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Memory Items A320 > Belair detailed Memory items > Flashcards

Belair detailed Memory items Flashcards

1
Q

“AVOID TERRAIN”

A

Simultaneously:

AP …………………………………………………OFF

PITCH……………………………………..PULL UP
Pull to full backstick and maintain in that position.

THRUST LEVERS ………………………..TOGA

SPEED BRAKES lever………………………CHECK RETRACTED

BANK……………….WINGS LEVEL or ADJUST
●When flight path is safe and the warning stops:
Decrease pitch attitude and accelerate.
●When speed is above VLS, and vertical speed is positive:
Clean up aircraft, as required.

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2
Q

“PULL UP”

A

Simultaneously:

AP …………………………………………………OFF

PITCH……………………………………..PULL UP
Pull to full backstick and maintain in that position.

THRUST LEVERS ………………………..TOGA

SPEED BRAKES lever…………………….CHECK RETRACTED

BANK…………….WINGS LEVEL or ADJUST

●When flight path is safe and the warning stops:
Decrease pitch attitude and accelerate.
●When speed is above VLS, and vertical speed is positive:
Clean up aircraft, as required.

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3
Q

″TERRAIN TERRAIN PULL UP″

A

Simultaneously:

AP …………………………………………………OFF

PITCH……………………………………..PULL UP
Pull to full backstick and maintain in that position.

THRUST LEVERS ………………………..TOGA

SPEED BRAKES lever……………………..CHECK RETRACTED

BANK……………..WINGS LEVEL or ADJUST
●When flight path is safe and the warning stops:
Decrease pitch attitude and accelerate.
●When speed is above VLS, and vertical speed is positive:
Clean up aircraft, as required.

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4
Q

″TERRAIN AHEAD PULL UP″

A

Simultaneously:

AP …………………………………………………OFF

PITCH……………………………………..PULL UP
Pull to full backstick and maintain in that position.

THRUST LEVERS ………………………..TOGA

SPEED BRAKES lever……………………..CHECK RETRACTED

BANK…………….WINGS LEVEL or ADJUST
●When flight path is safe and the warning stops:
Decrease pitch attitude and accelerate.
●When speed is above VLS, and vertical speed is positive:
Clean up aircraft, as required.

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5
Q

″TERRAIN AHEAD″

A

Adjust the flight path. Stop descent. Climb and/or turn, as necessary, based on
analysis of all available instruments and information.

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6
Q

″SINK RATE″

A

Adjust pitch attitude and thrust to silence the alert.

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7
Q

″DON’T SINK″

A

Adjust pitch attitude and thrust to silence the alert.

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8
Q

″TOO LOW GEAR″

A

Perform a go-around

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9
Q

″TOO LOW FLAPS″

A

Perform a go-around

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10
Q

″GLIDE SLOPE″

A

Establish the aircraft on the glideslope, or set the G/S MODE pb to OFF, if flight
below the glideslope is intentional (non precision approach (NPA))

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11
Q 
Red "Windshear" on PFD
and synthetic voice: 
“WINDSHEAR” 
“WINDSHEAR” 
“WINDSHEAR”

■ If before V1

A

The takeoff should be rejected only if significant airspeed variations occur below indicated V1 and
the pilot decides that there is sufficient runway remaining to stop the airplane.

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12
Q 
Red "Windshear" on PFD
and synthetic voice: 
“WINDSHEAR” 
“WINDSHEAR” 
“WINDSHEAR”

■ If after V1

A

THR LEVERS ………………………………TOGA

REACHING VR…………………………..ROTATE

SRS ORDERS ……………………………FOLLOW

Note:
1. Autopilot disengages if the angle of attack value goes above α prot.
2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then,
if necessary, to prevent a loss in altitude, increase the pitch attitude.

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13
Q 
Red "Windshear" on PFD
and synthetic voice: 
“WINDSHEAR” 
“WINDSHEAR” 
“WINDSHEAR”

■ Airborne, initial climb or landing

A

THR LEVERS AT TOGA………..SET OR CONFIRM

AP (if engaged)……………………………..KEEP

SRS ORDERS …………………………FOLLOW

DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR)
UNTIL OUT OF SHEAR.

CLOSELY MONITOR FLIGHT
PATH AND SPEED.

RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF SHEAR.

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14
Q 
When a predictive windshear alert 
″WINDSHEAR AHEAD″ 
or "
GO AROUND WINDSHEAR AHEAD"
is triggered, if the flight crew makes a positive verification that no hazard exists.....
A

then the alert may be disregarded, as long as:
‐ There are no other signs of possible windshear conditions, and

‐ The reactive windshear system is operational.

Known cases of spurious predictive windshear alerts have been reported at some airports, during either takeoff or landing, due to the specific obstacle environment.
However, always rely on any reactive windshear
(″WINDSHEAR″)

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15
Q

W/S AHEAD RED

Associated with an aural synthetic voice

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

●Before takeoff

A

Delay takeoff,

or

select the most favorable runway.

