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AA Airbus 319/320/321 > Chap 2 Limitations BOLD ITEMS > Flashcards

Chap 2 Limitations BOLD ITEMS Flashcards

1
Q

Maximum wind for takeoff and landing?

A

50 knots (A)

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2
Q

Maximum crosswind for takeoff and landing?

A

35 knots 1 (including gusts) (A)

1 Maximum crosswind values have been demonstrated with flight controls in normal law as well as direct law with and without yaw damper.

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3
Q

Maximum crosswind for landing Vis < 4000 or 3/4?

A

15 knots (A)

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4
Q

Maximum crosswind (including gusts) for Autoland (Vis > 4000 3/4)?

A

20 knots (2)

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5
Q

Maximum tailwind component for takeoff

(A320 and A321 with IAE engines)?

A

10 knots

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6
Q

Maximum tailwind component for takeoff

(All A319 and A320/321 with CFM engines)?

A

15 knots

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7
Q

Maximum tailwind component for landing

(Non- Sharklet)?

A

10 knots

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8
Q

Maximum tailwind component for landing

(Sharklet)?

A

15 knots

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9
Q

Maximum operating altitude?

A

39,000 feet (A)

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10
Q

Maximum operating altitude with flaps and/or slats extended?

A

20,000 feet

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11
Q

Maximum gear extension altitude?

A

25,000 feet

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12
Q

Maximum operating airspeed (SL to FL 246)?

A

350 KIAS

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13
Q

Maximum operating Mach number (> FL 246)?

A

.82M (Mmo)

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14
Q

Maximum taxi speed?

A

30 knots (A)

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15
Q

Maximum taxi speed for 90 degree turn?

A

10 knots (A)

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16
Q

Max Flap Operating Speed Flap Position 1 ?

A

A319/320: 230 Kias

A321: 235 Kias

17
Q

Max Flap Operating Speed Flap Position 1 + F?

A

A319/320: 215 Kias

A321: 225 Kias

18
Q

Max Flap Operating Speed Flap Position 2?

A

A319/320: 200 Kias

A321: 215 Kias

19
Q

Max Flap Operating Speed Flap Position 3?

A

A319/320: 185 Kias

A321: 195 Kias

20
Q

Max Flap Operating Speed Flap Position Full?

A

A319/320: 177 Kias

A321: 190 Kias

21
Q

Definition of Icing Conditions?

A
  • OAT (on the ground and for takeoff) or TAT (inflight) is 10 degrees or below, and
  • visible moisture in any form is present such as clouds, fog, with visibility of one mile or less, rain, snow, sleet and ice crystals, or
  • when operating on ramps, taxiways, or runways where the surface snow, ice, standing water, or slush my be ingested by engines, freeze on engines, nacelles, or engine sensor probes.
22
Q

When must the ENGINE ANTI-ICE System be on?

A

During all ground and flight operations when icing conditions exist or are anticipated, except during climbs and cruise when the temperature is BELOW -40 degrees C SAT. Engine Anit-ice must be on prior to and during descent in icing conditions, including temperatures below -40 degrees C SAT.

23
Q

CAUTION for Engine Anti-Ice?

A

Do not rely on visual airframe icing cues to select engine anti- ice ON. Use temperature and visual moisture criteria specified in this section. Delaying the use of engine anti-ice until ice buildup is visible from the flightdeck may result in severe engine damage and/or flameout.

24
Q

Approved Fuels?

A

JET A JET A1

25
Q

Fuel Temperature Limits:

Min?

Max?

A

Min: -36 C

Max: +54 C

26
Q

Maximum Allowed Wing Fuel Imbalance A319 (Sharklets) Inner Tanks (Outer Balanced)?

Tank Fuel Quantity (Heavier Tank):

At takeoff?

Maximum Allowed Imbalance:

At takeoff?

A

Tank Fuel Quantity (Heavier Tank):

  • Full
  • 6,613 lbs
  • 3,196 lbs

Maximum Allowed Imbalance:

  • 1,102 lbs
  • 2,314 lbs
  • 3,196 lbs
27
Q

Maximum Allowed Wing Fuel Imbalance A319 (Sharklets) Inner Tanks (Outer Balanced)?

Tank Fuel Quantity (Heavier Tank):

In flight and at landing?

Maximum Allowed Imbalance:

In flight and at landing?

A

Tank Fuel Quantity (Heavier Tank):

  • Full
  • 9,479 lbs
  • 4,960 lbs

Maximum Allowed Imbalance:

  • 3,306 lbs
  • 3,527 lbs
  • 4,960 lbs
28
Q

Maximum Allowed Wing Fuel Imbalance A319 (Sharklets) Outer Tanks,

At takeoff? Inflight and at landing?

