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A380 Limtations/Memory Items > A380 Limitation/memory > Flashcards

A380 Limitation/memory Flashcards

1
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

Clean? And Other?

A

Clean config………..-1 g to +2.5 g

Other config…………0 g to +2 g

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2
Q

Maximum T/off & Ldg Airfield Altitude

A

10,000 ft

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3
Q

Minimum TAT for operations

A

-53 deg

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4
Q

Runway slope (mean)

Minimum runway width?

A

± 2 %

45 m
* If the Runway + Shoulders is less than 58 m wide, the flight crew applies a specific procedure. Refer to PRO-NOR-SUP-SUP-MISC General.

  • The technique of turn on a runway or turn pad is not permitted on a contaminated runway.
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5
Q

Maximum certified crosswind at takeoff (gust included)?

Maximum certified crosswind at landing (gust included)?

A

35 kt

  • The maximum certified crosswind value is an AFM limitation. It is an engine limitation.
  • For information, maximum demonstrated crosswind at takeoff: 39 kt gusting 51 kt.

————————————————————————————

40 kt

  • The maximum certified crosswind value is an AFM limitation. It is an engine limitation.
  • For information, maximum demonstrated crosswind at landing: 42 kt gusting 56 kt.
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6
Q

Maximum tailwind at takeoff?

Maximum tailwind at landing?

A

For T/off:

15 kts
—————————————————————————
For Landing:

● If the airport pressure altitude is at or below 8 000 ft: 15 kts

● If the airport pressure altitude is above 8 000 ft: 10kts

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7
Q

MAXIMUM WIND FOR CABIN AND CARGO DOORS OPERATION?

A

MAXIMUM WIND FOR CABIN AND CARGO DOORS OPERATION
Maximum wind for cabin door operation……………………………………40 kt
Maximum wind is 50 kt, if the aircraft nose is oriented into the wind.

Maximum wind for cargo door operation………………………………….. 40 kt
Maximum wind is 50 kt, if the aircraft nose is oriented into the wind, or if the door is on the leeward
side.

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

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8
Q

COCKPIT WINDOW MAXIMUM SPEED for opening and closing?

A

Maximum opening speed……………………….250 kt
Note: Opening the cockpit window is not possible with the packs ON.

Maximum closing speed ………160 kt

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9
Q

MAXIMUM FLAPS/SLATS SPEEDS?

A

FLAPS 1………263kts
Flaps 1+F ……222kts
Flaps 2 ……….220kts
Flaps 3 ……….196kts
Flaps Full ……182kts

In conf 1+F, 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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10
Q

MAXIMUM OPERATING SPEED VMO/MMO?

A

VMO …………………………………………….340 kt
MMO……………………………………………0.89

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11
Q

Maximum Nosewheel steering Angle for tiller and rudder?

A

Via Tiller…70* till 40kts G/S then decreases linearly from40kts to 100kts

Via Rudder…6* till 100kts G/S

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12
Q

MAXIMUM SPEEDS WITH THE LANDING GEAR EXTENDED, Operating and gravity extended?

A
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13
Q

MAXIMUM TIRE SPEED?

A

Maximum ground speed ………..204 kt.

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14
Q

Maximum speed for Windscreen Wipers?

A

250kts

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15
Q

MINIMUM CONTROL SPEEDS, All Engines Operative VMCL & 2 Engines inoperative VMCL-2?

A

VMCL……………………………………..120 kt
VMCL-2…………………………………. 144 kt

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16
Q

Maximum Taxi Weight?
Maximum Takeoff Weight (MTOW)?
Maximum Landing Weight (MLW)?
Maximum Zero Fuel Weight (MZFW)?
Minimum Weight?

A

Maximum Taxi Weight….. 574 000 kg
MTOW………………………….. 572 000 kg
MLW……………………………… 391 000 kg
MZFW……………………………. 366 000 kg
Minimum Weight ……………270 000 kg

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17
Q

On the ground, for air-Conditioning, when can’t you have HP GRD air supply on?

A

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

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18
Q

What is the limitation for AIR-CONDITIONING WITH LP GROUND CARTS?

A

The airflow from the LP ground carts must not exceed 6.3 kg/sec.

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19
Q

Can you take off with PACKs OFF?

A

Takeoff with both packs OFF is prohibited.

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20
Q

What is the Maximum Positive Differential pressure?

What is the maximum negative Differential Pressure?

A

Maximum positive differential pressure…….9.65 psi
Maximum negative differential pressure …..- 0.725 psi

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21
Q

Minimum Height to use Autopilot after T/Off?

