A321 NEO Differences Flashcards

1
Q

Max weights?

A

MTOW 97400
MLW 97000
MLW7 79200
MZFW 75600

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2
Q

When to use low and high pack flow?

A

LOW: if number of occupants below 168

HIGH: for abnormally hot and humid conditions

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3
Q

When and why does PACKS indication appear on EWD above N1 indicators?

A

Indicates engines bleeds are supplying packs.

-on ground, at least 1 engine running
-during to/ga until thrust in CL detent
-in flight, when thrust is MCT

*Engine anti ice/wing anti ice indications also appear if selected on under same conditions

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4
Q

When and how does ACT begin auto transferring to centre tank?

A

30min after gear up.

Via pressurisation of tank, by closing ACT vent and opening air shutoff valve.

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5
Q

When does ACT transfer stop and restart?

A

Stops if centre tank exceeds 5750kg, by closing ACT transfer valve.

Reopens when below 5000kg.

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6
Q

Cargo agent 2 timing?

A

195 minutes for A321 NEO (vs 150 min for A321 CEO)

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7
Q

Flap extension speeds for A321 NEO?

A

1: 243
1+F: 225
2: 215
3: 195
Full: 186

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8
Q

When is aileron droop active on A321 NEO?

A

When flaps are extended- ailerons droop 10 deg.

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9
Q

Is continuous ignition automatically selected with engine anti ice ON?

A

No (for A321 NEO)

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10
Q

How do oxygen bottles feed on A321 NEO?

A

One to captain/3rd observer, other to FO/4th observer.

Also additional overpressure indicator on nose.

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11
Q

How do oxygen bottles feed on A321 NEO?

A

One to captain/3rd observer, other to FO/4th observer.

Also additional overpressure indicator on nose.

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12
Q

How do oxygen bottles feed on A321 NEO?

A

One to captain/3rd observed, other to FO/4th observer.

Also additional overpressure indicator on nose.

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13
Q

When does amber half box appear around each oxy ind on A321 NEO?

A

800psi

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14
Q

Seats, doors and overwing exits?

A

Seats 232

2 front/2 rear doors (dual lane slide rafts each side)

Emergency door 3 located after of wing (single lane slide each side)

2 top hinged overwing emergency exits (dual lane off wing slide each side)

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15
Q

Engine model and thrust output?

A

CFM International LEAP-1A

35000 lb thrust

Thrust measurement in % N1

460mm ground clearance

Bypass ratio 11:1

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16
Q

When is CORE-ICE PROT displayed on ENG SD page?

A

Variable bleed valves (VBVs) provide hot air to engine core to prevent ice crystal formation.

17
Q

When is ICE PROT-BOOST displayed on ENG SD?

A

7th stage HP compressor supplies hot air to a booster anti ice (BAI) valve to prevent ice crystal formation and also improved start performance in transient conditions.

18
Q

TOGA and MCT temp limit?

A

TOGA 1060 C

MCT 1025 C

19
Q

Start temp limits?

A

Ground 750 C

Flight 875 C

20
Q

Crosswind engine start?

A

45kt

21
Q

Maximum Certified Crosswind

A

35 takeoff

38 land

22
Q

Minimum oil quantity?

A

10.6Qt or

8.9Qt + 0.45Qt/hr

23
Q

Min oil pressure?

A

17.4 psi

24
Q

Max tailwind?

A

10 takeoff
15 landing

25
Q

Fixed reserve (1500ft)?

A

1100kg

26
Q

Wx & Traffic (FL200)

A

2,490-kg/hr (81.6TN ISA+10C)

27
Q

Tail strike awareness?

A

11.5deg /9.9deg LDG compressed

28
Q

Performance category?

A

D (400 ft agl / 5.28NM)

29
Q

Flare mode THS freeze?

A

100ft

30
Q

Rotation mode?

A

Active from 70kt to 10sec after liftoff and pitch attitude >8deg

Pitch rate demand control law providing tail strike protection.

31
Q

Approx idle parameters?

A

N1 20
N2 70
EGT 500
FF 300

32
Q

Crosswind above 20kt/tailwind takeoff?

A

Sidestick full forward

Increase thrust rapidly to 70 % N1 then, above 15 kt GS, progressively to reach takeoff thrust by 40 kt GS.