LIMITATIONS Flashcards

1
Q

321 FLAP SPEEDS

A

0 VMO / MMO CRUISE
1 243 kt HOLDING 1
1 + F 225 kt TAKEOFF
2 215 kt TAKEOFF/APPROACH
3 195 kt TAKEOFF/APPROACH/LANDING
FULL 186 kt LANDING

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2
Q

VMO / MMO

A

350kt / M 0.82

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3
Q

VLE
VLO EXTENSION
VLO RETRACTION

A

VLE 280
VLO EXT 250
VLO RET 220

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4
Q

TYRE SPEED

A

195 KT

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5
Q

VMCL

A

116 KT

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6
Q

WIPERS SPEED

A

230 KT

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7
Q

320 WEIGHTS

A

TAXI 77.400
TO 77.000
LDG 67.400
ZFW 64.300

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8
Q

321 WEIGHTS

A

TAXI 89.400
TO 89.000
LDG 79.200
ZFW 75.600

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9
Q

APU BLEED USE WITH HP START UNIT

A

MUST NOT APU BLEED AND HP AIR START UNIT SAME TIME

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10
Q

AVIONICS VENTS

A

oat <= 49 ilimitado
49< OAT <= 55 2H
55< OAT <= 60 1H
60< OAT <=64 0.5H

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11
Q

CABIN PRESSURE

A

MAX POSITVE 9.0
MAX NEGATIVE -1.0
SAFETY RELIEF VALVE 8.6 PSI

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12
Q

AUTO PILOTS USAGE TAKEOFF

A

100 FT or 5 SEC LIFTOFF

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13
Q

AUTO PILOTS USAGE APP FINAL APP/ VS or FPA mode

A

250 ft AGL

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14
Q

AUTO PILOTS USAGE CIRCLING APP

A

500 FT CAT C
600 FT CAT D

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15
Q

AUTO PILOTS USAGE ILS

A

160 FT

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16
Q

AUTO PILOTS USAGE LPV

A

160 FT

17
Q

AUTO PILOTS USAGE AFTER MANUAL GO AROUND

A

100 FT

18
Q

AUTO PILOTS USAGE ALL OTHER PHASE

A

500 FT

19
Q

AUTO PILOTS USAGE ILS CAT 2

A

80 FT

20
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I AIRBUS 321

A

HEAD WIND 15 KT
X WIND 10 KT
TAILWIND 10 KT

21
Q

MAXIMUM WIND CONDITIONS FOR ILS/MLS  CAT II OR CAT III AND FOR GLS  CAT I AIRBUS 320

A

HEADWIND 30 KT
X WIND 20 KT (15 KT OEI WITH AUTOMATIC ROLL OUT)
TAIL WIND 10 KT

22
Q

APU START

A

AFTER 3RD ATTEMPTS, 60 MINUTES OFF

23
Q

APU BLEED

A

Max altitude to assist engine start.. 20 000 ft
Max altitude for air conditioning and pressurization (single pack operation).. 20 000 ft
Max altitude for air conditioning and pressurization (dual pack operation)…15 000 ft
Use of APU bleed air for wing anti-ice is not permitted.

24
Q

MINIMUM FUEL QUANTITY FOR TAKEOFF

A

1500 KG

25
Q

FUEL IMBALANCE AT TAKEOFF A 321

A

FULL - 400KG
3000 KG - 400KG
700 KG - 700 KG

26
Q

DEFINITION OF ICING CONDITIONS

A

Icing conditions exist when the OAT (on ground or after takeoff) or the TAT (in flight) is at or
below 10 °C and visible moisture in any form is present (such as clouds, fog with visibility of 1 sm
(1 600 m) or less, rain, snow, sleet or ice crystals).
‐ Icing conditions also exist when the OAT on the ground and for takeoff is at or below 10 °C and
operating on ramps, taxiways or runways where surface snow, standing water or slush may be
ingested by the engines, or freeze on engines, nacelles or engine sensor probes

27
Q

BRAKE TEMPERATURE BRAKE FANS OFF

A

300 C

28
Q

TAXI WITH DEFLATED OR DAMAGED TIRES

A

‐ If maximum one tire per gear is deflated (consider three gears)
Maximum taxi speed during turn……………………………………………………………………………………. 7 kt
‐ If two tires are deflated on the same main gear (maximum one main gear)
Maximum taxi speed……………………………………………………………………………………………………. 3 kt
‐ For the nosewheel steering (NWS) angle
Maximum NWS angle………………………………………………………………………………………………….. 30

29
Q

IR GROUND ALIGNMENT

A

Ground alignment of the IRS is possible in latitudes between 73 ° North and 60 ° South

30
Q

Minimum Bottle Pressure to Cove5

A

▪ During emergency descent for all flight crewmembers and observers for 22 min
▪ During cruise at FL 100 for two flight crewmembers for 98 min.
* Protection against smoke with 100 % oxygen for all flight crewmembers and observers during
15 min at 8 000 ft cabin altitude.

31
Q

TEMP MAX and MIN for takeoff

A

-40 / + 55

32
Q

MAX CROSSWIND for TO and LD?

A

35 (gust included) for TO
38 (gust included) for LD

33
Q

MAX TAILWIND for TO and LDG?

A

15 KTs for TO
10 KTs for LDG

34
Q

MAX CROSSWIND for ENG START?

A

45 kts

35
Q

MAX ENG EGT

A

TOGA 1060
FLEX/MCT 1025
START FLIGHT 875
START GND 750

36
Q

MINIMUM OIL QTY?

A

highest value off
10.6 or
8.9 + 0.45qt per flight hour

37
Q

APU BATT RESTART FL LIMIT

A

FL 250

38
Q

MAX FUEL IMBALANCE FOR TO

A

500 KG

39
Q

FUEL IMBALANCE IN FLIGHT

A

1500 KG