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Spirit Airlines 2019 Limitations > Bold Italic Limitations Plus A Couple Others > Flashcards

Bold Italic Limitations Plus A Couple Others Flashcards

1
Q

Wingspan A319, A320

A

111 feet 10 inches

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2
Q

Wingspan A320 Sharklet, A321 Sharklet

A

117 feet 5 inches

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3
Q

Tailstrike with L/G struts compressed.

  • A319
  • A320
  • A320 NEO
  • A321
A
  • 13.9
  • 11.7
  • 11.7
  • 9.7
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4
Q

Maximum Certified Altitude

A

FL 398

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5
Q

Runway slope (mean)

A

+/-2%

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6
Q

Runway altitude

A

9200ft

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7
Q

Nominal runway width

A

45m (148feet)

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8
Q

Max demonstrated crosswind (takeoff and landing)

A

38 kt gust included

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9
Q

Max tailwind for takeoff

A

15 kt

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10
Q

Max tailwind landing

A

10kt

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11
Q

Max wind passenger door operation

A

65kt

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12
Q

Max cockpit window open speed

Not bolded

A

200kts

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13
Q
  • Max with landing gear extended (VLE)
  • Max landing gear extension (VLO extension)
  • Max landing gear retraction (VLO Retraction)
  • Max altitude landing gear may be extended
A
  • 280/.67
  • 250/.60
  • 220/.54
  • 25,000ft
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14
Q

Max tire speed (not bolded)

A

195kt

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15
Q

When taxi weight is higher than…..

A

167,550 in a 320 or 321 don’t exceed a taxi speed of 20kt during a turn

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16
Q

Max wiper speed

A

230kt

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17
Q
  • Max landing 319
  • max landing 320
  • max landing 320 sharklet
  • max landing NEO
  • max landing 321
A
  • 137,788
  • 145,505
  • 145,505
  • 148,591
  • 171,519
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18
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

19
Q
  • max positive differential pressure
  • max negative differential pressure
  • safety relief valve setting
A
  • 9.0 psi
  • -1.0 psi
  • 8.6psi
20
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

21
Q
  • takeoff with SRS mode
  • straight in NPA
  • circling approach
  • ILS approach when cat 2 or 3 not displayed on the FMA
  • Go around
  • all other phases
A
  • 100 AGL
  • applicable minimum
  • applicable circling mins minus 100 feet
  • 160 AGL
  • 100 AGL
  • 500ft (a319/a320) 900ft (a321)
22
Q

Use of the AP or FD in OPEN DES or DES mode…..

A

Is not permitted in approach, unless the FCU altitude is set at or above highest of:

Minimum or 500ft (319/320)
Minimum or 900ft (321)

23
Q

Takeoff with SRS mode

A

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

24
Q

Use of NAV mode in the terminal area

A

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

  • GPS primary is available, or
  • The appropriate RNP is checked or entered on the MCDU, and high accuracy is displayed, or
  • FMS navigation is crosschecked with NAVAID raw data
25
Q

If one engine is inoperative in a 319/321 it is NOT permitted….

A

To use the autopilot to perform NPA’s in the following modes:

  • FINAL APP
  • NAV V/S
  • NAV/FPA
  • Only FD use is permitted
26
Q

APU Start

A

After 3 consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt

27
Q

Thrust EGT limits for 319/320

A

TOGA- 635- 5 min or 10 min

MCT- 610

Starting- 635

28
Q

Thrust EGT limits 321

A

TOGA- 650- 5 min or 10min

MCT- 610

Starting- 635

29
Q

Thrust EGT limits NEO

A

TOGA- 1083- 5 min or 10min

MCT- 1043

Starting- 1083

30
Q

Oil temps CEO

  • min starting
  • min before idle exceeded
  • min before takeoff
  • min oil pressure
A
  • -40C
  • -10C
  • 50C
  • 60 Psi
31
Q

Oil NEO

  • Min starting temp
  • min temp before takeoff
  • Minimum pressure
A
  • -40C
  • 52C
  • 65psi
32
Q

Start limitation CEO

A
  • A standard automatic start that includes only one start attempt is considered one cycle
  • for ground starts (auto or manual) a 15 second pause is required between successive cycles
  • a 30 min cooling period is required subsequent to 3 failed cycles or 5 min of continuous crank
  • for a manual start observe a 2 min max cycle time
  • for crank observe a 5 min max cycle time
  • the starter must not be run when N2 is above 10% on ground and 18% in flight
33
Q

Start limitation NEO

A
  • a standard automatic start that includes up to 3 start attempts is considered one cycle
  • for ground starts (auto or manual) a 35s pause is required between successive cycles
  • a 15 min cooling period is required subsequent to 3 failed cycles or 15 min of continuous or cumulated crank
  • the starter must not be run when N2 is above 20%
34
Q

Reverse thrust

A

Max reverse should not be used below 70 it’s

Idle reverse is permitted down to aircraft stop

35
Q

FLEX is not permitted

A

On contaminated runways

36
Q

Max crosswind engine start

A

35kt

37
Q

Max altitude slats/flaps extended

A

20,000ft

38
Q

Fuel temp

A

If TAT reaches -34C monitor fuel on SD page that fuel temp remains higher than -36C

39
Q

Max fuel imbalance 320 sharklet/NEO on inner tanks (outer tanks balanced) at takeoff

A

Heavier tank full, 1102 lbs

40
Q

Max fuel imbalance 320 sharklet/NEO on inner tanks (outer tanks balanced) in flight and landing

A

Heavier tank full, 3306

41
Q

Max fuel imbalance 321 on inner tanks (outer tanks balanced) at takeoff

A

882

42
Q

Min fuel quantity for takeoff

Not bolded

A

3307

43
Q

Normal operating pressure of hydraulic (not bolded)

A

3000 psi. +/-200

44
Q

Brake temperature max for takeoff

A

300C brake fans off

Spirit Airlines 2019 Limitations (1 decks)

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