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Spirit Airbus A320 Training > 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

Nominal 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(N657NK-N687NK)
A321 NEO (N702NK-N715NK)

A

A321 171,519 pounds
A321 NEO 174,606 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 at takeoff with SRS

A

100 feet AGL and at least 5 s after takeoff.

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35
Q

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

A

Applicable minimums

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36
Q

Minimum hight Auto Pilot usage Circling Approach

A

Applicable circling min. -100 feet

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37
Q

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

A

0ft AGL if autoland

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38
Q

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

A

100 feet AGL

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39
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)

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40
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)

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41
Q

Takeoff with SRS mode

A

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

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42
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
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43
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

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44
Q

Honeywell APU Maximum altitude assisted engine start

A

20,000 feet

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45
Q

Hamilton APU maximum altitude engine start

A

20,000 feet

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46
Q

Hamilton APU maximum altitude air conditioning and pressurization single pack

A

20,000 feet

47
Q

Hamilton APU maximum altitude air conditioning and pressurization dual pack

A

15,000

48
Q

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

A

NO

49
Q

Honeywell APU maximum altitude air conditioning and pressurization single pack

A

22,500 feet

50
Q

Honeywell APU maximum altitude air conditioning and pressurization dual pack

A

15,000

51
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

52
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

53
Q

Power plant EGT limits for (901-986) 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

54
Q

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

A

-40 c

55
Q

Minimum oil temperature before IDLE (N502NK-N698NK)

A

-10 c

56
Q

Minimum oil temperature before takeoff (N502NK-N698NK)

A

50 c

57
Q

Max continuous oil temperature (502-698)

A

155 c

58
Q

Maximum transient oil temperature (502-698) for 15 Minutes

A

165 c

59
Q

Maximum oil pressure (502-698)

A

60 PSI

60
Q

Maximum continues oil temperature (901-986)

A

151 c

61
Q

Minimum oil temperature before takeoff (901-986)

A

52 c

62
Q

Minimum oil pressure (901-986)

A

65 PSI

63
Q

Maximum oil pressure (901-986)

A

270 PSI

64
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

65
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 3 failed cycles, or 4 minutes of continuous crank, or 5 min cumulated crank.
  • For manual start, Do not exceed the 2 minute maximum cycle time
  • The starter must not be run when N2 is above 10% on the ground and 18% inflight
66
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

67
Q

Starter limits (901-986)

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 3 failed cycles, or 15 minute of continuous or cumulative crank
  • Starter must not be run when N2 is above 20%
68
Q

When should max reverse thrust not be used

A

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

69
Q

Maximum altitude flaps/slats extended

A

20,000 feet

70
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

71
Q

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

A

882 pounds

72
Q

Minimum fuel quantity for TAKEOFF

A

3,307 pounds

73
Q

Maximum brake temperature for takeoff

A

300 c

74
Q

Flight Maneuvering Load Acceleration Limits

A

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

Other configuration……………..0g to +2.0g

75
Q

Takeoff is NOT permitted on which runway conditions

A

Wet Ice

76
Q

Takeoff is NOT recommended on which runway conditions

A

Water on top compact snow
Dry snow
Wet snow over ice

77
Q

Maximum Operating speed Vmo/Mmo

A

Vmo…………350kt Mmo………….M0.82

Mom…………M0.82

78
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

79
Q

APU Maximum N Speed

A

107%

80
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.

81
Q

Engine Start crosswind max speed

A

Engine is able to start in crosswind up to 35kt

82
Q

Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-986)

A

Maximum Asymmetry 1,102 LB

83
Q

Fuel Imbalance at TAKEOFF: Outer Tanks (Inner Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-986)

A

Maximum Asymmetry 815 LB

84
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

85
Q

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

A

100 feet AGL

86
Q

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

A

100 feet AGL

87
Q

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

A

100 feet AGL

88
Q

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

A

50 feet AGL

89
Q

ILS Category III Fail Operational (DUAL) Alert height?

A

100 feet AGL

90
Q

CAT III without DH: Minimum Runway Visual Range?

A

300 RVR

91
Q

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

A

7 knots

92
Q

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

A

3 knots

93
Q

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

A

30 degrees

94
Q

Nosewheel steering (NWS) Maximum NWS angle?

A

+/- 85 degrees

95
Q

ENG oil quantity check (V2500)?

A

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

96
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

97
Q

Airflow supplied by the ground cart shall not exceed?

A

2.60 lb/s

98
Q

MAX continuous load per generator?

A

100% (90KVA)

99
Q

MAX continuous load per TR?

A

200 AMP

100
Q

Hydraulic system normal operating pressure?

A

3,000 PSI +/- 200 PSI

101
Q

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

A

FL410

102
Q

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

A

160 ft AGL

103
Q

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

A

250 ft AGL

104
Q

When is reduced thrust at takeoff not permitted?

A

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

105
Q

Minimal Runway Width

A

30m, (99ft)

106
Q

The maximum wind for FWD and AFT cargo door operation?

A

40 Knots, or 50 Knots if aircraft nose is into the wind or if the FWD and AFT cargo doors are on the leeward side. The FWD and AFT cargo doors must be closed before wind exceeds 65 Knots.

107
Q

Maximum Flaps/Slats Speed flaps 1

A

230kt Holding

108
Q

Maximum Flaps/Slats Speed flaps 1+F

A

215kt Takeoff

109
Q

Maximum Flaps/Slats Speed flaps 2

A

200kt Takeoff/Approach

110
Q

Maximum Flaps/Slats Speed flaps 3

A

185kt Takeoff/Approach/Landing

111
Q

Maximum Flaps/Slats Speed flaps Full

A

177kt Landing

112
Q

Minimum Control Speed for Landing (VMCL)

A

VMCL 109kt

113
Q

If the wing fuel temperature exceeds 30C at engine start?

A

The altitude must be limited to 25,000ft until the center tank is empty.

Spirit Airbus A320 Training (52 decks)

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