David Dedmon
Quiz by , created more than 1 year ago

Quiz on Spirit A320 Limitations, created by David Dedmon on 17/09/2016.

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David Dedmon
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Spirit A320 Limitations

Question 1 of 77

1

A319, A320, A321 Wingspan

Select one of the following:

  • 111 feet 10 inches

  • 117 feet 10 inches

  • 111 feet 5 inches

Explanation

Question 2 of 77

1

A320, A321 sharklets wingspan

Select one of the following:

  • 117 feet 5 inches

  • 117 feet 10 inches

  • 111 feet 5 inches

Explanation

Question 3 of 77

1

A319 Max Landing weight

Select one of the following:

  • 137,788

  • 137,728

  • 137,505

Explanation

Question 4 of 77

1

A320 Max Landing Weight

Select one of the following:

  • 145,505

  • 145,788

  • 145,595

Explanation

Question 5 of 77

1

A321 Max Landing Weight

Select one of the following:

  • 171,519

  • 171,505

  • 171,788

Explanation

Question 6 of 77

1

What is the Maximum Operating Altitude?

Select one of the following:

  • FL 398

  • FL 389

  • FL 399

Explanation

Question 7 of 77

1

What is the Maximum runway slope?

Select one of the following:

  • +/- 2 %

  • +/- 2.5 %

  • -1/+2 %

Explanation

Question 8 of 77

1

What is the Maximum Runway Altitude?

Select one of the following:

  • 9,200 feet

  • 8,700 feet

  • 10,000 feet

Explanation

Question 9 of 77

1

What is the nominal runway width?

Select one of the following:

  • 148 feet

  • 150 feet

  • 146 feet

Explanation

Question 10 of 77

1

What is the max crosswind at landing (including any gust)?

Select one of the following:

  • 38 knots

  • 36 knots

  • 37 knots

Explanation

Question 11 of 77

1

What is the max takeoff tailwind?

Select one of the following:

  • 15 knots

  • 10 knots

  • 20 knots

Explanation

Question 12 of 77

1

What is the max landing tailwind?

Select one of the following:

  • 10 knots

  • 15 knots

  • 20 knots

Explanation

Question 13 of 77

1

What is the maximum wind for passenger door operation?

Select one of the following:

  • 65 knots

  • 55 knots

  • 63 knots

Explanation

Question 14 of 77

1

Max landing gear extended speed? (Vle)

Select one of the following:

  • 280 knots or Mach .67

  • 280 knots or Mach .68

  • 250 knots or Mach .67

Explanation

Question 15 of 77

1

What is the max landing gear extension speed?

Select one of the following:

  • 250 knots/M.60

  • 280 knots/M.67

  • 230 knots/M.56

Explanation

Question 16 of 77

1

What is the max landing gear retraction speed?

Select one of the following:

  • 220 knots/M.54

  • 230 knots/M.56

  • 250 knots/M.60

Explanation

Question 17 of 77

1

Max landing gear extension Altitude?

Select one of the following:

  • 25,000 feet

  • 15,000 feet

  • 20,000 feet

Explanation

Question 18 of 77

1

What is the max tire groundspeed?

Select one of the following:

  • 195 knots

  • 180 knots

  • 185 knots

Explanation

Question 19 of 77

1

What is the maximum wiper operation speed?

Select one of the following:

  • 230 knots

  • 250 knots

  • 220 knots

Explanation

Question 20 of 77

1

Fill the blank spaces to complete the text.

In the A320 and A321, if the taxi weight is higher than , do not exceed knots taxi speed when turning.

Explanation

Question 21 of 77

1

Fill the blank spaces to complete the text.

Do not operate a air cart and air from the simultaneously to avoid chatter of non-return valves.

Explanation

Question 22 of 77

1

Fill the blank spaces to complete the text.

Do not use a air cart when the is supplying bleed air to avoid .

Explanation

Question 23 of 77

1

Max positive cabin pressure differential

Select one of the following:

  • 9.0 psi

  • 8.8 psi

  • 8.6 psi

Explanation

Question 24 of 77

1

Max negative cabin pressure differential?

Select one of the following:

  • -1.0 psi

  • -2.0 psi

  • -1.5 psi

Explanation

Question 25 of 77

1

What is the minimum altitude for autopilot engagement during takeoff with SRS mode?

Select one of the following:

  • 100 feet

  • 160 feet

  • 1,000 feet

Explanation

Question 26 of 77

1

What is the minimum altitude for autopilot usage while flying a straight-in non-precision approach?

Select one of the following:

  • Applicable minimums.

  • Applicable minimums minus 100 feet.

  • 160 feet.

Explanation

Question 27 of 77

1

What is the minimum height for autopilot usage when performing a circling approach?

Select one of the following:

  • Applicable minimums minus 100 feet.

  • Applicable minimums.

