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Spirit Airlines Fall 2015 > Limitations > Flashcards

Limitations Flashcards

1
Q

Wingspan: 319, 320, 321

A

111 feet, 10 inches

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2
Q

Wingspan: 320S and 321S

A

117 feet, 5 inches

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3
Q

Max Landing Weight A319

A

137,788 lbs

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4
Q

Max Landing Weight A320

A

145,505 lbs

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5
Q

Max Landing Weight A321

A

171,519 lbs

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6
Q

Max Certified Altitude

A

FL398

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7
Q

Runway Slope

A

+/- 2%

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8
Q

Max Runway Altitude

A

Standard 320 series - 9,200 ft

A320 NEO - 6000 ft

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9
Q

Nominal Runway Width

A

148ft (98ft in accordance with “operations on narrow runways” procedure) A321 non-sharklet cannot do the narrow runway.

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10
Q

Max Crosswind various phases all aircraft

A

A319(20)(21) (landing) - 38 kts (gust included)
A320 NEO - 35kts for takeoff (engine limit)
- 38kts for landing
- 15kts for CAT II or III automatic approach

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11
Q

Max Tailwind - Takeoff

A

15 kts

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12
Q

Max Tailwind - Landing

A

10 kts

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13
Q

Max Wind for PAX Door Operation

A

65 kts

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14
Q

Landing Gear - Max with landing gear extended (Vle)

A

280 kts / M.67

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15
Q

Max landing gear extension (Vlo Extension)

A

250 kts / M.60

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16
Q

Max landing gear retraction (Vlo retraction)

A

220 kts / M.54

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17
Q

Max altitude landing gear may be extended

A

25,000 ft

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18
Q

Windshield Wipers In Use Max Speed

A

230 kts

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19
Q

What taxi weight and speed is there a limitation for not exceeding in a turn?

A

Weight higher then 167,550lbs

Cannot exceed 20 kts in a turn

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20
Q

Air Conditioning with LP Ground Unit

A

Do not use condition air simultaneously from PACKS and LP ground unit (to avoid chattering of non-return valves)

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21
Q

Air Conditioning with HP Ground Unit

A

Do not use HP ground unit when APU is supplying bleed air to avoid bleed system damage.

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22
Q

Cabin Pressure

Max positive differential pressure

A

9.0 psi

23
Q

Cabin Pressure

Max Negative differential pressure

A

-1.0 psi

24
Q

Minimum Height for Use of Autopilot

Takeoff in SRS mode

A

100 ft AGL

25
Q

Minimum Height for Use of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

26
Q

Minimum Height for Use of Autopilot

Circling Approach

A

Applicable Circling Minimums - 100 ft

27
Q

Minimum Height for Use of Autopilot

ILS approach when CAT 2 or CAT 3 is not displayed on the FMA

A

160 ft AGL

28
Q

Minimum Height for Use of Autopilot

Go-Around (AP or FD engagement)

A

100 ft AGL

29
Q

Minimum Height for Use of Autopilot

All other phases

A

500 ft AGL (319/320)

900 ft AGL (321)

30
Q

Minimum Height for Use of Autopilot

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

31
Q

Nav mode may be used in the terminal area, provided:

A
  • GPS PRIMARY is available, or
  • HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
  • NAVAID raw data is monitored
32
Q

Autopilot use Non-Precision Approaches with Engine-Out

A319/A321

A

If one engine is inoperative, it is not permitted to use the autopilot to perform NPA’s in the following modes: FINAL APP, NAV V/S, NAV/FPA
Only FD use is permitted

33
Q

Maximum Allowed Wing Fuel Imbalance

A320S and A320 NEO
At takeoff
Inner tanks (outer tanks balanced)

A

Inner tanks (outer tanks balanced)

Heavier tank - FULL
Imbalance other tank - 1,102lbs

34
Q

Maximum Allowed Wing Fuel Imbalance

A320S and A320 NEO
In flight and landing
Inner tanks (outer tanks balanced)

A

Inner tanks (outer tanks balanced)

Heavier tank - FULL
Imbalance other tank - 3,306lbs

35
Q

Maximum Allowed Wing Fuel Imbalance

587NK - 588NK
In flight and landing

A

Wing tanks

Heavier tank - FULL
Imbalance other tank - 2,910lbs

36
Q

Maximum Allowed Wing Fuel Imbalance

A321S
At takeoff

A

Wing tanks

Heavier tank - FULL
Imbalance other tank - 882lbs

37
Q

Brakes maximum temperature for takeoff (brake fans off)

A

300 C / 150 C if brake fans on

38
Q

APU Starter limit

A

After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles.

39
Q

APU bleed extraction for wing anti-ice is allowed or not?

A

Not allowed

40
Q

Thrust setting / EGT Limts

Starting

A

A319(20)(21) - 635C

A320 NEO - 1,018C

41
Q

Thrust setting / EGT Limts

Takeoff and Go-Around

A

A319, A320 - 5min (10min single engine) - 635C
A321 - 5min (10min single engine) - 650C
A320 NEO - 5min (10min single engine) - 1,083C

42
Q

Thrust setting / EGT Limts

MCT

A

A319(20)(21) - 610C

A320 NEO - 1,043C

43
Q

Oil Temperature

Minimum for starting

A

-40 C

44
Q

Oil Temperature

Minimum prior to exceeding idle

A

-10 C

45
Q

Oil Quantity

Minimum oil quantity

A

11 qts + est. consumption (~0.3 qt/hr)

46
Q

Engine Starter Limits A319(20)(21)

A

3 consecutive cycles:
- 2 cycles of 2 min each
- 3rd cycle of 1 min
Pause between start attempts of 15 sec.
Following 3 start attempts or 4 minutes of continuous cranking a 30min cooling period is required.
No running engagement of the starter, when N2 is above 10% on the ground, or 18% in flight.

47
Q

Minimum speed for maximum reverse thrust

A

70 kts or when airspeed starts to fluctuate

48
Q

When is takeoff with reduced thrust not permitted?

A

On contaminated runways

49
Q

Max crosswind engine is capable of starting in.

A

35kts

50
Q

Max Landing Weight A320 NEO

A

148,591 lbs

51
Q

Max operating altitude with slats and/or flaps extended

A

20,000 ft

52
Q

Fuel Temperature

A

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

53
Q

Minimum oil pressure A320 NEO

A

65 psi

54
Q

Engine Starter Limits A320 NEO

A
  • 3 consecutive start attempts, 35s between each cycle.
  • After 3 cycles, or after 15min of continuous cumulative cranking: A 15 min cooling period is necessary before a new start motoring cycle is attempted.
  • No running engagement of the starter, when N2 is above 20%.

Spirit Airlines Fall 2015 (4 decks)

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