BA7 FCOM Limitations Flashcards

1
Q

Introduction

How to differenciate between the fleet variants with registration?

A
  • 380-861 Engine Alliance GP7270 are ED/EO-series and EUA-EUL
  • 380-841 RR Trent 970 are EVA and EVB
  • 380-842 RR Trent 972 are EVM-EVS
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2
Q

Introduction

What are the type of speeds and altitudes used in the A380 limitations chapter?

IAS/EAC/CAS/TAS DA/PA/TA etc

A
  • Speed : IAS/Mach
  • Altitude: Pressure Altitude

unless otherwise noted

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3
Q

Flight Maneuvring Load Acceleration Limits

Clean Configuration

UAE A380 FCOM LIM-AG-F_CTL

A

-1 g to +2.5 g

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4
Q

Flight Maneuvring Load Acceleration Limits

Other Configuration

UAE A380 FCOM LIM-AG-F_CTL

A

0 g to +2 g

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5
Q

Operational Parameters

Max Pressure Altitude

UAE A380 FCOM LIM-AG-OPS

A

43,100 feet

Pressure Altitude

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6
Q

Operational Parameters

Temperature range at Max Pressure Altitude

UAE A380 FCOM LIM-AG-OPS

A

-78 to -35 º C

SAT

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7
Q

Operational Parameters

Min and Max T/O & LDG Altitude

UAE A380 FCOM LIM-AG-OPS

A

-2000 to 10,000 feet

Pressure Altitude

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8
Q

Operational Parameters

Max Temperature range at Sea Level

UAE A380 FCOM LIM-AG-OPS

A

-54 to 55ºC

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9
Q

Operational Parameters

Minimum TAT

UAE A380 FCOM LIM-AG-OPS

A

-53ºC

This is the only TAT temperature limitation. The rest are SAT

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10
Q

Operational Parameters

Mean RWY Slope

UAE A380 FCOM LIM-AG-OPS

A

+/- 2 %

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11
Q

Operational Parameters

Minimum RWY width

UAE A380 FCOM LIM-AG-OPS

A

45m

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12
Q

Operational Parameters

Under what RWY+stabilized shoulder width should crew apply a dedicated PRO NOR SUPP MISC?

UAE A380 FCOM LIM-AG-OPS

A

If the overall width of the RWY + Stabilized shoulders are < 58m

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13
Q

Operational Parameters

When is the 180º turn on a runway or turnpad not permitted?

Assuming the min 60m RWY

UAE A380 FCOM LIM-AG-OPS

A

When RWY is contaminated

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14
Q

Operational Parameters

Maximum certified XW at T/O

UAE A380 FCOM LIM-AG-OPS

A

35 kt

Gust included (Engine limitation)

with due consideration of combination of XW and TW PERF-TOF-TOC-OCD

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15
Q

Operational Parameters

Maximum demonstrated XW at T/O

UAE A380 FCOM LIM-AG-OPS

A

39 G 51

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16
Q

Operational Parameters

Maximum certified XW at LDG

Assuming the min 60m RWY

UAE A380 FCOM LIM-AG-OPS

A

40 kt

gust included (engine limitation)

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17
Q

Operational Parameters

Maximum demonstrated XW at LDG

Assuming the min 60m RWY

UAE A380 FCOM LIM-AG-OPS

A

42 G 56

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18
Q

Operational Parameters

Maximum TW at T/O

UAE A380 FCOM LIM-AG-OPS

A

15 kt

with due consideration of combination of XW and TW PERF-TOF-TOC-OCD

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19
Q

Operational Parameters

Maximum TW for LDG

380-861 Engine Alliance GP7270

UAE A380 FCOM LIM-AG-OPS

A
  • Airport Press. Altitude 8000 ft: 15kts
  • Airport > 8000 ft: 10kts

If ATC or ATIS TW is > 10kt FLAPS 3 is not permitted for LDG

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20
Q

Operational Parameters

Maximum TW for LDG

380-842/841 RR Trent 972/970

UAE A380 FCOM LIM-AG-OPS

A
  • Airport Press. Alt 8000 ft: 15kts
  • Airport Press. Alt > 8000 ft: 10kts
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21
Q

