Limitations QRH Flashcards

1
Q

Maximum taxi weight

A

233 900 / 230 900

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2
Q

Max take off weight (breaks release)

A

233 000 / 230 000 kg

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3
Q

Max landing weight

A

182 000 / 180 000 kg

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4
Q

Max zero fuel weight

A

170 000 / 168 000 kg

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5
Q

Min weight

A

116 000 / 116 000 kg

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6
Q

Runway slope

A

+/- 2

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7
Q

Runway altitude

A

12 500ft

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8
Q

Nominal runway width

A

45m

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9
Q

Max crosswind certified for take off

A

32kt (Gust included)

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10
Q

Maximum Crosswind demonstrated for landing

A

40kt

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11
Q

Max tailwind for take off

A

15kt

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12
Q

Max tailwind for landing

A

At or below 11 000ft - 15kt

Above 11 000ft - 10kt

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13
Q

Max headwind (ILS CAT II , AUTOLAND)

A

35kt

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14
Q

Max tailwind (ILS CAT II, AUTOLAND)

A

10kt

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15
Q

Wind limitations for (ILS CAT II, AUTOLAND)

Head, cross and tail

A

Max Headwind - 35kt
Max Crosswind - 20kt
Max Tailwind - 10kt

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16
Q

Max wind for pax door operation

A

40kt (50kt if aircraft nose into the wind)

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17
Q

Max wind FWD and AFT cargo door operation

A

40kt (50kt if aircraft nose into the wind)

*FWD / AFT cargo door must be closed before wind exceeds 60kt

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18
Q

Cockpit window open max speed

A

230kt (its not possible to open the window with pack ON)

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19
Q

Max speed flap position “0”

A

VMO / MMO. Cruise

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20
Q

Flap position 1

A

Conf 1 - 240kt - holding

Conf 1+F - 215kt - take off

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21
Q

Flap position 2

A

Conf 2* - 205kt - approach (slats/flaps correspond to conf 1)

Conf 2 - 196kt - take off / approach

22
Q

Flap position 3

A

Conf 3 - 186kt - take off/approach/landing

23
Q

Flap position FULL

A

Conf Full - 180kt - landing

24
Q

VMO / MMO

A

330 kt/ M 0.86

25
Q

Max speed LDG extended (VLE)

A

250kt / M 0.55

26
Q

Max speed with LDG operating (extension/retraction) VLO

A

250kt/M 0.55

27
Q

Max speed LDG gravity extension

A

200kt

28
Q

Max tire speed

A

204kt GS

29
Q

Max wiper operating speed

A

230kt

30
Q

CABIN PRESS

Max diferential? Safety valve release?

A

max diferencial positivo 9.25 psi
Max diferencial negativo -1 psi
Safety realief Valve setting 8.85 psi

31
Q

Max operating altitude

A

Slats/flaps retracted 41 450ft

*this is the minumum altitude at which is possible to mantain cabin press altitude below 8000ft

32
Q

Min height for use of AP on Takeoff

A

100ft

33
Q

Min height AP in FINAL APP, NAV FPA, NAV V/S, TRK FPA, HDG V/S

A

250ft

34
Q

Min AP Circling approach

A

500ft

35
Q

Min AP ILS APP CAT 1

A

160ft

36
Q

Min AP GO AROUND (AP or FD engagement)

A

100ft

37
Q

OIL max continuous temp

A

190*C

38
Q

Min OIL temp before takeoff

A

20*C

39
Q

Min OIL press

A

25 psi

40
Q

STARTER

A

Max continuous operation is 5 min.

Two 3 min duty cycles and consecutivo 1 min cycle with run down to zero N3 between each cycle.

After one continuous operation, or the 3 cycles , wait 30 min to allow the starter to cool.

No running engagement of the starter when the N3 is above 10% on ground, or 30% in flight.

41
Q

APU: max altitude to assist eng start

A

20 000ft

42
Q

APU: max altitude for air conditioning and pressurization

A

22 500ft (single pack )

17 500ft (dual pack)

43
Q

Max operating altitude with flaps and/or slats extended

A

20 000ft

44
Q

Min fuel qty for takeoff

A

5200 kg

45
Q

Max brakes temp for takeoff (brake fan off)

A

300*C

46
Q

Taxi with deflated or damaged tires

A

If maximum one tire per gear is deflated (not damaged) - 7 kt

If two tires deflated (not damaged) on de same MAIN gear (max one main gear) 3 kt

Max NWS angle 30*

If tire damage is suspected, the flight crew mus ask for an aircraft inspection prior to vacate rwy or taxi.

47
Q

Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless …

A

the FCU altitude is set to, or above, minimum or 500 ft, whichever is the highest.

48
Q

Take off and Go around engine limitations all engines operative

A

900 - 5 mins

920 - 20 secs

49
Q

Take off and Go around engine limitations 1 eng inop

A

Egt 900 - 10 min

50
Q

Time and egt limitation for MCT

A

850

time: no limit

51
Q

Max EGT for starting on gnd and in flt

A

gnd - 700

flt - 850