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Spirit > Limitations > Flashcards

Limitations Flashcards

1
Q

Wingspans

A

A319, A320, A321 - 111 feet, 10 inches

A319, A320, A321 Sharklet - 117 feet, 5 inches

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2
Q

Maximum Certified Altitude

A

FL 398

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3
Q

Max Landing Weights

A

A319 - 137,788

A320 - 145,505

A320 NEO - 148,591

A321 - 171,519

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4
Q

Airport Operations:

Runway Slope

Runway Altitude

Nominal Runway Width

A

Airport Operations:

Runway Slope- +/-2%

Runway Altitude- 9200’

Nominal Runway Width- 148 feet (45 meters)

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5
Q

Wind Limitations

Max tailwind for takeoff

Max wind for landing

Max wind for pax door operation

A

Max tailwind for takeoff- 15kt

Max tailwind for landing- 10kt

Max wind for pax door operation- 65kt

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6
Q

Crosswind

Max Demonstrated Crosswind for Landing

Max Certified Wind for takeoff (NEO)

A

Max Demonstrated Crosswind for Landing- 38 kt (gust included)

Max Certified Wind for takeoff (NEO)- 35 kt (gust included)

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7
Q

Speed Limitations

Gear Down Speeds
Max with landing gear extended (VLE)

Max landing gear extension (VLO Extension)

Max landing gear retraction (VLO Retraction)

Max altitude landing gear may be extended

A

Gear Down Speeds
Max with landing gear extended (VLE) ………………….280 kt/M0.67
Max landing gear extension (VLO Extension) ………….250 kt/M0.60
Max landing gear retraction (VLO Retraction)………….220 kt/M0.54
Max altitude landing gear may be extended …………….25,000 ft

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8
Q

Windshield Wipers in Use

Max Speed

A

230 kts

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9
Q

Taxi Speed

A320 A321

A

When the taxi weight is higher than 167,550 lb, do not exceed a taxi speed of 20 kt during a turn.

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10
Q

Air Condition/Pressurization/Ventilation

A

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

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11
Q

APU with HP ground unit

A

Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage

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12
Q

Cabin Pressure

Max Positive Differential Pressure

Max Negative Differential Pressure

A

Max Positive Differential Pressure… 9.0psi

Max Negative Differential Pressure…-1.0psi

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13
Q

Auto Flight

T.O. With SRS mode
Straight-in np approach
Circling Approach
ILS When Cat II or III not displayed in FMA
Go-Around (FD or autopilot engagement)
All other phases
Use of autopilot or fd in open des or des mode not permitted in approach, unless fma is set at or above:

A

T.O. With SRS mode 100’

Straight-in np approach- Applicable MDA

Circling Approach- MDA -100’

ILS When Cat II or III not displayed in FMA…160’

Go-Around (FD or autopilot engagement)…100’

All other phases - 500’AGL (319/320) 900’AGL (321)

Use of autopilot or fd in open des or des mode not permitted in approach, unless fma is set at or above: 500’AGL (319/320) 900’AGL (321)

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14
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
  • FMS navigation is cross-checked with NAVAID raw data
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15
Q

Non-Precision Approaches with engine-out

Applicable to N502NK thru N588NK, N657NK thru N678NK

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

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16
Q

Maximum Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out

Applicable to N901NK thru N905NK

A

Crosswind 15 kt

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17
Q

Flight Controls

Max operating altitude with slats and/or flaps extended

A

20,000’

18
Q

With All Engines Operative (AEO), Maximum Wind
Conditions for CAT II or CAT III Automatic Approach,
Landing and Roll Out

Applicable to N502NK thru N536NK

A

Tail wind: 5 kt

Crosswind: 15 kt

19
Q

With One Engine Operative (OEI), Maximum Wind
Conditions for CAT II or CAT III Automatic Approach,
Landing and Roll Out

Applicable to N502NK thru N536NK

A

Headwind: 15 kt
Tail wind: 5 kt
Crosswind: 10 kt

20
Q

Maximum Wind Conditions for CAT II or CAT III Automatic
Approach, Landing and Roll Out

Applicable to N601NK and thru N617NK
And N618NK thru N650NK

A

Crosswind: 15 kt

21
Q

Maximum Wind Conditions for CAT II or CAT III Automatic
Approach, Landing and Roll Out (continued)

Applicable to N901NK thru N905NK

A

Tail wind: 5 kt

Cross wind: 15 kt

22
Q

Maximum Wind Conditions for CAT II or CAT III Automatic
Approach, Landing and Roll Out (continued)

Applicable to N587NK, N588NK, N657NK thru N683NK

A

Cross wind: 15 kt

23
Q

Fuel Temperature

A

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

24
Q

Brakes

A

Maximum brake temperature for takeoff
(brake fans (if installed) off)
. . . . . . . . . . . . . . . . . . .. . . . . . . . . . 300°C

25
Q

APU Starter

A

APU Starter

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

26
Q

Thrust Setting/EGT Limits

Applicable to N502NK thru N653NK

A 
TAKEOFF and GO-AROUND 635 °C
5 min (10 min Only in case of engine failure)

MCT Unlimited 610 °C

STARTING 635 °C

27
Q

Thrust Setting/EGT Limits

Applicable to N588NK, N657NK thru N687NK

A 
TAKEOFF and GO-AROUND 650 °C
5 min (10 min Only in case of engine failure)

MCT Unlimited 610 °C

STARTING 635 °C

28
Q

Thrust Setting/EGT Limits

Applicable to N901NK thru N905NK

A 
T.O. and Go-around   1083 °C  
5 min (10 min Only in case of engine failure)

MCT Unlimited 1043 °C

STARTING 1018 °C

29
Q

Oil Temperature

N502NK thru N683NK

A

Minimum prior to exceeding idle . . -10 °C

Minimum starting temp. . . . . .-40 °C

30
Q

Minimum Oil Pressure

Applicable to N901NK thru N905NK

A

65 psi

31
Q

Starter

Applicable to N502NK thru N687NK

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 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.
32
Q

Starter

Applicable to N901NK thru N905NK

A
  • A standard automatic start that includes up to three 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%.
33
Q

Reverse Thrust

Applicable to N502NK thru N536NK, N601NK thru N650NK, N901NK thru N905NK

A

Maximum reverse should not be used below 70 kt (or when the airspeed indication starts to fluctuate). Idle reverse is permitted down to aircraft stop.

34
Q

Reverse Thrust

Applicable to N587NK, N588NK, N657NK thru N687NK

A

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

35
Q

Reduced Thrust Takeoff

A

Takeoff at reduced thrust is not permitted on contaminated runways.

36
Q

Crosswind Operation on Ground

Applicable to N502NK thru N683NK

A

This engine is capable of starting in crosswinds up to 35 kt.

37
Q

Crosswind Operation On Ground

N901NK thru N905NK

A

Engine Start
The engine is capable of starting in crosswinds up to 35 kt.

Takeoff
Engine crosswind limit at takeoff: 35 kt (gust included).

38
Q

Fuel Imbalance
Takeoff/Inflight and Landing
N618NK-N650NK (A320 Sharklet) & NEO’s

A

Takeoff - 1102

Inflight and Landing - 3306

39
Q

Fuel Imbalance
Inflight and Landing
N588NK (A321 Non-sharklet)

A

2910

40
Q

Fuel Imbalance Takeoff

N657NK-N687NK (A321 Sharklet)

A

882

41
Q

Tailstrike Pitch Attitude

A

Tailstrike Pitch Attitude

                          L/G Struts Compressed

A319 13.9°

A320 11.7°
NEO 11.7°

A321 9.7°

Spirit (7 decks)

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