Operational Parameters

Maximum Wind for CABIN Door Operation

UAE A380 FCOM LIM-AG-OPS

A
  • 40 kts
  • 50 kts if nose is upwind

Must be closed before wind reaches 60 kts

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22
Q

Operational Parameters

Maximum Wind for CARGO Door Operation

UAE A380 FCOM LIM-AG-OPS

A
  • 40 kts
  • 50 kts if nose is upwind or door is on leeward side

Must be closed before wind reaches 60 kts

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23
Q

General Speeds

Cockpit Window Maximum Opening Speed

UAE A380 FCOM LIM-AG-SPD

A

250 kts

Not possible with the packs ON

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24
Q

General Speeds

Cockpit Window Maximum Closing Speed

UAE A380 FCOM LIM-AG-SPD

A

160 kts

If you did not skip arms day during your A320/330 tenure

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25
Q

General Speeds

Max FLAPS 1

UAE A380 FCOM LIM-AG-SPD

A

263 kts

Phase: Holding

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26
Q

General Speeds

MAX FLAPS 1+F

Max and Auto Retraction System speed

UAE A380 FCOM LIM-AG-SPD

A

222 kts

Phase: T/O & APP

ARS retracts FLAPS at 212

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27
Q

General Speeds

Max FLAPS 2

UAE A380 FCOM LIM-AG-SPD

A

220 kts

Phase: T/O & APP

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28
Q

General Speeds

Max FLAPS 3

UAE A380 FCOM LIM-AG-SPD

A

196 kts

Phase: T/O, APP & LDG

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29
Q

General Speeds

Max FLAPS FULL

UAE A380 FCOM LIM-AG-SPD

A

182 kts

Phase: LDG

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30
Q

General Speeds

VMO

UAE A380 FCOM LIM-AG-SPD

A

340 kts

may not be deliberately exceeded in any regime of flight

At ISA the changeover altitude of 340kts to M0.89 is around FL300

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31
Q

General Speeds

MMO

UAE A380 FCOM LIM-AG-SPD

A

0.89 Mach

may not be deliberately exceeded in any regime of flight

At ISA the changeover altitude of M0.89 to 340kts is around FL300

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32
Q

General Speeds

Normal VLE/MLE

Max speed with landing gear Extended

UAE A380 FCOM LIM-AG-SPD

A

250 / M 0.55

Changeover altitude of 250kts to M 0.55 is around FL200

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33
Q

General Speeds

Normal VLO

Max speed with landing gear Operating

UAE A380 FCOM LIM-AG-SPD

A

250 kt / M 0.55

At ISA the changeover altitude of 250kts to M 0.55 is around FL200

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34
Q

General Speeds

Max speed for landing gear gravity extention

(VLE/VLO)

UAE A380 FCOM LIM-AG-SPD

A

220 kt / M 0.48

At ISA the changeover altitude of 220kts to M 0.48 is around FL200

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35
Q

Maximum Tire Speed

Maximum ground speed

UAE A380 FCOM LIM-AG-SPD

A

204 kt

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36
Q

Minimum Control Speeds

VMCL

380-861 Engine Alliance GP7270

UAE A380 FCOM LIM-AG-SPD

A

120 kt

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37
Q

Minimum Control Speeds

VMCL-2

380-861 Engine Alliance GP7270

UAE A380 FCOM LIM-AG-SPD

A

145 kts

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38
Q

Minimum Control Speeds

VMCL

380-842 Trent 972 / 380-841 Trent 970

UAE A380 FCOM LIM-AG-SPD

A

123 kt

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39
Q

Minimum Control Speeds

VMCL-2

380-842 Trent 972 / 380-841 Trent 970

UAE A380 FCOM LIM-AG-SPD

A

147 kt

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40
Q

Maximum Speed

Windshield Wipers

UAE A380 FCOM LIM-AG-SPD

A

250 kt

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41
Q

Minimum Control Speeds

What is the diffirence between VMCL and VMCL-2?

