Memory Items Flashcards
[MEM] LOSS OF BRAKING
If no braking:
REV - MAX
If needed, the flight crew may keep maximum reverse thrust until full aircraft stop.
BRAKE PEDALS - RELEASE
When the flight crew sets the A/SKID & N/W STRG sw to OFF, the alternate braking mode is activated. Consequently the PF should release the brake pedals before the PM selects the A/SKID off. This action avoids brutal braking application.
For information on the alternate braking mode, Refer to DSC-32-30-10 Operation.
A/SKID OFF - ORDER
The PF orders the PM to set the A/SKID & N/W STRG sw to OFF.
A/SKID & N/W STRG - OFF
BRAKE PEDALS - PRESS
MAX BRK PR - 1000 PSI
Limit brake pressure to approximately 1000 PSI. Monitor brake pressure on the BRAKES PRESS indicator.
If still no braking:
PARK BRAKE - USE
Use short successive parking brake applications to stop the aircraft.
[MEM] STALL RECOVERY
As soon as any stall indication (could be aural warning, “STALL STALL” red message on PFD, buffet…) is recognized, apply the immediate actions:
“STALL, I have control “
NOSE DOWN PITCH CONTROL - APPLY
This will reduce angle of attack
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 20000 ft :
FLAP1 - SELECT
NOTE - If a risk of ground contact exists, once clearly out of stall (no longer stall indications), establish smoothly a positive climb gradient.
[MEM] STALL WARNING AT LIFTOFF
If stall warnings trigger at liftoff, apply the following immediate actions:
“STALL, TOGA 15° “
THRUST - TOGA
At the same time:
PITCH ATTITUDE - 15 °
BANK - WINGS LEVEL
[MEM] UNRELIABLE SPEED INDICATION
If the safe conduct of the flight is impacted:
”UNRELIABLE SPEED ”
AP - OFF
A/THR - OFF
FD - 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
FLAPS (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
[MEM] EGPWS/GPWS CAUTIONS:
“TERRAIN TERRAIN”
“TOO LOW TERRAIN”
“TERRAIN AHEAD”
“OBSTACLE AHEAD”
During night or IMC:
Simultaneously:
AP - OFF
PITCH - PULL UP
Pull to full backstick and maintain in that position.
THRUST LEVERS - TOGA
SPEEDBRAKE lever - CHECK RETRACTED
BANK - WINGS LEVEL or ADJUST
Aircraft obtain the best climb performance when the wings are as level as possible. The flight crew can adjust bank while climbing, provided that turning is the safest action.
NOTE - For some airports, the operator may define a specific procedure.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
During daylight and VMC, with terrain and obstacles clearly in sight:
FLIGHT PATH - ADJUST
Adjust pitch, bank and thrust to silence the alert.
NOTE - For some airports, the operator may define a specific procedure.
[MEM] TCAS WARNING - RESOLUTION ADVISORY
Always follow RA orders, even if this results in crossing the intruder altitude, because these orders ensure the best altitude separation.
CAUTION - Be aware that the intruder may have a TCAS, and may maneuver in response to a coordinated RA order. Therefore, not following an RA order could compromise safe separation.
All RA, except any CLIMB RA during approach in CONF 3 or FULL:
AP (if engaged) - OFF
FDs - OFF
Respond promptly and smoothly.
VERTICAL SPEED - ADJUST or MAINTAIN
Adjust or maintain the vertical speed as required, depending on the green area, and/or to avoid the red area of the vertical speed scale.
NOTE - Avoid excessive maneuvers while attempting to maintain the vertical speed just outside the red area of the vertical speed scale, and within the green area. If necessary, use the full speed range between Vαmax and VMAX.
Respect stall, GPWS, or windshear warnings.
ATC - NOTIFY
When the “CLEAR OF CONFLICT” aural alert sounds:
ATC - NOTIFY
LATERAL AND VERTICAL GUIDANCE - ADJUST
Adjust the lateral and vertical guidance to resume normal navigation, in accordance with ATC clearance.
