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Spirit Airbus A320 Training > Limitations > Flashcards

Flashcards in Limitations Deck (86):
1

Flight Maneuvering Load Acceleration Limits

Clean configuration. . . . . . . . . . . . . . . . . . . . -1.0g to +2.5g
• Slats and flaps extended . . . . . . . . . . . . . . . . . 0g to +2.0g
• Slats extended and flaps retracted . . . . . . . . 0g to +2.0g

2

Maximum Certified Altitude

FL398

3

Runway slope

+/-2%

4

Runway Altitude

9,200 ft

5

Nominal Runway Width

45 m (148 ft)

6

Maximum demonstrated crosswind at landing

38 kt (gust included)

7

Maximum tailwind for takeoff

15 kt

8

Maximum tailwind for landing

10 kt

9

Maximum wind for passenger door operation

65 kt

10

Maximum certified crosswind for takeoff NEO

35 kt (gust included)

11

Max with landing gear extended (VLE)

280 kt/M.67

12

Max landing gear extension (VLO Extension)

250 kt/M.60

13

Max landing gear retraction (VLO Retraction)

220 kt/M.54

14

Maximum Tire Speed

Ground speed. . . 195 kt

15

Windshield Wipers In Use

Max speed . . . . . . . 230 kt

16

Cockpit Window Open

Max speed. . . . 200 kt

17

Airflow supplied by the ground cart shall not exceed

2.60 lb/s.

18

Max positive differential pressure

9.0 PSI

19

Max negative differential pressure

-1.0 PSI

20

Safety relief valve setting

8.6 PSI

21

Minimum Height For Use Of Autopilot

- After take/off with SRS mode 100 ft AGL
- Straight-in non-precision approach Applicable Minimum
- Circling Approach
- Applicable Circling Minimums - 100 ft.
- ILS approach when CAT 2 or CAT 3 is not displayed on the FMA 160 ft AGL
- Go-Around (AP or FD engagement) 100 ft AGL
- All other phases 500 ft AGL (A319/A320) 900 ft AGL (A321)
- 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: Highest of: Minimum or 500 ft (A319/A320) Minimum or 900 ft (A32

22

Takeoff with SRS mode

An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.

23

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

- 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.

24

Minimum decision height CATII

100ft

25

CATIII Minimum Runway Visual Range

75m

26

MAX continuous load per generator

100% (90 KVA)

27

MAX continuous load per TR (continuous)

200 A

28

Max operating altitude with slats and/or flaps extended is

20,000ft

29

The minimum fuel quantity for takeoff is

3307 lb and the WING TK LO LVL warning must not be displayed on the ECAM.

30

Tanks must be emptied in the following order:

Center tank then wing tanks. T/O on center tank prohibited

31

Hydraulic system normal operating pressure

3,000 PSI ± 200

32

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

300°C

33

The nosewheel steering angle is limited to

75° when using the handwheels

34

For towing and pushback, the nosewheel steering angle is limited to

95 degrees

35

Towbarless towing and pushback on the nose landing gear is approved for the “accepted towbarless towing vehicles,” but the nosewheel steering angle must be limited to

85 degrees

36

APU Starter

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

37

APU Rotor Speed

Maximum N (ECAM display) . . . . . . . . . . . . . 107 %

38

The APU automatically shuts down at

107 % N speed

39

Engine oil temperature minimum prior to exceeding idle

-10 °C

40

Engine oil temperature minimum prior to takeoff

50 °C

41

Engine oil maximum continuous temperature

155 °C

42

Engine oil maximum transient temperature (15 min)

165 °C

43

Minimum Engine oil starting temperature

-40 °C

44

Engine oil minimum Oil Quantity V2500, PW1100G

- 11 quarts, (average estimated consumption
~ 0.3 qt./h)
- (PW1100G) 14 quarts

45

Engine minimum Oil Pressure

60 PSI / 65 PSI (N901NK THRU N905NK)

46

Engine maximum oil pressure

270 PSI

47

Reverse Thrust limitations

- 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.

48

FLEX thrust

Takeoff at reduced thrust is not permitted on contaminated runways.

49

Crosswind Operation on Ground engine start

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

50

Crosswind Takeoff max CEO

38 kt (gust included)

51

A319, A320 Wingspans

- Wing 111'10

52

A320, A321 Sharklet dementions

- Wing 117'5 Difference

53

How man seats A320/A320 Shark Fins/A320 Neo

- 178/182
- NEO 182

54

How man seats A319

- 145

55

How man seats A321

- 218

56

How man seats A321 Shark Fins

- 228

57

Max landing weight A320/A320 shark fins

- 145,505

58

Max landing weight A319

- 137,788

59

Max landing weight A321/A21 shark fins

- 171,519

60

Max landing weight A320 Neo

- 148,591

61

Max Taxi Speed

- 167,550 lbs 20 KTS in a turn

62

Air Conditioning with LP Ground unit?

- Do not use conditioned air simultanously from PACKS and LP ground unit (to avoid chattering of non-return values)

63

APU with HP ground unit?

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

64

Max tail wind for CAT II, III?

- 5 knots (surface winds)

65

Max head wind for CAT II,III?

- 15 knots (surface winds)

66

Max fuel imbalance takeoff (A320-s, A320-NEO) (Outer tanks balanced)?

- Inner tanks: Heavier tank full 1,102

67

Max fuel imbalance in flight for landing? (A320-S, A320-NEO) (Outer tanks balanced)?

- Inner tanks: Heavier tank full 3,306

68

Max fuel imbalance landing (wing tanks) A321?

- Inner tanks: heavier tank full 2,910

69

Max fuel imbalance takeoff (wing tanks) A321-S?

- Inner tanks heavier tank full 882

70

Max Altitude for APU Start (on A/C power) and Operation

FL410

71

EGT Limit for Starting (CEO)

635 C

72

EGT Limit for Starting (A320-NEO)

1083 degrees C

73

EGT Limit for TOGA (A319/A320-CEO)

635 C (5 min/10 min in case of engine failure)

74

EGT Limit for TOGA (A321)

650 C (5 min/10 min in case of engine failure)

75

EGT Limit for TOGA (NEO)

1083 C (5 min/10 min in case of engine failure)

76

EGT Limit for MCT (CEO)

610 C

77

EGT Limit for MCT (NEO)

1043 C

78

Max Reverse Thrust should not be used below:

70 knots

79

Max reverse should not be used when (A319/A320):

Airspeed indication starts to fluctuate.

80

Reduced thrust takeoff is not permitted:

On contaminated runways.

81

Tailstrike Pitch Attitude A319 L/G Struts Compressed?

13.9 Degrees

82

Tailstrike Pitch Attitude A320 L/G Struts Compressed?

11.7 Degrees

83

Tailstrike Pitch Attitude A320 NEO L/G Struts Compressed?

11.7 Degrees

84

Tailstrike Pitch Attitude A321 L/G Struts Compressed?

9.7 Degrees

85

Max airport elevation for Cat II or Cat III Conf full or 3

5,575 Feet

86

Is Flex takeoff allowed on contaminated runway?

NO TOGA only