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16
Q

W/S AHEAD RED

Associated with an aural synthetic voice

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

●During the takeoff run

A

Reject takeoff !

Note: Predictive windshear alerts are inhibited above 100 kts until 50 ft.

17
Q

W/S AHEAD RED

Associated with an aural synthetic voice

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

●When airborne

A

THR LEVERS …………………………….TOGA

As usual, the slat/flap configuration can be changed, provided the windshear is not entered.

SRS ORDERS …………………………FOLLOW

If necessary, the flight crew may pull the sidestick fully back.

Note:
1. Autopilot disengages if the angle of attack value goes above α prot.
2. If the FD are not displayed, move toward an initial pitch attitude of 17.5 °. Then, if
necessary, to prevent a loss in altitude, increase the pitch attitude

18
Q

W/S AHEAD RED

Associated with an aural synthetic voice

“GO AROUND, WINDSHEAR AHEAD”.

■Landing

A

GO AROUND ……………………………PERFORM

If necessary, the flight crew may pull the sidestick fully back.
Note:
1. Autopilot disengages if the angle of attack value goes above α prot.
2. If the FD are not displayed, move toward an initial pitch attitude of 17.5 °. Then, if
necessary, to prevent a loss in altitude, increase the pitch attitude.

19
Q

W/S AHEAD AMBER

■ Before TAKEOFF

A

Delay takeoff until conditions improve.
Evaluate takeoff conditions:
• Using observations and experience,
• Checking weather conditions.
Select the most favorable runway (considering location of the likely windshear).
Use the weather radar or the predictive windshear system before commencing
takeoff to ensure that the flight path clears any potential problem areas.
Select TOGA thrust.
Monitor closely airspeed and airspeed trend during the takeoff run for early
signs of windshear.

20
Q

W/S AHEAD AMBER

■ During Approach

A

Delay landing or divert to another airport until conditions are more favorable.
Evaluate condition for a safe landing by:
• Using observations and experience,
• Checking weather conditions.
Use the weather radar.
Select the most favorable runway, considering also which has the most
appropriate approach aid.
Select FLAPS 3.
Use managed speed in the approach phase.
Check both FDs engaged in ILS, FPA or V/S.
Engage the autopilot, for a more accurate approach and earlier recognition of
deviation from the beam, when ILS is available

Note: ‐ When using the GS mini-function, associated with managed speed,
the system will carry extra speed in strong wind conditions.
‐ In case of strong or gusty crosswind greater than 20 kt, Refer to
FPE-IFL-VAP VAPP Determination without Failure.

21
Q

UNRELIABLE SPEED INDICATION

/

ADR CHECK PROC

A

●If the safe conduct of the flight is impacted

AP/FD………. ………………………………..OFF
A/THR ………….. ……………………………OFF
PITCH/THRUST:
Below THRUST RED ALT……………………………………15°/TOGA
Above THRUST RED ALT and Below FL 100……………………………………….10°/CLB
Above THRUST RED ALT and Above FL 100…………………………………………5°/CLB
FLAPS (if CONF 0(1)(2)(3)) ……………..MAINTAIN CURRENT CONF
if CONF FULL)…………………………SELECT CONF 3 AND MAINTAIN

SPEEDBRAKES…….CHECK RETRACTED
L/G……………………………………………UP
When at, or above MSA or Circuit Altitude:
Level off for troubleshooting
GPS ALTITUDE…………..Display on MCDU

22
Q

UNRELIABLE SPEED INDICATION

/

ADR CHECK PROC

●To level off for troubleshooting:

A

AP/FD……….. …………………………………..OFF
A/THR……….. …………………………………..OFF

Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction may occur.

23
Q

“TRAFFIC” “TRAFFIC”

A

Do not perform a maneuver based on a TA alone

24
Q 
Resolution advisory : 
All “CLIMB” and “DESCEND”
 or 
“MAINTAIN VERTICAL SPEED MAINTAIN”
 or 
“ADJUST VERTICAL SPEED ADJUST” 
or
“MONITOR VERTICAL SPEED"
A

AP (if engaged) …………………………OFF
BOTH FDs…. …………………………….OFF.
Note: Avoid excessive maneuvers while aiming to keep the vertical speed just
outside the red area of the VSI, and within the green area. If necessary,
use the full speed range between Vαmax and VMAX.

Respect stall, GPWS, or windshear warning.
Notify ATC.
●GO AROUND procedure must be performed when an RA “CLIMB” or
“INCREASE CLIMB” is triggered on final approach:
Note: Resolution Advisories (RA) are inhibited below 900 ft.
■ When “CLEAR OF CONFLICT” is announced:
Resume normal navigation in accordance with ATC clearance.
AP/FD can be re-engaged as desired.

