Limit Flash Cards

(60 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
_Starter_ (NEO; 901 - 905)\*
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
_Thrust Setting/EGT Limits_ ( A320; 901-905)\*
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
_Autopilot - Min Height for Use\*:_ Straight in Non Precision Approach
Applicable Minimun
28
Max Crosswind for Starting Engine\*
35 kts (NEOs)
29
Max Certified Crosswind for Takeoff\*
35 kts (gust included)
30
Max Wind for Passenger Door Operation\*
65 kts
31
_Max Wind Conditions for ILS CAT II or CAT III_ **A319 (502 - 536)** CONF FULL w/airport elevation ≤ 5,700 ft:
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
Reverse Thrust
Max should not be used \< 70 kt\* Idle permitted down to stop (Not A321)\*
33
Wingspan: A320 Sharklet / A321 Sharklet
117 ft, 5 inches
34
Minimum Oil Pressure\*
65 psi
35
_Thrust Setting/EGT Limits_ (A321; 588, 657-687)\*
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
_Starter_ (502 - 687)\*
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
Max w/Landing Gear Extended (VLE)
280 kts / M.67
38
Max Landing Gear Extension (VLO Ext)
250 kts / M.60
39
Max Tailwind for Takeoff\*
15 kts
40
Max Taxi Speed (All But A319)\*
Taxi weight \> **167,550 lbs,** do not exceed **20 kts** in turn
41
_Max Wind Conditions for ILS CAT II or CAT III_ A321
1. Headwind 40 kt CAT II / 30 kt CAT III 2. Tailwind 10 kt 3. **Crosswind 15 kt\***
42
_Max Brake Temp for Takeoff_ (Fans Off, if Installed)\*
300°C
43
_Tail Numbers for:_ A321 / Non Sharklet
588
44
Tail Numbers for: A319
502 - 536
45
_Max Landing:_ 502 - 536
137,788 lbs\*
46
_Tail Numbers for:_ A320 / NEO
901 - 905
47
_Max Operating Altitude_ w/Slats and/or Flaps Extended\*
20,000 ft
48
_Tail Numbers for:_ A320 / Sharklet
618 - 653
49
Packs Use With LP Air Conditioning Unit\*
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
_Non-Precision Approaches with Engine Out\*_ (A319/A321; 502 - 588, 657 - 687)
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
_Autopilot - Min Height for Use\*:_ ILS Appr. When Cat 2 or 3 is not displayed on FMA
160 ft AGL
52
_Max Wind Conditions for ILS CAT II or CAT III_ ## Footnote **NEOs**
1. Headwind 20 kt 2. **Tailwind 5 kt\*** 3. **Crosswind 15 kt\***
53
_Autopilot - Min Height for Use\*:_ Circling Approach
Applicable Circling Mins Minus 100 ft
54
_Oil Temperature (All but NEOs)_ 1. Minimum starting temperature\* 2. Minimum prior to exceeding idle\*
1. Minimum starting temperature: **-40°C** 2. Minimum prior to exceeding idle: **-10°C**
55
_Autopilot - Min Height for Use\*:_ Takeoff with SRS Mode
100 ft AGL
56
Runway Slope (mean)\*
+/-2%
57
APU Starter\*
**3** consecutive start attempts **60 min** before attempting a new start attempt
58
Max Altitude Landing Gear Extended
25,000 ft
59
Fuel Temperature\*
For JET A only, if **TAT reaches -34°C**, monitor on FUEL SD pg that fuel temperature remains **\> -36 °C**.
60
_Max Landing:_ 588; 657 - 687
171,519 lbs\*