A380 FCOM LIMITATIONS Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMIT CLEAN

A

-1 g to +2.5 g

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMIT Other than Clean Confg

A

0 g to +2 g

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3
Q

Max & min TKOF & LDG Pressure Alt?

A

10,000 ft & -2,000 ft

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4
Q

Min TAT @ Sea Level

A

-53º C

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5
Q

Max altitude

A

43,100 ft

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6
Q

Max OAT @ Sea Level

A

55º C

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7
Q

Max Runway slope (mean)

A

± 2 %

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8
Q

Minimum runway width

A

45 m

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9
Q

When does the Supplementary Procedure for setting TKOF THR apply?

A

When the Runway + Shoulders is less than 58 m

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10
Q

Is the technique of turn on a runway or turn pad permitted on a contaminated runway?

A

No

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11
Q

Max certified take-off crosswind (incl gusts)

A

35 kts

FYI max demonstrated crosswind at takeoff: 39 kt gusting 51 kt.

The maximum certified crosswind value is an AFM limitation. It is an engine limitation.

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12
Q

Max certified landing crosswind (incl gusts)

A

40 kts

FYI maximum demonstrated crosswind at landing: 42 kt gusting 56 kt.

The maximum certified crosswind value is an AFM limitation. It is an engine limitation.

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13
Q

FYI: maximum demonstrated crosswind at takeoff:

A

39 kt gusting 51 kt

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14
Q

FYI: maximum demonstrated crosswind at landing:

A

42 kt gusting 56 kt

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15
Q

Crosswind Limit: Dry / RWYCC 6

A

TKOF = 35 kt gust incl
LDG = 40 kt gust incl

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16
Q

Crosswind Limit: Wet / Good / RWYCC 5

A

TKOF = 35 kt gust incl
LDG = 40 kt gust incl

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17
Q

Crosswind Limit: Compacted Snow OAT ≤ -15º C / Good to Medium / RWYCC 4

A

TKOF & LDG = 27 kt gust incl

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18
Q

Crosswind Limit: Slippery Wet / Medium / RWYCC 3

A

TKOF & LDG = 20 kt gust incl

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19
Q

Crosswind Limit: Standing Water or Slush >3mm ≤13mm Wet / Medium to Poor / RWYCC 2

A

TKOF & LDG = 20 kt gust incl

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20
Q

Crosswind Limit: Ice (cold & dry) / Poor / RWYCC 1

A

TKOF & LDG = 15 kt gust incl

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21
Q

TKOF Max Tailwind

A

15 kt

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22
Q

What is “Engine Pumping”

A

Engine Stall

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23
Q

What are the Combination Crosswind / Tailwind limits?

A

At 35 kt Xwind any Twind.
At 15 kt Twind, Xwind > 30 kt

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24
Q

T.O PERF displays the following error message: “Risk of engine
pumping with this combination of Crosswind and Tailwind. Takeoff not allowed on QFU: ***”.

QFU = Runway Heading

A

Flight crew cannot run the computation. Combo Xwind/Twind outside limits.

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25
Q

Define: RWYCC 6 / AIREP Dry

A

Dry

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26
Q

Define: RWYCC 5 / AIREP Good

A
  • Damp
  • Wet - Up to 3mm / 1/8”
  • Slush - Up to 3mm
  • Dry Snow - Up to 3mm
  • Wet Snow - Up to 3mm
  • Frost
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27
Q

Define: RWYCC 4 / AIREP Good to Medium

A

Compacted Snow (OAT at or below -15° C)

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28
Q

Define: RWYCC 3 / AIREP Medium

A
  • Dry Snow - >3mm 1/8” to 100mm 4”
  • Wet Snow - >3mm 1/8” to 30mm 6/5”
  • Dry Snow any depth over Compacted snow
  • Wet Snow any depth over compacted snow
  • Compacted Snow OAT > -15º C
  • Slippery Wet
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29
Q

Define: RWYCC 2 / AIREP Medium to Poor

A
  • Standing Water or Slush > 3 mm 1/8” to 13 mm 1/2”
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30
Q

Define: RWYCC 1 / AIREP Poor

A

Ice (cold & dry)

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31
Q

Max altitude - gear extension

A

21,000’

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32
Q

Max altitude - Flaps/Slats extended

A

20,000’

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33
Q

Wind limitations for cabin door operation.

A

40 kt

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34
Q

Wind limitations for cabin door operation if aircraft nose into wind.

A

50 kt

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35
Q

When must Cabin & Cargo Doors be closed?

