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QF A380 > FCOM Limitations > Flashcards

FCOM Limitations Flashcards

1
Q

Flight manoeuvring load acceleration (clean)

A

-1g to + 2.5g

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2
Q

Flight manoeuvring load acceleration (other configurations)

A

0g to +2g

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3
Q

Max altitude

A

43,100’

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4
Q

Take-off and landing altitude limits (pressure altitude)

A

-2,000’ (-54 C to 55 C)
10’000’(-42 C to 35 C)

at MSL (-54 C to 55 C)

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5
Q

Runway limitations (slope)

A

+/- 2%

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6
Q

Minimum runway width

A

45m

(Special procedure if rwy with + shoulder is <58m wide)

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7
Q

Max certified crosswind - take-off

A

35 kt

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8
Q

Max certified crosswind - landing

A

40 kt

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9
Q

Max crosswind - take-off/landing (dry) (DRY)

A

35kt / 40kt

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10
Q

Max crosswind - take-off/landing (damp/wet) (GOOD)

A

35kt / 40kt

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11
Q

Max crosswind - take-off/landing (compacted snow) (GOOD to MEDIUM)

A

27 kt (both)

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12
Q

Max crosswind - take-off/landing (dry/wet snow) (MEDIUM)

A

20 kt (both)

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13
Q

Max crosswind - take-off/landing (standing water) (MEDIUM to POOR)

A

20 kt (both)

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14
Q

Max crosswind - take-off/landing (ice) (POOR)

A

15 kt

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15
Q

Max tailwind for take-off

A

15 kt

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16
Q

Max tailwind for landing (at/below 8,000’ PA)

A

15 kt

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17
Q

Max tailwind for landing (above 8,000’ PA)

A

10 kt

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18
Q

Wind limitations for cabin door operation

A

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

Doors must be closed before wind reaches 60 kt.

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19
Q

Wind limitations for cargo door operation

A

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

Doors must be closed before wind reaches 60 kt.

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20
Q

Cockpit window max opening speed

A

250 kt

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21
Q

Cockpit window max closing speed

A

160 kt

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22
Q

Flap/slat speed limit (Flap 0)

A

Vmo / Mmo

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23
Q

Flap/slat speed limit (Flap 1)

A

263 kt

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24
Q

Flap/slat speed limit (Flap 1+F)

A

222 kt

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25
Q

Flap speed limit (Flap 2)

A

220 kt

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26
Q

Flap/slat speed limit (Flap 3)

A

196 kt

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27
Q

Flap/slat speed limit (Flap FULL)

A

182 kt

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28
Q

Vmo /Mmo

A

340 kt / M0.89

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29
Q

Landing gear speed limit - extended (VLE) (kt / M)

A

250 kt / M 0.55

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30
Q

Landing gear speed limit - operating (VLO) (kt / M)

A

250 kt / M 0.55

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31
Q

Landing gear speed limit - gravity extension (VLE/VLO) (kt / M)

A

220 kt / M 0.48

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32
Q

Max tyre speed (ground speed)

A

204 kt

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33
Q

Windshield wipers - max speed

A

250 kt

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34
Q

Windshield wipers - max speed

A

250 kt

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35
Q

Weight limitations - max taxi

A

574,000 kg

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36
Q

Weight limitations - max take-off (MTOW)

A

572,000 kg

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37
Q

Weight limitations - max landing (MLW)

A

391,000 kg

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38
Q

Weight limitations - max zero fuel (MZFW)

A

366,000 kg

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39
Q

Weight limitations - min weight

A

270,000 kg

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40
Q

Max positive differential pressure

A

+9.65 psi

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41
Q

Max negative differential pressure

A

-0.725 psi

42
Q

Autopilot - min height (take-off)

A

100’ AGL (5 sec after take-off)

43
Q

Autopilot - min height (non-precision approach)

A

200’ AGL

44
Q

Autopilot - min height (circling approach)

A

200’ AGL

45
Q

Autopilot - min height (ILS - APPR1 on FMA)

A

160’ AGL

46
Q

Autopilot - min height (after manual go-around)

A

100’ AGL

47
Q

Autopilot - min height (all other phases)

A

500’ AGL

48
Q

Max headwind - Automatic approach landing and roll-out (GLS CAT I, ILS CAT II OTLR ILS CAT III)

A

38 kt

49
Q

Max tailwind - Automatic approach landing and roll-out (GLS CAT I, ILS CAT II or ILS CAT III) (at or below 8,000’ PA)

A

15 kt

50
Q

Max tailwind - Automatic approach landing and roll-out (GLS CAT I, ILS CAT II or ILS CAT III) (above 8,000’ PA)

