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A320 Limitations > Limitations 2019 > Flashcards

Limitations 2019 Flashcards

1
Q

Wingspans A319,A320

A

111 feet, 10 inches

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2
Q

Wingspan A320 Sharklet and A321 Sharklet

A

117 Feet, 5 inches

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3
Q

Tailstrike A319 Strut Compressed

A

13.9 degrees

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4
Q

Tailstrike A320,A320 NEO strut compressed

A

11.7

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5
Q

Tailstrike A321 strut Compressed

A

9.7

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6
Q

Tailstrike A319 strut extended

A

15.5

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7
Q

Tailstrike A320 strut extended

A

13.5

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8
Q

Tailstrike A320 NEO strut extended

A

13.7

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9
Q

Tailstrike A321 strut extended

A

11.2

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10
Q

Maximum certified altitude

A

FL398

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11
Q

Runway slope (mean)

A

+/- 2%

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12
Q

Runway Altitude

A

9,200 feet

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13
Q

Normal runway width

A

45m (148 feet)

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14
Q

Maximum demonstrated crosswind (takeoff and landing)

A

38 knots (guest included)

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15
Q

Maximum tailwind for takeoff

A

15 knots

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16
Q

Maximum tailwind for landing

A

10 knots

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17
Q

Maximum wind for passenger door operation

A

65 knots

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18
Q

Cockpit window open max speed

A

200 knots

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19
Q

Maximum speed with landing gear extended (VLE)

A

280 knots / M.67

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20
Q

Maximum speed landing gear extension (VLO)

A

250 Knots / M.60

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21
Q

Maximum speed landing gear retraction (VLO retract)

A

220 Knots / M.54

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22
Q

Maximum altitude landing gear may be extended

A

25,000 feet

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23
Q

Maximum tire speed (ground speed)

A

195 knots

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24
Q

When the taxi weight is higher than 167,550 pounds (76,000kg) taxi speed should not exceed during a turn

A

20 knots

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25
Q

Wipers maximum operating speed

A

230 knots

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26
Q

Maximum landing weight A320 NEO

A

148,591 pounds

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27
Q

Maximum landing weight A320

A

145,505 pounds

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28
Q

Maximum landing weight A319

A

137,788 pounds

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29
Q

Maximum landing weight A321

A

171,519 pounds

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30
Q

APU bleed use with air start unit

A

APU bleed should not be used at the same time when using a HP air start unit.

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31
Q

Maximum cabin pressure positive differential pressure

A

9.0 PSI

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32
Q

Maximum cabin pressure negative differential pressure

A

-1.0 PSI

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33
Q

Cabin pressure safety relief valve pressure setting is

A

8.6 PSI

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34
Q

Pack 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.

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35
Q

Minimum hight Auto Pilot usage at takeoff with SRS

A

100 feet AGL

36
Q

Minimum hight Auto Pilot usage Straight-in non-precision approach

A

Applicable minimums

37
Q

Minimum hight Auto Pilot usage Circling Approach

A

Applicable circling minimums

-100 feet

38
Q

Minimum hight Auto Pilot usage ILS approach with CAT 2 or 3 is NOT displayed on the FMA

A

160 Feet AGL

39
Q

Minimum hight Auto Pilot usage at Go-Around (AP or FD engagement)

A

100 feet AGL

40
Q

Minimum hight Auto Pilot usage All other phases of flight

A

500 feet AGL (A319,A320)

900 feet AGL (A321)

41
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:
Minimum or 500 feet (A319,A320)
900 feet (A321)

42
Q

Takeoff with SRS mode

A

An internal FMGS logic prevents auto pilot from engaging during the 5 seconds after liftoff

43
Q

NAV mode maybe used in the terminal area provided that

A
  • GPS primary is available
  • The appropriate RNP is checked or entered on the MCDU, and high accuracy is displayed or
  • FMS navigation is cross checked with nav aid raw data
44
Q

If one engine is inoperative, it is NOT permitted to use the autopilot to perform non-precision approaches in the following modes

A

FINAL APP, NAV, V/S, NAV, FPA only FD use is permitted

45
Q

Honeywell APU Maximum altitude assisted engine start

A

20,000 feet

46
Q

Hamilton APU maximum altitude engine start

A

20,000 feet

47
Q

Hamilton APU maximum altitude air conditioning and pressurization single pack

A

20,000 feet

48
Q

Hamilton APU maximum altitude air conditioning and pressurization dual pack

A

15,000

49
Q

Is APU bleed air able to be used for wing anti ice

A

NO

50
Q

Honeywell APU maximum altitude air conditioning and pressurization single pack

A

22,500 feet

51
Q

Honeywell APU maximum altitude air conditioning and pressurization dual pack

A

15,000

52
Q

Power plant EGT limits for (502-656,690-694)

