Memory Items COPY COPY Flashcards
EGPWS
Caution: During night or IMC conditions, apply the procedure immediately. Do not delay reaction for diagnosis.
Caution:During daylight VMC conditions, with terrain and obstacles clearly in sight, the alert may be considered cautionary.
MEMORY ITEMS
Simultaneously:
1.AP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2.PITCH. . . . . . . . . . . . . .PULL UP (pitch to full backstick and hold)
3.THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA
4.SPEEDBRAKES. . . . . . . . . . . . . . . . . . . . .CHECK RETRACTED
5.BANK . . . . . . . . . . . . . . . . . . . . . . . . .WINGS LEVEL or ADJUST
TCAS
MEMORY ITEMS for TCAS RA
- AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF (if engaged)
- FDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Emergency Decent
- CREW OXY MASKS (Both) - ON, Establish Crew Communication
- CHRONO (Both) - PRESS
Timing is required when maximizing passenger oxygen. - Descend with the autopilot and/or flight directors engaged:
- Turn the ALT selector knob and pull.
- Turn the HDG selector knob and pull.
Caution: Possible high terrain off the airway.
- Adjust the target SPD/MACH.
Note: Use of autopilot is also permitted in EXPEDITE mode. - THR LEVERS (if A/THR not engaged) - IDLE
- SPD BRK - FULL
Speedbrake extension will increase VLS. Avoid autopilot disconnection and automatic retraction of the speedbrakes by allowing speed to increase before using the speedbrakes.
UNRELIABLE AIRSPEED
Note: Respect all stall warnings if in ALTERNATE LAW.
1. AUTOPILOT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2. FLIGHT DIRECTOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. AUTOTHRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. Adjust Pitch/Thrust:
- Below THR RED ALT . . . . . . . . . . . . . . . . . . . . . . . . . 15°/TOGA
- Above THR RED ALT and below 10,000’ . . . . . . . . . . . . 10°/CLB
- Above THR RED ALT and above 10,000’. . . . . . . . . . . . . 5°/CLB
5. FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . Maintain current CONFIG
6. SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . Check retracted
7. GEAR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
When at or above MSA or circuit altitude, level off for troubleshooting
1.GPS Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . Display on MCDU
2.When flight path is stabilized:
• PROBE/WINDOW HEAT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Loss of Braking
- If AUTOBRAKE is selected:
- BRAKE PEDALS - PRESS
Note: This action will override the autobrake function. - If no braking is available:
- THRUST LEVERS - MAX REVERSE
- BRAKE PEDALS - RELEASE
- A/SKID & N/W STRG - OFF
- BRAKE PEDALS - PRESS
Note: Apply pressure with care since initial pedal force produces more braking action in alternate mode than in normal mode. - MAX BRK PRESS - 1000 PSI
Note: Monitor brake pressure on the BRAKES PRESS indicator. At low ground speed, adjust brake pressure as required. - If still no braking:
- PARKING BRAKE - ON
Note: Use short successive parking brake applications to stop the aircraft. If possible, delay the use of the parking brake until low speed, to reduce the risk of tire burst and lateral control problems.
Crew Incapacitation
“NO 1 CODE BRAVO CODE BRAVO”
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.Request assistance from any medically qualified passenger.
Check if a type qualified company pilot is on board to replace the incapacitated crew member.
Stall Recovery
- NOSE DOWN PITCH CONTROL………………………. APPLY
(Note: In case of lack of pitch authority, reducing thrust my be required) - BANK…………………………… WINGS LEVEL
When out of stall:
THRUST……………………… APPLY SMOOTHLY AS REQD SPEEDBRAKES……………… CHECK RETRACTED FLIGHT PATH...……………… RECOVER If in clean config and below 20,000' FLAP1………………………… SELECT
Stall Warning at Lift-Off
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.
Windshear
BEFORE V1
The takeoff should only be rejected if unacceptable airspeed variations occur below the indicated V1, and the pilot decides that there is sufficient runway remaining to stop the aircraft.
AFTER V1
THR LEVERS……………TOGA
REACHING VR…………..ROTATE
SRS ORDERS……………………FOLLOW
This includes the use of full backstick, if demanded.
Note: 1. If engaged, the autopilot disengages when α is greater than α prot.
2. If the FD bars are not available, use an initial pitch attitude up to 17.5 ° with fullbackstick, if necessary. If needed, to minimize the loss of height, increase this pitch attitude.
AIRBORNE, CLIMB OR APPROACH
THR LEVERS TOGA………………..SET OR CONFIRM
AP (if engaged)…………………….KEEP
SRS ORDERS…………………….FOLLOW This includes the use of full backstick, if demanded.
Note: 1. If engaged, the autopilot disengages when α is greater than α prot.
2. If the FD bars are not available, use an initial pitch attitude up to 17.5 ° with fullbackstick, if necessary. If needed, to minimize the loss of height, increase this pitch attitude.
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.
Windshear Ahead
DURING TAKEOFF RUN………………… REJECT TAKEOFF --- When Airborne THR LEVERS....................TOGA As usual, the slat/flap configuration can be changed, provided the windshear is not entered. SRS ORDERS................... FOLLOW
This includes the use of full backstick, if required.
Associated with an aural synthetic voice “GO AROUND, WINDSHEAR AHEAD”
GO-AROUND………………………..PERFORM
This includes the use of full backstick, if required.
