Limit Flash Cards

1
Q

Cabin Pressure: Max Positive Differential*

A

9.0 psi

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2
Q

Thrust Setting/EGT Limits

(A319; 502-536, A320; 601-653)*

A

Takeoff & Go-Around - 635°C for 5 min (10 min in case of engine failure)

MCT - 610°C

Starting - 635°C

Takeoff: Includes TOGA, FLEX, and DERATE (if installed) thrust modes.

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3
Q

NAV Mode May be Used in the Terminal Area Provided:*

A
  1. GPS Primary available, or
  2. High Accuracy displayed & appropriate RNP checked or entered on MCDU, or
  3. FMS navigation cross-checked with navaid raw data
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4
Q

Tail Numbers for:

A320 / Non Sharklet

A

601 - 617

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5
Q

Maximum Allowed Wing Fuel Imbalance

A321; 588

A

Flt / Landing

Full* / 2,910 lb

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6
Q

Max Landing:

901 - 905

A

148,591 lbs*

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7
Q

Max Wind Conditions for ILS CAT II or CAT III

A319 (502 - 536)

CONF FULL w/airport elevation > 5,700 ft:

A
  1. Headwind 20 kts (15 kt with One Engine Inoperative (OEI))
  2. Tailwind 5 kts*
  3. Crosswind 15 kts* (10 kts with One Engine Inoperative (OEI))
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8
Q

Tail Numbers for:

A320 / “Jet Pump” Fuel System

A

629 - 653

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9
Q

Autopilot - Min Height for Use*:

Use of AP or FD in Open DES or DES Mode Not Permitted in Appr. Unless the FCU altitude is set at or above

A

Highest of:

  1. Min or 500 ft AGL (A319/A320)
  2. Min or 900 ft AGL (A321)
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10
Q

Cabin Pressure:

Max Negative Differential*

A

-1.0 psi

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11
Q

Max Tailwind for Landing*

A

10 kts

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12
Q

Autopilot - Min Height for Use*:

All Other Phases

A
  1. 500 ft AGL (A319/A320)
  2. 900 ft AGL (A321)
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13
Q

Wingspan:

A319 / A320 / A321

A

111 ft, 10 inches

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14
Q

Tail Numbers for:

A321 Sharklet

A

657 - 687

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15
Q

Maximum Allowed Wing Fuel Imbalance

A320; 618 - 653, A320; 901 - 905*

A

Takeoff

  • Full* / 1,102 lb

Landing

  • Full* / 3,306 lb
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16
Q

Max Landing:

601 - 653

A

145,505 lbs*

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17
Q

Reduced Thrust Takeoff*

A

Not Permitted on contaminated runways

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18
Q

Max Landing Gear Retraction (VLO Ret)

A

220 kts / M.54

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19
Q

APU with HP Gound Unit*

A

Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage

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20
Q

Maximum Allowed Wing Fuel Imbalance

A321; 657 - 687

A

Takeoff

  • Full* / 882 lb
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21
Q

Max Demonstrated Crosswind at Landing*

A

38 kts (gust included)

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22
Q

Max Runway Altitude*

A

9,200 ft

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23
Q

Nominal Runway Width*

A

45 m (148 ft)

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24
Q

Autopilot - Min Height for Use*:

Go-around (AD or FD Engagement)

A

100 ft AGL

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25
Q

Starter

(NEO; 901 - 905)*

A
  1. One Cycle - Standard automatic start that includes up to 3 start attempts
  2. 35 sec pause between each cycle (on ground)
  3. 15 min cooling after 3 failed cycles or 15 min of continuous or cumulated cranking
  4. Starter must not be run when N2 >20%
26
Q

Thrust Setting/EGT Limits

( A320; 901-905)*

A
  1. Takeoff & Go-Around - 1,083°C for 5 min (10 min in case of engine failure)
  2. MCT - 1,043°C
  3. Starting - 1,018°C

Takeoff: Includes TOGA, FLEX, and DERATE (if installed) thrust modes.

