1

Question 0

Maximum tailwind for takeoff

Answer 0

15kt

Question 1

Maximum crosswind demonstrated for takeoff and landing

Answer 1

38kts. (demonstrated)

Question 2

Max tailwind for landing

Answer 2

10kt

Question 3

Maximum demonstrated cross wind for takeoff and landing
Dry runway
Wet runway
Contaminated runway

Answer 3

38kt (gust included)
33kt
10kt

Question 4

Maximum wind for passenger door operation

Answer 4

65kt

Question 5

Maximum wind for cargo door operation

Answer 5

40 kt/*50 kt * If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward side of the aircraft, operation of the cargo door is permitted in winds up to 50 knots. If wind speed begins to exceed these limitations, the cargo door must be closed before the wind speed exceeds 65 kts.

Question 6

Maximum VMO/MMO

Answer 6

350 kt/.82 mach

Question 7

SEVERE TURBULENT AIR PENETRATION SPEED

FL200 and below
Above FL200 through FL310
Above FL310

Answer 7

250kt
275kt
0.76 Mach

Question 8

Maximum altitude at which the landing gear may be extended

Answer 8

25,000 ft

Question 9

MAXIMUM FLAPS/SLATS SPEEDS
Lever position 1 (holding)
Slats 18
Flaps 0

Answer 9

230kts

Question 10

MAXIMUM FLAPS/SLATS SPEEDS
Position 1+F (Takeoff)
Slats 18 flaps 10

Answer 10

215kts

Question 11

MAXIMUM FLAPS/SLATS SPEEDS
Position 2
Slats 22 flaps 15

Answer 11

200 kts

Question 12

MAXIMUM FLAPS/SLATS SPEEDS
Position 3
Slats 22 flaps 20

Answer 12

185kts

Question 13

MAXIMUM FLAPS/SLATS SPEEDS
Position Full
Slats 27 flaps 40

Answer 13

177kts.

Question 14

Maximum Tire Speed (ground speed)

Answer 14

195kts

Question 15

Maximum speed for use of windshield wipers

Answer 15

230kts

Question 16

Maximum speed for opening cockpit window

Answer 16

200kts

Question 17

A320

When the taxi weight is higher than 167,550 lbs do not exceed a taxi speed of ___________ during a turn

Answer 17

20kts

Question 18

Max operating altitude with slats and/or flaps extended is

Answer 18

20,000 ft

Question 19

The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within the next ___________. of APU operation

Answer 19

10 hours

Question 20

APU
After three starter motor duty cycles, each separated by a __ ________ cool down, wait ____ __________ before attempting three more cycles.

Answer 20

One minute. 60 minutes

Question 21

Maximum altitude for APU electrical and start

Answer 21

39,000

Question 22

Maximum altitude for APU battery start

Answer 22

25,000

Question 23

Maximum altitude for APU pneumatics (1 pack w/electrical)

Answer 23

22,500 ft

Question 24

Maximum altitude for APU assisted engine start

Answer 24

20,000 ft

Question 25

Maximum altitude for APU pneumatics (2 packs w/electrical)

Answer 25

15,000 ft

Question 26

When visibility is less than or _______ or ____ the approach must be flown with the autopilot(s) engaged if operable.

Answer 26

4000 RVR. 3/4

Question 27

Autolands are prohibited if braking action is reported less than

Answer 27

Fair

Question 28

AUTOLAND WIND RESTRICTIONS
Headwind
Crosswind
Tailwind

Answer 28

30kts
15kts
10kts

Question 29

The minimum fuel quantity for takeoff is __________ The WING TK LO LVL warning must not be displayed on ECAM.

Answer 29

3300 lbs

Question 30

Maximum brake temperature for takeoff

Answer 30

300 degrees C

Question 31

MAXIMUM ALLOWED WING FUEL IMBALANCE
Inner tanks – Outer tanks balanced
Fuel quantity in heavier tank
Full

Answer 31

3305 lbs / 1102* lbs

*Takeoff imbalance limitations for Sharklet-equipped aircraft only (e.g., A/C 220, 227).

Question 32

MAXIMUM ALLOWED WING FUEL IMBALANCE
Outer tanks:
Maximum allowed imbalance

Answer 32

1520 lbs / 815* lbs

Takeoff imbalance limitation for Sharklet-equipped aircraft only (e.g., A/C 220, 227)

Question 33

MAX hydraulic pressure

Answer 33

3200 psi

Question 34

Takeoff at reduced thrust is prohibited

Answer 34

• on slippery or contaminated runways;
• when reported or known windshear is present, including predictive windshear indications or a windshear alert for the departure runway;

• when a Special Departure Procedure specifies full thrust for takeoff

Question 35

Maximum reverse should not be used below __________ (Idle reverse is allowed down to aircraft stop)

Answer 35

70 kts

Question 36

Starter limits

_____ consecutive cycles, each of ____________ duration, maximum

Answer 36

4 cycles. 2 minutes

Question 37

Starter limits

____________ between cycles to allow for starter relubrication

Answer 37

20 seconds

Question 38

Starter limits

After four cycles, ____________to allow starter to cool before attempting a new start or motoring.

Answer 38

15 minutes

Question 39

Do not engage the starter when the N2 is above _________

Answer 39

20%

Question 40

PERFORMANCE LIMITS (BELOW 500 FT)

Answer 40

Glideslope Deviation < one dot Localizer Deviation < 1/4 dot
Airspeed ±5 knots of target Max Rate of Descent 1000 fpm
Airspeed not below VLS
Bank not to exceed 7° -2.5° < Pitch < 10°

Question 41

Autobrakes (if available) are __________ for all CAT III approaches.

Answer 41

Required
Runways less than 8000 ft – Medium
Runways 8000 ft or longer – Low or Medium

Question 42

Weight Limits

Answer 42

Taxi. T/O. Landing. ZFW
A319 155,200 154,320 134,480 125,660
A319 IGW 167,320 166,440 137,780 128,960
A320 170,630 169,750 142,190 134,480
A320 IGW 170,630 169,750 145,500 137,780

Question 43

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

Answer 43

Clean configuration . . . . . . . . . . . . . . . . . . . . - 1 g to + 2.5 g

Slats and/or flaps extended . . . . . . . . . . . . . . 0 g to + 2 g