Limitations General Flashcards

1
Q

Auto brake arms/active min speed

A

72 kts

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2
Q

Maximum rudder trim after engine start

A

0.3 units

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3
Q

Nose wheel tyre pressure range

A

162 - 184 psi

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4
Q

Main wheel tyre pressure range

A

198 - 210 psi

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5
Q

Brake temperature limit for take off (no fans used)

A

300 degrees C

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6
Q

Brake temperature limit for take off with fans used

A

150 degrees C

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7
Q

Maximum recommended brake temperature with park brake applied

A

500 degrees C (350 degrees with fans on)

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8
Q

Brake temperature requiring maintenance action/report

A

800 degrees C ( thermal plugs? )

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9
Q

Minimum brake hydraulic accumulator pressure

A

Green band, 2700 psi?

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10
Q

Alternate brake check pressure range, min - max

A

2200 - 2700 psi

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11
Q

Number of full brake applications in accumulator only, no hydraulic pressure

A

7 ?

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12
Q

Radius of turn, minimum width for 180 A330-200

A

42m ?

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13
Q

Radius of turn, minimum width for 180 A330-300

A

45!? 46m ? 48m?

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14
Q

Hydraulic system normal operating pressure

A

3000 psi + - 200?

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15
Q

Minimum altitude for autopilot engagement after takeoff

A

100’ & 5 seconds

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16
Q

Minimum altitude for autopilot dis engagement for manual landing

A

80’ RA

17
Q

Minimum DA for auto app

A

100’ DA

18
Q

CAT 3 single, fail passive, minimum DA

A

50’

19
Q

Cat 3 fail operational alert

A

200’

20
Q

ILS/LOC tune minimum altitude change, locked freq & crs

A

700’ with App arm or engaged

21
Q

G/S warning deviation & A/P disengagement

A

More than 1 dot for 7sec above 200’

22
Q

LOC warning deviation & A/P disengagement

A

1/4 dot for more than 7 sec above 200’

23
Q

Autoland warning

A

Below 200’ for autopilot failure, LOC or G/S deviation, loss of loc above 15’ or g/s below 100’, RA diff by 15’?

24
Q

Maximum normal brake temperature, no maintenance action?

A

500 degrees C

25
Q

Battery charge cycle check, current and time

A

Below 60 amps after 10 sec (and decreasing)

26
Q

Cockpit window damage, outer or middle pane damaged, consequences

A

Nil, inner is structural

27
Q

Cockpit window damage, cracked inner pane consequences

A

Descend to FL230, diff press to 5 psi

28
Q

Over weight landing, ideal max v/s on touchdown

A

360 ‘/m

29
Q

Over weight landing, flap extension

A

Vfe next - 5 kts (auto thrust off?)

30
Q

Max reverse on an RTO permitted until

A

Stopping, no speed limit (normal ops limit 70 kts)

31
Q

If a/c stopped using auto brake max, how to get moving

A

stow speed brakes

32
Q

Decel light does not illuminate if

A

Deceleration rate less than 80% of selected rate.
Possible contamination etc & anti-skid not able to achieve rate.