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Spirit Oral Items > Limitations > Flashcards

Limitations Flashcards

1
Q

N502NK THRU N536NK

A

A319

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2
Q

N601NK THRU N617NK, N697NK, N698NK– Non Sharklet
* N618NK THRU N656NK, N690NK THRU N696NK – Sharklet
* N629NK THRU N656NK, N690NK THRU N696NK – “Jet Pump”
Fuel System
* N901NK THRU N990NK – NEO

A

A320

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3
Q

N657NK THRU N687NK – Sharklet
N702NK THRU N715NK - NEO

A

A321

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4
Q

Wingspan- A319/320

A

111’ 10”

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5
Q

Wingspan- A320Sharklet/NEO A321 Sharklet/NEO

A

117’ 5”

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6
Q

Tail strike pitch attitude

A319

A

13.9 degrees

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7
Q

Tail strike pitch attitude

A320/320NEO

A

11.7 Degrees

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8
Q

Tail strike pitch attitude

A321/NEO

A

9.7 degree’s

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9
Q

Maximum Certified Altitude

A

FL398

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10
Q

Max Runway Slope (mean)

A

+/-2%

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11
Q

Max Runway Altitude

A

9,200 FT

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12
Q

Nominal Runway Width

A

45 m (148 ft)

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13
Q

Maximum crosswind (takeoff and landing)

A

38 kt (gust included)

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14
Q

Maximum tailwind for takeoff

A

15 kt

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15
Q

Maximum tailwind for landing

A

10 kt

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16
Q

Maximum wind for passenger door operation

A

65 kt

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17
Q

Max with landing gear extended (VLE)

A

280 kt/M.67

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18
Q

Max landing gear extension (VLO Extension)

A

250 kt/M.60

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19
Q

Max landing gear retraction (VLO Retraction)

A

220 kt/M.54

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20
Q

Wipers Maximum Operating Speed

A

230 kt

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21
Q

When the takeoff weight is higher than _________ Do not exceed a taxi speed of _________

A

167,550 lb

20 kt

N601NK THRU N656NK, N690NK
THRU N698NK

(A320)

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22
Q

A319
Max Landing

A

137,788 lb

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23
Q

A320/A320 Sharklet
Max Landing

A

145,505 lb

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24
Q

A321

Max Landing

A

171,519 lb

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25
Q

A320NEO

Max Landing

A

148,591 lb

26
Q

A321 NEO Max landing weight

A

174,606 lb

27
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.

28
Q

Max positive differential pressure

A

9.0 PSI

29
Q

Max negative differential pressure

A

-1.0 PSI

30
Q

Minimum Use Height For Autopilot

At takeoff

A

100 ft AGL and at least 5 s after
takeoff

31
Q

Minimum Use Height For Autopilot

In approach with F-G/S, FINAL APP,
V/S, or FPA mode

A

250 ft AGL

32
Q

Minimum Use Height For Autopilot

In Circling Approach

A

600 ft AGL

33
Q

Minimum Use Height For Autopilot

ILS approach when CAT 1 is
displayed on the FMA

A

160 ft AGL

34
Q

Minimum Use Height For Autopilot

ILS approach when CAT 2 or CAT 3
(single or dual) is displayed on the
FMA

A

0 ft AGL if autoland

35
Q

Minimum Use Height For Autopilot

After a manual go-around

A

100 ft AGL

36
Q

Minimum Use Height For Autopilot

In all other phases

A

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

37
Q

Minimum Use Height For Autopilot

The AP or FD in OP DES or DES
mode can be used in approach.
However, its use is only permitted if
the FCU selected altitude is set to,
or above, the higher of the two:

A

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

38
Q

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

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 crosschecked with navaid raw data

39
Q

A319/A321

If one engine is inoperative, it is not permitted to use the autopilot to
perform NPAs in the following modes

A

FINAL APP
NAV V/S
NAV/FPA.

Only FD use is permitted.

40
Q

After three consecutive APU start attempts, the Flight Crew must wait

A

60 min before a new start attempt.

41
Q

A319/A320
N502NK THRU N656NK, N690NK
THRU N698NK

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

635 °C MAX EGT

42
Q

A321
N657NK THRU N687NK

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

650 °C MAX EGT

43
Q

A320NEO/A321NEO

Takeoff go around
Time/EGT Limit

A

All engines operative
5 min
One engine inoperative
10 min

1083 °C MAX EGT

44
Q

A319/A320
N502NK THRU N656NK, N690NK
THRU N698NK

MCT
Time/EGT Limit

A

Not limited

610 °C

45
Q

A321
N657NK THRU N687NK

MCT
Time/EGT Limit

A

Not limited
610 °C

46
Q

A320NEO/A32NEO

MCT
Time/EGT Limit

A

Not limited

1,043 °C

47
Q

Starting EGT Limits

A

A319/A320/A321 - 635 EGT

A320/A321 NEO - 1083 EGT

48
Q

A319/A320/A321

Minimum starting temperature
Minimum temperature before IDLE is exceeded

A

-40 C
-10 C

49
Q

A320NEO/A321NEO

Minimum Oil Pressure

A

65 PSI

50
Q

A319/A320/A321
Staring constraints

A
  • A standard automatic start that includes only one start attempt, is considered one cycle
  • For ground starts (automatic or manual), a 15s 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 a two-minute maximum cycle time
  • For crank, observe a 5 min maximum cycle time
  • The starter must not be run when N2 is above 10 % on-ground and 18 % in-flight.
51
Q

A320NEO/A321NEO
Starting constraints

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 cumulated crank
  • The starter must not be run when N2 is above 20%.
52
Q

Thrust reverser limits

A

Maximum reverse should not be used below 70 kt.

Idle reverse is permitted down to aircraft stop.

53
Q

FLEX takeoff limits

A

FLEX takeoff is not permitted on contaminated runways.

54
Q

ENGINE START crosswind limit

A

up to 35 kt.

55
Q

Maximum operating altitude with slats and/or flaps extended

A

20,000 ft

56
Q

JET A Temp limits

A

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

57
Q

A319/A320/A320NEO

Max Fuel Imbalance at Takeoff inner tanks

A

1,102 lb

58
Q

A319/A320/A320 NEO

Max Fuel Imbalance inner tanks In flight and Landin

A

3,306 lb

59
Q

A321/A321NEO

Max Fuel Imbalance wing tanks In flight and Landing

A

2,910 lb

60
Q

A321/A321NEO

Max Fuel Imbalance at Takeoff wing tanks

A

882 lb

61
Q

Maximum brake temperature for takeoff (brake fans (if installed) off)

A

300 °C

Spirit Oral Items (49 decks)

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