LIMITATIONS A319/320 Flashcards

1
Q

VOLOTEA Operative Weights 319

A
MTW: 66.400 kg   
MTOW*: 66.000 kg
MLW*: 61.000 kg / 62.500 kg
MZFW*: 57.000 kg / 58.500 kg
Min Weight: 35.400 kg
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2
Q

VOLOTEA Operative Weights 320

A
MTW: 77.400 kg / 78.400 kg  
MTOW*: 77.000 kg / 78.000 kg
MLW*: 64.500 kg
MZFW*: 61.000 kg
Min Weight: 37.230 kg
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3
Q

Vmo/Mmo

A

350 KIAS (<24.000´) / 0.82

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4
Q

VMCL / VMCA- / VMCG- (319)

A

111kts* / 110kts-* / 108kts-*(RWY 35M:+1.5, 30M:+2.5)

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5
Q

VMCL / VMCA- / VMCG- (320)

A

113kts* / 112kts-* / 112kts-*(RWY 35M:+1.5, 30M:+2.5)

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6
Q

Max Speeds/ALT Flaps/Slats

A
1 -> 230 
1+F -> 215 
2 -> 200 
3 -> 185 
FULL -> 177
Max ALT -> 20.000 ft
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7
Q

Max Speeds Landing Gear Extended

A

VLE - Extended -> 280 / M0.67
VLO - Extension -> 250 / M0.60
VLO - Retraction -> 220 / M0.54

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8
Q

Max Spd Cockpit Window Open

A

200 kts

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9
Q

Max Tire Speed

A

195 kts

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10
Q

Max Wiper Operating Speed

A

230 kts

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11
Q

Severe Turb Speed

A

> FL200/330: 275 KIAS/ .76 M

FL200 and below : 250 KIAS

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12
Q

Max Pressure Altitude /

For Take-Off and Landing

A
  1. 800 ft

- 2000* / 9200 ft*

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13
Q

Max Differential Pressure /

Max Safety Relief

A
  • 1.0/9.0psi

8. 6 psi

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14
Q

Maneuvering Load Limits /

Flaps/Slats extended

A
  • 1.0/+2.5g

0. 0/+2.0g

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15
Q

Temperature Limits TO/LDG

A

-40ºC*/+55ºC

Reducing to -52º/+38 ºC at 9200 ft

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16
Q

Temperature Limits FL398

A

-70ºC/-29ºC

~ Linearly from 0 ft

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17
Q

Max Runway Slope /

Min Runway Width

A

+/-2.0%

30m/ 45m (320)

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18
Q

Max Cross-wind DRY Runway

A

38 kts (26kt <45m)

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19
Q

Max Cross-wind Good - Medium - Poor

Rwy<45m

A

38 -(29)- 25 -(20)- 15

20 -(10)- 10 -(10)- N/A

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20
Q

Max Tailwind Component

A

10 kts (15kts)*

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21
Q

Max Wind Pax Door Operation /

Max Wind Cargo Doors

A
65 kts
40 kts (50 kts)
50 kts if the nose into the wind or cargo doors on the leeward side
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22
Q

Required Fire Fighting Category

A

RFF 6
ALTN: RFF4
RFF 4/5 may be accepted in certain conditions ref OM-A.8.1.2.G

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23
Q

Max Brake Temperature T/O

A

300º C

150º C (Brake fan ON)

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24
Q

ENG LIMITS TO/GA

A
Time Limit (Max) -> 5 min (10min OEI) 
Max TGT -> 950
OIL PRESS (Min/Max) -> 13 – 90 (~N2) 
OIL TEMP (Min/Max) -> -10 / 155
Max N1 / N2 -> 104 / 105
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25
Q

ENG LIMITS MCT

A
Time Limit (Max) -> NONE
Max TGT -> 915
OIL PRESS (Min/Max) -> 13 – 90 (~N2) 
OIL TEMP (Min/Max) -> 140
Max N1 / N2 -> 104 / 105
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26
Q

ENG LIMITS STARTING/ TRANSIENT

A
Time Limit (Max) -> N/A
Max TGT -> 725
OIL PRESS (Min/Max) -> - 
OIL TEMP (Min/Max) -> -40 / 155
Max N1 / N2 -> N/A
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27
Q

ENG Starter Duty Cycle

A

: 1 Standard automatic start cycle, includes up to 3 attempts.
: For ground starts, a 20 sec pause is required between cycles.
: 15 minutes cooling time, subsequent to 4 failed cycles.
: The starter must not be run when N2 is above 20%.

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28
Q

Fuel Temp Limits (JET A1/JP8/No3)*

A

-43 ºC / + 54 ºC

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29
Q

Minimum Fuel QTY for T/O

A

1.500 kg

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30
Q

LO LVL Warning ECAM

A

<750 kg 1 wingtank

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31
Q

Advisory imbalance (phs 2/6)

A

> 1500 kg difference

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32
Q

Total Fuel

A

18.729 kg* (Fuel density 0.785)

Outer Tanks : 691 kg x2
Inner Tanks : 5.435 kg x2*
Center Tank : 6.476 kg

33
Q

Check OXYGEN PRESS tables*

A

< 800 PSI 2CM,
< 1100 PSI 2CM+OBS,
< 1400 PSI 2CM+2OBS

34
Q

DO NOT PULL CB

A

SFCC, ECU/EEC, EIU

35
Q

Max VOLOTEA Taxi Speed

A

30 kts / 50 kts on the RWY

With TOM >76T -> 20 kts

36
Q

Min Taxi Strip for 180º Turn

A

20.5/ 22.8 m

37
Q

Max NWS angle

A
  • Taxi: 75º (30º tires deflated)
  • Towbarless: 85º
  • Towbar: 95º
38
Q

Wingspan

A

34.1 m

39
Q

Lenght

A

33.84 / 37.57 m

40
Q

Wheelbase

A

7,59 m

41
Q

Tailspan

A

12.45 m

42
Q

Height

A

11,75 m

43
Q

APU Limitations

A
  • NO APU BLEED together with HP ASU
  • Use of APU Bleed air for Wing Anti-ice is NOT permitted
  • During refueling/defuel allowed to start or shutdown, but not after start failure or auto shutdown.
  • Starting 3 attempts, then 60 min.
  • Max EGT running : 675 ºC*
  • Max Rotor (N) Speed : 107%
  • Max EGT for start
44
Q