A

At takeoff:

Outer Tank maximum allowed imbalance is 815 lbs.1

In flight and at landing:

Outer Tank maximum allowed imbalance is 1,521lbs.1

1Exception: The maximum outer wing tank imbalance (one full/one empty) is allowed provided:

The fuel content of one side (outer + inner) is equal to the content of the other side (outer + inner), or

On the side of the lighter outer tank, the inner tank fuel quantity is higher than the opposite inner tank quantity, up to a maximum of 6,614 lbs. higher.

29
Q

Maximum Allowed Wing Fuel Imbalance A321 (Sharklets):

Tank Fuel Quanitity (Heavier Tank):

At takeoff?

Max Allowed Imbalance:

At takeoff?

A

Tank Fuel Quanitity (Heavier Tank) At takeoff:

  • Full
  • 6,614 lbs
  • 1,543 lbs

Max Allowed imbalance At takeoff:

  • 882 lbs
  • 882 lbs
  • 1,543 lbs
30
Q

Maximum Allowed Wing Fuel Imbalance A321 (Sharklets):

Tank Fuel Quanitity (Heavier Tank):

Inflight and at landing?

Max Allowed Imbalance:

Inflight and at landing?

A

Tank Fuel Quanitity (Heavier Tank) Inflight and at landing:

In flight and at landing:

  • Full
  • 8,818 lbs
  • 5,180 lbs

Max Allowed Imbalance Inflight and at landing:

In flight and at landing:

  • 2,910 lbs
  • 3,196 lbs
  • 5,180 lbs
31
Q

What must be considered if a plane is dispatched with fuel in the center tanks?

A
  • wing tanks must be full. Otherwise, the center tank fuel must be treated as ballast (unusable fuel). (A)
  • Take off using center tank fuel is prohibited. (M)

Caution:

A321: If center tank is not full, dispatch with more than 200 pounds of total fuel in both ACTs is prohibited, unless directed by an MEL. (A)

32
Q

Autopilot usage: After Takeoff in SRS mode?

A

100 feet AGL

(an internal FMGC logic prevents the autopilot from engaging in the 5 seconds after liftoff)

33
Q

Max Winds for Automatic Appraoch, Landing,

and Roll Out (inluding gusts) A 319?

A

Headwind:

Visibility: Any

Limitation: 20 Knots (two engines), 15 Knots (single engine)

Tailwind:

Visibility: Any

Limitation: 10 Knots if landing elevation below 5,570’ MSL and if CONF FULL.

otherwise, 5 Knots.

Crosswind:

Visibility: >equal 4000 or 3/4

Limitation: 20 Knots (two engines), 10 Knots (single engine)

Visibility: <4000 or 3/4

Limitation: 15 Knots (two engines) (A)1, 10 Knots (single engine)

1 See paragraph 1.3.1 Operational Limits for visibility < 4000 or 3/4

34
Q

Max Winds for Automatic Appraoch, Landing,

and Roll Out (inluding gusts) A 320 and 321?

A

Headwind:

Visibility: Any

Limitation: 30 Knots

Tailwind:

Visibility: Any

Limitation: 10 Knots

Crosswind:

Visibility: >equal 4000 or 3/4

Limitation: 20 Knots

Visibility: <4000 or 3/4

Limitation: 15 Knots (A)1

1 See paragraph 1.3.1 Operational Limits for visibility < 4000 or 3/4

35
Q

CFM Engines Limits:

Takeoff and Go Around ?

Maximum Continuous ?

Starting (Ground & Flight) ?

A

Takeoff and Go Around: Max EGT 950 C, Time Limit 5 Mins1

Maximum Continuous: Max EGT 915 C, Time Limit Continuous

Starting (Ground & Flight): Max EGT 725 C, Four consecutive cycles, each 2 mins2

1 10 minutes with one engine out

2 15 minute colling period following 4 start attempts

36
Q

IAE Engines Limits:

Takeoff and Go Around ?

Maximum Continuous ?

Starting (Ground & Flight) ?

A

Takeoff and Go Around: Max EGT (A319, 320) 635 C (A321) 650 C, Time Limit 5 Mins1

Maximum Continuous: Max EGT 610 C, Time Limit Continuous

Starting2 (Ground & Flight)3: Max EGT 635 C, Three consecutive cycles, two for 2 mins, the 3rd one min4.

1 10 minutes with one engine out

2 No running engagement of the starter when the

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

3 Capable of starting in crosswinds up to 35 knots

4 Pause 15 seconds between start attempts. 30 minute cooling period

following 3 start attempts (or 4 min. continuous cranking)

37
Q

Max Reverse thrust limit ?

A
  • Max reverse thrust should not be used below 70 KIAS (or when IAS starts to fluctuate. Idle reverse is permitted to aircraft stop.
38
Q

APU: after how many starter motor duty cycles

do you have to wait and how long ?

A
  • 3 Starter motor duty cycles
  • must wait 60 mins before attempting 3 more cycles
39
Q
A

AA Airbus 319/320/321 (2 decks)

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