AP/FD - AS RQRD
[MEM] WINDSHEAR WARNING - REACTIVE WINDSHEAR - Takeoff - Before V1
If Windshear is detected, both PFDs display a WINDSHEAR message. An associated aural WINDSHEAR alert sounds three times.
If the flight crew detects WINDSHEAR, apply the following recovery technique:
If there are significant variations in airspeed, and in airspeed trend below the indicated V1, reject the takeoff.
If windshear occurs during the takeoff roll, the aircraft may reach V1 later (or sooner) than expected. The flight crew should ensure that there is sufficient runway remaining to stop the aircraft, if necessary.
[MEM] WINDSHEAR WARNING - REACTIVE WINDSHEAR - Takeoff - After V1
If Windshear is detected, both PFDs display a WINDSHEAR message. An associated aural WINDSHEAR alert sounds three times.
If the flight crew detects WINDSHEAR, apply the following recovery technique:
If after V1:
THR LEVERS - TOGA
REACHING VR - ROTATE
SRS ORDERS - FOLLOW
If necessary, the flight crew may pull the sidestick fully back.
NOTE - If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then, if necessary to prevent a loss of altitude, increase the pitch attitude.
[MEM] WINDSHEAR WARNING - REACTIVE WINDSHEAR - Airborne - initial climb or landing
If Windshear is detected, both PFDs display a WINDSHEAR message. An associated aural WINDSHEAR alert sounds three times.
If the flight crew detects WINDSHEAR, apply the following recovery technique:
”WINDSHEAR TOGA ”
Airborne - initial climb or landing:
THR LEVERS AT TOGA - SET OR CONFIRM
AP (if engaged) - KEEP ON
SRS ORDERS - FOLLOW
If necessary, the flight crew may pull the sidestick fully back.
NOTE - The autopilot disengages, if the angle of attack value goes above alpha prot.
If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then, if necessary to prevent a loss of altitude, increase the pitch attitude.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR.
CLOSELY MONITOR THE FLIGHT PATH AND THE SPEED.
SMOOTHLY RECOVER TO NORMAL CLIMB OUT OF WINDSHEAR.
EMER DESCENT - PF
CREW OXY MASKS - USE
ALT - TURN PULL
HDG - AS RQRD
SPD - PULL
NOTE: The initial altitude set in the FCU should always be FL180 or MEA.
If structural damage:
SPD/MACH pb - PUSH
CHRONO - START
FMA - ANNOUNCE
If A/THR not active:
THR LEVERS - IDLE
SPD BRK - FULL
Request ECAM ACTIONS (If applicable)
Request QRH procedure (If applicable)
When ALT* engages
SPD BRK - RETRACT
SPD - ADJUST
Ensure A/THR is ON
CM1 - When the aircraft reaches a safe flight level:
PA: “Flight attendants, you may now circulate. Flight Director, to the interphone, agents de bord, vous pouvez maintenant circuler. Directeur de vol, à l’interphone”.
NOTE: Finally, subsequent to an emergency descent, once the oxygen masks are removed, the flight crew should perform all of the following:
- Close the oxygen stowage mask compartment.
- Press the PRESS TO RESET oxygen control slide, to deactivate the mask microphone, and to cut off the oxygen.
EMER DESCENT - PM
CREW OXY MASKS - USE
SIGNS - ON
FMA - CHECK
ATC - NOTIFY
EMERGENCY DESCENT PA - ANNOUNCE:
“This is the captain, fasten your seatbelt. Ici le commandant, attachez votre ceinture”.
Accomplish ECAM Actions (If applicable).
Accomplish QRH procedure (If applicable).
If cabin altitude > 14000 ft:
MASKS MAN ON - PRESS
PA: “Attention, put on your oxygen mask, Attention, mettez votre masque à oxygène”.
