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Airbus Limitations > Airbus Limitations > Flashcards

Airbus Limitations Flashcards

0
Q

NON - PRECISION APPROACHES with ENGINE – OUT. 319/321

A

If one engine is inoperative it is not permitted to use the autopilot to perform NPAs in the following modes FINAL APP, NAV V/S,
NAV/FPA.

Only FD use is permitted.

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1
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.

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2
Q

NON-PRECISION APPROACHES WITH ENGINE OUT. A320

A

If one engine is inoperative, it is permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/FPA

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3
Q

FLIGHT CONTROLS

Max operating altitude with slats and/or flaps extended is?

A

20,000 ft

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4
Q

CROSSWIND OPERATION ON GROUND

ENGINE START

A

This engine is capable of starting in crosswinds up to 35 knots

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5
Q

TAKEOFF AT REDUCED THRUST.

A

Is not permitted on contaminated runways

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6
Q

MAXIMUM REVERSE SHOULD NOT BE USED BELOW?

A

70 Knots

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7
Q

ENGINE STARTER

3 CONSECUTIVE CYCLES:

A
  • 2 cycles of 2 minutes each,
  • 3rd cycle of one minute.
    Pause between start attempts: 15 I seconds.
    Cooling Period: Following three startling attempts or 4 minutes of continuous cranking: 30 minutes.
    No running engagement of the starter when N2 is above 10%
    on the ground or 18% inflight
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8
Q

Maximum Reverse Thrust should not be used below?

A

70 KNOTS

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9
Q

OIL TEMPERATURE

Minimum starting temperature.

A

-40 C

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10
Q

OIL TEMPERATURE

Minimum prior to exceeding idle

A

-10 C

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11
Q

THRUST SETTING/EGT LIMITS

A319/A320

Starting:

Takeoff &Go-Around:

A

635* C

Time limit:

5 Minutes

10 minutes if engine failure

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12
Q

THRUST SETTINGS/EGT LIMITS

A321

A

650° C

TIME LIMIT:
5 Minutes
10 Minutes if single engine.

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13
Q

THRUST SETTING/EGT LIMITS

MCT. (temp./time)

A

610 C

TIME LIMIT: UNLIMITED

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14
Q

APU STARTING

APU starting with normal aircraft power supply and operation. (Max Alt.)p

A

FL 410

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15
Q

APU STARTING

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

A

25,000 ft

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16
Q

APU STARTER.

After three starter motor duty cycles

A

Wait 60 minutes before attempting 3 more cycles.

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17
Q

BRAKES

Maximum brake temperature for takeoff (Brake fans off)

A

300 C

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18
Q

FOR JET A ONLY, IF TAT REACHES,

-34 C

A

Monitor on FUEL SD page that fuel temperature remains higher than
-36C

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19
Q

MAXIMUM ALLOWED WING FUEL IMBALANCE

A321 587@588

A

Fuel tank quantity in heavier tank =full

maximum allowed imbalance
2910 lbs

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20
Q

MAXIMUM ALLOWED WING FUEL IMBALANCE.

APPLICABLE TO N619NK and SUBSEQUENT

A

Inner tanks with other tanks balanced

Tank fuel quantity in heavier tank= full.
Maximum allowed in balance=1,102 lbs.
Outer tanks. Maximum allowed imbalance. = 815 lbs.

21
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT

Take off 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 feet AGL (A319/A320)

900 feet AGL (A321)

27
Q

MINIMUM HEIGHT FOR USE OF AUTOPILOT:

Use of the AP or FD In OPEN DES MODE 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

WEIGHT LIMITATIONS

A319 MAX LANDING

A

137,788 lbs

29
Q

WEIGHT LIMITATIONS

MAXIMUM LANDING

Applicable to N601NK thru 617

Applicable to 618. and subsequent

A

145,505 lbs

30
Q

WEIGHT LIMITATIONS

MAX LANDING
A321

A

171,519 lbs.

31
Q

TAXI SPEED (A320/321)

When the taxi weight is higher than 167,550 lbs, do not exceed a taxi speed of?

A

20 Knots during a turn

32
Q

GEAR DOWN SPEEDS

MAX WITH LANDING GEAR EXTENDED. Vle

A

280 kt/ M .67

33
Q

GEAR DOWN SPEEDS

MAX LANDING GEAR EXTENSION (Vlo EXTENSION)

A

250 knots

34
Q

GEAR DOWN SPEEDS.

MAX LANDING GEAR RETRACTION (Vlo RETRACTION)

A

220 knots

35
Q

GEAR DOWN SPEEDS

MAX ALTITUDE LANDING GEAR MAY BE EXTENDED

A

25,000 ft

36
Q

WINDSHIELD WIPERS IN USE

MAX SPEED

A

230 knots

37
Q

MAX CABIN DIFF PX

A

+8.6

-1.0. Psi

38
Q

Max REV should not be used when airspeed…….

A

Starts to fluctuate

39
Q

MIN OIL QUANTITY

A

11qts + 0.3 qt/hr

40
Q

APU BLEED EXTRACTION

MAX ALT 2 packs
MAX ALT 1pack

A

2 PACKS. 15,000 ft

1 PACK. 20,000 ft

Air Bleed extraction from APU for wing Anti-Ice is not permitted

41
Q

LANDING GEAR

Max brake temp for takeoff
Brake fans off

A

300c

42
Q

Wingspans

    1. 321
  2. 321 Sharklet
A

111’ 10”

117’5”

43
Q

Runway slope. Mean

A

+or -2%

44
Q

Max runway altitude

A

9200 feet

45
Q

Nominal runway width

A

148 feet

46
Q

Max demonstrated Crosswind

A

38 knots gust included

47
Q

Max tailwind - takeoff

A

15 knots

48
Q

Max tailwind- landing

A

10 knots

49
Q

Max wind for passenger door operation

A

65 knots

Airbus Limitations (10 decks)

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