Memory Items Flashcards
LOSS OF BRAKING
LOSS OF BRAKING I have control
Reversers Max
Brk Pedals Release
When the flight crew sets the A-SKID to OFF, the control of the braking system is transferred from the BCS to the EBCU, and the emergency braking mode is activated.
In emergency braking:
A-SKID is not available. Hydraulic pressure applied to the brakes is automatically limited, in order to limit risk of tire burst.
Hydraulic pressure is automatically limited to 1 000 PSI at landing (landing brake law), 1 700 PSI for taxi-out and Take-Off (take-off brake law).
It is possible to revert from landing brake law to take-off brake law by set parking brake to position ON.
A/Skid. Off
Brk Pedals Press
If still no Braking
Park Brk. On
The ultimate braking mode is activated. If the ground spoilers are not extended, the parking brake only is activated
The EBCU controls ultimate braking on the WLG brakes.
The PARK BRK handle controls ultimate braking on the BLG brakes
Emergency Descent
Emergency Descent I have Control
Crew Masks On
Signs On
Emer Descent Initiate
Alt……. Turn and Pull
Hdg….. Turn and Pull
Spd…….Pull
FMA……..Announce
If A/Thr not Active
All Thr levers Idle
Sod Brk Lever Full
When in IDLE thrust, high speed and with speed brake extended, the rate of descent is approximately 6 000 ft/min . To descend from cruise altitude to FL 100, it takes approximately 5 min and 40 NM.
Only if the cabin altitude goes above 14 000 ft, the flight crew must press the MASK MAN ON pb
STALL RECOVERY
Stall I have control
Push ……… Nose down pitch
Roll………… Wings level
Power……..When out of stall increase smoothly
Stabilize…..Speedbrake check retracted Flt Path recover smoothly
Below 20 000Ft… Flap 1
STALL WARNING AT LIFTOFF
STALL, TOGA 12.5°
Thrust…… TOGA
Pitch……….12.5Deg
Bank……….Wings Level
UNRELIABLE AIR SPEED INDICATION
UNRELIABLE SPEED
AP………….OFF
A/THR…….OFF
FD………….OFF
Before thrust reduction
ALL THR LEVERS……TOGA
After Thr Reduction MCT then set Clb Thr
Pitch
Below 10 000Ft…………….12.5Deg
Between 10&25 000Ft….10Deg
Above 25 000Ft……………..5Deg
If Flap lever set Full…………Flap3
Flaps & Gear……………………Maintain Current Conf
Speed Brk………………………..Check Retracted
TAWS CAUTION
PULL UP TOGA
AP ………..…….Off
Pitch……………Full up
Thr Levers … TOGA
SPD BRk………Check retracted
Bank…………….Wings Level
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
During daylight and VMC conditions, with terrain and obstacles clearly in sight
Flight Path ………… Adjust
SINK RATE
DON’T SINK
GLIDESLOPE
SINK RATE
Above 1 000 ft AAL IMC or above 500 ft AAL VMC
Flight Path …….. Adjust
Below 1 000 ft AAL IMC or below 500 ft AAL VMC
Go Round ………..Consider
DON’T SINK
Flight Path …….. Adjust
GLIDESLOPE
Above 1 000 ft AAL IMC or above 500 ft AAL VMC
Flight Path …….. Adjust
When conditions require a deliberate approach below glideslope:
G/S MODE………… OFF
Below 1 000 ft AAL IMC or below 500 ft AAL VMC
Go Round ………..Consider
TOO LOW GEAR”, “TOO LOW FLAPS
Go Round ………..Consider
TAWS WARNING
PULL UP TOGA
If the TAWS triggers one of the PULL UP alerts
AP ………..…….Off
Pitch……………Full up
Thr Levers … TOGA
SPD BRk………Check retracted
Bank…………….Wings Level
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL CLEAR OF OBSTACLE.
TCAS WARNING - RESOLUTION ADVISORY
If AP/FD TCAS mode is armed
TCAS Blue
TCAS, I have control
All RA, except any CLIMB RA during approach in CONF 3 or FULL
If the AP is off:
FD Orders ………. Follow
AP can be engaged
Vertical SPD……….Monitor
Any CLIMB RA during approach in CONF 3 or FULL:
GO Around ……….. Perform
Follow the SRS GA mode
Respect stall, GPWS, or windshear warning
ATC………………………. Notify
The flight crew must apply the basic TCAS procedure, if an RA is triggered, and the AP/FD TCAS does not engage
All RA, except any CLIMB RA during approach in CONF 3 or FULL
AP ………….OFF
FDs…………OFF
Respond promptly and smoothly
V/S………….Adjust or Maintain
When the “CLEAR OF CONFLICT” aural alert sounds:
ATC …………Notify
Lateral And Vertical Guidance …… Adjust
AP/FD ………As required
WINDSHEAR WARNING - REACTIVE WINDSHEAR
On ground, at takeoff
During the takeoff roll, WINDSHEAR, WINDSHEAR, WINDSHEAR alert is inhibited. Windshear recognition is based on the flight crew observation.
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
Before V1
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.
After V1
THR Levers ……….. TOGA
Reaching VR………..Rotate Normally
SRS Orders …………Follow
When airborne, during initial climb, or at landing
THR Levers ……….. TOGA
AP if Engaged………Keep on
SRS Orders ………….Follow
If the angle-of-attack value goes above alpha prot, the autopilot disengages.
If the FD is not available, select an initial pitch attitude of 12.5 °. Then, if necessary, increase the pitch attitude, in order to minimize the decrease in altitude
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR.
CAREFULLY MONITOR FLIGHT PATH AND SPEED.
RECOVER SMOOTHLY TO CLIMB, WHEN OUT OF WINDSHEAR.