A

Before wind reaches 60 kt

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36
Q

Wind limitations for cargo door operation

A

40 kt

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37
Q

Wind limitations for cargo door operation if aircraft nose into wind

A

50 kt

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38
Q

Max opening speed Cockpit window

A

250 kts

Opening the cockpit window is not possible with the packs ON.

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39
Q

Max closing speed Cockpit window

A

160 kts

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40
Q

Autoland - Max headwind

A

38 kt

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41
Q

Autoland - Max tailwind (<8000’)

A

15 kt

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42
Q

Autoland - Max crosswind

A

30 kt

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43
Q

Can HF comms be used during refuelling?

A

No

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44
Q

Flaps/Slats - Max speed - Config 1

A

263 kts

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45
Q

Flaps/Slats - Max speed - Config 1+F

A

222 kts

When the aircraft reaches a speed of 212 kt, the Auto Retraction System (ARS) automatically retracts the flaps to conf 1.

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46
Q

Flaps/Slats - Max speed Config 2

A

220 kts

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47
Q

Flaps/Slats - Max speed Config 3

A

196 kts

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48
Q

Flaps/Slats - Max speed Config Full

A

182 kts

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49
Q

Vmo / Mmo

A

340 kts / M0.89

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50
Q

Max speed - Landing Gear extended (VLE)

A

250 kts / M0.55

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51
Q

Max speed - Landing Gear operating (VLO)

A

250 kts / M0.55

52
Q

Max speed - Landing Gear gravity extension (VLE/VLO)

A

220 kts / M0.48

53
Q

TIRE SPEED: Max Grd Spd

A

204 kt

54
Q

MIN CONTROL SPEED: VMCL

A

120 kt

55
Q

MIN CONTROL SPEED: VMCL-2

A

144 kt

Min Control Airspeed for LDG with 2 engines inoperative

56
Q

Windshield wipers Max speed

A

250 kts

57
Q

Max TaxI Weight

A

574,000kg

58
Q

Max take-off weight (MTOW)

A

572,000 kg

59
Q

Max landing weight (MLW)

A

391,000 kg

60
Q

Max zero fuel weight (MZFW)

A

366,000 kg

61
Q

Minimum Weight

A

270,000 kg

62
Q

During an air turnback or diversion, is a landing at above MLW permitted?

A

Yes, provided that the flight crew follows the overweight landing
procedure.

63
Q

Can HP ground air be used if APU Bleed is on?

A

No

64
Q

Limit when using airflow from the LP ground carts?

A

Airflow must not exceed 6.3 kg/sec

This limit is managed by contracted
ground services.

65
Q

Can you take off with both packs OFF?

A

No, it’s prohibited.

66
Q

Max cabin Overpressure Diff. Pressure

A

+9.65 psi

67
Q

Max negative cabin Diff. Pressure

A

-0.725 psi

68
Q

Min Cab Alt Selection

A

-2,000 ft

69
Q

Max Norm. Pos Diff Pressure

A

+8.7 psi

70
Q

Max Cabin Alt Selections

A

14,000 ft

71
Q

Max Norm Cab Alt

A

7,500 ft

At 43,100 ft

72
Q

Autopilot use - min height - takeoff

A

100 ft AGL & at least 5 secs after liftoff

An internal PRIM logic prevents the autopilot from engaging during 5 s after liftoff.

73
Q

Autopilot use - min height - Non-Precision Approach

A

200 ft AGL

74
Q

Autopilot use - min height - Circling Approach

A

200 ft AGL

75
Q

Autopilot use - min height - ILS approach with APPR1 on FMA

A

160 ft AGL

76
Q

Autopilot use - min height - manual go around

A

100 ft AGL

77
Q

Autopilot use - min height - all other phases

A

500 ft AGL

78
Q

Can the AP or FD in OP DES or DES mode be used in approach.

A

Yes, but only is the AFS CP selected altitude is set to or above the higher of MDA / MDH or 500 ft AGL

79
Q

Can all AP/FD modes be used with or without autothrust?

A

Yes, except if specified.

80
Q

Can Autothrust be used with or without AP/FD, in selected or managed speed/Mach?

A

Yes

81
Q

Flight Management

A
82
Q

Auto LDG Max Headwind

This limitation applies to auto approach, or auto landing & auto roll-out of:
GLS CAT I, ILS CAT II or ILS CAT III.

