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Spirit - New Hire - Dec '22 > Limitations - Dec '22 > Flashcards

Limitations - Dec '22 Flashcards

1
Q

A319/A320 Wingspan

A

111ft 10in.

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2
Q

A320/A321 with Sharklets wingspan

A

117ft 5in

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3
Q

A319 tail clearance (struts compressed)

A

13.9°

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4
Q

A320 tail clearance (struts compressed)

A

11.7°

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5
Q

A321 tail clearance (struts compressed)

A

9.7°

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6
Q

Maximum Certified Altitude

A

FL 398

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7
Q

Maximum runway slope (mean)

A

+/- 2%

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8
Q

Maximum runway altitude

A

9,200ft

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9
Q

Nominal runway width

A

45m (148ft)

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10
Q

Maximum demonstrated crosswind (including gust)

A

38kts

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11
Q

Maximum tailwind for take-off

A

15kts

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12
Q

Maximum tailwind for landing

A

10kts

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13
Q

Maximum wind for passenger door operation

A

65kts

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14
Q

Maximum window open speed

A

200kts

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15
Q

VMO/MMO

A

350kts/0.82M

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16
Q

Maximum tire speed

A

195kts (ground speed)

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17
Q

Maximum speed with landing gear extended (VLE)

A

280kts/0.67M

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18
Q

Maximum speed for gear extension (VLO EXT)

A

250kts/0.60M

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19
Q

Maximum speed for gear retraction (VLO RET)

A

220kts/0.54M

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20
Q

Maximum altitude with gear extended

A

25,000ft

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21
Q

Maximum taxi speed in a turn with weight above 167,550lbs

A

20kts

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22
Q

Maximum wiper operating speed

A

230kts

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23
Q

Maximum positive pressure differential

A

9.0PSI

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24
Q

Maximum negative pressure differential

A

-1.0PSI

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25
Q

Use of APU bleed air and HP Air start cart

A

Prohibited

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26
Q

Use of PACKS with LP conditioned air connected

A

Prohibited

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27
Q

Max Landing Weight (N502NK thru N536NK) (A319)

A

137,788 lbs

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28
Q

Max Landing Weight (N601NK thru N617NK) (A320 - NonSharklet)

A

145,505 lbs

29
Q

Max Landing Weight (N618NK thru N656NK, N690NK thru
N694NK) (A320 - Sharklet)

A

145,505 lbs

30
Q

Max Landing Weight (N901NK thru N974NK) (A320Neo)

A

148,591 lbs

31
Q

Max Landing Weight (N657NK thru N687NK) (321 - Sharklet)

A

171,519 lbs

32
Q

Min height for AP engagement - T/O with SRS mode

A

100ft AGL

33
Q

Min height for AP engagement - straight-in non-precision
approach CANT FIND in COM

A

Applicable Minimums

34
Q

Min height for AP engagement - circling approach

A

600 ft

35
Q

Min height for AP engagement - ILS (CAT 2 or 3 not displayed
in FMA)

A

160ft AGL

36
Q

Min height for AP or FD engagement – Go-around

A

100ft AGL

37
Q

Min height for AP engagement for all other phases of flight

A

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

38
Q

Use of AP or FD in OP DES or DES mode is not permitted in
approach unless the FCU altitude is set at or above:

A

Highest or MDA or 500ft (319/320)
Highest of MDA or 900ft (321)

39
Q

Take-off with SRS mode – An internal FMGS logic prevents the
AP from engaging during:

A

The fist 5 seconds after lift
off

40
Q

After three APU start attempts, the crew must wait:

A

60 minutes

41
Q

Minimum oil temperature for start

A

-40°C

42
Q

Minimum oil temperature before exceeding IDLE

A

-10°C

43
Q

Minimum oil temperature for take-off (CEO)

A

50°C

44
Q

Minimum oil temperature for take-off (NEO)

A

52°C

45
Q

Minimum oil pressure (CEO)

A

60PSI

46
Q

Minimum oil pressure (NEO)

A

65PSI

47
Q

Maximum crosswind for engine start

A

35kts

48
Q

Maximum altitude for slats or flaps

A

20,000ft

49
Q

Maximum fuel imbalance at T/O for inner tanks (A319/A320)

A

1,102 lbs

50
Q

Maximum fuel imbalance at T/O for inner tanks (N657NK
thru N687NK) (A321)

A

882 lbs

51
Q

Maximum fuel imbalance for landing and in-flight (A319/A320)

A

3,306 lbs

52
Q

Maximum fuel imbalance for landing and in-flight
(N657NK thru N687NK) (A321)

A

2,910 lbs

53
Q

Maximum brakes temperature for T/O without brake fans?

