Bold Italic Limitations Plus A Couple Others

Question 1

Wingspan A319, A320

Answer 1

111 feet 10 inches

Question 2

Wingspan A320 Sharklet, A321 Sharklet

Answer 2

117 feet 5 inches

Question 3

Tailstrike with L/G struts compressed.

• A319
• A320
• A320 NEO
• A321

Answer 3

• 13.9
• 11.7
• 11.7
• 9.7

Question 4

Maximum Certified Altitude

Answer 4

FL 398

Question 5

Runway slope (mean)

Answer 5

+/-2%

Question 6

Runway altitude

Answer 6

9200ft

Question 7

Nominal runway width

Answer 7

45m (148feet)

Question 8

Max demonstrated crosswind (takeoff and landing)

Answer 8

38 kt gust included

Question 9

Max tailwind for takeoff

Answer 9

15 kt

Question 10

Max tailwind landing

Answer 10

10kt

Question 11

Max wind passenger door operation

Answer 11

65kt

Question 12

Max cockpit window open speed

Not bolded

Answer 12

200kts

Question 13

• Max with landing gear extended (VLE)
• Max landing gear extension (VLO extension)
• Max landing gear retraction (VLO Retraction)
• Max altitude landing gear may be extended

Answer 13

• 280/.67
• 250/.60
• 220/.54
• 25,000ft

Question 14

Max tire speed (not bolded)

Answer 14

195kt

Question 15

When taxi weight is higher than…..

Answer 15

167,550 in a 320 or 321 don’t exceed a taxi speed of 20kt during a turn

Question 16

Max wiper speed

Answer 16

230kt

Question 17

• Max landing 319
• max landing 320
• max landing 320 sharklet
• max landing NEO
• max landing 321

Answer 17

• 137,788
• 145,505
• 145,505
• 148,591
• 171,519

Question 18

APU bleed use with air start unit

Answer 18

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 19

• max positive differential pressure
• max negative differential pressure
• safety relief valve setting

Answer 19

• 9.0 psi
• -1.0 psi
• 8.6psi

Question 20

Packs use with LP air conditioning unit

Answer 20

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 21

• takeoff with SRS mode
• straight in NPA
• circling approach
• ILS approach when cat 2 or 3 not displayed on the FMA
• Go around
• all other phases

Answer 21

• 100 AGL
• applicable minimum
• applicable circling mins minus 100 feet
• 160 AGL
• 100 AGL
• 500ft (a319/a320) 900ft (a321)

Question 22

Use of the AP or FD in OPEN DES or DES mode…..

Answer 22

Is not permitted in approach, unless the FCU altitude is set at or above highest of:

Minimum or 500ft (319/320)
Minimum or 900ft (321)

Question 23

Takeoff with SRS mode

Answer 23

An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff

Question 24

Use of NAV mode in the terminal area

Answer 24

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

• 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 25

If one engine is inoperative in a 319/321 it is NOT permitted....

Answer 25

To use the autopilot to perform NPA's in the following modes: - FINAL APP - NAV V/S - NAV/FPA * Only FD use is permitted

Question 26

APU Start

Answer 26

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

Question 27

Thrust EGT limits for 319/320

Answer 27

TOGA- 635- 5 min or 10 min MCT- 610 Starting- 635

Question 28

Thrust EGT limits 321

Answer 28

TOGA- 650- 5 min or 10min MCT- 610 Starting- 635

Question 29

Thrust EGT limits NEO

Answer 29

TOGA- 1083- 5 min or 10min MCT- 1043 Starting- 1083

Question 30

Oil temps CEO - min starting - min before idle exceeded - min before takeoff - min oil pressure

Answer 30

- -40C - -10C - 50C - 60 Psi

Question 31

Oil NEO - Min starting temp - min temp before takeoff - Minimum pressure

Answer 31

- -40C - 52C - 65psi

Question 32

Start limitation CEO

Answer 32

- A standard automatic start that includes only one start attempt is considered one cycle - for ground starts (auto or manual) a 15 second 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 a 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 33

Start limitation NEO

Answer 33

- a standard automatic start that includes up to 3 start attempts is considered one cycle - for ground starts (auto or manual) a 35s 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 34

Reverse thrust

Answer 34

Max reverse should not be used below 70 it's | Idle reverse is permitted down to aircraft stop

Question 35

FLEX is not permitted

Answer 35

On contaminated runways

Question 36

Max crosswind engine start

Answer 36

35kt

Question 37

Max altitude slats/flaps extended

Answer 37

20,000ft

Question 38

Fuel temp

Answer 38

If TAT reaches -34C monitor fuel on SD page that fuel temp remains higher than -36C

Question 39

Max fuel imbalance 320 sharklet/NEO on inner tanks (outer tanks balanced) at takeoff

Answer 39

Heavier tank full, 1102 lbs

Question 40

Max fuel imbalance 320 sharklet/NEO on inner tanks (outer tanks balanced) in flight and landing

Answer 40

Heavier tank full, 3306

Question 41

Max fuel imbalance 321 on inner tanks (outer tanks balanced) at takeoff

Answer 41

882

Question 42

Min fuel quantity for takeoff | Not bolded

Answer 42

3307

Question 43

Normal operating pressure of hydraulic (not bolded)

Answer 43

3000 psi. +/-200

Question 44

Brake temperature max for takeoff

Answer 44

300C brake fans off