A

100ft AGL and at least 5 sec after lift off

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22
Q

Minimum height to disconnect autopilot from a Non-precision approach?

A

200ft AGL

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23
Q

Minimum height to disconnect autopilot from Circling approach?

A

200ft AGL

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24
Q

Minimum height to disconnect Autopilot from a ILS approach with CAT1/APPR1 displayed on the FMA?

A

160ft AGL

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25
Q

Minimum height to engage Autopilot from a manual Go-Around?

A

100ft AGL

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26
Q

Minimum height for Autopilot connected for all other Approaches?

A

500ft AGL

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27
Q

Can you use the A/P or F/D in OP DES or DES mode during a approach?

A

YES. However the Altitude set on the AFS CP must be set to, or above, the higher of MDA or 500ft AGL

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28
Q

Can you use NAV mode after T/Off without GPS PRIMARY?

A

Yes, as long as the FMS runway position update has been checked

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29
Q

Can you use NAV mode in the Terminal Area if GPS PRIMARY is not available?

A

YES, as long as HIGH accuracy is displayed and the appropriate RNP is checked or entered. Or the FMS navigation is crosschecked with navaid raw data.

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30
Q

Can a VOR, VOR/DME, NDB, NDB/DME approach without GPS PRIMARY available be flown?

A

Yes, as long as FMS navigation is crosschecked with reference to Navaid raw data.

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31
Q

Can a VOR, VOR/DME, NDB, NDB/DME, or BARO-VNAV guidance for an ILS (G/S out), LOC, LOC-BC be flown with the FLS function?

A

Yes, provide F-APP or F-APP+RAW capability is displayed on the FMA

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32
Q

Can you use FLS function for an RNAV(GNS) approach with LNAV/VNAV minima or LNAV minima?

A

Yes, provided F-APP capability is displayed on the FMA

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33
Q

Maximum Headwind for Auto approach, Landing and Rollout?

A

38kts

Note: Wind limitation is based on the surface wind reported by ATC or ATIS. If the ND indicates a
current wind speed that exceeds the above-noted autoland limitations, but the ATC or ATIS
reports a surface wind speed within the limitations, then the flight crew can perform an
automatic landing. If the ATC or ATIS reports a surface wind speed beyond the limitations, the
flight crew can only perform a CAT I automatic approach without autoland

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34
Q

Maximum Tailwind for Auto Approach, Landing and Rollout?

A

Airport below 8000ft pressure altitude:
15kts

Airport above 8000ft press Alt:
10kts

Note: Wind limitation is based on the surface wind reported by ATC or ATIS. If the ND indicates a
current wind speed that exceeds the above-noted autoland limitations, but the ATC or ATIS
reports a surface wind speed within the limitations, then the flight crew can perform an
automatic landing. If the ATC or ATIS reports a surface wind speed beyond the limitations, the
flight crew can only perform a CAT I automatic approach without autoland

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35
Q

Maximum X-Wind for Auto Approach, Landing and Rollout?

A

30kts

Note: Wind limitation is based on the surface wind reported by ATC or ATIS. If the ND indicates a
current wind speed that exceeds the above-noted autoland limitations, but the ATC or ATIS
reports a surface wind speed within the limitations, then the flight crew can perform an
automatic landing. If the ATC or ATIS reports a surface wind speed beyond the limitations, the
flight crew can only perform a CAT I automatic approach without autoland

36
Q

Can a One Engine Inoperative Auto Approach, Landing be conducted?

A

Yes, Automatic approach and automatic landing are approved in CONF 3 and CONF FULL, if engine
out procedures are completed before reaching 1 000 ft in approach.

37
Q

Can TWO ENGINES INOPERATIVE ON THE OPPOSITE SIDE Auto approach and Landing be conducted?

A

Yes, Automatic approach and automatic landing are approved in CONF 3, if engine out procedures
are completed before reaching 1 000 ft in approach.

38
Q

During APU start, how long must you wait after setting the APU MASTER SW pb to ON before setting the APU START pb to ON?

A

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.

39
Q

In the case of an aborted APU start or APU shutdown, how long must you wait for another Start attempt?

A

flight crew must wait 60 s before a new
start attempt.
This 60 s period is due to the ECB inhibition logic after an aborted APU start or APU shutdown.

40
Q

Max EGT for APU start on the ground & In-flight?

A

700* on the ground

800* In-flight

41
Q

After 3 consecutive start attempts of the APU, how long must you wait before another star attempt?

A

flight crew must wait 60 min before a new start attempt.
This 60 min period is to allow the APU starter to cool down

42
Q

What are the APU limits reference to the aircraft speed?