A

300°C

54
Q

Use of FLEX on a contaminated runway

A

Prohibited

55
Q

FLEX thrust is prohibited when the OAT is within

A

10°C of the FLEX Temp

56
Q

Maximum reverse thrust use is not allowed below

A

70kts

57
Q

IDLE thrust reverse is permitted down to

A

Aircraft stop

58
Q

APU Max Altitude for bleed air extraction (Single PACK)

A

20,000ft

59
Q

APU Max Altitude for bleed air extraction (Both PACKs)

A

15,000ft

60
Q

Thrust setting EGT Limits (N502NK thru
N656NK, N690NK thru N698NK) [A319/A320]
-All engine operating – T/O & Go-around
-One engine inoperative – T/O & Go-around
-Max Continuous Thrust
-Engine Start

A

-635°C
-635°C
-610°C
-635°C

61
Q

Thrust setting EGT Limits (N657NK thru
N687NK) [A321]
-All engine operating – T/O & Go-around
-One engine inoperative – T/O & Go-around
-Max Continuous Thrust
-Engine Start

A

-650°C
-650°C
-610°C
-635°C

62
Q

Thrust setting EGT Limits (N901NK thru
N974NK) [A320neo]
-All engine operating – T/O & Go-around
-One engine inoperative – T/O & Go-around
-Max Continuous Thrust
-Engine Start

A

-1083°C
-1083°C
-1043C
-1083°C

63
Q

Thrust setting time limit
-All engines operating – T/O & Go-around thrust time limit
-One engine inoperative – T/O & Go-around thrust time limit
-Max Continuous Thrust time limit

A

-5 Minutes
-10 Minutes
-No Time Limit

64
Q

Fuel Temp Restrictions for Jet-A

A

If the TAT reaches -34°C, monitor the fuel SD page, the fuel temperature must
remain above -36°C

65
Q

NAV mode maybe used in the terminal area provided that:

A
  • GPS Primary is available, or
  • Required RNP is checked or entered in the MCDU and high accuracy is displayed, or
  • FMS navigation is crosschecked with raw data
66
Q

If one engine is inoperative, use of the AP is not permitted to perform non-precision
approaches in the following modes (use of FD is permitted)

A
  • FINAL APP
  • NAV V/S
  • NAV FPA
67
Q

Starter Limits (N502NK thru N698NK) [CEO]
A standard automatic start that includes only XX start attempt is considered one cycle.
For ground starts (automatic or manual), a XX second pause is required between successive
cycles.
A XX minute cooling period is required, subsequent to XX failed cycles or XX minutes of
continuous crank.
For manual start, observe a XX minute maximum cycle time
For crank, observe a XX minute maximum cycle time
The starter must not run when the N2 is above XX on the ground and XX% in flight

A

-One
-15 Second
-30 Minute
-3 Failed Cycles
-5 Min Cont. Crank
-2 Min max cycle for man. Start
-5 Min max cycle time for crank
-10% N2 on Ground
-18% N2 in flight

68
Q

Starter Limits (N901NK thru N974NK) [NEO]
A standard automatic start that includes up to XX start attempts is considered one cycle.
For ground starts (automatic or manual), a XX seconds pause is required between successive
cycles.
A XX minute cooling period is required subsequent to XX failed cycles, or XX minutes of
continuous or cumulative crank.
The starter must not be run when the N2 is above XX%

A

-Two
-35 Second pause
-15 minute
-3 Failed cycles
-15 Min. continous or cumulative crank
-20% N2 ground/flight

69
Q

Minimum height for autopilot:
In approach with Final APP, V/S, or FPA mode:

A

250ft AGL

Spirit - New Hire - Dec '22 (1 decks)

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