A320 LIMITATIONS

Question 1

For CAT III fail operation (dual) approach with DH require:

A) Alert height of 100ft.

B) Two AP in CMD

C) One Auto Throttle (Minimum)

D) All answers are correct

Answer 1

D) All answers are correct

Question 2

the maximum N2 for to engage starter on the ground is:

A) 0,45

B) 0,33

C) 0,1

D) 0,31

Answer 2

C) 0,1

or 10 %

Question 3

Reverse thrust should not be use below:

A) 110 KIAS

B) 90 KIAS

C) 70 KIAS

D) 112 KIAS

Answer 3

C) 70 KIAS

Question 4

The APU EGT for start below 20000 ft is _degrees C

A) 900

B) 1000

C) 1200

D) 875

Answer 4

A) 900

Question 5

The maximum altitude for flap and slat extension :

A) 41000

B) 25000

C) 37000

D) 20000

Answer 5

D) 20000

Question 6

The maximum speed for gear extension is:

A) 245

B) 250

C) 320

D) 255

Answer 6

B) 250

Question 7

The maximum EGT for the APU start above 25,000 ft is _______ degrees C:

A) 370

B) 200

C) 982

D) 785

Answer 7

C) 982

Question 8

Maximum brake temperature for takeoff without brake fans is:

A) 300 Knots

B) 350 Knots

C) 220 Degrees C

D) 300 Degrees C

Answer 8

D) 300 Degrees C

Question 9

The actual N speed for the APU is _______ %:

A) 105

B) 100

C) 115

D) 112.5

Answer 9

A) 105

Question 10

Using Jet A, if TAT drops below -34 degrees C, monitor ECAM to see fuel temperature remains above ____ degrees C

A) -36

B) -45

C) -20

D) -60

Answer 10

A) -36

Question 11

Minimum oil pressure is ___ psi:

A) 160

B) 3000

C) 60

D) 150

Answer 11

C) 60

Question 12

The maximum wind to open cargo doors is ___ knots :

A) 20

B) 30

C) 40

D) 50

Answer 12

C) 40

Question 13

The N1 limit for the APU is:

A) 11%

B) 105%

C) 115%

D) 107%

Answer 13

D) 107%

Question 14

The service ceiling for this aircraft is _________ ft in order to keep cabin altitude below 8,000 ft

A) 37000

B) 41000

C) 39000

D) 25000

Answer 14

D) 25000

Question 15

This aircraft has a maximum airport pressure altitude of _______ ft

A) 8500

B) 9200

C) 12

D) 9500

Answer 15

C) 12

Question 16

Fuel tanks are located in:

A) Wing

B) Wing root

C) Tail

D) A & B are correct

Answer 16

B) Wing root

Question 17

Minimal runway width is ____ meters:

A) 45

B) 50

C) 55

D) 53

Answer 17

A) 45

Question 18

This aircraft has operating certificates for:

A) VFR/IFR

B) Extended over-water flights

C) Flight in icing conditions

D) All answers are correct

Answer 18

D) All answers are correct

Question 19

The maximum speed for landing gear retraction is:

A) 220 Knots

B) 145 Knots

C) 210 Knots

D) 230 Knots

Answer 19

A) 220 Knots

Question 20

The maximum crosswind for CAT II or CAT III autolanding is:

A) 25 knots

B) 10 knots

C) 20 knots

D) A & B are correct

Answer 20

C) 20 knots

Question 21

Fuel tanks are located in:

A) Wing

B) Wing root

C) Tail

D) A & B are correct

Answer 21

D) A & B are correct

Question 22

The maximum negative pressurization differential is:

A) -8.65 psi

B) -1.0 psi

C) -6.85 psi

D) -0.685 psi

Answer 22

B) -1.0 psi

Question 23

Large control inputs (stop to stop) in pitch, roll or yaw can cause:

A) Structural failure

B) Loss of control

C) Loss of altitude

D) Increase in airspeed

Answer 23

A) Structural failure

Question 24

Maximum tire speed is:

A) 195 Knots

B) 250 Knots

C) 185 Knots

D) 320 Knots

Answer 24

A) 195 Knots

Question 25

The minimum runway requirement for this aircraft is:

A) 5000 ft

B) 2400 ft

C) 4500 ft

D) Found in the performance section of the AFM

Answer 25

D) Found in the performance section of the AFM