A

In the case of an all engine failure/flame out, the APU can operate at any aircraft speed.
Otherwise, the APU can operate, when the aircraft speed is below M 0.56

43
Q

With A/C speed less than M 0.56, what is the Max altitude to start the APU?

A

20,000ft

44
Q

With the APU running, what is the maximum altitude to use APU electrical & bleed?

A

22,500ft

45
Q

How many APU generators can be used on the ground and in-flight?

A

On ground, both APU generators can operate. On ground, each APU generator can supply up to 120 KVA.

In flight, up to 22 500 ft, only one APU generator can operate.

46
Q

Can APU Bleed be used for Wing Anti-ice?

A

Use of APU bleed air for wing anti-ice is not permitted

47
Q

Take Off/Go-Around Time and EGT limits for one Engine inoperative & all Engines operative?

A

All engines operative 5 min & 900 °C One engine inoperative 10 min & 900*C

48
Q

MCT EGT limit?

A

850*C

49
Q

Starting EGT limits for on the Ground & In-flight?

A

On the ground 700C
In-Flight 850C

50
Q

Maximum continuous Oil temperature

A

196 °C

51
Q

Minimum starting Oil temperature

A

-40*C

52
Q

Minimum Oil temperature prior to takeoff?

A

40 °C

53
Q

What are the minimum Oil quantity based on flight times?

A

Note: One of the following actions or oil system characteristics can cause indications of reduced
oil quantity on the ENG SD page:
- If oil drains from the oil tank to the engine after oil servicing, or
- If engine crank or engine run are performed on the engine before the flight.
As a result, if the oil quantity indicated on the ENG SD page is less than the FCOM
minimum oil quantity, perform one of the following:
- Check that the oil tank level, that was reported in the technical logbook, is above the FCOM minimum oil quantity, or
- Check in the technical logbook that the oil tank was fully filled

54
Q

What are the maximum shaft speeds for N1, N2 and N3?

A

N1 max ……………………………………..97.2 %
N2 max ……………………………………..98.7 %
N3 max ……………………………………..97.8

55
Q

What are the Starter limit times reference to continuous starter operations?

What is the cooling off period for the last cycle?

What value must N3 be below before re-engaging the starter?

A

Maximum continuous starter operation is 5 min:
- 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

56
Q

What speed should Max Reverse thrust not be used above?

A

Maximum reverse should not be used below 70 kt (or when the indication starts to fluctuate). Idle
reverse is allowed down to aircraft stop

57
Q

Can you use Reduced thrust on contaminated runways?

What is the Maximum and minimum Flex temperatures?

A

Takeoff at reduced thrust is not allowed on contaminated runways.

The flex temperature must not be:
- Higher than ISA + 60 °C
- Lower than the flat rating temperature or actual OAT.

58
Q

Can you apply TOGA thrust when performance is based on a derated take off?

Can you use a combination of FLEX take off and Derated Take off?

Can you use Derated Thrust on a contaminated runway?

A

Selection of TOGA thrust is not permitted when a Derated Takeoff is performed, except when
requested in any abnormal or emergency procedures.

The use of reduced thrust takeoff (FLEX takeoff) is not permitted in conjunction with Derated Takeoff.
The flight crew selects the derate level on the MFD PERF TO page. This prevents the simultaneous
selection of both a derate level and a TFLEX.

The use of Derated Takeoff is permitted regardless of the runway condition (dry, wet or contaminated)

59
Q

Max altitude with Slats/Flaps extended?

A

20 000 ft

60
Q

Minimum Fuel Temperature?

Maximum Fuel temperature?

A

The minimum fuel temperature is the actual freezing point of the fuel used for the flight.

+53 °C

61
Q

What is the consideration of Jet A fuel uploaded from the US?

A

Preflight, review the Technical Log and check the previous flights. If any of the two previous flights
were from the USA (where Jet A fuel is uplifted), the fuel freeze point for the next sector must be considered to be -40 °C.
If any of the two previous flights were from the USA, and a fuel freeze temperature of -47 °C is required for the planned flight, e.g polar operations, check that the Technical Log has been annotated with the fuel freeze point for Jet A1 fuel, -47 °C. If the Technical Log is not annotated, Flight Crew must contact Engineering

62
Q

Maximum Allowed Wing Imbalance at Takeoff, in Flight , and Landing?

