Question 3

Ground Clearance Tailstrike pitch L/G Struts Compressed

Answer 3

A319 13.9°
A320 11.7°
A320 NEO 11.7°
A321 9.7°

Question 4

Maximum Certified Altitude

Answer 4

FL398

Question 5

Runway Slope (mean)

Answer 5

+/-2%

Question 6

Runway Altitude

Answer 6

9200ft

Question 7

Nominal Runway Width

Answer 7

45m (148ft)

Question 8

Crosswind, t/o and ldg

Answer 8

38kt (gust included)

Question 9

Tailwind, t/o

Answer 9

15kt

Question 10

Tailwind, ldg

Answer 10

10kt

Question 11

Passenger door operation winds

Answer 11

65kt

Question 12

V_LE

Answer 12

280kt/M.67

Question 13

V_{LO extension}

Answer 13

250kt/M.60

Question 14

V_{LO retraction}

Answer 14

220kt/M.54

Question 15

Windshield Wipers (when sweeping)

Answer 15

230kt

Question 16

Taxi speed in Turn (t/o > 167550lb/76000kg)

Answer 16

20kt

Question 17

Max Landing A319

Answer 17

137,788lb

Question 18

Max Landing A320 CEO

Answer 18

145,505lb

Question 19

Max Landing A320 NEO

Answer 19

148,591lb

Question 20

Max Landing A321 Sharklet

Answer 20

171,519lb

Question 21

Max Landing A321 NEO

Answer 21

174,606lb

Question 22

APU Bleed air and Air Start Unit

Answer 22

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 23

Cabin Differential Pressure

Answer 23

-1.0 to 9.0 PSI

Question 24

Packs and LP Air Conditioning Unit

Answer 24

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 25

Autopilot engage, t/o

Answer 25

100'AGL and at least 5 s after t/o

Question 26

Autopilot disengage, approach

Answer 26

* F-G/S, FINAL APP, V/S, or FPA mode: 250'AGL * Circling: 600'AGL * ILS CAT1: 160'AGL * ILS CAT2 or 3: 0'AGL if autoland

Question 27

Autopilot engage, after manual go-around

Answer 27

100'AGL

Question 28

Autopilot min. use height, in all other phases

Answer 28

A319/A320: 500'AGL A321: 900'AGL

Question 29

The AP or FD in OP DES or DES mode can be used in approach; however, only permitted if FCU selected altitude:

Answer 29

Altitude set to, or above, the highest of: A319/A320: MDA/MDH or 500'AGL A321: MDA/MDH or 900'AGL

Question 30

Nav Mode use in the terminal area:

Answer 30

-GPS Primary is available, or -The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or -FMS navigation is crosschecked with navaid raw data

Question 31

Approaches with Engine-Out: Autopilot use

Answer 31

If one engine is inop, it is not permitted to use the autopilot to perform NPAs in FINAL APP, NAV V/S, NAV/FPA. Only FD use is permitted

Question 32

APU Start

Answer 32

After 3 consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt

Question 33

Thrust Setting/EGT Limits A319, A320 CEO

Answer 33

* T/o and GA, all engines operative: 5 min, 635°C * T/o and GA, one engine inop: 10 min, 635°C * MCT: no time limit, 610°C * Starting, on ground or in flight: 635°C ## Footnote T/o includes TOGA and FLEX thrust modes

Question 34

Thrust Setting/EGT Limits A321 Sharklet

Answer 34

* T/o and GA, all engines operative: 5 min, 650°C * T/o and GA, one engine inop: 10 min, 650°C * MCT: no time limit, 610°C * Starting, on ground or in flight: 635°C ## Footnote T/o includes TOGA and FLEX thrust modes

Question 35

Thrust Setting/EGT Limits NEO

Answer 35

* T/o and GA, all engines operative: 5 min, 1083°C * T/o and GA, one engine inop: 10 min, 1083°C * MCT: no time limit, 1043°C * Starting, on ground or in flight: 1083°C ## Footnote T/o includes TOGA and FLEX thrust modes

Question 36

Oil: CEO

Answer 36

* Min starting temp: -40°C * Min temp before exceeding IDLE: -10°C

Question 37

Oil: NEO

Answer 37

* Minimum oil pressure: 65PSI

Question 38

Starter: CEO

Answer 38

* A standard automatic start that includes only one start attempt, is considered one cycle * For ground starts (automatic or manual), a 15 s pause is required between successive cycles * A 30 min cooling period is required subsequent to 3 failed cycles or 5 min of continuous crank * For manual start, observe a 2-min max cycle time * For crank, observe a 5-min max cycle time * The starter must not be run when N2 is above 10% on-ground, and 18% in-flight

Question 39

Starter: NEO

Answer 39

* A standard automatic start that includes up to two start attempts, is considered one cycle * For ground starts (automatic or manual), a 35 s pause is required between successive cycles * A 15 min cooling period is required subsequent to 3 failed cycles or 15 min of continuous or cumulated crank * The starter must not be run when N2 is above 20%

Question 40

Reverse Thrust, max and idle

Answer 40

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

Question 41

Reduced Thrust T/O

Answer 41

FLEX t/o is not permitted on contaminated runways

Question 42

Crosswind, engine start

Answer 42

The engine is able to start in crosswind up to 35kt

Question 43

Flaps/Slats extended altitude

Answer 43

Max 20000ft

Question 44

Fuel Temperature

Answer 44

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

Question 45

Fuel Imbalance: A319, A320

Answer 45

* T/o; heavier inner tank (outer tanks balanced) at full: 1102lb max asymmetry * In flight & ldg; heavier inner tank at full: 3306lb max asymmetry

Question 46

Fuel Imbalance: A321

Answer 46

* T/o; heavier tank at full: 882lb max asymmetry

Question 47

Brake Temperature

Answer 47

Max brake temp for t/o (brake fans off): 300°C