25
Q

Emergency Descent

PF

A

• CREW OXY MASKS…………………………..ON
(Establish communication)

• ALT Selector Knob ……………………..Turn left and pull
(Selects lower altitude and open descent)
• HDG Selector Knob………………Turn off airway and pull
• SPD/MACH Selector Knob ………………Pull
(Opens speed/mach window to allow selected speed)

• THR LEVERS (if A/THR not engaged) ……………………..IDLE
If A/THR is engaged, check that THR IDLE is displayed on the FMA
•FMA ……………………………………….Check
Confirm THR IDLE/OPEN DES/HDG
• SPD BRK…………………………….FULL

26
Q

Emergency Descent

PM

A

• CREW OXY MASKS……………………….ON
(Establish communication)

  • SIGNS…………………………………..ON
  • ENG MODE SELECTOR………….IGN
  • ATC…………………………………….Notify
  • “EMERGENCY DESCENT!” x2……..announce PA

IF CAB ALT > 14,000 feet:
PAX OXY MASKS……………….MAN ON

@level off:
“DESCENT COMPLETED”x2…….announce PA

27
Q

LOSS OF BRAKING

A

●IF NO BRAKING AVAILABLE:
REV………….. ………………………….MAX
BRAKE PEDALS ……………..RELEASE
A/SKID & N/W STRG……………….OFF
BRAKE PEDALS…………………..PRESS
MAX BRK PR……………………..1000 PSI

●IF STILL NO BRAKING:
PARKING BRAKE ………….SHORT AND SUCCESSIVE APPLICATIONS

28
Q

STALL RECOVERY

in Flight

A

callout: “STALL, I have control”.

NOSE DOWN PITCH CONTROL……..APPLY

Note: In case of lack of pitch down authority, reducing thrust may be necessary.

BANK…………… …………WINGS LEVEL

●When out of stall (no longer stall indications) :
THRUST…. …………………………..INCREASE SMOOTHLY AS NEEDED

Note: In case of one engine inoperative, progressively compensate the thrust asymmetry with
rudder.
SPEEDBRAKES……CHECK RETRACTED
FLIGHT PATH…………………RECOVER SMOOTHLY
●If in clean configuration and below 20 000 ft:
FLAP 1 ……………………….SELECT
Note: If a risk of ground contact exists, once clearly out of stall (no longer stall indications),
establish smoothly a positive climb gradient.

29
Q

STALL WARNING

AT LIFT-OFF

A

Callout: “STALL, TOGA 15°”

Spurious stall warning may sound in NORMAL law, if an angle of attack probe is damaged. In this case, apply immediately the following actions:
THRUST………… ……………………….TOGA
At the same time:
PITCH ATTITUDE…………………………….15°
BANK…………… ……………….WINGS LEVEL

Note: When a safe flight path and speed are achieved and maintained, if stall warning continues,consider it as spurious.

30
Q

CREW INCAPACITATION

A

“I Have control!”………………………announce
-take over pb………………………………..use
-onside AP……………………………….engage
-“CABIN CREW MEMBER TO THE COCKPIT PLEASE” (2 ×)………………………..announce
-ATC………………………declare emergency
-ensure incap Pilot cannot interfere with controls
-request assistance from medical qualified Pax and check for qualified Company Pilot
-Land as soon as practicable
-arrange medical assistance after landing
-prepare the Approach earlier than usual
-request Radar vectoring and a Long
Approach to reduce the workload
-perform the landing from you usual seat

31
Q

Abnormal V Alpha Prot

Speed above Vls and aircraft goes to continious nose down pitch rate

A

Speed above Vls
Aircraft goes into a continious nose down pitch rate which cannot be stopped with backward sidestick inputs IMMEDIATELY APPL:

  • ONE ADR…………………………KEEP ON
  • TWO ADRs…………………………………OFF
32
Q

Abnormal V alpha prot

  • the Alpha max strip (red strip) completely hides the
    Alpha prot strip (black and amber strip)
  • the aircraft is in a stabilized wings level flight ( no load factor increase)
A

ONE ADR…………………………………KEEP ON
TWO ADRs……………………………………….OFF

Caution: the VSW (black and red strip) could be displayed erroneous

FPV USE……………………………….CONSIDER

33
Q

Abnormal V Alpha prot

  • the Alpha Prot Strip (black and amber strip) rapidly moves by more
    than 30 kts
    -during flight maneuvers (load factor increase)
    -autopilot is ON
    -speedbrakes are retracted
A

ONE ADR…………………………………KEEP ON
TWO ADRs……………………………………….OFF

Caution: the VSW (black and red strip) could be displayed erroneous

FPV USE……………………………….CONSIDER

34
Q

New Golden Rules

A

1 .Fly, navigate and communicate:
In this order and with appropriate tasksharing

  1. Use the appropriate level of
    automation at all times
  2. Understand the FMA at all times
  3. Take action if things do not go as
    expected

Memory Items A320 (1 decks)

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