Autoland Limitations

A
  • Headwind 20 kts/ 30kts (320)
  • Crosswind 20 kts
  • Tailwind 10 kts
    OEI A319: 15/ 10/ 10 - 5kts with CONF3 or ELEV>5750ft
  • A/THR must be used in selected or managed speed
  • At least 1 AP in APPR mode for CAT2 and CAT3 SINGLE, both for CAT3 DUAL
  • OEI CAT2/CAT3 SINGLE, if procedures completed before 1000 ft.
  • Depending on situation, provided runway approved for automatic ldg, allowed up to 69 t.*
  • Automatic roll-out using 1 thrust reverser, max winds 15/10/10(5)
  • Elevation < 9200 ft MSL*
  • Not allowed < -1000 ft pressure altitude
  • Glide Slope 2.5º - 3.15º
  • Runway Width minimum 45m
45
Q

Autopilot Limitations

A
  • > 100 ft AGL at T/O, and at least 5 sec after lift-off; or after manual Go-Around
  • > 160 ft AGL with ILS CAT1 on FMA
  • > 250 ft AGL in approach with FINAL APP, V/S or FPA mode
  • > 500 ft AGL in Circling approach and in all other phases.
  • With OEI, AP not permitted to perform NPA in: FINAL APP, NAV V/S, NAV/FPA. Only FD.
46
Q

Instrument Altimeter Tolerance

A

PFD 1 and 2 -> 20 ft
PFDs and ISIS -> 100 ft
PFDs and Mech.SBY -> 300 ft

47
Q

RVSM Altimeter Tolerance

A

PFD 1 or 2 -> 25 ft
PFDs and Apt ELEV -> 75 ft
In FLT PFD 1 and 2 -> 130 ft
General RVSM Requirement: Minimum of 2 Altimeters 200 ft

48
Q

Center of Gravity Limits

A

12-40 % / 13-45 % (320)

49
Q

Icing Conditions

A

OAT/TAT < 10 oC and Visible Moisture (clouds, fog <1sm, rain, snow, etc) or contamination on ramps, taxiways or runways.

50
Q

Severe Ice Accretion

A

when accumulation on the airframe aprox > 5mm

51
Q

Max Contamination

A

Runway is considered contaminated > 3 mm

  • Dry Snow: 100 mm
  • Wet Snow: 30mm
  • Slush/Water: 12,7 mm
52
Q

Maximum differential pressure to open ram air inlet

A

1 PSI

53
Q

Max continuous load per generator

A

100% (90KVA)

54
Q

Max TR load

A

200A

55
Q

CAT II ILS min DH and autopilot disconnect height

A

Min DH = 100 feet AGL (RA)

Min Autopilot disconnect height = 80 feet AGL

56
Q

Taxi with deflated tires speeds for one, two deflated same gear and NWS limit

A

1 = 7 kts
2 = 3 kts
NWS angle limit = 30 degrees

57
Q

Lo LVL OIL ECAM mesare for APU

A

APU can be started and run for 10 hours, maintenance action us required within this period

58
Q

Max alt for APU start on batteries only

A

25.000 feet

59
Q

APU one pack alt

A

22.500 feet

60
Q

APU two pack alt

A

15.000 feet

61
Q

Min engine oil qty

A

9.5 + 0.5 hour

62
Q

FLEX limitations

A

Not reduced by more than 25% of max THR. Max FLEX = ISA+55, must not be lower than actual OAT.
Do not use one contaminated runways.

63
Q

APU altitude limitations for
ground mode,
starts on bats only and
100% gen load

A

Ground mode = 14500ft
Starts on bats only = 25000ft
100% gen load = 30000ft

64
Q

Max APU altitude

A

41000ft

65
Q

Engine. No running engagement of starter

A

20% N1

66
Q

Max taxi speed

A

30kts on taxiways
50kts on runways
20kts weight above 76T and in turns

67
Q

Brakes temp limits requiring maintenance

A
  • Tem on same gear differ by more than 150º and one is more than 600º or less than 60º
  • The two gears differ by more than 200º
  • Fuse plug melted
  • Brake above 900º
68
Q

Max airflow from ground carts

A

1.2 kg/s

69
Q

Air from Packs and LP ground cart simultaneously

A

Forbidden to avoid chattering of non return valves

70
Q

APU bleed with HP ground air

A

Do NOT use HP ground air with APU Bleed to avoid bleed air system damage

71
Q

MAX cabin alt selection

A

14000ft

72
Q

Cabin ALT warning

A

9550ft

73
Q

MAX normal cabin ALT

A

8000ft

74
Q

MAX fuel imbalance at takeoff for inner tanks (outer tanks balanced)

A

500kg

75
Q

MAX fuel imbalance at takeoff for outer tanks (inner tanks balanced)

A

370kg

76
Q

MAX fuel imbalance in flight and landing for outer tanks (inner tanks balanced)

A

690kg

77
Q

ENG Vibration during flight

A

?

78
Q

ENG Vibration during start

A

?

79
Q

Hydraulics normal pressure

A

3000PSI +/- 200PSI