A320 LIMITATIONS Flashcards
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
D) All answers are correct
the maximum N2 for to engage starter on the ground is:
A) 0,45 B) 0,33 C) 0,1 D) 0,31
C) 0,1
or 10 %
Reverse thrust should not be use below:
A) 110 KIAS B) 90 KIAS C) 70 KIAS D) 112 KIAS
C) 70 KIAS
The APU EGT for start below 20000 ft is _degrees C
A) 900 B) 1000 C) 1200 D) 875
A) 900
The maximum altitude for flap and slat extension :
A) 41000 B) 25000 C) 37000 D) 20000
D) 20000
The maximum speed for gear extension is:
A) 245 B) 250 C) 320 D) 255
B) 250
The maximum EGT for the APU start above 25,000 ft is _______ degrees C:
A) 370 B) 200 C) 982 D) 785
C) 982
Maximum brake temperature for takeoff without brake fans is:
A) 300 Knots B) 350 Knots C) 220 Degrees C D) 300 Degrees C
D) 300 Degrees C
The actual N speed for the APU is _______ %:
A) 105 B) 100 C) 115 D) 112.5
A) 105
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
A) -36
Minimum oil pressure is ___ psi:
A) 160 B) 3000 C) 60 D) 150
C) 60
The maximum wind to open cargo doors is ___ knots :
A) 20 B) 30 C) 40 D) 50
C) 40
The N1 limit for the APU is:
A) 11% B) 105% C) 115% D) 107%
D) 107%
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
D) 25000
This aircraft has a maximum airport pressure altitude of _______ ft
A) 8500 B) 9200 C) 12 D) 9500
C) 12
Fuel tanks are located in:
A) Wing B) Wing root C) Tail D) A & B are correct
B) Wing root
Minimal runway width is ____ meters:
A) 45 B) 50 C) 55 D) 53
A) 45
This aircraft has operating certificates for:
A) VFR/IFR B) Extended over-water flights C) Flight in icing conditions D) All answers are correct
D) All answers are correct
The maximum speed for landing gear retraction is:
A) 220 Knots B) 145 Knots C) 210 Knots D) 230 Knots
A) 220 Knots
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
C) 20 knots
Fuel tanks are located in:
A) Wing B) Wing root C) Tail D) A & B are correct
D) A & B are correct
The maximum negative pressurization differential is:
A) -8.65 psi B) -1.0 psi C) -6.85 psi D) -0.685 psi
B) -1.0 psi
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
A) Structural failure
Maximum tire speed is:
A) 195 Knots B) 250 Knots C) 185 Knots D) 320 Knots
A) 195 Knots