  • Applicable minimums minus 200 feet.

Explanation

Question 28 of 77

1

What is the minimum height for autopilot usage during an ILS when CAT2 or CAT3 is not displayed on the FMA?

Select one of the following:

  • 160 feet.

  • 100 feet.

  • 200 feet.

Explanation

Question 29 of 77

1

What is the minimum altitude for autopilot or flight director engagement during a go-around?

Select one of the following:

  • 100 feet.

  • 1000 feet.

  • 150 feet.

Explanation

Question 30 of 77

1

If not specified, the minimum altitude for autopilot engagement in the A319/A320 is

Select one of the following:

  • 500 feet AGL

  • 900 feet AGL

  • 1000 feet AGL

Explanation

Question 31 of 77

1

If not specified, the minimum altitude for autopilot engagement in the A321 is

Select one of the following:

  • 900 feet AGL

  • 500 feet AGL

  • 400 feet AGL

Explanation

Question 32 of 77

1

Fill the blank spaces to complete the text.

logic prohibits autopilot engagement during takeoff with SRS mode for seconds after liftoff.

Explanation

Question 33 of 77

1

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)

Select one of the following:

  • Highest of minimums or 500 feet.

  • Highest of minimums or 900 feet.

  • Highest of minimums or 1000 feet.

Explanation

Question 34 of 77

1

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)

Select one of the following:

  • Highest of minimums or 900 feet.

  • Highest of minimums or 500 feet.

  • Highest of minimums or 1000 feet.

Explanation

Question 35 of 77

1

Select from the dropdown lists to complete the text.

Nav mode may be used in the terminal area provided: ( GPS Primary is available, RNAV Primary is available ), OR, ( HIGH Accuracy is displayed, high accuracy is not displayed ) and the appropriate RNP is checked and entered on the MCDU, OR, ( NAVAID raw data is monitored, A/THR FMA Speed is not selected. ).

Explanation

Question 36 of 77

1

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.

Select one of the following:

  • True
  • False

Explanation

Question 37 of 77

1

Max altitude for operating with flaps or slats extended

Select one of the following:

  • 20,000 feet

  • 25,000 feet

  • 15,000 feet

Explanation

Question 38 of 77

1

Max inner tank fuel imbalance at takeoff 618-643NK

Select one of the following:

  • Heavier tank full, 1,102lbs max imbalance

  • Heavier tank full, 882 lbs max imbalance.

  • Heavier tank full, 2,910 lbs max imbalance.

Explanation

Question 39 of 77

1

Max inner tanks full imbalance at takeoff 657-672NK

Select one of the following:

  • Heavier tank full, 882 lbs max imbalance.

  • Heavier tank full, 1,102 lbs max imbalance.

  • Heavier tank full, 3,306 lbs max imbalance.

Explanation

Question 40 of 77

1

Max allowed inner tanks wing fuel imbalance in flight and landing 618-643NK

Select one of the following:

  • 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.

Explanation

Question 41 of 77

1

Max allowed inner tanks wing fuel imbalance in flight and landing 587-588NK

Select one of the following:

  • Heavier tank full, 2,910 lbs max imbalance.

  • Heavier tank full, 3,306 lbs max imbalance.

  • Heavier tank full, 882 lbs max imbalance.

Explanation

Question 42 of 77

1

What is the minimum fuel quantity for takeoff?

Select one of the following:

  • 3,307 lbs.

  • 3,306 lbs

  • 2,910 lbs

Explanation

Question 43 of 77

1

What is the maximum brake temperature for takeoff (brake fans off)?

Select one of the following:

  • 300 degrees C

  • 150 degrees C

  • 200 degrees C

Explanation

Question 44 of 77

1

Fill the blank spaces to complete the text.

After APU starter motor duty cycles, wait minutes before attempting more cycles.

Explanation

Question 45 of 77

1

What is the max altitude for APU start on battery power (emergency electrical configuration)?

Select one of the following:

  • 25,000 feet

  • 20,000 feet

  • 15,000 feet

Explanation

Question 46 of 77

1

Max APU starting altitude with normal AC power supply and operation

Select one of the following:

  • 41,000 feet

  • 15,000 feet

  • 20,000 feet

Explanation

Question 47 of 77

1

Max altitude for APU with two packs operating?

Select one of the following:

  • 15,000 feet.

  • 20,000 feet.

  • 25,000 feet.

Explanation

Question 48 of 77

1

Max altitude for APU with one pack operating?

Select one of the following:

  • 20,000 feet.

  • 15,000 feet.

  • 25,000 feet.

Explanation

Question 49 of 77

1

APU air bleed extraction for the use of wing anti-ice is not permitted.

Select one of the following:

  • True
  • False

Explanation

Question 50 of 77

1

What is the engine starting EGT temperature limit?

