Rejected Take-off Below V1
- Brakes….. Full Braking
- Power levers (All 3)….. Idle
- AIRBRAKES….. AB2
- Thrust Reverser….. As required
Engine Failure At Or After V1
At Vr Rotate the airplane with full aft stick until a positive flight path is achieved.
At V2 Maintain V2 by pitch up and down adjustments, limited to +20° pitch attitude (no thrust adjustment).
When a positive flight path is established:
• Landing Gear….. Up
• AT NOT LESS THAN 400 FT AAL….. Level Flight Acceleration
Slats-Flaps may be set to SF 1 as soon as V+10 is attained.
- AT VFR….. SF 0
- WHEN IN CLEAN CONFIGURATION….. Set and maintain Vfto
5 MINUTES MAX. AFTER TAKE-OFF THRUST POWER SETTING
• Power Levers….. CL
Go Around - One Engine Inoperative (Approach with SF3)
• TOGA….. PUSH
Rotate the airplane until a positive flight path is achieved.
• Power Levers….. TO
• SLATS/FLAPS….. SF 2
• Landing Gear….. Up
• SLATS/FLAPS….. SF 1
• AT NOT LESS THAN 800 FT AAL….. Level Flight Acceleration
• At VFR….. SLATS/FLAPS - SF 0
• WHEN IN CLEAN CONFIGURATION….. Set and maintain Vfto
• Power Levers….. CL
Direct Laws
• Sidestick….. Neutral Position
Maneuver with caution.
Back-up
Use pitch trim for pitch control and rudder pedals for roll control.
Control Surface Jam
- Maneuver with caution
* Maintain current speed or reduce below red tape if more restrictive, and maintain configuration.
Inoperative CCD
• Revert Corresponding CCD to inner position
or
• Use other side CCD
DU Failure
- All DUs….. On - Dim
- All DUs….. AUTO
- Each Blank Display: DU….. OFF
- Each red crossed display: DU….. REV
OXY: PAX SUPPLY FAIL
Failure of pax oxygen delivery system
• PAX OXYGEN rotary knob….. O’RIDE
• Passenger masks….. Don - Checked
OXY: PAX SUPPLY FAIL - remains on:
• Apply EMERGENCY DESCENT procedure
Unreliable Airspeed
• Disregard Flight Path Vector in affected PDUs, SFD and HUD
• Disengage AP/AT
• Maneuver with caution
Level the wings
- Pitch….. 4°
- Power levers….. Gently adjusted to Max Climb
Apply UNRELIABLE AIRSPEED emergency procedure (section EMERGENCY - SPECIFIC EMERGENCY SITUATIONS)
Increase Speed Alert
- Power setting….. Adjust
- AP….. Disengage
- Path angle….. Adjust to increase speed
Overspeed Alert
- AP….. Disengage
- Adjust power setting and / or path to decrease speed
- AIRBRAKES….. As required
- Pull up maneuver engaged by FBW system should not be counteracted by the crew
Rudder Trim Runaway
- Counteract using pedals and the manual yaw trim
- Crew must apply continuous pressure on pedals if airplane is not auto-trimmed.
- Engine differential thrust can be set to compensate a possible slipping tendancy.
Pitch Trim Runaway
- Counteract using sidestick
- Counteract using the manual pitch trim
- TRIM EMERG….. ON
(FCS: THS DEGRAD, FCS: ALTN LAWS ACTIVE and AFCS: AP FAIL appear)
Unwanted Disconnection of Autothrottle
- AT/DISC….. Push
- Try to re-engage the autothrottle.
If the re-engagement cannot be achieved:
• Continue the flight without the autothrottle.
Unwanted Disconnection of Autopilot
- SIL or AP quick disconnect….. Push
* Reengage autopilot in normal flight conditions.
Unusual Attitude Recovery - Nose Down
- Autopilot and Autothrottle….. Disconnect
- Power levers…… Idle
- Bank….. Wings Level
- AIRBRAKES….. As required
- Nose up pitch control….. Smoothly apply
WHEN NOSE IS CLOSE TO HORIZON:
• AIRBRAKES….. AB0
• Thrust….. Adjust
Unusual Attitude Recovery - Nose Up
- Autopilot and Autothrottle….. Disconnect
- Power levers…… TO
- Bank the aircraft by the shortest way….. 80° to 90° Bank
- AIRBRAKES….. AB 0
WHEN AIRCRAFT NOSE IS CLOSE TO HORIZON:
• Bank….. Wings Level
• Thrust….. Adjust
Stall
SIMULTANEOUSLY and smoothly: • Autopilot and Autothrottle..... Disconnect • Pitch control..... Nose down • Bank..... Wings level • Power levers..... TO • AIRBRAKES..... AB 0
AFTER STALL RECOVERY:
• Pitch Attitude….. Close to Horizon
• Thrust….. Adjust
TCAS Alert
- Autopilot….. Disconnect
* TCAS RA Guidance….. Follow
Windshear Recovery
- TOGA pushbutton….. Press
- Autopilot….. Disconnected - Check
- Flight Director….. Follow
- Power Levers….. TO
- SLATS/FLAPS….. SF 2 maximum
At pilot’s discretion, according to airplane height and vertical speed:
• Landing gear handle….. Up
Disregard possible amber Low Speed Cue, “increase speed” aural warning and basic mode EGPWS aural alert during windshear recovery.
Pull Up
- Autopilot….. Disconnect
- Level the wings
- Sidestick fully aft
- Power Levers….. TO
- SLATS/FLAPS….. SF2 Maximum
- Landing Gear….. Up
Rapid Decompression
- Operating Technique CREW RESPIRATORY PROTECTION procedure….. Applied
- Operating Technique EMERGENCY DESCENT procedure….. Applied
Emergency Descent
The following procedure assumes structural integrity of the airplane.
If structural integrity is questioned:
• Limit airspeed to lowest practicable value
• Avoid high maneuvring load factors
- FASTEN BELT….. ON
- Autopilot….. Disconnect
- Power levers (all 3)….. Idle
- AIRBRAKES….. AB 2
- Descent airspeed….. Mmo / Vmo smooth air conditions
- Transponder….. 7700