Note: 1. If engaged, the autopilot disengages when α is greater than α prot.
2. If the FD is not available, use a pitch initial attitude up to 17.5 °. If necessary tominimize the loss of height, increase this pitch attitude.
Engine Failure During Cruise (Standard Strategy -to maximize the flight time while descending)
Engine Failure During Cruise (continued)
Standard Strategy
The goal is to maximize the flight time while descending to the engine out cruise altitude. This strategy applies when high terrain is not a factor.
MEMORY ITEMS for Standard Strategy
1.THRUST LEVERS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MCT
2.A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
3.CRUISE FL . . . . . . . . . . . . . . . . . . . . . . . DETERMINE and PULL
4.SPEED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PULL
5.ECAM ACTIONS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . PERFORM
6.ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
The PF will perform the following driftdown procedure:
•Set Max Continuous Thrust (MCT) on operable engine.
•Disconnect A/THR.
•Pull to select present speed.
•Determine Cruise FL (REC MAX as displayed on PROG page). Set in FCU and PULL to initiate descent.
•Select a heading to keep clear of the airway, if appropriate.
•Order PM to perform ECAM actions.
•Notify ATC of intentions.
After descent is initiated:
•Select target speed (M.78 / 300) in the FCU.
Note:The speed target of M.78/300 knots is chosen to ensure the aircraft is within the stabilized windmill engine relight inflight envelope.
Caution:Do not decelerate below Green Dot.
•Determine Long Range Cruise altitude (refer to LRC Performance Charts). Set on the FCU and continue descent, unless ATC clearance indicates lower.
•Set the above altitude in the PROG page (L1 - CRZ Altitude).
When reaching Long Range Cruise altitude:
•Engage A/THR.
•Activate managed speed to Long Range Cruise speed (refer to LRC Performance Chart if data on PROG page is not available).
Note:One engine out ceiling information is also available in the QRM.
Standard Strategy (continued):
The REC MAX altitude provides a 0.3 G buffet margin. It is the altitude at which level flight can be maintained at engine-out long range cruise speed, with MCT set on the operating engine, anti-ice off, and the failed engine windmilling.
The driftdown altitude is often higher than the recommended maximum altitude because buffet margins are not provided at the driftdown altitude. For this reason, the flight crew should select a level-off altitude that is at or below the engine-out REC MAX altitude displayed on the PROG page
Engine Failure During Cruise (Obstacle Strategy -maximize the flight distance while descending)
Engine Failure During Cruise
Obstacle Strategy
The goal is to maximize the flight distance while descending to the engine out cruise altitude. This becomes especially critical in areas of high terrain.
MEMORY ITEMS for Obstacle Strategy
1.THRUST LEVERS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MCT
2.A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
3.SPEED. . . . . . . . . . . . . . . . . . . .SELECT GREEN DOT and PULL
4.CRUISE FL . . . . . . . . . . . . . . . . . . . DETERMINE and set in FCU
5.ECAM ACTIONS. . . . . . . . . . . . . . . . . . . . . . PERFORM
6.ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
The PF will perform the following driftdown procedure:
•Set Max Continuous Thrust (MCT) on operable engine.
•Disconnect A/THR.
•Select green dot speed in the FCU and maintain altitude while slowing to green dot.
•Set Cruise FL (Green Dot Level Off Altitude displayed on PERF CRZ page or from Single Engine Gross Flight Path Descent Chart) in the FCU and pull for OP DES 3-5 kts prior to green dot.
•Select a heading to keep clear of the airway, if appropriate.
•Order PM to perform ECAM actions.
•Notify ATC of intentions.
After descent is initiated:
•Maintain green dot and MCT.
•Periodically adjust FCU speed to maintain green dot.
•If V/S becomes less than 500 fpm, select V/S mode.
When reaching green dot level off altitude and terrain is not a factor:
•Set Long Range Cruise altitude on the FCU and PULL for OP DES (refer to LRC Performance Charts), unless ATC clearance indicates lower.
•Set the above altitude in the PROG page (L1 - CRZ Altitude).
When reaching Long Range Cruise Altitude:
•Engage A/THR.
•Activate managed speed and accelerate to Long Range Cruise speed (refer to Long Range Cruise Performance chart if data on PROG page is not available).
Note:One engine out ceiling information is also available in the QRM
Engine Failure: ABOVE acceleration altitude and above thrust reduction altitude
1) Leave autopilot in
2) Thrust leavers to MCT (it will say THR MCT on FMA) (Going to TOGA would engage SRS/GA TRK)
3) Check climb gradient
If sid requires climb gradient of more than 2.5% (denoted by having a minimum climb gradient on there (if below 2.5% required then gradient not mentioned on SID), then carry out a turn to best area for terrain avoidance. Do not continue the SID.
Engine Failure: ABOVE thrust reduction altitude but BELOW acceleration altitude
1) Leave autopilot in
2) Thrust leavers to TOGA (it will say THR MCT on FMA, but as below accel it will still be in SRS mode)
3) Check climb gradient
If SID requires climb gradient of more than 2.5% (denoted by having a minimum climb gradient on there (if below 2.5% required then gradient not mentioned on SID), then carry out a turn to best area for terrain avoidance. Do not continue the SID.
