A321 CEO Dfferences Flashcards

1
Q

What is the A321 length?

A

44.51m

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2
Q

How many seats?

A

230

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3
Q

What is the engine thrust?

A

33 000lb of thrust

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4
Q

MTOW?

A

93 000kg

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5
Q

How do wing dimensions compare to A320?

A

Same- which means a higher wing loading.

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6
Q

MLW?

A

77 800kg

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7
Q

MZFW?

A

73 800kg

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8
Q

Minimum runway width for 180 deg turn?

A

32m- A321 operations not permitted on 30m runways.

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9
Q

What does ECON flow pb do (if fitted)?

A

ON: ECON flow is selected (less than 167 pax)

OFF: normal flow is selected. Normal flow provides 20% more than ECON flow.

Manual selection not available during single pack or with bleed supplied by APU. In the cases high flow- 40% more than ECON flow.

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10
Q

In what config are CAT II and CAT III fail passive autoland approved?

A

Configuration 3 and full.

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11
Q

Forward and aft cargo detectors and loops?

A

Forward: 4 detectors (2 compartments) linked to 2 detection loops.

Aft: 6 detectors (3 compartments) linked to 3 detection loops.

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12
Q

Flap extension speeds A321 CEO?

A

1: 235
1+F: 225
2: 215
3: 195
Full: 190

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13
Q

When will speed brakes auto retract in the A321?

A

Config 3 and Config FULL (versus A320 Conf FULL only)

A321 FULL speedbrake available in both manual and automatic flight.

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14
Q

What fuel tanks does A321 have?

A

Centre and Wing tanks only (no inner/outer).

Centre tank uses jet pumps to transfer fuel into each wing tank.

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15
Q

What sequence do A321 fuel tanks feed?

A

-centre tank; fuel transfers into the wing tanks (after 250kg used from the wing tanks)

-wing tanks

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16
Q

When does low fuel memo appear in A321?

A

Fuel quantity in either wing is below 1500kg.

17
Q

When fuel is gravity fed from centre tank to wing tanks, why is 2000kg unusable?

A

This assists in a forward CG.

18
Q

What engines are on A321 and thrust??

A

IAE V2533-A5

33 000lb thrust

19
Q

A321 starting temp limit, toga time limits and max continuous?

A

Starting: 635 deg

Toga: 650 deg (5min)

1 inop: 650 (10min)

Max cont: 610 deg

20
Q

What is the purpose of auto flap retraction on A321?

A

At heavy takeoff weight, S speed may be higher than MAX speed for config 1+F (225kt).

Continue to accelerate and at 210kt auto flap retraction will occur and MAX speed will move to 235kt.

21
Q

What is a risk of speed brake extension with high wing loading in A321?

A

VLS may increase above the target speed

22
Q

At high weights during deceleration, green dot can be above Vfe next. How can Conf 1 be selected?

A

Selected a lower. Eg. If green dot is 235kt, select 225kt.

23
Q

A321 tailstrike- pitch attitude awareness:

A

Landing gear not compressed- 11 deg
Landing gear compressed- 9.5 deg

24
Q

On A321 CEO, does final landing config provide a margin above VLS?

A

Only on sharklet aircraft- 5kt margin on PFD.

On non-shark jet aircraft if speed additives not already applied to PERF APPR, 2-3kt can be added to restore margin.

25
Q

Turbulence penetration speed?

A

275kts to 20000ft,
305kts into 0.76.