A

Feed tanks 1 / Feed tanks 4……. ………3 000 kg
Feed tank 2 / Feed tank 3……………….. 3 000 kg
Left inner tank / Right inner tank……. 3 000 kg
Left mid tank / Right mid tank………… 2 500 kg
Left outer tank / Right outer tank……. 1 200 kg

note: In abnormal conditions (i.e. fuel system failures) the above-mentioned maximum fuel
imbalance values may be exceeded without significantly affecting the aircraft handling
qualities. The aircraft remains fully controllable in all phases of the flight.

63
Q

MINIMUM FUEL QUANTITY BEFORE PUSHBACK?

A

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.

If before pushback, the fuel quantity in one or more feed tanks is less than 4 000 kg with fuel available
in transfer tanks, the following alerts may appear during the flight:
- FUEL FQMS 1 FAULT followed a few minutes later by
- FUEL FQMS 1+2 FAULT
- FUEL MAN XFR PROCEDURE.

64
Q

Maximum brake temperature for takeoff?

A

300*

65
Q

Maximum altitude at which the landing gear can be extended ?

A

21 000 ft
The speed limitation for landing gear extension is 250 kt/M 0.55. The Landing Gear Control and Indication System (LGCIS) uses only speed limitation to inhibit the landing gear extension. To avoid any inadvertent landing gear extension out of speed limit when the aircraft flies in Mach, the cross-over
altitude corresponding to the speed of 250 kt/M 0.55 is introduced as the highest altitude target to extend the landing gear. This altitude is 21 000 ft. Nevertheless in the case of emergency, respecting the M 0.55 speed limitation, the flight crew can extend the landing gear if necessary.

66
Q

In some situations, after a rejected takeoff or after a landing, the flight crew may need to taxi the aircraft
with deflated tires.
What are the limitations to apply in order to be able to taxi or to tow the aircraft with deflated tires:

A
  • No deflated nose landing gear tire in the case of towbarless towing
  • Maximum taxi speed: 3 kt
  • Maximum nosewheel steering (NWS) angle: 30 °
  • Up to 9 tires can be deflated with the following maximum of deflated tires per landing gear:
  • One deflated tire on the nose landing gear, or/and
  • Two deflated tires per body landing gear provided they are not on the same axle, or/and
  • Two deflated tires per wing landing gear provided they are not on the same axle.

The following exceptions apply in order to be able to taxi the aircraft with deflated tires:
- For runway vacating only, the two deflated tires on the body or wing landing gear can be on the same axle.
- For taxi, the two deflated tires can be located on the center axle of the body landing gear.

67
Q

During refueling, What external lights, can you only select?

A
  • Navigation and Obstruction lights (NAV sw)
  • LOGO lights (LOGO sw)
  • WING and Engine Scan lights (WING sw).
68
Q

In NAV mode, the IR will not provide valid magnetic heading and magnetic track angle in beyond what Latitudes?

A
  • North of 82 ° North
  • North of 73 ° North between 90 ° and 120 ° West (magnetic polar region)
  • South of 60 ° South.
    When flying at latitudes beyond these limits, TRUE reference must be selected.
69
Q

The use of OANS is approved for certain flight phases only, what are they for TAXI, T/OFF, CRZ/DESC/APP, ROLL OUT For LANDING?

A

TAXI: The use of OANS is authorized on both PF and PM displays.

#TAKEOFF:
The use of OANS is not authorized on PF display.
#CRUISE, DESCENT AND APPROACH:
The use of OANS is authorized on either PF or PM display for:
- BTV
- Taxi preparation.
#ROLL OUT AFTER TOUCHDOWN:
The use of OANS is authorized:
- On PM display
- On PF display at taxi speed

Note: Direct visual observation out of the cockpit windows remains the primary means of taxiing.
If there is a conflict between outside and OANS display, the reference will be the outside
view

70
Q

What are some of the precision runway conditions when planning to use the BTV (Brake to Vacate) function?

A
  • Any wet runway including a PFC or grooved surface must be considered wet
  • Any wet runway declared as Slippery Wet must be considered contaminated
  • Any wet runway associated with a Braking Performance Level less than “5 Good” must be considered contaminated.

**The use of BTV is prohibited on contaminated runway.

71
Q

The TAWS function should be inhibited (TERR SYS button set to OFF on the MFD SURV/CONTROLS
page) when?

