Question 1
Question
A319, A320, A321 Wingspan
Answer
-
111 feet 10 inches
-
117 feet 10 inches
-
111 feet 5 inches
Question 2
Question
A320, A321 sharklets wingspan
Answer
-
117 feet 5 inches
-
117 feet 10 inches
-
111 feet 5 inches
Question 3
Question
A319 Max Landing weight
Question 4
Question
A320 Max Landing Weight
Question 5
Question
A321 Max Landing Weight
Question 6
Question
What is the Maximum Operating Altitude?
Question 7
Question
What is the Maximum runway slope?
Answer
-
+/- 2 %
-
+/- 2.5 %
-
-1/+2 %
Question 8
Question
What is the Maximum Runway Altitude?
Answer
-
9,200 feet
-
8,700 feet
-
10,000 feet
Question 9
Question
What is the nominal runway width?
Answer
-
148 feet
-
150 feet
-
146 feet
Question 10
Question
What is the max crosswind at landing (including any gust)?
Answer
-
38 knots
-
36 knots
-
37 knots
Question 11
Question
What is the max takeoff tailwind?
Answer
-
15 knots
-
10 knots
-
20 knots
Question 12
Question
What is the max landing tailwind?
Answer
-
10 knots
-
15 knots
-
20 knots
Question 13
Question
What is the maximum wind for passenger door operation?
Answer
-
65 knots
-
55 knots
-
63 knots
Question 14
Question
Max landing gear extended speed? (Vle)
Answer
-
280 knots or Mach .67
-
280 knots or Mach .68
-
250 knots or Mach .67
Question 15
Question
What is the max landing gear extension speed?
Answer
-
250 knots/M.60
-
280 knots/M.67
-
230 knots/M.56
Question 16
Question
What is the max landing gear retraction speed?
Answer
-
220 knots/M.54
-
230 knots/M.56
-
250 knots/M.60
Question 17
Question
Max landing gear extension Altitude?
Answer
-
25,000 feet
-
15,000 feet
-
20,000 feet
Question 18
Question
What is the max tire groundspeed?
Answer
-
195 knots
-
180 knots
-
185 knots
Question 19
Question
What is the maximum wiper operation speed?
Answer
-
230 knots
-
250 knots
-
220 knots
Question 20
Question
In the A320 and A321, if the taxi weight is higher than [blank_start]167,550[blank_end], do not exceed [blank_start]20[blank_end] knots taxi speed when turning.
Question 21
Question
Do not operate a [blank_start]LP[blank_end] air cart and air from the [blank_start]packs[blank_end] simultaneously to avoid chatter of non-return valves.
Question 22
Question
Do not use a [blank_start]HP[blank_end] air cart when the [blank_start]APU[blank_end] is supplying bleed air to avoid [blank_start]bleed system damage[blank_end].
Answer
-
HP
-
APU
-
bleed system damage
Question 23
Question
Max positive cabin pressure differential
Question 24
Question
Max negative cabin pressure differential?
Answer
-
-1.0 psi
-
-2.0 psi
-
-1.5 psi
Question 25
Question
What is the minimum altitude for autopilot engagement during takeoff with SRS mode?
Answer
-
100 feet
-
160 feet
-
1,000 feet
Question 26
Question
What is the minimum altitude for autopilot usage while flying a straight-in non-precision approach?
Question 27
Question
What is the minimum height for autopilot usage when performing a circling approach?
Question 28
Question
What is the minimum height for autopilot usage during an ILS when CAT2 or CAT3 is not displayed on the FMA?
Answer
-
160 feet.
-
100 feet.
-
200 feet.
Question 29
Question
What is the minimum altitude for autopilot or flight director engagement during a go-around?
Answer
-
100 feet.
-
1000 feet.
-
150 feet.
Question 30
Question
If not specified, the minimum altitude for autopilot engagement in the A319/A320 is
Answer
-
500 feet AGL
-
900 feet AGL
-
1000 feet AGL
Question 31
Question
If not specified, the minimum altitude for autopilot engagement in the A321 is
Answer
-
900 feet AGL
-
500 feet AGL
-
400 feet AGL
Question 32
Question
[blank_start]FMGS[blank_end] logic prohibits autopilot engagement during takeoff with SRS mode for [blank_start]5[blank_end] seconds after liftoff.
