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Spirit Airlines - Flows > LIMITATIONS BOLD 2-27-19 (date indicates when updated) If you find an error or need an update on any card in this class text 563-564-9569 > Flashcards

LIMITATIONS BOLD 2-27-19 (date indicates when updated) If you find an error or need an update on any card in this class text 563-564-9569 Flashcards

1
Q

A319 A320 WINGSPAN

A

111’ 10”

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2
Q

A320 SHARKLET A321 SHARKLET WINGSPAN

A

117’ 5”

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3
Q

TAILSTRIKE ATTITUDE 319

A

13.9

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4
Q

TAILSTRIKE ATTITUDE 320 and A320 NEO

A

11.7

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5
Q

TAILSTRIKE ATTITUDE 321

A

9.7

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6
Q

MAX certified altitude

A

FL 398

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7
Q

Runway Slope

A

+/- 2%

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8
Q

Runway Altitude

A

9,200ft

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9
Q

Nominal Runway Width

A

148 ft (45m)

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10
Q

Max Crosswind Takeoff and Landing

A

38 kt (gust included)

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11
Q

Max tailwind takeoff

A

15 kt

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12
Q

Max tailwind landing

A

10 kt

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13
Q

Max wind for passenger door operation

A

65 kt

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14
Q

Max Landing Gear Extended V Le

A

280 kt /.67M

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15
Q

Max Landing Gear Extension (V Lo Extension)

A

250 kt /.60M

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16
Q

Max Landing Gear Retraction (V Lo Retraction)

A

220 kt /.54M

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17
Q

Max altitude landing gear may be extended

A

25,000 ft

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18
Q

MAX Weight and Speed Limit in taxi turn

A

When Higher than 167550 lb Max speed in turn 20 kt

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19
Q

Windshield Wiper Use Max Speed

A

230 kt

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20
Q

A319 MAX LANDING

A

137,788

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21
Q

A320 MAX LANDING

A

145,505

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22
Q

A320 NEO MAX LANDING

A

148,591

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23
Q

A321 MAX LANDING

A

171,519

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24
Q

APU with HP Ground Unit

A

Do not use HP ground unit when APU supplies bleed air to avoid system damageto prevent any adverse effect on the Air Conditioning system.

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25
Q

MAX Positive differential cabin Pressure

A

9.0 PSI

26
Q

MAX Negative differential cabin Pressure

A

-1.0 PSI

27
Q

Air Conditioning with LP Ground Unit

A

Do not use conditioned air simultaneously from PACKS and LP ground unitto prevent anyadverse effect on the Air Conditioning system.

28
Q

Minimum Height for use of Autopilot Takeoff with SRS mode

A

100 ft AGLTAKEOFF WITH SRS MODE-AN INTERNAL FMGS LOGIC PREVENTS THE AUTOPILOT FROM ENGAGING DURING THE 5 SECONDS AFTER LIFTOFF

29
Q

Minimum Height for use of AutopilotStraight-in Non-Precision approach

A

Applicable Minimum

30
Q

Minimum Height for use of AutopilotCircling Approach

A

Applicable Circling Minimum -100ft

31
Q

Minimum Height for use of Autopilot ILS Approach when CAT 2 or CAT 3 is not displayed on FMA

A

160 FT AGL(80 ft if displayed)

32
Q

Minimum Height for use of AutopilotGo- Around (AP or FD engagement)

A

100ft AGL

33
Q

Minimum Height for use of Autopilot All other Phases

A

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

34
Q

Minimum Height for use of Autopilot AP OR FD in OPEN DES or DES mode

A

not permitted in approach, unless FCU altitude is set at or above highest of:Minimums or 500 ft (A319/320)Minimums or 900 ft (A321)

35
Q

NAV mode may be used in terminal area provided:

A
  • GPS PRIMARY is available, or
  • The appropriate RNP is checked or entered on the MCDU, andHIGH accuracy is displayed, or
  • FMS navigation is crosschecked with navaid raw data.
36
Q

Non-Precision Approaches With Engine Out A319 and A321 only

A 
If one engine is inoperative it IS NOT PERMITTED to use the autopilot to perform NPAs in the following modes:	
* FINAL APP	
* NAV V/S	
* NAV/FPA
ONLY FD use is permitted
37
Q

