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A320 > Limitations > Flashcards

Limitations Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

A
  • CLEAN = -1G TO +2.5G

- OTHER = 0G TO +2G

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2
Q

MAX PRESSURE ALTITUDE

A

39,800’

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3
Q

RUNWAY SLOPE

A

+/-2%

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4
Q

MAX RUNWAY ALTITUDE

A

9,200’

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5
Q

MINIMUM RUNWAY WIDTH

A

30M

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6
Q

NOMINAL RUNWAY WIDTH

A

45M

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7
Q

MAX CROSSWIND TAKEOFF AND LANDING

A

38KT (GUSTS INCLUDED)

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8
Q

MAX TAILWIND TAKEOFF

A

10KT

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9
Q

MAX TAILWIND LANDING

A

10KT

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10
Q

MAX WIND FOR PASSENGER DOOR OPERATION

A

65KT

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11
Q

MAX WIND FOR FWD AND AFT CARGO DOOR OPERATION

A
  • 40KT

- 50KT IF THE AIRCRAFT’S NOSE IS INTO WIND OR IF THE FWD AND AFT CARGO DOORS ARE ON THE LEEWARD SIDE

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12
Q

WHEN MUST THE FWD AND AFT CARGO DOORS BE CLOSED BY

A

BEFORE WIND SPEED EXCEEDS 65KT

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13
Q

COCKPIT WINDOW OPEN MAX SPEED

A

200KT

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14
Q

MAX FLAP/SLAT SPEEDS

A 
1 - 230KT
1+F - 215KT
2 - 200KT
3 - 185KT
FULL - 177KT
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15
Q

VMO

A

350KT

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16
Q

MMO

A

0.82M

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17
Q

VLE

A

280/0.67M

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18
Q

VLO(ext)

A

250KT/0.60M

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19
Q

VLO(ret)

A

220KT/0.54M

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20
Q

MAX TIRE SPEED

A

195KT (GROUND SPEED)

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21
Q

VMCL

A

109KT

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22
Q

VMCG

A

ROUGHLY 110KT

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23
Q

MAX TAXI SPEED LIMITATION

A

WHEN > 76T = MAX 20KT DURING A TURN

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24
Q

MAX WIPER OPERATING SPEED

A

230KT

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25
Q

MRW

A

77.4T

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26
Q

MTOW

A

77.0T

27
Q

MLW

A

64.5T

28
Q

MZFW

A

61.0T

29
Q

MINIMUM WEIGHT

A

37.23T

30
Q

IS THE AIRCRAFT PERMITTED TO LAND ABOVE MLW

A

IN EXCEPTIONAL CIRCUMSTANCES (IN FLIGHT TURN BACK OR DIVERSION), AN IMMEDIATE LANDING AT WEIGHT ABOVE MLW IS PERMITTED, PROVIDED THE PILOT FOLLOWS THE OVERWEIGHT LANDING PROCEDURE

31
Q

APU BLEED USE WITH HP AIR START UNIT

A

DO NOT USE BLEED AIR FROM THE APU BLEED AND HP AIR START UNIT AT THE SAME TIME, TO PREVENT AN ADVERSE EFFECT ON THE BLEED AI SYSTEM

32
Q

AVIONICS VENTILATION

A

DURING GROUND OPERATION, THE FLIGHT CREW MUST LIMIT THE TIME THAT THE AIRCRAFT ELECTRICAL POWER SUPPLY IS USED, IN NORMAL AVIAONICS VENTIALTION SYSTEM CONFIGURATION AS FOLLOWS:

  • OAT =/< 49 = NO LIMIT
  • 49 < OAT =/< 55 = 2H
  • 55 < OAT =/< 60 = 1H
  • 60 < OAT =/< 64 = 0.5H
33
Q

MAX CABIN DIFFERENTIAL PRESSURE

A

+9.0 psi

34
Q

MAX NEGATIVE CABIN DIFFERENTIAL

A

-1.0 psi

35
Q

SAFETY RELIEF VALVE SETTING

A

+8.6 psi

36
Q

PACKS USE WITH LP AIR CONDITIONING UNIT

A

FLIGHT CREW MUST NOT USE CONDITIONED AIR FROM THE PACKS AND FROM THE LP AC UNIT AT THE SAME TIME, TO PREVENT ANY ADVERSE EFFECT ON THE AC SYSTEM

