Memory Items

Question 1

EGPWS

Answer 1

“PULL UP, TOGA”
Simultaneously
AP………………………………………………………………….OFF
PITCH……………………………………………………..PULL UP
Pull to full back stick and maintain in that position
THRUST LEVERS……………………………………………………………..TOGA
SPEED BRAKE lever…………………………………….CHECK RETRACTED
BANK…………………………………………………WINGS LEVEL or ADJUST

Question 2

REACTIVE WINDSHEAR

Answer 2

“WINDSHEAR, TOGA”
THR LEVERS AT TOGA…………………SET OR CONFIRM
AP (if engaged)………………………………………..KEEP ON
SRS ORDERS………………………………………………………………FOLLOW

DO NOT CHANGE CONFIGURATION UNTIL OUT OF WINDSHEAR.
CLOSELY MONITOR FLIGHT PATH AND SPEED.
RECOVER TO NORMAL CLIMB OUT OF WINDSHEAR.

Notes:

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

Question 3

UNRELIABLE SPEED INDICATION

Answer 3

“UNRELIABLE SPEED”
* If the safe conduct of the flight is impacted
AP/FD……………………………………………………………..OFF
A/THR…………………………………………………………….OFF
PITCH/THRUST
Below THRUST RED ALT……………………………….15 degrees / TOGA
Above THRUST RED ALT and Below FL 100 …….. 10 degrees / CLB
Above THRUST RED ALT and Above FL 100………..5 degrees / CLB
FLAPS (if CONF 0,1,2,3)……………………MAINTAIN CURRENT CONF
FLAPS (if CONF)………………………SELECT CONF 3 AND MAINTAIN
SPEEDBRAKES………………………………………….CHECK RETRACTED
L/G……………………………………………………………………………………UP
When at or above MSA or Circuit Altitude: Level off troubleshooting

Question 4

TCAS

Answer 4

"TCAS, I have control"
AP (if engaged).   OFF
BOTH FDs.  OFF
Respond promptly and smoothly to an RA by adjusting or maintaining the pitch, 
as required, to reach the green area and/or avoid the red area of the vertical 
speed scale.

Question 5

EMERGENCY DESCENT

Answer 5

"EMERGENCY DESCENT"
CREW OXY MASKS.  USE
SIGNS.  ON
EMER DESCENT.   INITIATE
* If A/THR is not active:
THR LEVERS.  IDLE
SPD BRK.  FULL
When descent established
SPEED.  MAX/APPROPRIATE
ENG MODE SEL.  IGN
ATC.  NOTIFY
EMER DESCENT (PA).  ANNOUCE
ATC XDPR 7700.  CONSIDER
MAX FL.   100/MEA-MORA
*If CAB ALT is above 14 000ft:
PAX OXY MASKS.   MAN ON

Question 6

LOSS OF BRAKING

Answer 6

“LOSS OF BRAKING”
* 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

Question 7

STALL RECOVERY

Answer 7

“STALL, I have control”
As soon as any stall indication (could be aural warning, buffet…) is recognized, apply the immediate
actions:
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 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.

Question 8

STALL WARNING AT LIFT-OFF

Answer 8

“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.