27
Q

Autopilot - Min Height for Use*:

Straight in Non Precision Approach

A

Applicable Minimun

28
Q

Max Crosswind for Starting Engine*

A

35 kts (NEOs)

29
Q

Max Certified Crosswind for Takeoff*

A

35 kts (gust included)

30
Q

Max Wind for Passenger Door Operation*

A

65 kts

31
Q

Max Wind Conditions for ILS CAT II or CAT III

A319 (502 - 536)

CONF FULL w/airport elevation ≤ 5,700 ft:

A
  1. Headwind 20 kts (15 kt with One Engine Inoperative (OEI))
  2. Tailwind 10 kts
  3. Crosswind 15 kts* (10 kts with One Engine Inoperative (OEI))
32
Q

Reverse Thrust

A

Max should not be used < 70 kt*

Idle permitted down to stop (Not A321)*

33
Q

Wingspan: A320 Sharklet / A321 Sharklet

A

117 ft, 5 inches

34
Q

Minimum Oil Pressure*

A

65 psi

35
Q

Thrust Setting/EGT Limits

(A321; 588, 657-687)*

A
  1. Takeoff & Go-Around - 650°C for 5 min (10 min in case of engine failure)
  2. MCT - 610°C
  3. Starting - 635°C

Takeoff: Includes TOGA, FLEX, and DERATE (if installed) thrust modes.

36
Q

Starter

(502 - 687)*

A
  1. One Cycle - Standard automatic start that includes only one start attempt
  2. 15 sec pause between each cycle (on ground)
  3. 30 min cooling after 3 starts or 5 min continuous cranking
  4. Manual Start - 2 minute max cycle time
  5. Crank - 5 minute max cycle time
  6. Starter - not be run when N2 >10% on ground & 18% in flight
37
Q

Max w/Landing Gear Extended (VLE)

A

280 kts / M.67

38
Q

Max Landing Gear Extension (VLO Ext)

A

250 kts / M.60

39
Q

Max Tailwind for Takeoff*

A

15 kts

40
Q

Max Taxi Speed (All But A319)*

A

Taxi weight > 167,550 lbs, do not exceed 20 kts in turn

41
Q

Max Wind Conditions for ILS CAT II or CAT III

A321

A
  1. Headwind 40 kt CAT II / 30 kt CAT III
  2. Tailwind 10 kt
  3. Crosswind 15 kt*
42
Q

Max Brake Temp for Takeoff

(Fans Off, if Installed)*

A

300°C

43
Q

Tail Numbers for:

A321 / Non Sharklet

A

588

44
Q

Tail Numbers for: A319

A

502 - 536

45
Q

Max Landing:

502 - 536

A

137,788 lbs*

46
Q

Tail Numbers for:

A320 / NEO

A

901 - 905

47
Q

Max Operating Altitude

w/Slats and/or Flaps Extended*

A

20,000 ft

48
Q

Tail Numbers for:

A320 / Sharklet

A

618 - 653

49
Q

Packs Use With LP Air Conditioning Unit*

A

Do not use conditioned air from the packs and the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

50
Q

Non-Precision Approaches with Engine Out*

(A319/A321; 502 - 588, 657 - 687)

A

If one engine inop., it is not permitted to use the autopilot to perform NPA’s in the following modes:

Final APP

NAV V/S

NAV / FPA

Only FD use is permitted

51
Q

Autopilot - Min Height for Use*:

ILS Appr. When Cat 2 or 3 is not displayed on FMA

A

160 ft AGL

52
Q

Max Wind Conditions for ILS CAT II or CAT III

NEOs

A
  1. Headwind 20 kt
  2. Tailwind 5 kt*
  3. Crosswind 15 kt*
53
Q

Autopilot - Min Height for Use*:

Circling Approach

A

Applicable Circling Mins Minus 100 ft

54
Q

Oil Temperature (All but NEOs)

  1. Minimum starting temperature*
  2. Minimum prior to exceeding idle*
A
  1. Minimum starting temperature: -40°C
  2. Minimum prior to exceeding idle: -10°C
55
Q

Autopilot - Min Height for Use*:

Takeoff with SRS Mode

A

100 ft AGL

56
Q

Runway Slope (mean)*

A

+/-2%

57
Q

APU Starter*

A

3 consecutive start attempts

60 min before attempting a new start attempt

58
Q

Max Altitude Landing Gear Extended

A

25,000 ft

59
Q

Fuel Temperature*

A

For JET A only, if TAT reaches -34°C, monitor on FUEL SD pg that fuel temperature remains > -36 °C.

60
Q

Max Landing:

588; 657 - 687

A

171,519 lbs*