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Spirit Airbus A320 Training > Limitations 2017 > Flashcards

Limitations 2017 Flashcards

1
Q

Flight Maneuvering Load Acceleration Limits

A

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

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2
Q

Maximum Certified Altitude

A

FL398

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3
Q

Runway slope

A

+/-2%

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4
Q

Runway Altitude

A

9,200 ft

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5
Q

Nominal Runway Width

A

45 m (148 ft)

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6
Q

Maximum demonstrated crosswind at landing

A

38 kt (gust included)

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7
Q

Maximum tailwind for takeoff

A

15 kt

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8
Q

Maximum tailwind for landing

A

10 kt

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9
Q

Maximum wind for passenger door operation

A

65 kt

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10
Q

Maximum certified crosswind for takeoff NEO

A

35 kt (gust included)

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11
Q

Max with landing gear extended (VLE)

A

280 kt/M.67

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12
Q

Max landing gear extension (VLO Extension)

A

250 kt/M.60

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13
Q

Max landing gear retraction (VLO Retraction)

A

220 kt/M.54

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14
Q

Maximum Tire Speed

A

Ground speed. . . 195 kt

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15
Q

Windshield Wipers In Use

A

Max speed . . . . . . . 230 kt

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16
Q

Cockpit Window Open

A

Max speed. . . . 200 kt

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17
Q

Airflow supplied by the ground cart shall not exceed

A

2.60 lb/s.

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18
Q

Max positive differential pressure

A

9.0 PSI

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19
Q

Max negative differential pressure

A

-1.0 PSI

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20
Q

Safety relief valve setting

A

8.6 PSI

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21
Q

Minimum Height For Use Of Autopilot

A
  • 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
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22
Q

Takeoff with SRS mode

A

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

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23
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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24
Q

Minimum decision height CATII

A

100ft

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25
Q

CATIII Minimum Runway Visual Range

A

75m

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26
Q

MAX continuous load per generator

A

100% (90 KVA)

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27
Q

MAX continuous load per TR (continuous)

A

200 A

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28
Q

Max operating altitude with slats and/or flaps extended is

A

20,000ft

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29
Q

The minimum fuel quantity for takeoff is

A

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

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30
Q

Tanks must be emptied in the following order:

A

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

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31
Q

Hydraulic system normal operating pressure

A

3,000 PSI ± 200

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32
Q

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

A

300°C

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33
Q

The nosewheel steering angle is limited to

A

75° when using the handwheels

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34
Q

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

A

95 degrees

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35
Q

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

A

85 degrees

36
Q

APU Starter

A

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

37
Q

APU Rotor Speed

A

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

38
Q

The APU automatically shuts down at

A

107 % N speed

39
Q

Engine oil temperature minimum prior to exceeding idle

A

-10 °C

40
Q

Engine oil temperature minimum prior to takeoff

A

50 °C

41
Q

Engine oil maximum continuous temperature

A

155 °C

42
Q

Engine oil maximum transient temperature (15 min)

A

165 °C

43
Q

Minimum Engine oil starting temperature

A

-40 °C

44
Q

Engine oil minimum Oil Quantity V2500, PW1100G

A
  • 11 quarts, (average estimated consumption
    ~ 0.3 qt./h)
  • (PW1100G) 14 quarts
45
Q

Engine minimum Oil Pressure

A

65 PSI (N901NK THRU N905NK)

46
Q

Engine maximum oil pressure

A

270 PSI

47
Q

Reverse Thrust limitations

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.
48
Q

FLEX thrust

A

Takeoff at reduced thrust is not permitted on contaminated runways.

49
Q

Crosswind Operation on Ground engine start

A

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

50
Q

Crosswind Takeoff max CEO

A

38 kt (gust included)

51
Q

A319, A320 Wingspans

A
  • Wing 111’10
52
Q

A320, A321 Sharklet dementions

A
  • Wing 117’5 Difference
53
Q

How man seats A320/A320 Shark Fins/A320 Neo

A
  • 178/182

- NEO 182

54
Q

How man seats A319

A
  • 145
55
Q

How man seats A321

A
  • 218
56
Q

How man seats A321 Shark Fins

A
  • 228
57
Q

Max landing weight A320/A320 shark fins

A
  • 145,505
58
Q

Max landing weight A319

A
  • 137,788
59
Q

Max landing weight A321/A21 shark fins

A
  • 171,519
60
Q

Max landing weight A320 Neo

A
  • 148,591
61
Q

Max Taxi Speed

A
  • 167,550 lbs 20 KTS in a turn
62
Q

Air Conditioning with LP Ground unit?

A
  • Do not use conditioned air simultanously from PACKS and LP ground unit (to avoid chattering of non-return values)
63
Q

APU with HP ground unit?

A
  • Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage.
64
Q

Max tail wind for CAT II, III?

A
  • 5 knots (surface winds)
65
Q

Max head wind for CAT II,III?

A
  • 15 knots (surface winds)
66
Q

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

A
  • Inner tanks: Heavier tank full 1,102
67
Q

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

A
  • Inner tanks: Heavier tank full 3,306
68
Q

Max fuel imbalance landing (wing tanks) A321?

A
  • Inner tanks: heavier tank full 2,910
69
Q

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

A
  • Inner tanks heavier tank full 882
70
Q

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

A

FL410

71
Q

EGT Limit for Starting (CEO)

A

635 C

72
Q

EGT Limit for Starting (A320-NEO)

A

1083 degrees C

73
Q

EGT Limit for TOGA (A319/A320-CEO)

A

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

74
Q

EGT Limit for TOGA (A321)

A

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

75
Q

EGT Limit for TOGA (NEO)

A

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

76
Q

EGT Limit for MCT (CEO)

A

610 C

77
Q

EGT Limit for MCT (NEO)

A

1043 C

78
Q

Max Reverse Thrust should not be used below:

A

70 knots

79
Q

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

A

Airspeed indication starts to fluctuate.

80
Q

Reduced thrust takeoff is not permitted:

A

On contaminated runways.

81
Q

Tailstrike Pitch Attitude A319 L/G Struts Compressed?

A

13.9 Degrees

82
Q

Tailstrike Pitch Attitude A320 L/G Struts Compressed?

A

11.7 Degrees

83
Q

Tailstrike Pitch Attitude A320 NEO L/G Struts Compressed?

A

11.7 Degrees

84
Q

Tailstrike Pitch Attitude A321 L/G Struts Compressed?

A

9.7 Degrees

85
Q

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

A

5,575 Feet

86
Q

Is Flex takeoff allowed on contaminated runway?

A

NO TOGA only

Spirit Airbus A320 Training (52 decks)

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