Question 33
Question
Use of the autopilot or flight director in OPEN DES or DES mode is not permitted in approach, unless the FCU is set to an altitude at or above(A319/A320)
Answer
-
Highest of minimums or 500 feet.
-
Highest of minimums or 900 feet.
-
Highest of minimums or 1000 feet.
Question 34
Question
Use of the autopilot or flight director in OPEN DES or DES mode is not permitted in approach, unless the FCU is set to an altitude at or above (A321)
Answer
-
Highest of minimums or 900 feet.
-
Highest of minimums or 500 feet.
-
Highest of minimums or 1000 feet.
Question 35
Question
Nav mode may be used in the terminal area provided: [blank_start]GPS Primary is available[blank_end], OR, [blank_start]HIGH Accuracy is Displayed[blank_end] and the appropriate RNP is checked and entered on the MCDU, OR, [blank_start]NAVAID raw data is monitored[blank_end].
Answer
-
GPS Primary is available
-
RNAV Primary is available
-
NAVAID raw data is monitored
-
A/THR FMA Speed is not selected.
-
HIGH Accuracy is displayed
-
high accuracy is not displayed
Question 36
Question
In the A319 and A321, with one engine inoperative, it is not permitted to use the autopilot to perform non-precision approaches in the following modes: FINAL APP, NAV V/S, NAV/FPA. Only flight director use is permitted.
Question 37
Question
Max altitude for operating with flaps or slats extended
Answer
-
20,000 feet
-
25,000 feet
-
15,000 feet
Question 38
Question
Max inner tank fuel imbalance at takeoff 618-643NK
Answer
-
Heavier tank full, 1,102lbs max imbalance
-
Heavier tank full, 882 lbs max imbalance.
-
Heavier tank full, 2,910 lbs max imbalance.
Question 39
Question
Max inner tanks full imbalance at takeoff 657-672NK
Answer
-
Heavier tank full, 882 lbs max imbalance.
-
Heavier tank full, 1,102 lbs max imbalance.
-
Heavier tank full, 3,306 lbs max imbalance.
Question 40
Question
Max allowed inner tanks wing fuel imbalance in flight and landing 618-643NK
Answer
-
Heavier tank is full, 3,306 lb max imbalance.
-
Heavier tank is full, 2,910 lbs max imbalance.
-
Heavier tank full, 1,102 lbs max imbalance.
Question 41
Question
Max allowed inner tanks wing fuel imbalance in flight and landing 587-588NK
Answer
-
Heavier tank full, 2,910 lbs max imbalance.
-
Heavier tank full, 3,306 lbs max imbalance.
-
Heavier tank full, 882 lbs max imbalance.
Question 42
Question
What is the minimum fuel quantity for takeoff?
Answer
-
3,307 lbs.
-
3,306 lbs
-
2,910 lbs
Question 43
Question
What is the maximum brake temperature for takeoff (brake fans off)?
Answer
-
300 degrees C
-
150 degrees C
-
200 degrees C
Question 44
Question
After [blank_start]3[blank_end] APU starter motor duty cycles, wait [blank_start]60[blank_end] minutes before attempting [blank_start]3[blank_end] more cycles.
Question 45
Question
What is the max altitude for APU start on battery power (emergency electrical configuration)?
Answer
-
25,000 feet
-
20,000 feet
-
15,000 feet
Question 46
Question
Max APU starting altitude with normal AC power supply and operation
Answer
-
41,000 feet
-
15,000 feet
-
20,000 feet
Question 47
Question
Max altitude for APU with two packs operating?
Answer
-
15,000 feet.
-
20,000 feet.
-
25,000 feet.
Question 48
Question
Max altitude for APU with one pack operating?
Answer
-
20,000 feet.
-
15,000 feet.
-
25,000 feet.
Question 49
Question
APU air bleed extraction for the use of wing anti-ice is not permitted.
Question 50
Question
What is the engine starting EGT temperature limit?
Answer
-
635 degrees C
-
650 degrees C
-
610 degrees C
Question 51
Question
What is the max engine MCT temperature?
