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A320 AIRNZ TRAINING > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

LEARN FCOM LIMITATIONS

1
Q

WHAT SHOULD YOU PERFORM IF A FUEL SPILL OCCURS?

A

A NORMAL APU SHUTDOWN

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2
Q

MAX ALTITUDE FOR AIR CON AND PRESSURISATION ON APU ONLY (DUAL PACKS OPS ON APU)

A

15,000 FEET

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3
Q

MAX ALTITUDE FOR AIR CON AND PRESSURIZATION ON APU (SINGLE PACK OPS ON APU) - MOST CONSERVATIVE ON FLEET

A

20,000 FEET

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4
Q

MAX ALT FOR START ASSIST WITH APU

A

20,000 FEET

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5
Q

WHAT IS THE WAIT TIME AFTER 3 CONSECUTIVE START ATTEMPTS OF APU

A

60 MINUTES

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6
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT

AFTER MANUAL GO-AROUND

A

100 FEET AGL

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7
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT

ALL OTHER PHASES (321)

A

900 FEET AGL

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8
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT

ALL OTHER PHASES (320)

A

500 FEET AGL

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9
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT

AFTER TAKE OFF (HEIGHT AND TIME)

A

100 FEET AGL OR 5 SECONDS AFTER LIFT OFF

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10
Q

MIN ALT FOR AUTOPILOT WITH

ILS CAT 1 DISPLAYED

A

160 FEET RAD ALT

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11
Q

MIN ALT FOR AUTOPILOT IN NPA/APV USING

FINAL APP, V/S, FPA

A

250 FEET AGL

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12
Q

TOGA THRUST LIMIT TIME SINGLE ENGINE

CEO/NEO

A

10 MINUTES

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13
Q

MAXIMUM REVERSE SHOULD NOT BE USED BELOW

A

70 KNOTS

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14
Q

THE ENGINE IS ABLE TO START IN CROSSWIND UP TO HOW MUCH

A

35 KNOTS

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15
Q

COOLING PERIOD REQUIRED AFTER THREE FAILED START CYCLES (CEO)

(ONE CYCLE IS ONE FAILED START ATTEMPT, COMPARED TO NEO WHERE ONE CYCLE IS THREE ATTEMPTS)

A

30 MINUTES

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16
Q

COOLING PERIOD REQUIRED AFTER 5 MINUTES OF CONTINUOUS CRANK (CEO)

A

30 MINUTES

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17
Q

FOR GROUND STARTS (AUTO OR MAN) A ____ SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES (CEO) (NB. WE ARE PROBABLY GOING TO CALL MOC ANYWAY PRIOR TO TRYING AGAIN)

A

15 SECONDS

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18
Q

THE STARTER MUST NOT BE RUN ABOVE WHAT N2 ON GROUND / IN FLIGHT (CEO)

A

10% / 18%

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19
Q

COOLING PERIOD REQUIRED AFTER THREE FAILED START CYCLES (NEO)

(ONE CYCLE = THREE ATTEMPTS)

A

15 MINUTES

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20
Q

COOLING PERIOD REQUIRED AFTER 5 MINUTES OF CONTINUOUS CRANK (NEO)

A

15 MINUTES

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21
Q

FOR GROUND STARTS A ____ SECOND PAUSE IS REQUIRED BETWEEN SUCCESSIVE CYCLES (NEO)

A

35 SECONDS

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22
Q

THE STARTED MUST NOT BE RUN ABOVE WHAT N2

NEO

A

20 %

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23
Q

MAX OPERATING ALTITUDE WITH SLATS/FLAPS EXTENDED

A

20,000 FEET

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24
Q

A320 CEO

INNER FUEL TANKS MAX ASYMMETRY (OUTER TANKS BALANCED WITH ONE FULL)

A

500 KG

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25
Q

A320 CEO

OUTER FUEL TANKS MAX ASYMMETRY (INNER TANKS BALANCED)

A

370 KG

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26
Q

A320/1 NEO

FUEL TANKS MAX ASYMMETRY (HEAVIER TANK FULL)

A

400 KG

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27
Q

WHEN IS ICE ACCRETION CONSIDERED SEVERE

A

WHEN ACCUMULATION REACHES 5MM THICKNESS ON THE AIRFRAME

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28
Q

MAX G LOADING CLEAN

A

+2.5G / -1.0G

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29
Q

MAX G LOADING NOT CLEAN

A

0.0G / +2.0G

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30
Q

CARGO DOOR MAX WIND

A

40 KNOTS

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31
Q

CARGO DOOR MAX WIND IF ON LEEWARD SIDE OR NOSE INTO WIND

A

50 KNOTS

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32
Q

COCKPIT WINDOW OPEN MAX SPEED

A

200 KNOTS

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33
Q

MAX TAXI SPEED IN TURN IF ABOVE 76,000KG

A

20 KNOTS

34
Q

MAX COMPANY CROSSWIND LIMIT
DRY
DAMP/WET UP TO 3MM
SLUSH/DRY OR WET SNOW/FROST UP TO 3MM

A

35KT
30KT
25KT

35
Q

MAX DEMONSTRATED CROSSWIND (T/O OR LDG)

A

38 KNOTS INCL GUSTS

36
Q

A320 MAX LANDING WEIGHT

A

66,000KG

37
Q

A321 MAX LANDING WEIGHT

A

79,200KG

38
Q

VLO (RETRACTION)

