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Limitations Flashcards

(64 cards)

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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
Max negative differential pressure
-1.0 psi
26
Low Pressure (LP) ground unit:
* 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
High Pressure (HP) ground unit:
•Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage.
28
Avionics Ventilation System
49°C No limit
29
Minimum Altitude for Autopilot Use | Takeoff with SRS mode
100’ AGL
30
Minimum Altitude for Autopilot Use | Takeoff without SRS mode
900’ AGL
31
Minimum Altitude for Autopilot Use | Go-around
100’ AGL
32
Use of AP or FD in OP DES or DES mode is not authorized during approach below
Minimums, 500’ (A319/320), 900’ (A321), whichever is higher.
33
Autoland Engine Inoperative Approaches/Flap settings.
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
The use of an autopilot to fly a Non-Precision Engine Inoperative Approach.
Using NAV or FINAL APP lateral modes is not authorized. Only FD is permitted in this case.
35
NAV mode may be used in the terminal area, provided
* GPS PRIMARY is available, * HIGH accuracy is displayed, or * Navaid raw data is monitored.
36
Maximum field elevation for an autoland is
* 9200’ (A319) * 6500’ (A320) * 5750’ (A321)
37
Autolands may be accomplished using flaps
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
Category IIIB | • The FMA must display
CAT 3 DUAL
39
Category IIIA | •The FMA must display
CAT 3 DUAL or CAT 3 SINGLE
40
Category I | •The FMA must display
CAT 3 DUAL or CAT 3 SINGLE. | •Autolands to CAT I runways are authorized.
41
Automatic Landing Maximum Wind | Tailwind
10 knots
42
Automatic Landing Maximum Wind | Crosswind
15 knots
43
Automatic Landing Maximum Wind | Headwind
30 knots
44
Max continuous load per generator
100% (90 kVA)
45
Max continuous load per TR
200 A
46
Maximum altitude with flaps and/or slats extended
20,000’
47
For Jet A only, if TAT reaches
-34°C, monitor ECAM FUEL page that fuel temperature remains warmer than -36°C
48
Minimum Fuel Quantity for Takeoff
3307 lbs and the WING TK LO LVL warning must not be displayed on the ECAM
49
Normal hydraulic operating pressure
3000 psi +/- 200 psi
50
Maximum brake temperature for takeoff
300°C | brake fans off
51
The APU starter duty cycle
3 consecutive start attempts. After the third start attempt, wait 60 minutes before attempting 3 more cycles
52
Air bleed extraction from the APU for wing anti-ice
Is not permitted
53
The APU may be started (with normal A/C power supply) and operated up to
39,100’
54
The maximum altitude for a battery start (emergency electrical configuration) of the APU
FL250
55
The maximum altitude for APU Air bleed extraction
FL200 with one pack operating and FL150 with two packs operating
56
Oil temperature | Minimum prior to exceeding idle
-10°C
57
Oil temperature | Minimum prior to takeoff
50°C
58
Oil temperature | Maximum continuous temperature
155°C
59
Oil temperature | Maximum transient temperature
165°C | 15 min
60
Oil temperature | Minimum starting temperature
-40°C
61
Minimum oil pressure
60 psi
62
Engine Starter Limitations
``` 2 minutes on 15 seconds off 2 minutes on 15 seconds off 1 minute on 30 minutes off ```
63
Running engagement of the starter
N2 is above 10% on ground, or 18% in flight
64
Takeoff at reduced thrust
Is not permitted on contaminated runways or known windshear conditions

Airbus (3 decks)

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