UAE A380 FCOM DSC-22-27-10-30 3/8

A

VMCL considers one critical (either outbord engine) failing VMCL-2 considers two engines failing on the same side

Both consider max bank of 5º at TOGA, Gear up and GA FLAPS

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42
Q

Weights

List the following:
1. MTW
2. MTOW
3. MLW
4. MZFW
5. Minimum Weight

WV 003

UAE A380 FCOM LIM-AG-WGHT

A
  1. 512 000 kg
  2. 510 000 kg
  3. 395 000 kg
  4. 373 000 kg
  5. 270 000 kg

MTOW, MLW, MZFW vary with CG

MLW 395 tons and MW 270 tons are the only common value in all variants

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43
Q

Weights

List the following:
1. MTW
2. MTOW
3. MLW
4. MZFW
5. Minimum Weight

WV 0012

UAE A380 FCOM LIM-AG-WGHT

A
  1. 571 000 kg
  2. 569 000 kg
  3. 395 000 kg
  4. 366 000 kg
  5. 270 000 kg

MTOW, MLW, MZFW vary with CG

MLW 395 tons and MW 270 tons are the only common value in all variants

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44
Q

Weights

List the following:
1. MTW
2. MTOW
3. MLW
4. MZFW
5. Minimum Weight

WV 0011

UAE A380 FCOM LIM-AG-WGHT

A
  1. 577 000 kg
  2. 575 000 kg
  3. 395 000 kg
  4. 369 000 kg
  5. 270 000 kg

MTOW, MLW, MZFW vary with CG

MLW 395 tons and MW 270 tons are the only common value in all variants

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45
Q

AIR

Packs OFF T/O

UAE A380 FCOM LIM-AIR

A

Prohibited

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46
Q

AIR

Limitation when using APU bleed air

UAE A380 FCOM LIM-AIR

A

Do Not Use HP ground air supply or WAI

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47
Q

AIR

Max airflow from LP ground carts

UAE A380 FCOM LIM-AIR

A

Must not exceed 6.3 kg/sec

48
Q

AIR

Max Positive ∆P

and Max normal ∆P

UAE A380 FCOM LIM-AIR

A

9.2 psi

Max normal 8.7 psi

49
Q

AIR

Max Negative ∆P

UAE A380 FCOM LIM-AG-AIR

A

-0.725 psi

50
Q

AFS General

Min height for AP engagement at T/O

UAE A380 FCOM LIM-AFS-10

A

100 ft AGL and 5 s after liftoff

Internal PRIM logic

51
Q

AFS General

Min height for AP use: NPA

UAE A380 FCOM LIM-AFS-10

A

200 ft

52
Q

AFS General

Min height for AP use: Circling

UAE A380 FCOM LIM-AFS-10

A

200 ft

53
Q

AFS General

Min height for AP use: ILS APPR1

UAE A380 FCOM LIM-AFS-10

A

160 ft

54
Q

AFS General

Min height for AP use: After manual GA

UAE A380 FCOM LIM-AFS-10

A

100 ft

55
Q

AFS General

Min height for AP use: All other phases

UAE A380 FCOM LIM-AFS-10

A

500 ft

56
Q

AFS General

What are the approaches the FMS Landing System (FLS) not been certified for?

UAE A380 FCOM LIM-AFS-10

A

Not certified for ILS, GLS, IGS, LDA, SDF or RNAV(GNSS) w/LPV minima

57
Q

AFS

What is the main differnce in approach types can be flown in F-APP or FAPP+RAW?

UAE A380 FCOM LIM-AFS-10

A

F-APP+RAW: All the certified ones except RNAV(GNSS) w/LNAV or LNAV/VNAV minima which require F-APP capability

58
Q

Maximum Wind Conditions for Automatic App, LDG, and Roll-out

Max HW, XW, and TW for
380-861 Engine Alliance GP7270

GLS CAT I. ILS CAT II/III

UAE A380 FCOM LIM-AFS-10

A

HW: 38kts
XW: 30
TW:
* Airport Press. Alt 8000 ft: 15kts
* Airport Press. Alt > 8000 ft: 10kts

If ATC or ATIS TW is > 10kt FLAPS 3 is not permitted for LDG

Notwithstanding ND indications

59
Q

Maximum Wind Conditions for Automatic App, LDG, and Roll-out

Max HW, XW, and TW for 380-842 RR Trent 972 & 380-841 RR Trent 970

GLS CAT I. ILS CAT II/III

UAE A380 FCOM LIM-AFS-10

A

HW: 38kts
XW: 30
TW:
* Airport Press. Alt 8000 ft: 15kts
* Airport Press. Alt > 8000 ft: 10kts

Notwithstanding ND indications

60
Q

Autoland

What are the approved configurations for engine out autoland in OEI and TEI?

