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a320 limitations, memory items, proficiency items copy > A320 Limitations > Flashcards

A320 Limitations Flashcards

1
Q

319, 320, 321 Wingspan

A

111 ft. 10 in.

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2
Q

320 Sharklet, 321 Sharklet Wingspan

A

117 ft. 5 in.

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3
Q

319 Tailstrike Pitch Attitude

A

13.9 Compressed

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4
Q

A320 (IAE and NEO) Tailstrike Pitch Attitude

A

11.7 Compressed

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5
Q

A321 Tailstrike Pitch Attitudes

A

9.7 Compressed

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6
Q

Max certified altitude

A

FL398

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7
Q

Runway slope

A

+- 2%

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8
Q

Max runway altitude

A

9,200 ft

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9
Q

Nominal runway width

A

148 ft (45 meters)

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10
Q

Max demonstrated crosswind takeoff AND landing (dry runway)

A

38 kts (gust included)

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11
Q

Max tailwind for takeoff

A

15 kts

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12
Q

Max tailwind for landing

A

10 kts

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13
Q

Max wind for passenger door operation

A

65 kts

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14
Q

Max with landing gear extended - Vle

A

280 kts/M.67

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15
Q

Max landing gear extension (Vlo Extension)

A

250 kts/M.60

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16
Q

Max landing gear retraction (Vlo Retraction)

A

220 kts/M.54

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17
Q

Max altitude gear may be extended

A

25,000 ft

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18
Q

Max speed for windshield wiper use

A

230 kts

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19
Q

ONLY the A320/A321; when taxi weight is higher than___________, do not exceed a taxi speed of ____ kts during a turn.

A

167,550 lbs, 20 kts

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20
Q

A319 Landing Weight

A

137,788 lbs

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21
Q

A320 Landing Weight

A

145,505 lbs

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22
Q

A320 Landing Weight (NEO)

A

148,591 lbs

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23
Q

A321 Landing Weight CEO

A

171,519 lbs

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24
Q

APU Bleed Use with Air Start Unit

A

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent any adverse effect on the Bleed Air System.

25
Q

Max positive pressure differential

A

9.0 psi

26
Q

Max negative differential pressure

A

-1.0 psi

27
Q

PACKS use with LP Air Conditioning Unit

A

The Flight Crew must not use conditioned air from the PACKS and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning system.

28
Q

Min height for AP use for take off

A

100 ft AGL and 5s after TO

29
Q

Minimum height for AP use for circling approach

A

600 AGL

30
Q

Minimum height for AP use on ILS when CAT 1 displayed on FMA

A

160 ft AGL

31
Q

Minimum height for use of AP or FD engagement on Go-Around

A

100 ft AGL

32
Q

Minimum height for AP for all other phases

A

500 ft AGL (A319/A320)

900 ft AGL (A321)

33
Q

Use of AP or FD in OPEN DES or DES is not permitted in approach unless the FCU altitude is set at or above

A

Highest of:
Minimums or 500 ft AGL (A319/A320)
Minimums or 900 ft AGL (A321)

34
Q

NAV mode may be used in terminal area if

A
  1. GPS primary is available, or
  2. HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
  3. FMS navigation is cross-checked with navaid raw data.
35
Q

If one engine is inop on 319/321, you cannot use AP to perform non precision approaches in the following modes.

A

FINAL APP, NAV V/S, NAV/FPA.

Only FD use is permitted.

36
Q

APU starter limits

A

3 consecutive start attempts then 60 min cool down.

37
Q

EGT limit for Takeoff or GA (319 and 320 Classic)

A

635 C for 5 min, 10 min if engine failure

38
Q

EGT limit for MCT (319, 320 Classic, 321)

A

610 C, Unlimited time

39
Q

EGT limit for start, ground or flight (319, 320 Classic, 321)

A

635 C

40
Q

EGT limit for Takeoff or GA (A321)

A

650 C for 5 min, 10 min if engine failure

41
Q

EGT limit for Takeoff or GA (NEO)

A

1083 C for 5 min, 10 min if engine failure

42
Q

EGT limit for start, ground or flight (320 NEO)

A

1083 C

43
Q

EGT limit for MCT (NEO)

A

1043 C, Unlimited time

44
Q

Minimum oil temp for engine start (IAE)

A

-40 C

45
Q

Minimum oil temp prior to exceeding idle (IAE)

A

-10 C

46
Q

Minimum oil pressure (NEO)

A

65 PSI

47
Q

Starter Limitations (IAE)

A
  • 1 auto start attempt = 1 cycle
  • Ground starts (auto or manual) 15 seconds between cycles
  • 3 failed cycles or 5 min of continuous cranking: 30 minutes cool
  • For manual start, observe a 2 minute max cycle time
  • For crank, observe a 5 min. max cycle time
  • Starter must not run when N2 above 10% on ground, or 18% in flight
48
Q

Starter Limitations (NEO)

A
  • 2 auto start attempts = 1 cycle
  • Ground starts (auto or manual ) 35 seconds between each cycle.
  • 3 failed cycles or 15 minutes of consecutive or cumulative cranking; 15 minute cooling period
  • Starter must not run when N2 is above 20%.
49
Q
  • Max reverse thrust should not be used below…

- Idle reverse permitted down to…

A
  • 70 kts

- Aircraft stop

50
Q

Flex T/O is not permitted on (IAE and NEO)

A

Contaminated runways

51
Q

Engine Start Crosswind Limit

A

35 kts

52
Q

Max Altitude with Slats/Flaps extended is

A

20,000 ft.

53
Q

Jet A only, if TAT reaches ____, monitor on Fuel SD page that fuel temperature remains higher than _____.

A

-34C, -36C

54
Q

Max INNER tank fuel imbalance at TAKEOFF (319, 320)

A

If heavier tank FULL, then 1102 lbs.

55
Q

Max INNER tank fuel imbalance IN-FLIGHT and LANDING (319, 320)

A

If heavier tank FULL, then 3306 lbs.

56
Q

Max WING tank fuel imbalance at TAKEOFF (321 Sharklet)

A

If heavier tank FULL, then 882 lbs.

57
Q

Max brake temp for takeoff (brake fans off)

A

300 C

58
Q

321 Neo Max Landing Weight

A

174,606

59
Q

Min Height for AP in approach with F-G/S, FINAL APP, V/S, or FPA mode

A

250 AGL

a320 limitations, memory items, proficiency items copy (3 decks)

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