A
  • For operation from/to runways not incorporated into the TAWS database,
  • For specific approach procedures, which have previously been identified as potentially producing false terrain alerts. The TAWS should be inhibited when the aircraft position is less than 15 NM from the airfield.
72
Q

LOSS OF BRAKING memory item

A

Call out by PF: “LOSS OF BRAKING”

REV……………………………MAX
Brake Pedals……………..Release
A-Skid order………………OFF
Brake Pedals……………..Press
*if still no braking
PARK BRK………………….ON

73
Q

EMERG DESCENT memory item

A

Call out by PF: “EMERGENCY DESCENT”

OXY Masks…………………..ON
SIGNs…………………………..ON
EMER Descent………………Initiate
*if A/Thr not active
All THR LVRs………………….IDLE
SPEED BRAKE………………..FULL

74
Q

STALL RECOVERY memory item

A

Call out by PF: “STALL, I HAVE CONTROL”

NOSE DOWN Pitch…………Apply
BANK angle……………………Wings Level
*Indications out of the stall
THRUST…………………Increase smoothly
SPEEDBRAKES………..ensure retracted.
FLIGHT PATH………..Recover smoothly
*If blw FL200 and in clean config
FLAP 1…………………………….Select

75
Q

STALL WARNING AT LIFT OFF memory item

A

Call out by PF: “STALL, TOGA 12.5°”

THRUST……………….TOGA
PITCH…………………..12.5*
BANK angle………….Wings Level

76
Q

UNRELIABLE AIRSPEED memory item

Before thrust reduction

A

Call out by PF: “UNRELIABLE SPEED”

AP………………………OFF
A/THR…………………OFF
FD………………………OFF
All THR LVRs………..TOGA
PITCH trgt……………12.5*

77
Q

UNRELIABLE AIRSPEED memory item

After thrust reduction

A

Call out by PF: “UNRELIABLE SPEED”

IF SAFE conduct of FLIGHT IMPACTED:

AP………………………OFF
A/THR…………………OFF
FD………………………OFF
if derated CLB engaged
((All THR LVRs………..MCT then CLB))
All THR LVRs………..CLB
PITCH trgt……………12.5 blw 10000
……………10* 10000-25000
……………5* above 25000
In CLB: Adjust Pitch TRGT
*if Flap Lever is set to Full
FLAPS………………….select CONF 3
SPEED BRAKES………check retracted

78
Q

TAWS CAUTION memory item

OBSTACLE AHEAD
TERRAIN AHEAD
TERRAIN TERRAIN
TOO LOW TERRAIN

A

“Pull Up TOGA”

AP………………………OFF
PITCH………………..FULL UP
THRUST LVRS…….TOGA
Speed Brake………Retracted
BANK angle………..WINGS Level
*Can adjust bank provided that turning is the safest action
DONT CHANGE CONFIGURATION

79
Q

TAWS WARNING memory item

PULL UP
TERRAIN AHEAD PULL UP
OBSTACLE AHEAD PULL UP

A

Call out by PF: “PULL UP TOGA”

AP……………………OFF
PITCH……………….PULL UP
THRUST LVRS…..TOGA
SPEED BRAKE…..check retracted
BANK angle………Wings Level
DONT CHANGE COFIG UNTIL CLEAR OF OBSTACLE

80
Q

TCAS CAUTION memory item

A

Call out by PF: “TCAS, I have control”

DO NOT PERFORM A MANEUVER BASED ON A TA ALONE

81
Q

TCAS WARNING RESOLUTION ADVISORY

A

TCAS does not trigger RA’s:
* below 900’AGL on desc
* below 1100’AGL on climb

Call out by PF: “TCAS, I have control”

AP (if engaged)……………..OFF
FDs……………………………….OFF
VERTICAL SPEED…………..Adjust or maintain

*if during approach with CONF 3
A/P & F/D can remain engaged during the G/A

82
Q

WINDSHEAR WARNING REACTIVE WINDSHEAR

A

Call out by PF: “WINDSHEAR TOGA”

The PRIMs perform the reactive windshear detection.
It is available:
During takeoff: From 50 ft or 3 s after liftoff, and until reaching 1 300 ft
During landing: From 1 300 ft to 50 ft.

83
Q

RTO procedure

A
84
Q

TAWS CAUTION memory item

GLIDESLOPE

and

TOO LOW GEAR
TOO LOW FLAPS

A

> 1000’ IMC or >500’ VMC
Flight path………….Adjust
<1000’ IMC or >500’ VMC
GO-AROUND………Consider

GO-AROUND……….PERFORM

85
Q

TAWS CAUTION memory item

SINK RATE

and

DONT SINK

A

> 1000’ IMC or >500’ VMC
Flight path………….Adjust
<1000’ IMC or >500’ VMC
GO-AROUND………Consider

FLIGHT PATH…………Adjust

A380 Limtations/Memory Items (1 decks)

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