Limitations A380 Flashcards

1
Q

Certified max number of pax

A

853

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2
Q

MTOW

A

572,000 kg

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3
Q

MLW

A

391,000 kg

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4
Q

MZFW

A

366,000kg

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5
Q

Max Alt

A

43,100ft

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6
Q

Nose wheel steering limit

A

70 degrees

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7
Q

Max taxi weight

A

574,000kg

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8
Q

Vmo / MMO

A

Above FL 300 - 0.89M
Below FL 300 - 340kts

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9
Q

Max G load

A

Clean: -1 to +2.5g
Other: 0 to +2g

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10
Q

VLE & VLO

A

250kt / 0.5t M

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11
Q

VLE / VLO Gravity Extension max speed

A

220kts / 0.48M

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12
Q

Cockpit window limits

A

Max opening speed - 250kts
Max closing speed - 160kts
Max wiper speed - 250 kts

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13
Q

Max cabin pressure differentials

A

9.2 psi and -0.725 psi

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14
Q

Autopilot height limits (AGL)

A

Takeoff - 100ft (5s after lift off)
NPA - 200ft
Circling - 200ft
ILS CAT1 - 160ft
After manual Go Around- 100ft
All other phases - 500ft

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15
Q

Max fuel temp

A

53 degrees Celsius (CBT)

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16
Q

Max brake temp take off

A

300 degrees Celsius

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17
Q

Max tire speed

A

204kts (Think 4 main sets of gear)

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18
Q

Max APU start

A

20,000ft. Can provide bleed air and elec up to 22,500ft
Max EGT 700 on ground and 800 in flight

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19
Q

Windshield wipers max speed

A

250kts

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20
Q

Max positive and negative differential pressure

A

9.65 to -0.725

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21
Q

Min height for AP after take off?

A

100ft and at least 5s after after lift off

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22
Q

Min height for use of AP - NPA

A

200ft AGL

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23
Q

Min height for use of AP - after manual Go Around

A

100ft AGL

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24
Q

Min height for use of AP - ILS with CAT1 displayed on FMA

A

160ft

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25
Q

Min height for use of AP - all other phases

A

500ft

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26
Q

Min and max fuel temps

A

The freezing point of the fuel and +53C

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27
Q

Max allowed wing fuel imbalance

A
  • Feed tanks 1/4 or Feed tanks 2/3 - 3000 kgs
  • Left and Right Inner Tanks - 3000 kgs
  • Left and Right MID Tanks - 2500 kgs
  • Left and Right Outer Tanks - 1200 kgs
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28
Q

Max brake temp for take off

29
Q

TOGA time limit ALL engines, 1 inop and EGT limit for TOGA

A
  • 5 Mins All Engines
  • 10 Mins 1 Inop
  • 900C EGT Limit applies for both cases
30
Q

MCT EGT Limit?

31
Q

Starting EGT Limit on ground and inflight

A
  • 700C on Ground
  • 850C in Flight (Same as MCT EGT Limit)
32
Q

Min oil temp starting

A

-40C (Neg 40)

33
Q

Min oil temp prior to Take Off

A

40C (Positive 40C)

34
Q

Max Continuous Oil Temp

35
Q

Minimum Oil Quantities

A

6 qts + 0.5 qt/h
OAT less than 0 and Flight below 14 hours - 13 qts
OAT at or MORE than 0 and Flight below 8 hours - 10 qts

36
Q

Max Reverse not used below what speed?

A

70 kts (Idle Rev allowed down to stop).

37
Q

Max certified crosswind take off

A

35kts - Gust included

38
Q

Max certified crosswind landing

A

40kts - Gusts included

39
Q

Max Alt with Flaps/Slats Extended

40
Q

Max Altitude with Gear Extended

41
Q

Minimum TAT

42
Q
  • Runway Slope (Mean)
  • Min Runway Width
A

+ or - 2% AND 45m

43
Q

Max Tailwind For Takeoff

44
Q

Max Tailwind For Landing

A

Airport pressure Alt ABOVE 8000ft: 10 Kts

Airport pressure Alt at or BELOW 8000ft: 15 Kts

45
Q

Max Wind Cabin Door Operation

A

40 Kts (50 Kts if aircraft nose into wind)

The cabin and cargo door must be closed BEFORE the wind reaches 60 kt.

