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Airbus A320 > LIMITATIONS memory (double diamond) > Flashcards

LIMITATIONS memory (double diamond) Flashcards

Aircraft limitations expected to be from memory.

1
Q

MAX takeoff & landing TAILWIND component

A

10 kts

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2
Q

MAX crosswind component (Allegiant)

A

29 kts

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3
Q

MAX takeoff & landing pressure altitude

A

9200 ft PA

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4
Q

MAX wind for PAX door operation

A

65 kts

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5
Q

MAX wind for CARGO door operation

A

40 kts (50 kts if nose is oriented into the wind)

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6
Q

MAX wind with PAX or CARGO door open

A

65 kts

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7
Q

MAX speed with flight deck window open

A

200 kts

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8
Q

MAX speed for operation of windshield wipers

A

230 kts

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9
Q

Turbulent air penetration speed BELOW 20,000’

A

TURB AIR penetration speed BELOW 20,000’

maintain 250 KIAS

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10
Q

Turbulent air penetration speed AT or ABOVE 20,000’

A

TURB AIR penetration speed AT or ABOVE 20,000’ Maintain 275 KIAS until intercepting .76 Mach

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11
Q

GROUND AIRCONDITIONING with AC PACKS

A

Do NOT use low pressure ground conditioned air simultaneously with air from the aircraft packs

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12
Q

HP (high pressure) ground air with APU air

A

Do NOT use HP ground (starting) air simultaneously with APU air

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13
Q

AUTOPILOT engagement on takeoff (min altitude)

A

Autopilot may not be engaged below 100’ AGL on takeoff (Allegiant)

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14
Q

ILS AUTOLAND autopilot certification

A

The autopilot is certified to remain engaged throughout the auto landing / rollout or automatic go around

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15
Q

Precision approach with manual landing autopilot limitations

A

Disconnect the autopilot no lower than 50 ft below the DA

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16
Q

Non-precision approach autopilot limitation

A

Disconnect the autopilot no lower than 50 ft below the DDA

17
Q

Visual Approach (ILS APPR mode not used) autopilot limitation

A

Disconnect the autopilot no lower than 500 HAA

Unless CAT 3 DUAL or CAT 3 SINGLE is displayed on the FMA, the autopilot must be disconnected at either 50 ft below the DA/DDA for the approach or 112 ft AGL, whichever is higher

18
Q

MAX flap / slat extension altitude

A

Do not extend the flaps or slats above FL200

19
Q

MAX fuel imbalance between inner wing tanks

A

MAX fuel imbalance between inner wing tanks 3,300 pounds

20
Q

Outer wing tank imbalance

A

An outer wing tank imbalance of 1,550 lbs (one tank empty / one tank full) is allowed provided the total fuel (outer + inner) in each wing is approximately equal

21
Q

Fuel must be transferred as necessary to comply with these restrictions

A

Fuel must be transferred as necessary to comply with these restrictions

22
Q

Fuel Management:

The center tank fuel must be emptied before the wing tanks are emptied unless…

A

The center tank fuel must be emptied before the wing tanks are emptied unless…
the center tank fuel is treated as ballast

23
Q

Takeoff using center fuel…

A

Takeoff using center fuel…

is prohibited

24
Q

Max altitude for landing gear extension

A

Do not extend the landing gear above FL250

25
Q

VLO(E) Max landing gear extension speed

A

Max landing gear extension speed 250 KIAS

26
Q

VLO(R) Max landing gear retraction speed

A

Max landing gear retraction speed 220 KIAS

27
Q

VLE Max landing gear extended speed

A

Max landing gear extended speed 280 KIAS / M.67

28
Q

Landing gear tire speed

A

Landing gear tires are limited to 195 kts GS

29
Q

MAX brake temperature for takeoff

A

MAX brake temperature for takeoff 300 C

30
Q

Brake limitations:

Power setting with parking brake on

A

Do not apply thrust on both engines in excess of 75% N1 with the parking brake on

31
Q

APU starter duty cycle

A

The APU starter motor duty cycle is 3 consecutive starts, or attempts, with a :01 minute cooling period between attempts. After the 3rd attempt, a :60 MIN cooling period must be allowed

32
Q

Engine Starter Duty Cycle Limits

A

There can be a maximum of 4 consecutive cycles of the engine starter within a :09 MIN period. Each cycle can last up to :02 MIN (maximum) then it must be followed by a :20 SEC rest After the fourth cycle, a period of :15 MIN must be allowed for cooling

33
Q

Engine Starter Engagement max N2

A

The starter must not be allowed to engage when the engine N2 RPM is above 20%

34
Q

Minimum OIL QTY (ECAM indication) before engine start

A
  1. 5 quarts PLUS estimated consumption of .5 qt/hr

note: At idle, oil qty indications may decrease by up to 6 qts

35
Q

Engine OIL system:

Minimum Starting temperature

A

minimum starting temperature -40 C

36
Q

Engine OIL system:

Minimum takeoff temperature

A

Minimum takeoff temperature -10 C

Airbus A320 (4 decks)

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