Memory Items Flashcards
Windshear ahead
Before take off -delay or go for most favourable runway Airborne - thrust - toga - AP- keep on if engaged - SRS orders - follow Can change config till in Windshear
If encountered on landing
- go around must be performed
Windshear
“WINDSHEAR TOGA”
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: 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.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR. CLOSELY MONITOR FLIGHT PATH AND SPEED. RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR.
EGPWS
“PULL UP TOGA”
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
Best climb performance is obtained when close to wings level. Then, for “TERRAIN AHEAD PULL UP” or for “OBSTACLE AHEAD PULL UP”, and if the crew concludes that turning is the safest way of action, a turning maneuver can be initiated. 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.
EMER DESCENT
“EMERGENCY DECENT”
CREW OXY MASKS……………………………………………………..ON
EMER DESCENT………………………..ANNOUNCE(PA)
The flight crew must inform the cabin of emergency descent on the PA system. SIGNS………………………………………………..ON EMER
DESCENT……………………………………………..INITIATE
Descend with the autopilot engaged: ‐ Turn the ALT selector knob and pull ‐ Turn the HDG selector knob and pull ‐ Adjust the target SPD/MACH. Use of the autopilot is also permitted in EXPEDITE mode
THR LEVERS (if A/THR not engaged)........................................................ IDLE ‐ If autothrust is engaged, check that THR IDLE is displayed on the FMA ‐ If not engaged, retard the thrust levers. SPD BRK ..........................................................FULL
Unreliable speed
“UNRELIABLE SPEED”
AP/FD…… OFF
ATHR……. 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.
Loss of braking
“LOSS OF BRAKING”
IF NO BRAKING AVAILABLE: REV………..MAX
BRAKE PEDALS……. RELEASE
Brake pedals should be released when the A/SKID & N/W STRG sw is switched OFF, since the pedal force or displacement produces more braking action in alternate mode than in normal mode.
A/SKID & N/W STRG……………………… OFF Braking system reverts to alternate mode.
BRAKE PEDALS……..PRESS
Apply brake with care, since initial pedal force or displacement produces more braking action in alternate mode than in normal mode.
MAX BRK PR…………1000 PSI Monitor brake pressure or BRAKES PRESS indicator.
Limit brake pressure to approximately 1 000 PSI and, at low ground speed, adjust brake pressure as required.
If STILL NO BRAKING: PARKING BRAKE…………………………………….SHORT AND SUCCESSIVE APPLICATIONS Use short successive parking brake applications to stop the aircraft.
Stall recovery
“STALL, I HAVE CONTROL”
NOSE DOWN PITCH CONTROL…….APPLY
BANK..WINGS LEVEL When out of stall (no longer stall indications) : THRUST….INCREASE SMOOTHLY AS NEEDED
SPEEDBRAKES……… CHECK RETRACTED
FLIGHT PATH ………RECOVER SMOOTHLY
If in clean configuration and below 20 000 ft : FLAP1………. SELECT
Stall warning at lift off
“STALL TOGA 15”
THRUST…………TOGA
At the same time: PITCH ATTITUDE..15°
BANK..WINGS LEVEL
Crew incapacitation
“ATTENTION, PURSER TO COCKPIT PLEASE” the purser or any other cabin attendant must proceed to the cockpit immediately. The cabin attendant must then:
-Tighten and manually lock the shoulder harness of the incapacitated crew member
-Push the seat completely aft
-Recline the seat back. It takes 2 people to remove the dead weight of an unconscious body from a seat without endangering any controls and switches. If it is not possible to remove the body, one cabin attendant must remain in the cockpit to take care of and observe the incapacitated crew member.
In coordination with the purser: Request assistance from any medically qualified passenger.
-Check if a type qualified company pilot is on board to replace the incapacitated crew member.
TCAS
Traffic advisory: “TRAFFIC” messages:
“TCAS, I HAVE CONTROL”
Do not perform a maneuver based on a TA alone. Resolution advisory: All “CLIMB” and “DESCEND” or “MAINTAIN VERTICAL SPEED MAINTAIN” or “LEVEL OFF, LEVEL OFF” or “MONITOR VERTICAL SPEED” type messages:
AP (if engaged)….OFF
BOTH FDs………..OFF
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.