Answer
-
610 degrees C
-
635 degrees C
-
650 degrees C
Question 52
Question
In the A319 and A320, what are the time and temperature limits for two-engine and single-engine takeoffs and go-arounds?
Answer
-
Two engine: 5 minutes at 635C. Single engine: 10 minutes at 635C.
-
Two engine: 5 minutes at 650C. Single engine: 10 minutes at 650C.
-
Two engine: 5 minutes at 610C.
Single engine: 10 minutes 610C.
Question 53
Question
In the A321, what is the max time and temperature during takeoff or go-around?
Answer
-
Two engine: 5 minutes at 650C.
Single engine: 10 minutes at 650C.
-
Two engine: 5 minutes at 635C
Single engine: 10 minutes at 635C.
-
Two engine: 10 minutes at 635C
Single engine: 10 minutes at 650C
Question 54
Question
Starter motor limit [blank_start]2[blank_end] cycles of [blank_start]2[blank_end] minutes each, [blank_start]1[blank_end] cycle of [blank_start]1[blank_end] minute.
Question 55
Question
What is the minimum time required between each consecutive start attempt?
Answer
-
15 seconds
-
30 seconds
-
20 seconds
Question 56
Question
The required starter motor cooling period after [blank_start]3[blank_end] consecutive cycles or [blank_start]4[blank_end] consecutive minutes of cranking is [blank_start]30[blank_end] minutes.
Question 57
Question
No running engagement of the starter motor is permitted when [blank_start]N2[blank_end] is above [blank_start]10[blank_end] percent on the ground or [blank_start]18[blank_end] percent in flight.
Question 58
Question
What is the minimum engine oil starting temperature?
Question 59
Question
What is the minimum engine oil temperature required prior to exceeding idle power?
Question 60
Question
The minimum oil quantity required for each flight is [blank_start]11[blank_end] quarts plus an estimated hourly consumption rate of ~ [blank_start].3[blank_end] quarts per hour of expected flight time.
Question 61
Question
The minimum operating oil pressure is
Question 62
Question
Maximum reverse thrust should not be used below what speed?
Answer
-
70 knots.
-
60 knots.
-
80 knots.
Question 63
Question
On what tail numbers should max reverse use be discontinued when speed begins to fluctuate?
Answer
-
502-534 and 601-646NK.
-
587-588 and 601-646NK.
-
502-534 and 618-643NK.
Question 64
Question
Is takeoff with reduced thrust permitted on a contaminated runway?
Question 65
Question
The engines are capable of starting in crosswinds of up to
Answer
-
35 knots
-
38 knots
-
65 knots
Question 66
Question
What is the max landing weight for A320s 901-905NK?
Question 67
Question
What is the maximum runway altitude for tail numbers 901-905NK?
Question 68
Question
What is the maximum certified crosswind for takeoff for tail numbers 901-905NK?
Answer
-
35 knots.
-
38 knots.
-
36 knots
Question 69
Question
What is the max crosswind for CAT2 or CAT3 autoland on 901-905NK?
Answer
-
15 knots
-
20 knots
-
10 knots
Question 70
Question
What is the maximum EGT limit for tail numbers 901-905NK during takeoff or go around?
Answer
-
Two engine 5 minutes at 1083C
One engine 10 minutes at1083C
-
Two engine 5 minutes 1059
One engine 10 minutes 1059
-
Two engine 5 minutes 1102
one engine 10 minutes 1102
Question 71
Question
What is the max MCT for tail numbers 901-905NK?
Question 72
Question
What is the max EGT starting temperature limit for 901-905NK?
Question 73
Question
What is the minimum oil pressure for tail numbers 901-905NK?
Question 74
Question
During engine start on 901-905NK, how much time is required between each start cycle?
Answer
-
35 seconds
-
30 seconds
-
15 seconds
Question 75
Question
On 901-905NK, after [blank_start]3[blank_end] consecutive start cycles or [blank_start]15[blank_end] minutes of continuous cranking, a [blank_start]15[blank_end] minute cooling period is required.
Question 76
Question
What is the max certified crosswind for takeoff in 901-905NK?
Question 77
Question
What is the maximum crosswind to perform a CAT II or III in 901-905NK?
Answer
-
15 knots
-
20 knots
-
10 knots