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
MINIMUM HEIGHT FOR USE OF AUTOPILOT ILS APPROACH WHEN CAT 2 OR CAT 3 IS NOT DISPLAYED ON THE FMA
160 ft AGL
25
MINIMUM HEIGHT FOR USE OF AUTOPILOT GO AROUND (AP or FD) ENGAGEMENT
100 ft AGL
26
MINIMUM HEIGHT FOR USE OF AUTOPILOT ALL OTHER PHASES
500 feet AGL (A319/A320) 900 feet AGL (A321)
27
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:
Highest of : minimum or 500 ft (A319/A320) minimum or 900 ft (A321)
28
WEIGHT LIMITATIONS A319 MAX LANDING
137,788 lbs
29
WEIGHT LIMITATIONS MAXIMUM LANDING Applicable to N601NK thru 617 Applicable to 618. and subsequent
145,505 lbs
30
WEIGHT LIMITATIONS MAX LANDING A321
171,519 lbs.
31
TAXI SPEED (A320/321) When the taxi weight is higher than 167,550 lbs, do not exceed a taxi speed of?
20 Knots during a turn
32
GEAR DOWN SPEEDS MAX WITH LANDING GEAR EXTENDED. Vle
280 kt/ M .67
33
GEAR DOWN SPEEDS MAX LANDING GEAR EXTENSION (Vlo EXTENSION)
250 knots
34
GEAR DOWN SPEEDS. MAX LANDING GEAR RETRACTION (Vlo RETRACTION)
220 knots
35
GEAR DOWN SPEEDS MAX ALTITUDE LANDING GEAR MAY BE EXTENDED
25,000 ft
36
WINDSHIELD WIPERS IN USE | MAX SPEED
230 knots
37
MAX CABIN DIFF PX
+8.6 | -1.0. Psi
38
Max REV should not be used when airspeed.......
Starts to fluctuate
39
MIN OIL QUANTITY
11qts + 0.3 qt/hr
40
APU BLEED EXTRACTION MAX ALT 2 packs MAX ALT 1pack
2 PACKS. 15,000 ft 1 PACK. 20,000 ft Air Bleed extraction from APU for wing Anti-Ice is not permitted
41
LANDING GEAR | Max brake temp for takeoff Brake fans off
300c
42
Wingspans 319. 320. 321 320. 321 Sharklet
111' 10" 117'5"
43
Runway slope. Mean
+or -2%
44
Max runway altitude
9200 feet
45
Nominal runway width
148 feet
46
Max demonstrated Crosswind
38 knots gust included
47
Max tailwind - takeoff
15 knots
48
Max tailwind- landing
10 knots
49
Max wind for passenger door operation
65 knots