UAE A380 FCOM LIM-AFS-10

A
  • OEI: CONF 3 anf FULL
  • Two ENG INOP on opposite side: CONF 3

if EO Proc. completed before 1000 AAL

61
Q

Autoland

What are the demostrated and authorized RWY surface conditions for CAT III B Autoland Operation?

UAE A380 FCOM LIM-AFS-10

A

Dry and Wet up to 3mm

62
Q

Autoland

List the IAP and airport limitations for which autoland has been demostrated for GLS I and CAT II/III autoland:

UAE A380 FCOM LIM-AFS-10

A
  • GS= -2.5 to -3.5
  • Airport Altitude: -1000. to 9200”
  • Weight: 305 - MLW (395)
  • Vapp= VLS + (5 to 15)

Can perform autoland up to MTOW depending on situtaion

Pressure Altitude

63
Q

Autoland

Minimum FMA capability to land GLS 1 and CAT II/III for approach and autoland:

UAE A380 FCOM LIM-AFS-10

A

GLS CAT I : LAND 1 (Autoland optional)
CAT II: LAND 2 (Autoland mandatory in normal ops)
CAT III Fail-Passive: LAND3 SINGLE (Autoland mandatory)
CAT III Operational: LAND3 DUAL (autoland mandatory)

64
Q

Approach Capability

What is the alert height?

Follow up: Define it.

UAE A380 FCOM LIM-AFS-10

A

200 RA. Height above runway where a failure in the ground equipment or aircraft systems warrants a GA. If such failures happen below AH then the autoland may be continued subject to that the AUTOLAND light does not get illuminated.

65
Q

APU

How long crew must wait for a new start attempt in case of an aborted APU start or APU shutdown? And up to how many attempts are allowed before a cooling period?

Must Know

UAE A380 FCOM LIM-APU

A

60 s wait time between three start attempts followed by a 60 min wait.

66
Q

APU

APU Max N1/N2

UAE A380 FCOM LIM-APU

A

106% / 102%

67
Q

APU

APU Max EGT during start On ground and In-flight

UAE A380 FCOM LIM-APU

A

700ºC On Ground
800°C In-flight

68
Q

APU

APU Max EGT running

UAE A380 FCOM LIM-APU

A

900ºC during 30s
935º during 0.5s

69
Q

APU

APU Max indicated EGT

UAE A380 FCOM LIM-APU

A

900ºC

70
Q

APU

What is the operational envelope of the APU

UAE A380 FCOM LIM-APU

A

Below M0.56

71
Q

APU

APU Generator operational range on ground and in flight

Must Know

UAE A380 FCOM LIM-APU

A
  • On Ground: Both generators run at 120KVA
  • Inflight: Only one APU GEN operate up to 22500
72
Q

APU

APU Bleed air operational envelope and limitation

Must Know

UAE A380 FCOM LIM-APU

A

Below 22500 whilst below 0.56M

Cannot be used in conjunction with WAI

73
Q

COMM

What COM may not be used during refueling?

Must Know

UAE A380 FCOM LIM-COM

A

HF

74
Q

ELEC

What is a limitation that applies to electrical outlets?

UAE A380 FCOM LIM-ELEC

A

May not be used in T/O and LDG

75
Q

Engines

When is SOFT GA prohibited?

UAE A380 FCOM LIM-ENG

A

GA Gradient > 8%

76
Q

Engine

List the EGT and thrust time limits for EA engines in TOGA/MCT/Start in flight and on ground

Must Know

UAE A380 FCOM LIM-ENG

A
77
Q

Engine

List the EGT and thrust time limits for RR engines in TOGA/MCT/Start in flight and on ground