37
Q

AP MIN USE HEIGHTS

A
  • AT TAKEOFF - 100’ AND AT LEAST 5S AFTER LIFTOFF
  • MANUAL GO AROUND - 100’
  • ILS WITH CAT 1 DISPLAYED ON FMA - 160’
  • IN APP WITH FINAL APP/ VS/ FPA - 250’
  • CIRCLING APPROACH - 500’
  • IN ALL OTHER PHASES - 500’
    THE AP OR FD IN OP DES OR DES MODE CAN BE USED IN APPROACH. HJOWEVER, ITS USE IS ONLY PERMITTED IF THE FCU ALTITUDE IS SET TO, OR ABOVE, THE HIGHER OF THE TWO:
    • MDA/MDH; OR
    • 500’ AGL
38
Q

APU START LIMITATION

A

AFTER 3 CONSECUTIVE START ATTEMPTS, THE FLIGHT CREW MUST WAIT 60 MIN BEFORE A NEW START ATTEMPT

39
Q

APU MAX ROTOR SPEED

A

107%

40
Q

APU EGT LIMITS (V SERIES AND YUD)

A 
V:
    - RUNNING (5S CONFIRMATION FOR SHUTDOWN) = 682
    - RUNNING (IMMEDIATE SHUTDOWN) = 700 TO 742
    - START (<25,000') = 900
    - START (>25,000') = 982 
YUD:
    - RUNNING = 675
    - START (<35,000') = 1090
    - START (>35,000') = 1120
41
Q

APU START/SHUTDOWN DURING REFUELING/DEFUELING

A

DURING REFUELING/DEFUELING, APU STARTS OR HSUTDOWN ARE PERMITTED PROVIDED:

- IF APU FAILED TO START OR AUTOMATIC SHUTDOWN = DO NOT START APU
- IF FUEL SPILL - PERFORM A NORMAL APU SHUTDOWN
42
Q

APU OPERATIONAL ENVIRONMENT (ELEC AND BLEED/ ELEC ONLY/ ELEC EMER CONFIG START)

A
  • ELEC EMER CONFIG ( BATT RESTART LIMIT) = 25,000’
  • ELEC AND BLEED: (ELEC ONLY ABOVE THESE VALUES)
    • YUD = 22,500’
    • V = 20,000’
43
Q

APU MAX ALTITUDE TO ASSIST ENGINE START

A

20,000’

44
Q

APU MAX ALTITUDE FOR PRESSURISATION

A 
SINGLE PACK:
    - V = 20,000'
    - YUD = 22,500'
DUAL PACK:
    - 15,000'
45
Q

WHAT LIMITATION EXISTS FOR THE APU BLEED USE

A

USE OF APU BLEED AIR FOR WING ANTI-ICE IN NOT PERMITTED

46
Q

ENGINE THRUST/ TIME/ EGT LIMITS

A
  • TOGA:
    • AEO = 5 MINS AT 635
    • SEO = 10 MINS AT 635
  • MCT = NO TIME LIMIT AT 610
  • STARTING (ON GROUND OR IN FLIGHT) = NO TIME LIMIT AT 635
47
Q

MAX N1/N2

A

100%

48
Q

ENGINE OIL LIMITATIONS (TEMP/ PRESSURE/ QUANTITY)

A 
TEMPS:
- MIN OIL TEMP BEFORE START = -40
- MIN OIL TEMP BEFORE ABOVE IDLE = -10
- MIN OIL TEMP BEFORE TAKEOFF = +50
- MAX OIL TEMP CONTINOUS = +155
- MAX OIL TEMP 15 MIN TRANSIENT = +165
PRESSURE:
- MINIMUM OIL PRESSURE = 60 psi
QTY:
- 11qt + 0.3qt/h of operation
49
Q

ENGINE STARTER LIMITATIONS

A
  • STANDARD AUTOMATIC START THAT INCLUDE ONLY 1 START ATTEMPT IS CONSIDERED 1 CYCLE
  • FOR MANUAL START 2 MINS MAX CYCLE
  • FOR CRANK 5 MIN MAX CYCLE
  • FOR GROUND STARTS (AUTO/MANUAL) 15s PAUSE BETWEEN SUCCESSIVE CYCLES
  • 30 MIN COOLING PERIOD IS REQUIRED, SUBSEQUENT TO 3 FAILED CYCLES OR 5 MINS OF CONTINOUS CRANKING
  • STARTER MUST NOT BE ENGAGED IF N2:
    • > 18% IN FLIGHT
    • > 10% ON GROUND
50
Q

