Emergency Ops Useful Info Flashcards

1
Q

Abnormal operation of slats/flaps

A

Control laws may change
Selected speed must be used
Approach attitudes change
Go around procedure may have to be modified
Approach and landing distance will increase.

If this happens during approach.
Pull speed
Delay approach to allow for completion of ECAM procedure.
Carry out QRH landing with slats/flaps jammed procedure.

Update approach briefing.
Auto pilot may be used to 500ft AGL

Consider tail strike
Go around speeds and configuration
Use of selected speed in a go around is a must.
Increased fuel consumption.

Overspeed red and black strip computed from actual flap/slat position. If not there use tabulated speeds.

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2
Q

Hydraulic systems unique systems

A

Green: Emer gen, NwS, L/G (separated by priority valve).
Flaps and slats
Normal brakes
Blue: Altn brake/park brake
Slats, BCM
Yellow: Flaps, BCM.

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3
Q

If you lose DC essential bus

A

Ac says cat III single but you are only permitted to do cat I approach.
This is due to LHS W/S heat being out of operation.

Fire push buttons must be used to shut down engines on the ground.

Speaker needs to be turned up on Pm side as RMP 1 is U/S

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4
Q

Some electrical failures can lead to the loss of the AP 2 pb light, LG lights, brake pressure indicator panel.

A

Make sure this is on on the FMA or in the respective status page.

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5
Q

Tripped CB on the ground

A

Can be reset with co-ordination of maintenance. NOT TO BE DONE with any Fuel pump CBs.

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6
Q

With landing gear stuck down fuel consumption is increased by a factor

A

of 2.8 ( roughly 3).

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7
Q

Emergency ELEC Approach considerations

A

Delay selection of land recovery until SLaT/Flap extension required.
A/THR not available
APPR mode not available as RAs both inop.
LOC mode is available.
AP1 and FD 1 become unavailable when land recovery pressed. (FPV is available).
Anti skid available when land recovery bus pressed as it repowers BSCU 1.
Consider higher intercept of GP to give more time to stabilise aircraft.
If both gens have been deliberately switched off by the crew (in case of smoke) consider turning them on for landing.

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8
Q

Smoke non required Memory actions

A

Masks if required: on/100% emergency
Vent extract: OvRD
Cabin Fans: Off
Galley: Off
Signs: on

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9
Q

Smoke procedure memory actions

A

Masks if required: on/100% emergency
Vent extract: OvRD
Cabin Fans: Off
Galley: Off
Signs: on

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10
Q

Decel light

A

Means auto brake is working to 80% at least of selected rate. Might not come on if on a contaminated runway with autobrake working properly due to effect of anti skid.

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11
Q

Level 1 caution

A

No aural warning… crew awareness.

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12
Q

Level 2 caution

A

Has aural warning
ECAM actions apply
(Awareness then action)

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13
Q

Level 3 warning

A

Aural warning. Immediate action required.

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14
Q

Do not press the IDG push button switch

A

Until GEN FAULT light comes on.
For more than 3 seconds as this could cause damage to the disconnect solenoid.

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15
Q

Engine out cat II and Cat III autoland approaches

A

Only approved with conf 3

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16
Q

Should a single FMGC fail

A

Autopilot will work on the unaffected side. ATHr remains operative. Might need to reengage auto pilot. tHR lock could appear.

An aircraft can be dispatched with FM2 U/S

17
Q

In the case of a dual FMGC fail

A

AP both sides lost. Try to reengage just incase. ATHr May still work depending on the nature of the failure.

NaV tuning and automatic pressurisation are now no longer available.

Only 4 buttons available on the MCDU. DIR FPLN PROG and MCDU MENU.

GPWS TERR is Lost
CAT 1 only approach available.

18
Q

Queued faults on ECAM are

A

Queued on the RHS of the EWD. Asterisks mean secondary failures. Overflow arrow indicates additional procedures which cannot be displayed.

19
Q

When flying with the BUsS

A

DO NOT use the speed brakes.

20
Q

When the BUSS is active.

A

AP FD and A/THR are inoperative
Alternate law applies
Stall warning remains operative
Cabin pressure must be controlled manually.
FPV might be available once all ADRs are switched off.
Altitudes are based on GPS data.
Vertical speed indications are no longer available.

21
Q

When above FL 250 and experiencing unreliable speed indications

A

Keep one ADR on to prevent BUSS activation.

22
Q

When altitude unreliable with u reliable airspeed

A

Disregard
Altitude
IAS/TAS
Wind
V/S

Can use
Ground speed
GPS altitude
RA
Cabin alt