A

38 kt

83
Q

Auto LDG Max Tailwind ≤ 8000 ft PA

This limitation applies to auto approach, or auto landing & auto roll-out of:
GLS CAT I, ILS CAT II or ILS CAT III.

A

15 kt

84
Q

Auto LDG Max Tailwind > 8000 ft PA

This limitation applies to auto approach, or auto landing & auto roll-out of:
GLS CAT I, ILS CAT II or ILS CAT III.

A

10 kt

85
Q

Auto LDG Max Crosswind

This limitation applies to auto approach, or auto landing & auto roll-out of:
GLS CAT I, ILS CAT II or ILS CAT III.

A

30 kt

86
Q

Deflated tyres - Max taxy/tow speed

A

3 kts

87
Q

Deflated tyres - Max number nose landing gear

A

1

88
Q

Deflated tyres - Max number overall

A

9

89
Q

Deflated tyres - Max number body landing gear

A

2 per body landing gear (not on same axle)
Vacate only - 2 deflated on same axle
Taxy - 2 deflated on centre axle only.

90
Q

Deflated tyres - Max number wing landing gear

A

2 per wing landing gear (not on same axle)
Vacating - 2 deflated on same axle.

91
Q

One abnormal wing or body landing gear - Max speed

A

5 kts

92
Q

One abnormal wing or body landing gear - Max NWS angle

A

50 deg

93
Q

One abnormal wing or body landing gear - taxi crosswind limit

A

35 kts (BLG - Dry and wet runway/taxiway)

94
Q

Max brake temp for take-off

A

300 C

95
Q

RAM air only opens when diff is blow what psi?

A

1 psi

96
Q

Fuel - wing imbalance

A

Feed tanks 1/4: 3000 kg
Feed tanks 2/3: 3000 kg
Inner tanks: 3000 kg
Mid tanks: 2500 kg
Outer tanks: 1200 kg

97
Q

Fuel - min temp - JET A

A

-40 C

98
Q

Fuel - min temp - JET A1

A

-47C

99
Q

APU - Max guaranteed start altitude

A

20,000’

100
Q

APU - Max speed for use (non Emerg / Emerg config)

A

<M0.56 / Vmo/Mmo

101
Q

APU - Max altitude for Bleed Air and Electrical Power

A

22,500’

102
Q

APU - Max number of generators in flight

A

1

103
Q

APU - Wait between setting APU MASTER sw ON and setting APU START sw ON

A

5 seconds

104
Q

APU - Wait before new start after aborted start / shutdown

A

60 seconds

105
Q

APU - Max consecutive start attempts and associated cooling time

A

3
60 mins

106
Q

Can electrical outlets be used during takeoff and landing

A

No

107
Q

Engines - Minimum oil temp for starting

A

-40 C

108
Q

Engines - min oil temp for take-off

A

40 C

109
Q

Engines - min oil quantity pre-flight (OAT<0 C)

A

13 qts minimum
Flight time >/=14 hrs: 6 qts + 0.5 qts/hr

110
Q

Engine - min oil quantity pre-flight (>/=0 C)

A

10 qts minimum
Flight time >/=8 hrs: 6 qts + 0.5 qts/hr

111
Q

Starter - Duty cycle

A

2 cycles of 2 min + 1 cycle of 1 min (N3 = 0 between cycles)
Or
1 x 5 min cycle

Wait 30 mins after last cycle

112
Q

Starter duty cycle - wait time between cycles

A

30 mins

113
Q

Starter - N3 limits for running engagement (on ground / in flight)

A

10 % / 30 %

114
Q

Maximum reverse thrust should not be used below what speed?

A

70 kts

115
Q

Can take-off with reduced thrust be performed on a contaminated runway?

A

No

116
Q

Flex temp limits for reduced thrust takeoff (min /max)

A

Min: Flat rating temp or actual OAT

Max: ISA +60 C

117
Q

Engine - EGT limit (TOGA - AEO)

A

900 C for 5 mins

118
Q

Engine - EGT limit (TOGA - OEI)

A

900 C for 10 mins

119
Q

Engine - EGT limit (MCT)

A

850 C

120
Q

Engine - EGT limit (Start - on ground)

A

700 C

121
Q

Engine - EGT limit (start - in flight)

A

850 C

122
Q

BTV is prohibited on:

A
  • contaminated runway
  • RWY 13R/L VOR/GPS CANARSIE at JFK if last coded point is above 700’ RA
123
Q

Can OANS be used by PF during take-off?

A

No

124
Q

Can OANS be used by PF during rollout?

A

Once at taxy speed

125
Q
A