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A320 Spirit > Limitations > Flashcards

Limitations Flashcards

1
Q

Max landing gear extension speed (VLO Extension)

A

250 knots/M.60

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2
Q

Max Taxi Speed (A320 CEO)

A

Takeoff weight higher than 167,550 lbs: 20 knots in a turn

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3
Q

A319 Max Landing Weight

A

137,788 lbs

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4
Q

A320-NEO Max Landing Weight

A

148,591 lbs

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5
Q

A321-S Max Landing Weight

A

171,519 lbs

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6
Q

Min Height for AP - All Other Phases

A

500 ft AGL (A319/A320)
900 ft AGL (A321)

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7
Q

A319/A321: If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes:

A

FINAL APP
NAV V/S
NAV/FPA
* Only FD use is permitted.

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8
Q

EGT Limit for MCT (NEO)

A

1043 C

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9
Q

Minimum Oil Temperature Before Takeoff (NEO)

A

52 C

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10
Q

Engine Starter (CEO)

A
  • A standard automatic start that includes only one start attempt is considered one cycle
  • For ground starts (automatic or manual), a 15 s pause is required between successive cycles
  • A 30 min cooling period is required, subsequent to three failed cycles or 5 min of continuous crank
  • For manual start, observe two-minute maximum cycle time
  • For crank, observe 5 min maximum cycle time
  • The starter must not be run when N2 is above 10% on-ground and 18% in-flight
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11
Q

Engine Starter (NEO)

A
  • A standard automatic start that includes up to two start attempts, is considered one cycle
  • For ground starts (automatic or manual), a 35 s pause is required between successive cycles
  • A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulative crank
  • The starter must not be run when N2 is above 20%
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12
Q

Maximum Operating Speed Vmo Mmo

A

350 knots/M.82

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13
Q

A320-S Max Landing Weight

A

145,505 lbs

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14
Q

NAV mode may be used in the terminal area, provided:

A
  • GPS PRIMARY is available, or
  • The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or
  • FMS navigation is cross-checked with navaid raw data.
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15
Q

EGT Limit for Takeoff and Go-around (TOGA and FLEX) (A321)

A

650 C (5 min/10 min in case of engine failure)

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16
Q

Minimum Oil Temperature Before Takeoff (CEO)

A

50 C

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17
Q

Max Fuel Imbalance - Takeoff (A319/A320-all)

A

Inner tanks: (Heavier tank full) 1,102 lbs

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18
Q

Max Fuel Imbalance - In Flight and at Landing (A319/A320-all)

A

Inner tanks: (Heavier tank full) 3,306 lbs

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19
Q

Max Fuel Imbalance - Takeoff (A321-S)

A

Wing tanks: (Heavier tank full) 882 lbs

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20
Q

Max Altitude for APU Start on Battery Power

A

25,000 ft

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21
Q

Load Limits

A

Clean Configuration: -1.0g to +2.5g
Other Configuration: 0g to +2.0g

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22
Q

A319/A320 Wingspan

A

111 feet, 10 inches

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23
Q

A320-S/A321-S Wingspan

A

117 feet, 5 inches

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24
Q

A319 Tailstrike Pitch Attitude

A

L/G Struts Compressed: 13.9

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25
Q

A320 Tailstrike Pitch Attitude

A

L/G Struts Compressed: 11.7

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26
Q

A321 Tailstrike Pitch Attitude

A

L/G Struts Compressed: 9.7

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27
Q

Maximum Certified Altitude

A

FL398

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28
Q

Runway Slope

A

+/- 2%

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29
Q

Max Runway Altitude

A

9,200 ft

30
Q

Nominal Runway Width

A

45 m (148 ft)

31
Q

Minimum Runway Width

A

98 ft with “Operations on Narrow Runways” procedure

32
Q

Max Crosswind (takeoff and landing)

A

38 knots (gust included)

33
Q

Max Tailwind - Takeoff

A

15 knots

34
Q

Max Tailwind - Landing

A

10 knots

35
Q

Max Wind for PAX Door Operation

A

65 knots

36
Q

Cockpit Window Open Maximum Speed

A

200 knots

37
Q

Max landing gear retraction speed (VLO Retraction)

A

220 knots/M.54

38
Q

Max Tire Speed

A

195 knots GS

39
Q

Wipers Maximum Operating Speed

A

230 knots

39
Q

A320 Max Landing Weight

A

145,505 lbs

40
Q

A321-NEO Max Landing Weight

A

174,606 lbs

41
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.

42
Q

Max Positive Differential Pressure

A

9.0 PSI

43
Q

Max Negative Differential Pressure

A

-1.0 PSI

44
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.

45
Q

Min Height for AP - Takeoff with SRS Mode

A

100 ft AGL and at least 5 seconds after takeoff

46
Q

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

A

250 ft AGL

47
Q

Min Height for AP - Circling Approach

A

600 ft AGL

48
Q

Min Height for AP - ILS approach with CAT 1 displayed

A

160 ft AGL

49
Q

Min Height for AP - ILS approach with CAT 2 or 3 displayed

A

0 ft AGL if Autoland
80 ft AGL if no Autoland (Ops Specs C071)

50
Q

Min Height for AP - Manual Go-Around

A

100 ft AGL

51
Q

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

A

Highest of:

MDA/MDH or 500 ft (A319/A320)

MDA/MDH or 900 ft (A321)

52
Q

APU Starter Cycles

A

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.

53
Q

EGT Limit for Starting (CEO)

A

635 C

54
Q

EGT Limit for Starting (NEO)

A

1083 C

55
Q

EGT Limit for Takeoff and Go-around (TOGA and FLEX) (A319/A320-CEO)

A

635 C (5 min/10 min in case of engine failure)

56
Q

EGT Limit for Takeoff and Go-around (TOGA and FLEX) (NEO)

A

1083 C (5 min/10 min in case of engine failure)

57
Q

EGT Limit for MCT (CEO)

A

610 C

58
Q

Minimum Oil Temperature for Starting

A

-40 C

59
Q

Minimum Oil Temperature Before IDLE is exceeded (CEO)

A

-10 C

60
Q

Minimum Oil Pressure (CEO)

A

60 PSI

61
Q

Minimum Oil Pressure (NEO)

A

65 PSI

62
Q

Max Reverse Thrust should not be used below:

A

70 knots (Idle reverse is permitted down to aircraft stop.)

63
Q

FLEX takeoff is not permitted:

A

On contaminated runways.

64
Q

Max Crosswind for Engine Start

A

35 knots

65
Q

Max Altitude for Flaps and/or Slats

A

20,000 ft

66
Q

For JET A only, if TAT reaches _______, monitor on FUEL SD page that fuel temperature remains higher than _______.

A

-34 C/-36 C

67
Q

Max Brake Temp for Takeoff (brake fans off)

A

300 C

68
Q

Max Altitude for APU Start (on A/C power) and Operation

A

FL410

69
Q

Holding Speeds ICAO

A

Altitude Upper Speed Limit
Up to 14,000 ft 230 KIAS
14,000 ft - 20,000 ft 240 KIAS
20,000 ft - 34,000 ft 265 KIAS
Above 34,000 ft .83 Mach

70
Q

Holding Speeds FAA

A

Levels Normal
To 6,000’ inclusive 200 KIAS
Above 6,000’ to 14,000’ 230 KIAS
Above 14,000’ 265 KIAS

A320 Spirit (54 decks)

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