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Spirit Airbus A320 May 2023 > Limitations 2023 > Flashcards

Limitations 2023 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 degrees

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5
Q

Tailstrike A321 Strut Compressed

A

9.7 degrees

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6
Q

Tailstrike A319 Strut Extended

A

15.5 degrees

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7
Q

Tailstrike A320 Strut Extended

A

13.5 degrees

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8
Q

Tailstrike A320 NEO Strut Extended

A

13.7 degrees

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9
Q

Tailstrike A321 Strut Extended

A

11.2 degrees

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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 tire speed (ground speed)

A

195 knots

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23
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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24
Q

Wipers maximum operating speed

A

230 knots

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25
Q

Maximum landing weight A320 NEO

A

148,591 pounds

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26
Q

Maximum landing weight A320

A

145,505 pounds

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27
Q

Maximum landing weight A319

A

137,788 pounds

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28
Q

Maximum landing weight A321

A

171,519 pounds

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29
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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30
Q

Maximum cabin pressure positive differential pressure

A

9.0 PSI

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31
Q

Maximum cabin pressure negative differential pressure

A

-1.0 PSI

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32
Q

Cabin pressure safety relief valve pressure setting is

A

8.6 PSI

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33
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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34
Q

Minimum hight Auto Pilot usage Circling Approach

A

600ft AGL

-100 feet

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35
Q

Minimum height Auto Pilot usage ILS approach with CAT 2 or 3 (single or dual) is displayed on the FMA

A

0ft AGL if autoland

36
Q

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

A

100 feet AGL

37
Q

Minimum hight Auto Pilot usage All other phases of flight

A

500 feet AGL (A319,A320)
900 feet AGL (A321)

900 feet AGL (A321)

38
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)

39
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
40
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

41
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

42
Q

Power plant EGT limits for (657-687) A321 ceo

A

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

43
Q

Power plant EGT limits for (901-986) A320 NEO

A

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

44
Q

Minimum starting oil temperature (N502NK-N698NK) (901-986)

45
Q

Minimum oil temperature before IDLE is exceeded (N502NK-N698NK)

46
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

47
Q

Starter limits (502-698) CEO

A
  • One start is one cycle
  • ground starts (automatic or manual), 15 s pause between successive cycles
  • 30 minute cooling period after 3 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
48
Q

What is considered a engine start cycle for (901-986)

A

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

49
Q

Starter limits (901-986) NEO

A
  • 2 starts is 1 cycle
  • For ground start (automatic or manual) a 35 second pause is required between successive cycles
  • A 15 minute cooling period is required, subsequent to 3 failed cycles, or 15 minute of continuous or cumulative crank
  • Starter must not be run when N2 is above 20%
50
Q

Minimum speed for max reverse

A

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

51
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

52
Q

Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687) A321

A

882 pounds

53
Q

Minimum fuel quantity for TAKEOFF

A

3,307 pounds

54
Q

Maximum brake temperature for takeoff

55
Q

CG limits

A

Clean configuration………-1.0g to +2.5g

Other configuration…………0g to +2.0g

56
Q

Takeoff is NOT permitted on which runway conditions

57
Q

Takeoff is NOT recommended on which runway conditions

A

Water on top compact snow
Dry snow
Wet snow over ice

58
Q

Maximum Operating speed Vmo/Mmo

A

Vmo…………350kt Mmo………….M0.82

Mom…………M0.82

59
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

60
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.

61
Q

Engine Start crosswind max speed

A

Engine is able to start in crosswind up to 35kt

62
Q

Maximum operating altitude with slats and/or flaps extended

63
Q

Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-990)

A

Maximum Asymmetry 1,102 LB

64
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

65
Q

Automatic Approach, Landing, and Rollout ILS Category II Minimum Decision height?

A

100 feet AGL

66
Q

Special Authorization CAT II (SA CAT II) Minimum decision height?

A

100 feet AGL

67
Q

Other than standard CAT II (OTS CAT II) minimum decision height?

A

100 feet AGL

68
Q

ILS Category III FAIL Passive (single) minimum decision height?

A

50 feet AGL

69
Q

ILS Category III Fail Operational (DUAL) Alert height?

A

100 feet AGL

70
Q

CAT III without DH: Minimum Runway Visual Range?

71
Q

Maximum one tire per gear is deflated (consider three gear) Maximum taxi speed during turn?

72
Q

If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed?

73
Q

For the nose wheel steering (NWS) angle Maximum NWS angle with damage tire?

A

30 degrees

74
Q

Nosewheel steering (NWS) Maximum NWS angle?

A

+/- 85 degrees

75
Q

ENG oil quantity 502-698 CEOs

A

(V2500): Check that the oil quantity is at or above 11 qt. +
estimated consumption (average estimated consumption
~ 0.3 qt./h).

76
Q

ENG oil quantity check for (PW1100G):

A

Above 14 quarts, if OTS -30 Check that the oil quantity is at, or above 16.5 quarts

77
Q

Airflow supplied by the ground cart shall not exceed?

78
Q

MAX continuous load per TR?

79
Q

Hydraulic system normal operating pressure?

A

3,000 PSI +/- 200 PSI

80
Q

Max altitude for APU start (on A/C power) and operations?

81
Q

Minimum use of autopilot ILS approach when CAT1 is displayed on the FMA

A

160 ft AGL

82
Q

Minimum use of autopilot in approach with FINAL APP, V/S, or FPA mode?

A

250 ft AGL

83
Q

When is reduced thrust at takeoff not permitted?

A

Contaminated runways, when outside temperature is within 10 degrees of flex temperature.

84
Q

Autopilot Minimum ILS CAT 1 on FMA

85
Q

A321 NEO Max Landing Weight

Spirit Airbus A320 May 2023 (53 decks)

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