Select one of the following:

  • 635 degrees C

  • 650 degrees C

  • 610 degrees C

Explanation

Question 51 of 77

1

What is the max engine MCT temperature?

Select one of the following:

  • 610 degrees C

  • 635 degrees C

  • 650 degrees C

Explanation

Question 52 of 77

1

In the A319 and A320, what are the time and temperature limits for two-engine and single-engine takeoffs and go-arounds?

Select one of the following:

  • 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.

Explanation

Question 53 of 77

1

In the A321, what is the max time and temperature during takeoff or go-around?

Select one of the following:

  • 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

Explanation

Question 54 of 77

1

Fill the blank spaces to complete the text.

Starter motor limit cycles of minutes each, cycle of minute.

Explanation

Question 55 of 77

1

What is the minimum time required between each consecutive start attempt?

Select one of the following:

  • 15 seconds

  • 30 seconds

  • 20 seconds

Explanation

Question 56 of 77

1

Fill the blank spaces to complete the text.

The required starter motor cooling period after consecutive cycles or consecutive minutes of cranking is minutes.

Explanation

Question 57 of 77

1

Fill the blank spaces to complete the text.

No running engagement of the starter motor is permitted when is above percent on the ground or percent in flight.

Explanation

Question 58 of 77

1

What is the minimum engine oil starting temperature?

Select one of the following:

  • -40C

  • -34C

  • -10C

Explanation

Question 59 of 77

1

What is the minimum engine oil temperature required prior to exceeding idle power?

Select one of the following:

  • -10C

  • 0C

  • -40C

Explanation

Question 60 of 77

1

Fill the blank spaces to complete the text.

The minimum oil quantity required for each flight is quarts plus an estimated hourly consumption rate of ~ quarts per hour of expected flight time.

Explanation

Question 61 of 77

1

The minimum operating oil pressure is

Select one of the following:

  • 60 psi

  • 55 psi

  • 45 psi

Explanation

Question 62 of 77

1

Maximum reverse thrust should not be used below what speed?

Select one of the following:

  • 70 knots.

  • 60 knots.

  • 80 knots.

Explanation

Question 63 of 77

1

On what tail numbers should max reverse use be discontinued when speed begins to fluctuate?

Select one of the following:

  • 502-534 and 601-646NK.

  • 587-588 and 601-646NK.

  • 502-534 and 618-643NK.

Explanation

Question 64 of 77

1

Is takeoff with reduced thrust permitted on a contaminated runway?

Select one of the following:

  • Yes

  • No

Explanation

Question 65 of 77

1

The engines are capable of starting in crosswinds of up to

Select one of the following:

  • 35 knots

  • 38 knots

  • 65 knots

Explanation

Question 66 of 77

1

What is the max landing weight for A320s 901-905NK?

Select one of the following:

  • 148591

  • 148532

  • 145505

Explanation

Question 67 of 77

1

What is the maximum runway altitude for tail numbers 901-905NK?

Select one of the following:

  • 6000 feet

  • 9200 feet

  • 7000

Explanation

Question 68 of 77

1

What is the maximum certified crosswind for takeoff for tail numbers 901-905NK?

Select one of the following:

  • 35 knots.

  • 38 knots.

  • 36 knots

Explanation

Question 69 of 77

1

What is the max crosswind for CAT2 or CAT3 autoland on 901-905NK?

Select one of the following:

  • 15 knots

  • 20 knots

  • 10 knots

Explanation

Question 70 of 77

1

What is the maximum EGT limit for tail numbers 901-905NK during takeoff or go around?

Select one of the following:

  • 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

Explanation

Question 71 of 77

1

What is the max MCT for tail numbers 901-905NK?

Select one of the following:

  • 1043 C

  • 1083 C

  • 610 C

Explanation

Question 72 of 77

1

What is the max EGT starting temperature limit for 901-905NK?

Select one of the following:

  • 1018 C

  • 1043 C

  • 1083 C

Explanation

Question 73 of 77

1

What is the minimum oil pressure for tail numbers 901-905NK?

Select one of the following:

  • 65 psi

  • 60 psi

  • 55 psi

Explanation

Question 74 of 77

1

During engine start on 901-905NK, how much time is required between each start cycle?

Select one of the following:

  • 35 seconds

  • 30 seconds

  • 15 seconds

Explanation

Question 75 of 77

1

Fill the blank spaces to complete the text.

On 901-905NK, after consecutive start cycles or minutes of continuous cranking, a minute cooling period is required.

Explanation

Question 76 of 77

1

What is the max certified crosswind for takeoff in 901-905NK?

Select one of the following:

  • 35

  • 38

  • 30

Explanation

Question 77 of 77

1

What is the maximum crosswind to perform a CAT II or III in 901-905NK?

Select one of the following:

  • 15 knots

  • 20 knots

  • 10 knots

Explanation

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