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Spirit Airlines > Limitations > Flashcards

Limitations Flashcards

1
Q

Load Acceleration Limits

A
  • Clean Configuration: -1.0g to +2.5g
  • Other Configuration: 0g to +2.0g
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2
Q

A319/A320 Wingspan

A

111 ft
10 in.

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3
Q

A320 Sharklet,
A321 Sharklet Wingspan

A

117 ft.
5 in.

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4
Q

A319 Tailstrike Pitch Attitude

A

L/G Struts Compressed:
13.9 degrees

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5
Q

A320/A320 NEO Tailstrike Pitch Attitude

A

L/G Struts Compressed:
11.7 degrees

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6
Q

A321 Tailstrike Pitch Attitude

A

L/G Struts Compressed:
9.7 degrees

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7
Q

Maximum Certified Altitude

A

FL398

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8
Q

Runway Slope

A

+/- 2%

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9
Q

Max Runway Altitude

A

9,200 ft

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10
Q

Nominal Runway Width

A

45 m (148 ft)

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11
Q

Max Crosswind (takeoff and landing)

A

38 knots (gust included)

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12
Q

Max Tailwind - Takeoff

A

15 knots

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13
Q

Max Tailwind - Landing

A

10 knots

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14
Q

Max Wind for PAX Door Operation

A

65 knots

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15
Q

Cockpit Window Open Maximum Speed

A

200 knots

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16
Q

Maximum Operating Speed
Vmo Mmo

A

350 knots/M.82

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17
Q

Max speed with landing gear extended
(VLE)

A

280 knots/M.67

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18
Q

Max landing gear extension speed
(VLO Extension)

A

250 knots/M.60

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19
Q

Max landing gear retraction speed
(VLO Retraction)

A

220 knots/M.54

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20
Q

Max Taxi Speed (A320)

A

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

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21
Q

Wipers Maximum Operating Speed

A

230 knots

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22
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.

Why? B/c causes overpressure issues (two sources)

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23
Q

Cabin Pressure:
Max Positive Differential Pressure

A

9 PSI

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24
Q

Cabin Pressure:
Max Negative Differential Pressure

A

-1.0 PSI

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25
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.

Why? B/c causes overpressure issues (two sources)

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26
Q

Min Height for AP -
At Takeoff

A

100 ft AGL and at least 5 seconds after takeoff

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27
Q

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

A

250 ft AGL

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28
Q

Min Height for AP -
In Circling Approach

A

600 ft AGL

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29
Q

Min Height for AP -
ILS approach when CAT 1 is displayed on the FMA

A

160 ft AGL

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30
Q

Min Height for AP -
ILS approach when CAT 2 or 3 displayed
on the FMA

A

0 ft AGL if Autoland

31
Q

Min Height for AP -
After a Manual Go-Around

A

100 ft AGL

32
Q

Min Height for AP -
In All Other Phases

A

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

33
Q

The use of AP or FD in OPEN DES or DES mode is only permitted in approach, when the FCU altitude is set at or above, the higher of the two:

A

Highest of:
MDA/MDH or 500 ft (A319/A320)
MDA/MDH or 900 ft (A321)

Why? b/c in OPEN DES, you’ll be at THR IDLE, speed is controlled by pitch, thrust won’t be able to spooled up

34
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.
35
Q

A319/A321: If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs (non-precision approaches) in the following modes:

A
  • FINAL APP
  • NAV V/S
  • NAV/FPA
  • *Only FD use is permitted.
36
Q

APU Start

A

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

37
Q

Thrust Setting/EGT Limits:
A319/320 CEO
EGT Limit for T/O & Go-Around

A

**635 C
(Time Limit:
All engines op - 5 mins
One engine inop - 10 mins)

38
Q

Thrust Setting/EGT Limits:
A321 CEO
EGT Limit for T/O & Go-Around

A

**650 C
(Time Limit:
All engines op - 5 mins
One engine inop - 10 mins)

39
Q

Thrust Setting/EGT Limits:
A320/A321 NEO
EGT Limit for T/O & Go-Around

A

**1,083 C
(Time Limit:
All engines op - 5 mins
One engine inop - 10 mins)

40
Q

Thrust Setting/EGT Limits:
A319/320 CEO
Max. Continuous Thrust (MCT)

A

610 C

41
Q

Thrust Setting/EGT Limits:
A321 CEO
Max. Continuous Thrust (MCT)

A

610 C

42
Q

Thrust Setting/EGT Limits:
A320/A321 NEO
Max. Continuous Thrust (MCT)

A

1,043 C

43
Q

Thrust Setting/EGT Limits:
A319/320 CEO
Starting

A

635 C

44
Q

Thrust Setting/EGT Limits:
A321 CEO
Starting

A

635 C

45
Q

Thrust Setting/EGT Limits:
A320/A321 NEO
Starting

A

1,083 C

46
Q

Minimum Oil Temperature for Starting
(All CEO/NEO)

A

-40 C

47
Q

Minimum Oil Temperature Before IDLE is exceeded (CEO)

A

-10 C

48
Q

Minimum Oil Temperature Before Takeoff (CEO)

A

50 C

49
Q

Minimum Oil Temperature Before Takeoff (NEO)

A

52 C

50
Q

Minimum Oil Pressure (CEO)

A

60 PSI

51
Q

Minimum Oil Pressure (NEO)

A

65 PSI

52
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
53
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%
54
Q

Max Reverse Thrust should not be used below:

A

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

Other: max reverse is most effective at high speeds

55
Q

FLEX takeoff is not permitted:

A

On contaminated runways.

56
Q

Max Crosswind for Engine Start

A

35 knots

57
Q

Max Altitude for Flaps and/or Slats

A

20,000 ft

58
Q

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

A

-34 C/
-36 C

59
Q

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

A

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

60
Q

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

A

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

61
Q

Max Fuel Imbalance -
Takeoff
(A321-S)

A

Wing tanks: (Heavier tank full)
882 lbs

62
Q

Max Brake Temp for Takeoff (brake fans off)

A

300 C

Other:
- Cannot take off w/ brake fans on
- If over 300, get down to 150 with fans and then fans come off

63
Q

Max Altitude for APU Start on Battery Power

A

25,000 ft

64
Q

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

A

FL410

65
Q

A319 Max Landing Weight

A

137,788 lbs

66
Q

A320 (CEO) Max Landing Weight

A

145,505 lbs

67
Q

A320-S Max Landing Weight

A

145,505 lbs

68
Q

A320 (NEO) Max Landing Weight

A

148,591 lbs

69
Q

A321-S Max Landing Weight

A

171,519 lbs

70
Q

A321 (NEO) Max Landing Weight

A

174,606 lbs

71
Q

Max Tire Speed

A

Ground Speed 195 Kts

72
Q

Min. Oil Quantity (CEO)

A

11 qts + 0.3 for every hr of flight

73
Q

Min. Oil Quantity (NEO)

A

14 qts

Spirit Airlines (6 decks)

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