A319,A320

A

Takeoff go around All engines 5 min, EGT 635
Takeoff go around One engine 10 min, EGT 635
Takeoff go around MCT No limit EGT 610
Starting on ground 635
Starting in air 635

53
Q

Power plant EGT limits for (657-687) A321

A

Takeoff go around All engines 5 min, EGT 650
Takeoff go around One engine 10 min, EGT 650
Takeoff go around MCT No limit, EGT 610
Start on the ground 635
Start in flight 635

54
Q

Power plant EGT limits for (901-928) A320 NEO

A

Takeoff go around all engines 5 min, EGT 1083
Takeoff go around one engine 10 min, EGT 1083
Takeoff go around MCT no limit EGT 1043
Start on the ground 1083
Start in the air 1083

55
Q

Minimum oil temperature (N502NK-N698NK) (901-928)

A

-40 c

56
Q

Minimum oil temperature before IDLE (N502NK-N698NK)

A

-10 c

57
Q

Minimum oil temperature before takeoff (N502NK-N698NK)

A

50 c

58
Q

Max continuous oil temperature (502-698)

A

155 c

59
Q

Maximum transient oil temperature (502-698)

A

165 c

60
Q

Maximum oil pressure (502-698)

A

60 PSI

61
Q

Maximum continues oil temperature (901-928)

A

151 c

62
Q

Minimum oil temperature before takeoff (901-928)

A

52 c

63
Q

Minimum oil pressure (901-928)

A

65 PSI

64
Q

Maximum oil pressure (901-928)

A

270 PSI

65
Q

What is considered a engine start cycle for (502-698)

A

A standard automatic start that includes only one start attempt, is considered one cycle

66
Q

Starter limits (502-698)

A
  • For ground starts (automatic or manual), a 15 second pause is required between successive cycles
  • A 30 minute cooling period is required, subsequent to three failed cycles or 5 minutes of continuous crank
  • For manual start, observe a 2 minute maximum cycle time
  • For crank, observe a 5 minute maximum cycle time
  • The starter must not be run when N2 is above 10% on the ground and 18% inflight
67
Q

What is considered a engine start cycle for (901-928)

A

A standard automatic start that includes up to 2 start attempts, is considered one cycle

68
Q

Starter limits (901-928)

A
  • For ground start (automatic or manual) a 35 second pause is required between successive cycles
  • A 15 minute cooling period is required, subsequent to three failed cycles, or 15 minute of continuous or cumulative crank
  • Starter must not be run when N2 is above 20%
69
Q

When should max reverse thrust not be used

A

Below 70 knots, Idle reverse is permitted down to aircraft stop.

70
Q

Maximum altitude flaps/slats extended

A

20,000 feet

71
Q

Maximum fuel imbalance INFLIGHT and at LANDING Inner tanks (outer tanks balanced) Tank fuel quantity (heavier tank) (502-536 / 601-656 / 690-698 / 901-928)

A

3,306 pounds

72
Q

Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687)

A

882 pounds

73
Q

Minimum fuel quantity for TAKEOFF

A

3,307 pounds

74
Q

Maximum brake temperature for takeoff

A

300 c

75
Q

Flight Maneuvering Load Acceleration Limits

A

Clean configuration……………..-1.0g to +2.5g

Other configuration……………..0g to +2.0g

76
Q

Takeoff is NOT permitted on which runway conditions

A

Wet Ice

77
Q

Takeoff is NOT recommended on which runway conditions

A

Water on top compact snow
Dry snow
Wet snow over ice

78
Q

Maximum Operating speed Vmo/Mmo

A

Vmo…………350kt

Mom…………M0.82

79
Q

Can the APU be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed

A

Yes, maintenance action is required within the next 10 hours of APU operation

80
Q

APU Maximum N Speed

A

107%

81
Q

How many start attempts on the APU

A

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

82
Q

Engine Start crosswind max speed

A

Engine is able to start in crosswind up to 35kt

83
Q

Maximum operating altitude with slats and/or flaps extended

A

20,000ft

84
Q

Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-928)

A

Maximum Asymmetry 1,102 LB

85
Q

Fuel Imbalance at TAKEOFF: Outer Tanks (Inner Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-928)

A

Maximum Asymmetry 815 LB

86
Q

Fuel Temperature

A

For JET A only, if TAT reaches -34 c, monitor on FUEL SD page that fuel temperature remains higher than -36 C

A320 Limitations (7 decks)

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