Must know

UAE A380 FCOM LIM-ENG

A
78
Q

Engine

EA ENG OIL max continuous temperature

UAE A380 FCOM LIM-ENG

A

177º during 5s
163º during 20 min

79
Q

Engine

EA ENG OIL min start temp

UAE A380 FCOM LIM-ENG

A

-40ºC

80
Q

Engine

EA ENG OIL min temp before T/O

Must Know

UAE A380 FCOM LIM-ENG

A

50ºC

81
Q

Engine

RR Max Continuous OIL Temp

UAE A380 FCOM LIM-ENG

A

196ºC

82
Q

Engine

RR Eng Oil min start temperature

UAE A380 FCOM LIM-ENG

A

-40ºC

83
Q

Engine

RR Eng Oil min temperature before T/O

Must Know

UAE A380 FCOM LIM-ENG

A

40ºC

84
Q

Engine

EA and RR ENG OIL min press

UAE A380 FCOM LIM-ENG

A

25 PSI

85
Q

Engine

EA ENG min oil qty

Must Know

UAE A380 FCOM LIM-ENG

A
  • FT < 10h = 10 qts
  • FT ≥ 10h = 6+0.4/hr qts
86
Q

Engine

RR ENG min oil qty w/ OAT ≥ 0ºC

Must Know

UAE A380 FCOM LIM-ENG

A
  • FT < 8h = 10 qts
  • FT ≥ 8 h = 6+0.5 qt/h
87
Q

Engine

RR ENG min oil qty w/ OAT < 0ºC

Must Know

UAE A380 FCOM LIM-ENG

A
  • FT < 14h = 13 qts
  • FT ≥ 14h = 6+0.5 qt/h
88
Q

Engine

EA ENG max N1/N2

UAE A380 FCOM LIM-ENG

A

111% / 118.7 %

89
Q

Engine

RR ENG Max N1/N2/N3

UAE A380 FCOM LIM-ENG

A

97.2% / 98.7% / 97.8%

90
Q

Engine

Starter Limits EA Engines

Must Know

UAE A380 FCOM LIM-ENG

A

3 Attempts of 5 min each (15 min total). Followed by 30 min cooldown

91
Q

Engines

Starter limit RR

UAE A380 FCOM LIM-ENG

A

Either
* One 5 minute cycle
* 3 cycles at 2-2-1 minutes (N3 must roll to zero between attempts)

Followed by a 30 min cooldown time

92
Q

Flight Controls

Max Altitude with Flaps/Slats extended

UAE A380 FCOM LIM- F-CTL

A

20,000 ft

93
Q

Min Fuel Temperature for:
1. JET A
2. JET A1
3. RP-3 (China)
4. TS-1 (Russia)

UAE A380 FCOM LIM-FUEL

A
  1. -40ºC
  2. -47ºC
  3. -47ºC
  4. -50ºC
94
Q

Max Fuel Temperature

UAE A380 FCOM LIM-FUEL

A

+53ºC

95
Q

Max imbalance for FEED TKs

UAE A380 FCOM LIM-FUEL

A

3000kg

96
Q

Max imbalance INNER TKS

UAE A380 FCOM LIM-FUEL

A

3000kgs

97
Q

Max Imbalance MID TKs

UAE A380 FCOM LIM-FUEL

A

2500kg

98
Q

Max Imbalance OUTER TKs

UAE A380 FCOM LIM-FUEL

A

1200kg

99
Q

Max BRK Temp at T/O

UAE A380 FCOM LIM-LG

A

300ºC

100
Q

BWS Fault

What are the limitations associated with BWS Fault?

UAE A380 FCOM LIM-LG

A
  • 180º turn on 60m RWY Forbidden
  • 180º turn on turn pad not recommended if RWY Wet
101
Q

Max Landing Gear Extention Altitude

UAE A380 FCOM LIM-LG

A

21 000 ft

102
Q

Taxi with Deflated Tires

When towing or taxiing with deflated tires what are the:
* NWS limit
* Taxi speed limit
* Maximum amount of deflated tires
* Distribution of said deflated tires and their exceptions

UAE A380 FCOM LIM-LG

A
  • NWS Limit of 30º and Max taxi 3 kt
    Max 9 deflated tires with a max combination of:
    1. One on the Nose gear
    2. Two on BLG not on same axle with exception to central axle (i)
    3. Two on WLG not on same axle (i)

No deflated nose landing gear in case of towbarless towing.

(i) Deflated tires can be on same axle for vacating RWY only.

103
Q

Max taxi, NWS angle and wind limits to taxi or tow with abnormal landing gear

UAE A380 FCOM LIM-LG

A

Max taxi 5 kt
Max NWS 5º
ABN BLG: Max X-Wind 35kts (i)
ABN WLG: Max X-wind for landing (ii)

(i) On Dry and Wet twy/rwy (gust included)
(ii) Depending on twy/rwy surface condition

104
Q

What lights can be used during refueling?

