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A-320 > Limitations > Flashcards

Limitations Flashcards

0
Q

What is the maximum landing weight for the A-320?

A

145,505 lbs.

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1
Q

What is the maximum landing weight for the A-319?

A

137,788 lbs.

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2
Q

What is the maximum landing weight for the A-321

A

171,519 lbs.

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3
Q

What is the maximum certified altitude?

A

FL398

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4
Q

Mean Runway Slope

A

+/- 2%

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5
Q

Max Runway Altitude

A

9200’

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6
Q

Nominal Runway Width

A

148’

A319 and A320 can operate to
runways as narrow as 98 ft when operated in accordance with
the “Operations on Narrow Runways” procedure.

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7
Q

Max Demonstrated Crosswind

A

38 knots (gust included)

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8
Q

Max Tailwind - Takeoff

A

15 knots

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9
Q

Max Tailwind - Landing

A

10 knots

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10
Q

Max Wind for PAX Door Operation

A

65 knots

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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

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13
Q

Max landing gear retraction (VLO Retraction)

A

220 kt

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14
Q

Max altitude landing gear may be extended

A

25,000 ft

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15
Q

Windshield Wipers In Use

• Max speed…

A

230 kt

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16
Q

Taxi Speed (A320/A321)

A

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

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17
Q

Air Conditioning With LP Ground Unit

A

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

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18
Q

Air Conditioning With HP Ground Unit

A

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

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19
Q

Cabin Pressure

• Max positive differential pressure. . . . . . . . . . .

A

8.6 psi

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20
Q

Cabin Pressure

• Max negative differential pressure . . . . . . . . . .

A

-1.0 psi

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21
Q

Minimum Height For Use Of Autopilot

Takeoff with SRS mode

A

100 ft AGL

22
Q

Minimum Height For Use Of Autopilot

Straight-in non-precision approach

A

Applicable Minimum

23
Q

Minimum Height For Use Of Autopilot

Circling Approach

A

Applicable Circling

Minimums - 100 ft.

24
Q

Minimum Height For Use Of Autopilot

ILS approach when CAT 2 or CAT 3
is not displayed on the FMA

A

160 ft AGL

25
Q

Minimum Height For Use Of Autopilot

Go-Around (AP or FD engagement)

A

100 ft AGL

26
Q

Minimum Height For Use Of Autopilot

All other phases

A

500 ft AGL (A319/A320)

900 ft AGL (A321)

27
Q

Minimum Height For Use Of Autopilot

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:

A

Highest of:
Minimum or 500 ft (A319/A320)
Minimum or 900 ft (A321)

28
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
  • NAVAID raw data is monitored.
29
Q

Non-Precision Approaches with Engine-Out
A319/A321
If one engine is inoperative, it is not permitted to use the autopilot to
perform NPAs in the following modes:

A

FINAL APP, NAV V/S,
NAV/FPA.
Only FD use is permitted.

30
Q

Max operating altitude with slats and/or flaps extended:

A

20,000 ft.

31
Q

APPLICABLE TO N618NK AND SUBSEQUENT

Fuel Imbalance At Takeoff
Inner Tanks (Outer Tanks Balanced)
Tank Fuel Quantity

(Heavier Tank) Maximum Allowed Imbalance

A

Full 1102 lbs.

32
Q

APPLICABLE TO N618NK AND SUBSEQUENT

Fuel Imbalance At Takeoff
Outer Tanks (Inner Tanks Balanced)
Maximum Allowed Imbalance

A

815 lbs

33
Q

APPLICABLE TO N587NK, N588NK
Wing Tanks
Maximum Allowed Imbalance

Tank Fuel Quantity Maximum Allowed Imbalance
(Heavier Tank)

A

Full 2,910 lbs

34
Q

For Jet A only, if TAT reaches:

A

-34°C, monitor on FUEL SD page

that fuel temperature remains higher than -36°C

35
Q

Minimum Fuel Quantity for Takeoff:

A

3,307 lbs.

36
Q

Maximum brake temperature for takeoff (brake fans off)

A

300°C

37
Q

APU Starter

A

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

38
Q

APU Bleed Extraction

Max altitude with two PACKS operating

A

15,000 ft

39
Q

APU Bleed Extraction

Max altitude with one PACK operating

A

20,000 ft

40
Q

Maximum altitude for APU start on
battery power (emergency electrical
configuration)

A

25,000 ft

41
Q 
APU starting (with normal A/C power 
supply) and operation
A

FL 410

42
Q

Thrust Setting/EGT Limits

Starting

A

635°C

43
Q

Thrust Setting/EGT Limits

Takeoff & Go-Around
A319/A320

A

635°C

5 min
10 min
If Engine Failure

44
Q

Thrust Setting/EGT Limits

Takeoff & Go-Around
A321

A

650°C

5 min
10 min
If Engine Failure

45
Q

Thrust Setting/EGT Limits

MCT

A

610°C

46
Q

Oil Temperature

• Minimum starting temperature

A

-40°C

47
Q

Oil Temperature

• Minimum prior to exceeding idle

A

-10°C

48
Q

Minimum oil quantity . . .

A

11qts + est. consumption (~0.3 qt/hr)

49
Q

Engine Starter Duty Cycles

A

3 consecutive cycles:
- 2 cycles of 2 minutes each,
- 3rd cycle of 1 minute.
Pause between start attempts: 15 seconds.
Cooling period, following 3 start attempts or 4 minutes of continuous
cranking: 30 minutes.

No running engagement of the starter, when N2 is above 10% on
ground, or 18% in flight.

50
Q

Maximum reverse should not be used below…

A

70 kts.

APPLICABLE TO N502NK THRU N534NK
N601NK AND SUBSEQUENT:

Maximum reverse should not be used when airspeed indication starts to fluctuate.

51
Q

Takeoff at reduced thrust is not permitted on?

A

contaminated runways

52
Q

This engine is capable of starting in crosswinds up to:

A

35 knots.

A-320 (1 decks)

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