46
Q

Max wind cargo door operation

A

40 Kts (50 Kts if aircraft nose into wind or door on leeward side)
* The cabin and cargo door must be closed BEFORE the wind reaches 60 kt.

47
Q

Flaps 1 Max Speed

A

263 Kts
* Slats 20°
No Flaps out

48
Q

Flaps 1 + F CONF ARS (Auto Retract System) Speed AND Max Speed

A

212 kts it auto retracts - Max speed 222 Kts
1 + F CONF:
* Slats 20 °
* Flaps 8 °

49
Q

Flaps 2 MAX Speed

A

220 Kts
* Slats 20°
* Flaps 17°

50
Q

Flaps 3 MAX Speed

A

196 Kts
* Slats 23°
* Flaps 26°

51
Q

Flaps FULL MAX Speed

A

182 Kts
* Slats 23°
* Flaps 33°

52
Q

V MCL

A

123 kts
Minimum Control Speed in the landing configuration, the speed at which an aircraft can be controlled with one engine inoperative during approach and landing

53
Q

V MCL-2

A

147 kts
VMCL-2 refers to the minimum control speed at landing with two engines on the same side inoperative, a concept relevant for aircraft with four or more engines.

54
Q

Air Cond with HP Ground Air Supply…

A

Do not use HP ground air supply, when APU supplies bleed air.

55
Q

Packs OFF Take off?

A

No - Take off with both PACKS OFF is Prohibited

56
Q

Auto Land Max Headwind, Tail and Crosswind

A
  • 38 Kts Headwind
  • 30 Kts Crosswind
  • Tailwind
    Pressure Alt at or ABOVE 8000ft 10 kts
    Pressure Alt BELOW 8000ft 15 kts
57
Q

Time Limit between APU MASTER SW and APU START ON

A

5 Seconds

During the APU start, the flight crew must wait 5 s after setting the APU MASTER SW pb-sw to ON, before setting the APU START pb to ON. These 5 s correspond to the time the ECB needs to power up when the APU MASTER SW pb-sw is set to ON.

58
Q

APU Start Attempts

A

60 Seconds between start attempts. After 3 consecutive start attempts - 60 mins.

59
Q

APU Rotor Speeds Limits (N1 and N2)

A

N1 - 106%
N2 - 102%

60
Q

APU Max EGT Running

A

900 ° C during 30 secs
935 ° C during 0.5 sec

61
Q

Max EGT APU start

A

800 ° C In Flight
700 ° C on Ground (Same as Engine on ground start limit)

62
Q

APU Max Aircraft speed

A

0.56M unless ALL engines have failed then it will work any speed

63
Q

APU Generators- How many can operate ground and flight

A

Both on ground - Only 1 in flight (up to 22,500ft)

64
Q

Engine EGT Starting limits

A

700 °C on Ground
850 °C In Flight

65
Q

Max continuous engine starter operation

A

5 mins

Two consecutive cycles of 2 min duration maximum, plus one additional cycle of 1 min, with a run down to zero N3 between each cycle, or

One 5 min cycle.

Wait 30 min after the last cycle to allow the starter to cool.

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

66
Q

FLEX Thrust Temp Limits

A

Higher than ISA + 60 °C

Lower than the flat rating temperature or actual OAT.

67
Q

Min Feed Tank Fuel Quantity before pushback

A

4000kg
Before pushback, if at least one fuel transfer tank is not empty, ensure that the fuel quantity in each feed tank is more than 4 000 kg.

Note:
If the fuel quantity in one or more feed tanks is less than 4 000 kg with fuel available in transfer tanks, perform an automatic ground transfer using the AUTO GND XFR pb-sw to adjust feed tanks fuel distribution.

68
Q

During Refuelling which lights CAN be used?

A
  • NAV
  • LOGO
  • WING