REVERSE THRUST LIMITATIONS

A
  • PROHIBITED IN FLIGHT
  • BACKING AIRCRAFT WITH REVERSE IS PROHIBITED
  • MAX REV SHOULD NOT BE USED BELOIW 70KT. IDLE REV IS PERMITTED TO AC STOP
51
Q

REDUCED THRUST TAKEOFF (FLEX)

A
  • NOT PERMITTED ON CONTAM,INATED RUNWAY
  • TFLEX CANNOT BE:
    • > TFLEX MAX (ISA + 55/72)
    • < TREF
    • < OAT
52
Q

ENGINE START CROSSWIND LIMITATION

A

35KT

53
Q

MAX ALTITUDE WITH FLAP/SLATS EXTENDED

A

20,000’

54
Q

MIN AND MAX FUEL TEMPERATURE (JET A1)

A
  • MIN = -43

- MAX = +54

55
Q

MAX FUEL IMBALANCE AT TAKEOFF

A
  • INNER TANKS (OUTER TANKS BALANCED)
    • HEAVIER TANKS SIDE:
      • FULL = 500KG
      • 3000KG = 1050KG
      • 1450KG = 1450KG
  • OUTER TANKS (INNER TANKS BALANCED)
    - 370KG
56
Q

MAX FUEL IMBALANCE IN FLIGHT AND LANDING

A
  • INNER TANKS (OUTER TANKS BALANCED)
    • HEAVIER TANK SIDE:
      • FULL = 1500KG
      • 4300KG = 1600KG
      • 2250KG = 2250KG
  • OUTER TANKS (INNER TANKS BALANCED)
    • 690KG (1 FULL/ 1 EMPTY)
      only if:
    • LEFT SIDE = RIGHT SIDE; OR,
    • INNER TANK OF THE LIGHTER OUTER TANKS SIDE IS HEAVIER THAN THE OPPOSITE INNER TANK BY UP TO 3,000KG
      IN EXCEPTIONAL CIRCUMSTANCES (I.E FUEL SYSTEM FAILURE) THE ABOVE-MENTIONED VALUES FOR MAX FUEL IMBALANCE MAY BE EXCEEDED WITHOUT SIGNIFICANT EFFECT TO THE AC HANDLING QUALATIES
57
Q

MINIMUM FUEL QTY FOR TAKEOFF

A

1,500KG

58
Q

DEFINITION OF ICING CONDITIONS

A

WHEN:

- OAT (ON GROUND OR AFTER TAKEOFF) OR TAT (IN FLIGHT) IS =/< +10 AND VISIBLE MOISTURE IN ANY FORM IS PRESENT (1,600M FOG)
- OAT ON GROUND AND FOR TAKEOFF IS =/< +10 AND OPERATING ON RAMPS, TAXIWAYS OR RUNWAYS WHERE SURFACE SNOW, STANDING WATER OR SLUUSH MAY BE INGESTED BY THE ENGINES, OR FREEZE ON ENGINES, NACELLES OR ENGINE SENSOR PROBES
59
Q

DEFINITION OF SEVERE ICE ACCRETION

A

5MM OF ICE ACCRETION

60
Q

RAIN REPELLENT

A

ONLY USE IN CASE OF MODERATE TO HEAVY RAIN

61
Q

MAX BRAKE TEMPERATURE FOR TAKEOFF

A

300

62
Q

MAX NWS ANGLE

A

+/- 85

63
Q

TAXI WITH DEFLATED OR DAMAGED TIRES

A
  • IF MAX 1 TIRE PER GEAR IS DEFLATED (CONSIDER ALL 3 GEAR) = MAX TURN = 7KT
  • IF 2 TIRES DEFLATED ON SAME MAIN GEAR (MAX 1 GEAR) = MAX TAXI = 3KT
  • NWS ANGLE = 30
64
Q

MINIMUM FLIGHT CREW OXYGEN PRESSURE COVERS WHAT

A
  • PREFLIGHT CHECKS
  • USE OF OXY WHEN 1 FC MEMBER IN FLIGHT DECK
  • UNUSABLE
  • NORMAL SYSTEM LEAKAGE
  • PROTECTION AGAINST THE MOST DEMANDING OF:
    • DEPRESS IN NORM:
      • EMER DESCENT FOR ALL CREW AND OBS 13MINS
      • CRUISE AT FL100 FOR 2 FC FOR 103MINS
    • SMOKE WITH 100%:
      • ALL FC AND OBS 15MINS AT CABIN ALT 8,000’

A320 (5 decks)

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