APU starter motor duty cycles

A

After 3 cycles wait 60 minutes before attempting 3 more cycles

38
Q

APU ALTITUDE LIMITS

A

APU BLEEDMax altitude to assist engine start . . . . .. . . . . . . . . 20,000 ftMax altitude for air conditioning and pressurization(single pack operation) . . . . . . . . . . . . . . . . . . . . . . 20,000 ftMax altitude for air conditioning and pressurization(dual pack operation) . . . . . . . . . . . . . . . . . . . . . . . . . 15,000 ftUse of APU bleed air for wing anti-ice is not permitted.Max Alt for electric …………………………………………. 25000ft

39
Q

THRUST/EGT LIMITSA319, A320 (not NEO), A321Starting

A

635 C

40
Q

THRUST/EGT LIMITSA320 NEOSTARTING

A

1018 C EGT

41
Q

THRUST/EGT LIMITSA319, A320 (not NEO), A321MCT

A

Unlimited time 610

42
Q

THRUST/EGT LIMITSA320 NEOMCT

A

unlimited time1043 C EGT

43
Q

THRUST/EGT LIMITSA319 A320 (not NEO)Takeoff and Go Around

A

5 minutes 2 engines10 minutes 1 engine 635 C EGT

44
Q

THRUST/EGT LIMITSA321Takeoff and Go Around

A

5 minutes 2 engines10 minutes 1 engine650 C EGT

45
Q

THRUST/EGT LIMITSA320 NEOTakeoff and Go Around

A

5 minutes 2 engines10 minutes 1 engine1083 C EGT

46
Q

OIL Temp minimum starting temp

A

-40 C

47
Q

OIL Temp minimum prior to exceeding idle

A

-10 C(min temp for oil for takeoff is +50 C ecam will alert if below)

48
Q

OIL A320 NEO Minimum Oil Pressure

A

65 PSI

49
Q

Min OIL QUANTITY

A

11 qts. + Est. Consumption (~0.3 qt/hr)(not in limitations but need to know)

50
Q

STARTER A319,A320.A321 (not NEO)

A

STARTER A319,A320.A321 (not NEO)-a standard automatic start that includes only one start attempt is considered one cycle-For ground starts (automatic or manual) a 15 sec pause is required between successive cycles -A 30 min cooling period is required, subsequent to the three failed cycles or 5 min of continuous crank-For Manual start, observe a 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

51
Q

STARTER A320 NEO

A

STARTER A320 NEO-3 consecutive start attempts is one cycle -For ground starts (auto or manual)35 s between each cycle -After 3 cycles, or after 15 min of continuous or cumulative cranking: A 15 min cooling period is necessary before a new start motoring cycle is attempted.-No starter, engagement when N2 is above 20 %.

52
Q

REVERSE THRUST

A

Maximum reverse should not be used below 70 kt (Idle reverse is permitted down to aircraft stop)

53
Q

REDUCED THRUST (FLEX)

A

Takeoff at reduced thrust is not permitted on contaminated runways or into known windshear

54
Q

MAX CROSSWIND DURING START

A

35 Kts

55
Q

FLAPS and SLATS MAX operating altitude with slats and/or flaps extended

A

20,000 ft

56
Q

For JET A only, if TAT reaches:

A

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

57
Q

A320 Sharklet And A320 NEO MAX allowed wing fuel imbalance at TAKEOFF

A

Outer tank balanced Tank fuel quantity heavier tank FULL- MAX inner tank imbalance= 1102 lb

58
Q

A320 Sharklet And A320 NEO MAX allowed wing fuel imbalance at landing

A

Outer tank balanced Tank fuel quantity heavier tank FULL- MAX inner tank imbalance=3306lbs

59
Q

A321 Sharklet MAX allowed wing tank fuel imbalance at TAKEOFF

A

Tank fuel quantity heavier tank FULL- MAX imbalance= 882 lb

60
Q

MAX brake temperature for takeoff (brake fans off)

A

300 C

Spirit Airlines - Flows (45 decks)

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