UAE A380 FCOM LIM-LT

A
  • NAV
  • LOGO
  • WING
105
Q

Latitude ground alignment limit

UAE A380 FCOM LIM-NAV

A
  • 82º N
  • 78.25º S
106
Q

IR will not provide valid magnetic heading and track at:

UAE A380 FCOM LIM-NAV

A
  • North of 82ºN
  • South of 60ºS
  • North of 73º (90ºW-120ºW)

True must be selected in those cases

107
Q

LDPA limitation?

(and their workarounds)

UAE A380 FCOM LIM-PEA

A
  • Will not take into account the 10kt TW limit when the AD elevation is > 8000.
  • Cannot calculate OVWGHT LDG in CONF 3 CAT II Approach with GA Flaps at 1+F (1)
  • Error when Vapp is too high due failures or HW (2)

(1) Calculate CONF 2 for GA and another one with Normal approach type w/ Autoland and use the most limiting one
(2) Reduce HW component if too high or reduce Vpilot

108
Q

IFPA Limitation?

UAE A380 FCOM LIM-PEA

A
  • Cannot incorporate MEL
  • CDL does not auto-populate
  • Cannot use Mach to make calculations with NSC (1)
  • Cannot calculate TURB speed if CRZ below cross over (2)
  • Will Show Mach 0.0 if MAX Alt is below entered CRZ ALT
  • ATMO Cannot calculate with CDL or accounts NSC
  • Plan with optimum profile may fail
  • CLB does not consider auto-derate (3)

Non Standard Config (e.g. L/G extended)

(1) Use a CAS Entry (Convert Mach to CAS with ATMO)
(2) Use Fixed Speed
(3) Use Open CI

109
Q

TOPA limitations?

(and their workarounds)

UAE A380 FCOM LIM-PEA

A
  • May not give FLEX results when conditions allow (1)
  • It disregards a second computation using a rounded up value if TOPA rounds the TOW (2)
  • LOADSHEET transferred TOW to TOPA App is rounded up.
  • ACFT STS will clear after 60 min of inactivity
  • CDL number of missing items hidden in ACFT STS box (3)

(1) Add 100 kg and calculate again
(2) pilots should enter the TOW in KG
(3) Use scroll bar

110
Q

LOADSHEET App Limitation?

UAE A380 FCOM LIM-PEA

A
  • If manual fuel distribution used, it has to be exact as there is no tolerance
  • Cannot calculate with max FOB (-150kg)
  • Does not consider MEL affecting fuel distribution
111
Q

BTV Limitation

UAE A380 FCOM LIM-ROP

A
  • Cannot be used on contaminated RWY
  • Cannot use with ECAM impacting LDG PERF
  • Prohibited for JFK 13R/L CANARSIE and VOR App.
112
Q

ROW/ROP Limitations

UAE A380 FCOM LIM-ROP

A
  • Thrust credit always given
  • Only WET/DRY RWY
  • Does not consider fails affecting LDG PERF
113
Q

TAWS limitations?

UAE A380 FCOM LIM-SURV

A

Must be inhibited for RWYS not on database
Must only be inhibited 15nm from fields where approaches have produced false alerts

114
Q

OANS Limitations?

UAE A380 FCOM LIM-NAV

A
  • Taxi: Allowed on Both PM and PF Displays
  • Takeoff: Not Authorized for PF
  • CRZ/DES/APP: PF or PM to prepare BTV and Taxi prep
  • ROLLOUT: Allowed for PM. PF at Taxi Speed only
115
Q

Printer Limitations?

UAE A380 FCOM LIM-PRT

A

If a discrepancy exists between OIT display and printed information, the OIT takes precedence

116
Q

Minumim Cabin OXY Pressure for Three class config?

UAE A380 FCOM LIM-OXY

A
  • 1300 psi for normal DARD
  • 1650 for Himalayan DARD
117
Q

Minumim Cabin OXY Pressure for Two class config?

UAE A380 FCOM LIM-OXY

A
  • 1350 psi for normal DARD
  • 1750 for Himalayan DARD