MAX SPEED LANDING GEAR RETRACTION

A

220 KNOTS / M 0.54

39
Q

MAX TAILWIND FOR T/O AND LANDING

A

15 KNOTS

40
Q

MAX WIND SPEED FOR PASSENGER DOOR OPERATION

A

65 KNOTS

41
Q

CAN WE DO SPECIAL AUTHORISATION ILS

A

NOT PERMITTED

42
Q

THE FWD AND AFT CARGO DOORS MUST BE CLOSED BEFORE WHAT WIND SPEED

A

65 KNOTS

43
Q

MAXIMUM WINDOW WIPERS OPERATING SPEED

A

230 KNOTS

44
Q

WITH PASSENGERS ON BOARD, DON’T EXCEED ____ MINUTES WITHOUT AIR CON SUPPLY

A

20 MINUTES

45
Q

SEVERE TURB PENETRATION SPEED (CEO)

A

RECHECK THIS ANSWER

46
Q

DEFINE ICING CONDITIONS

A

OAT/TAT <= +10DEG TO SAT -40DEG

WITH VISIBLE MOISTURE

47
Q

LANDING CALC REQUIRED FOR ALL RUNWAYS LESS THAN _____M

A

2000M

48
Q

VLE

MAX SPEED WITH GEAR EXTENDED

A

280KT / M0.67

49
Q

VLO (EXTEND)

MAX SPEED FOR EXTENSION

A

250KTS / M0.60

50
Q

MAXIMUM TIRE SPEED

A

195KTS

51
Q

VMCA

A

114KIAS

MAX SPEED @ -2000’

52
Q

WE CAN USE APU BLEED AIR AND AIR FROM HP START UNIT AT THE SAME TIME FOR STARTING

TRUE / FALSE

A

FALSE

YOU CAN GET SHUDDER IN THE NON RETURN VALVE

53
Q

MAX POSITIVE DIFFERENTIAL PRESSURE

A

9.0 PSI (+/- 0.1 PSI)

54
Q

MAX NEGATIVE DIFFERENTIAL PRESSURE

A

-1.0 PSI

55
Q

SAFTEY VALVE RELIEF SETTING

A

8.6 PSI (+/- 0.1 PSI)

56
Q

LP AIR CONDITIONING UNIT AND PACKS MUST BE USED AT THE SAME TIME WHEN ON THE GROUND.

TRUE / FALSE

A

FALSE.

PACKS MUST BE OFF WHEN USING LP GROUND AIR TO PREVENT ADVERSE AFFECTS ON THE AIR CON SYSTEM.

57
Q

MIN ALT FOR AUTOPILOT CIRCLING APPROACH CAT C/D

A

500’ CAT C

600’ CAT D

58
Q

RESTRICTIONS WITH USING OP DES / DES IN APPROACH WITH AP ENGAGED

A

FCU MUST BE SET TO HIGHER OF MDA/MDH OR 500’ AGL

59
Q

MAX SLOPE

A

+/- 2%

60
Q

MINIMAL RUNWAY WIDTH

A320 / A321

A

30M

61
Q

SELECT WHICH CONFIG FOR TAILWIND LANDINGS GREATER THAN 10KTS?

A

FLAPS FULL

62
Q

VMO/MMO

WHAT ABOUT IN ALTERNATE LAW?

A

350/M0.82

REDUCES TO 320KT IN ALT LAW

63
Q

VMCL

MIN CONTROL SPEED FOR LANDING
HIGHEST ON FLEET

A

116KIAS

64
Q

REQUIRED RNP VALUES FOR…

ENROUTE
TERMINAL
APPROACH

AP ON

A
  1. 0 E
  2. 5 T
  3. 3 A
65
Q

MIN DH CAT 2 DUAL

A

100’ RADIO

66
Q

MIN DH CAT 3 SINGLE

A

50’ RADIO

67
Q

CAT 3 DUAL ALERT HEIGHT

A

100’ RADIO

68
Q

MAX TOGA TIME TWO ENG

A

5 MINS

69
Q

ENGINE WARM UP TIME REQD

A

2MINS FOR SOME A/C TO COMPLETE CENTRE TANK PUMP TEST

5MINS IF AOG>2HOURS TO REDUCE THERMAL SHOCK

70
Q

MINIMUM OIL PRESSURE

A

65PSI (MOST LIMITING)

71
Q

MINIMUM OIL TEMP BEFORE T/O

A

50 DEG

72
Q

MIN OIL REQD ON PM ECAM CHECK BEFORE WALK-AROUND CEO/NEO

A

11QT PLUS 0.3Q PER INTENDED FLIGHT HOUR NEXT SECTOR

14QT FOR NEO

73
Q

MIN FUEL TEMP JET A1

A

-43 DEG

74
Q

MAX BRAKE TEMP FOR T/O

WHAT ABOUT WITH FANS ON?

A

300DEG

150DEG

75
Q

MAX TAXI SPEED WITH MAX ONE TIRE PER GEAR DEFLATED (NOT DAMAGED)

WHAT ABOUT TWO?

A

7KTS

3KTS

IF ITS DAMAGED YOU MUST ASK FOR AN INSPECTION PRIOR TO VACATING RWY.

76
Q

A320

MLG WIDTH
WINGSPAN
LENGTH

A
  1. 6m
  2. 1m (NS) / 35.8 (S)
  3. 57m
77
Q

A321

MLG Width
Wingspan
Length

A
  1. 59m
  2. 8m
  3. 51m
78
Q

MAX OPERATING ALT

A

39,800’

79
Q

SEVER TURBULENCE PENETRATION SPEED

A321

A

RECHECK

80
Q

FUEL SAVINGS FROM

TOD

3000’

A

TOD - 1040kg

3000’ - 550kg

81
Q

MIN SPEED WITH ICE ACCRETION

CONF 1,2,3

CONF FULL

WAI INOP

A

VLs + 10kts

VLs + 5kts

VLs + 10kts or GREEN DOT

ADD PILOT INCREMENT AS SPEED COMES BACK DURING THE FLARE

A320 AIRNZ TRAINING (2 decks)

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