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Limitations Flashcards

1
Q

Max runway slope

A

+/- 2%

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2
Q

Max runway altitude

A

9200’

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3
Q

Nominal runway width

A

150’
Note:A319 and A320 can operate to runways as narrow as 98’ when operated in accordance with the “Narrow Runway Operations” procedure in the Supplemental section.

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4
Q

Max crosswind demonstrated

A

38 knots (gust included)

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5
Q

Max tailwind - takeoff

A

15 knots

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6
Q

Max tailwind - landing

A

10 knots

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7
Q

Max wind for pax door operation

A

65 knots

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8
Q

Max wind for cargo door opening

A

40 knots (50 knots if nose is into the wind or door is on leeward side)

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9
Q

Max wind before cargo door must be closed

A

65 knots

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10
Q

Load Acceleration Limits

Clean configuration

A

-1g to +2.5g

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11
Q

Load Acceleration Limits

Slats and flaps extended

A

0g to +2.0g

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12
Q

Max takeoff weight

A

169,700 lbs

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13
Q

Max landing weight

A

145,500 lbs

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14
Q

A319/A320 Turbulent Air Penetration Speed

A
  • At or above FL200, maintain 275 knots/.76 Mach.

* Below FL200, maintain 250 knots.

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15
Q

A321 Turbulent Air Penetration Speed

A
  • At or above FL200, maintain 300 knots/.76 Mach.

* Below FL200, maintain 270 knots.

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16
Q

Max with landing gear extended

A

280 knots/M.67

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17
Q

Max landing gear extension

A

250 knots

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18
Q

Max landing gear retraction

A

220 knots

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19
Q

Max altitude landing gear may be extended

A

FL250

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20
Q

Tires: Max ground speed

A

195 knots

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21
Q

Windshield Wiper In Use

Max speed

A

230 knots

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22
Q

Cockpit Window Open

Max speed

A

200 knots

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23
Q

A320/A321 Taxi Speed

Max speed during a turn if weight

A

> 167,500 lbs . . . . .20 knots

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24
Q

Max positive differential pressure

A

8.6 psi

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25
Q

Max negative differential pressure

A

-1.0 psi

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26
Q

Low Pressure (LP) ground unit:

A
  • Do not use conditioned air simultaneously from pack and LP ground unit (to avoid chattering of non-return valves).
  • Airflow supplied by the ground cart shall not exceed 2.60 lb/s.
27
Q

High Pressure (HP) ground unit:

A

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

28
Q

Avionics Ventilation System

A

49°C No limit

29
Q

Minimum Altitude for Autopilot Use

Takeoff with SRS mode

A

100’ AGL

30
Q

Minimum Altitude for Autopilot Use

Takeoff without SRS mode

A

900’ AGL

31
Q

Minimum Altitude for Autopilot Use

Go-around

A

100’ AGL

32
Q

Use of AP or FD in OP DES or DES mode is not authorized during approach below

A

Minimums, 500’ (A319/320), 900’ (A321), whichever is higher.

33
Q

Autoland Engine Inoperative Approaches/Flap settings.

A

CAT II and III fail passive autoland are approved in configuration 3 and FULL, and only if engine-out procedures are completed before reaching 1000 feet on approach.

34
Q

The use of an autopilot to fly a Non-Precision Engine Inoperative Approach.

A

Using NAV or FINAL APP lateral modes is not authorized. Only FD is permitted in this case.

35
Q

NAV mode may be used in the terminal area, provided

A
  • GPS PRIMARY is available,
  • HIGH accuracy is displayed, or
  • Navaid raw data is monitored.
36
Q

Maximum field elevation for an autoland is

A
  • 9200’ (A319)
  • 6500’ (A320)
  • 5750’ (A321)
37
Q

Autolands may be accomplished using flaps

A

FLAPS 3 or FLAPS FULL up to the maximum landing weight of the aircraft.
Note:In case of emergency, an autoland may be performed up to 152,117 lbs (A319).

38
Q

Category IIIB

• The FMA must display

A

CAT 3 DUAL

39
Q

Category IIIA

•The FMA must display

A

CAT 3 DUAL or CAT 3 SINGLE

40
Q

Category I

•The FMA must display

A

CAT 3 DUAL or CAT 3 SINGLE.

•Autolands to CAT I runways are authorized.

41
Q

Automatic Landing Maximum Wind

Tailwind

42
Q

Automatic Landing Maximum Wind

Crosswind

43
Q

Automatic Landing Maximum Wind

Headwind

44
Q

Max continuous load per generator

A

100% (90 kVA)

45
Q

Max continuous load per TR

46
Q

Maximum altitude with flaps and/or slats extended

47
Q

For Jet A only, if TAT reaches

A

-34°C, monitor ECAM FUEL page that fuel temperature remains warmer than -36°C

48
Q

Minimum Fuel Quantity for Takeoff

A

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

49
Q

Normal hydraulic operating pressure

A

3000 psi +/- 200 psi

50
Q

Maximum brake temperature for takeoff

A

300°C

brake fans off

51
Q

The APU starter duty cycle

A

3 consecutive start attempts. After the third start attempt, wait 60 minutes before attempting 3 more cycles

52
Q

Air bleed extraction from the APU for wing anti-ice

A

Is not permitted

53
Q

The APU may be started (with normal A/C power supply) and operated up to

54
Q

The maximum altitude for a battery start (emergency electrical configuration) of the APU

55
Q

The maximum altitude for APU Air bleed extraction

A

FL200 with one pack operating and FL150 with two packs operating

56
Q

Oil temperature

Minimum prior to exceeding idle

57
Q

Oil temperature

Minimum prior to takeoff

58
Q

Oil temperature

Maximum continuous temperature

59
Q

Oil temperature

Maximum transient temperature

A

165°C

15 min

60
Q

Oil temperature

Minimum starting temperature

61
Q

Minimum oil pressure

62
Q

Engine Starter Limitations

A 
2 minutes on
15 seconds off
2 minutes on
15 seconds off
1 minute on
30 minutes off
63
Q

Running engagement of the starter

A

N2 is above 10% on ground, or 18% in flight

64
Q

Takeoff at reduced thrust

A

Is not permitted on contaminated runways or known windshear conditions

Airbus (3 decks)

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