A

10 kt

51
Q

Max crosswind - Automatic approach landing and roll-out (GLS CAT I, ILS CAT II or ILS CAT III)

A

30 kt

52
Q

Minimum decision height - Automatic approach landing and roll-out (GLS CAT I)

A

200’

53
Q

Minimum decision height - Automatic approach landing and roll-out (ILS CAT II)

A

100’

54
Q

Minimum decision height - Automatic approach landing and roll-out (ILS CAT II)

A

100’

55
Q

Minimum decision height - Automatic approach landing and roll-out (SA CAT II)

A

100’

56
Q

Minimum decision height - Automatic approach landing and roll-out (OTS CAT II)

A

100’

57
Q

Minimum decision height - Automatic approach landing and roll-out (OTS CAT II)

A

100’

58
Q

Minimum decision height - Automatic approach landing and roll-out (ILS CAT III fail passive)

A

50’

59
Q

Minimum RVR - Automatic approach landing and roll-out (ILS CAT III fail-operational)

A

75m RVR

60
Q

APU start limits - min time from APU MASTER SW ON before APU START SW ON

A

5 sec

61
Q

APU start limits - min time between failed start and new attempt

A

60 sec

62
Q

APU start limits - duty cycle

A

3 consecutive start attempts, then 60 min wait

63
Q

APU - Max N1

A

106 %

64
Q

APU - Max N2

A

102 %

65
Q

APU - Max EGT

A

900 C

66
Q

APU - Max EGT (APU start - on ground)

A

700 C

67
Q

APU - Max EGT (APU start - in flight)

A

800 C

68
Q

APU - Max EGT (APU running)

A

900 C for 30 sec (935 C for 0.5 sec)

69
Q

APU operation - Max aircraft speed

A

Normal - M 0.56
Engine failure (any speed)

70
Q

APU - Max altitude for start in-flight

A

20,000’

71
Q

APU - Max altitude for start in-flight

A

20,000’

72
Q

APU - Max altitude for Bleed Air and Elecrical.Power in-flight

A

22,500’

73
Q

EGT limit - TOGA (AEO)

A

900 C (5 min)

74
Q

EGT limit - TOGA (OEI)

A

900C (10 mins)

75
Q

EGT limit - Maximum Continuous Thrust (MCT)

A

850 C

76
Q

EGT limit - Maximum Continuous Thrust (MCT)

A

850 C

77
Q

EGT limit - starting (on-ground)

A

700 C

78
Q

EGT limit - starting (in-flight)

A

850 C

79
Q

EGT limit - starting (in-flight)

A

850 C

80
Q

Oil - Max continuous temp

A

196 C

81
Q

Oil - Min temp (Start)

A

-40 C

82
Q

Oil - Min temp (take-off)

A

40 C

83
Q

Oil quantity (OAT <0 C)

A

Flight time <14h - 13 qts
=/>14h - 6 qts + 0.5 qt/hr

84
Q

Oil quantity (OAT =/> 0 C)

A

Flight time <8h - 10 qts
=/>8h - 6 qts + 0.5 qt/hr

85
Q

Engine starter limits - duty cycle

A

5 mins

(2 x 2 min + 1 × 1 min - N3 = 0 between cycles OR
1 × 5 min cycle)

86
Q

Engine starter limits - cool down between duty cycles

A

30 mins

87
Q

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

A

10 % / 30 %

88
Q

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

A

10 % / 30 %

89
Q

Min fuel temp (JET A)

A

-40 C

90
Q

Min fuel temp (JET A1)

A

-47 C

91
Q

Fuel limits - Max allowed wing fuel imbalance

A

Feed tanks - 3000 kg
Inner tanks - 3000 kg
Mid tanks - 2500 kg
Outer tanks - 1200 kg

92
Q

Max brake temp for take-off

A

300 C

93
Q

Max altitude with landing gear extended

A

21,000’

94
Q

Taxy with deflated tyres - Max speed

A

3 kt

95
Q

Taxy with deflated tyres - Max speed

A

3 kt

96
Q

Taxy with deflated tyres - Max NWS angle

A

30 deg

97
Q

Taxy with deflated tyres - Max number of deflated tyres (total)

A

9

98
Q

Taxy with deflated tyres - Max number of deflated tyres (nose landing gear)

A

1

99
Q

Taxy with deflated tyres - Max number of deflated tyres (body landing gear)

A

2 (not on same axle unless centre axle - except runway vacating - any axle)

100
Q

Taxy with deflated tyres - Max number of deflated tyres (wing landing gear)

A

2 (not on same axle - except runway vacating)

101
Q

Minimum TAT

A

-53 C

QF A380 (3 decks)

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