0-PROF ITEMS

Question 1

CREW INCAPACITATION

Answer 1

- Maintain aircraft control
- Use of takeover pb as appropriate
- Perform callouts & checklist aloud

- Notify ATC

- Call Lead FA
- Restrain incapacitated crewmember
- Locate additional pilot on-board
> Company, Type-rated, jumpseater
- Locate medical assistance
*- If unable to re-locate crewmember, 1 FA must remain to monitor

- Land at nearest suitable airport

FCTM

Question 2

ONE ENGINE INOPERATIVE - OBSTACLE STRATEGY

Answer 2

1. After initial engine failure procedures are complete, maintain current cruise altitude
2. THRUST LEVERS = Set all to MCT
3. A/THR = OFF
4. HDG = Set and Pull as appropriate
5. Determine OEI/DriftDown Ceiling (PERF-CRZ Page)
6. ATC = Notify
7. Cabin Crew = TEST
8. SPD = Set Green Dot and Pull
   9.ALT = Set DriftDown and Pull
9. When appropriate, begin OEB/ECAM actions
10. When clear of obstales, continue Standard Strategy

FCTM

Question 3

SEVERE TURBULENCE

Answer 3

SIGNS - ON

SPEED & THRUST - ADJUST
*Do not chase Mach or airspeed
*Initial SPD target of .76 or 275
‐ Reference “Speed and Thrust Setting for Recommended Turbulence Speed” tables.

AUTO PILOT - KEEP ON

If excessive thrust variations:
A/THR - DISCONNECT

*If the Flight Crew flies the aircraft manually, they may expect large variations in altitude, but should not chase altitude.

DESCENT TO OR BELOW OPT FL - CONSIDER
‐ Consider descending to or below OPT FL in order to increase buffet margin.

For approach:
A/THR - ON

MANAGED SPEED - USE
Note: For landing:
‐ Configuration FULL, or 3, can be used
‐ CONF FULL provides better handling capability in turbulent conditions, however, CONF 3 provides more energy and less drag.

Question 4

STALL RECOVERY

Answer 4

“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

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 :
CONFIG 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 5

STALL WARNING AT LIFTOFF

Answer 5

“STALL TOGA 15”

If stall warnings trigger at liftoff, apply the following immediate actions:
THRUST - TOGA

PITCH ATTITUDE - 15°

BANK - WINGS LEVEL

Question 6

WINDSHEAR WARNING

Answer 6

> = On ground:

+ If before V1:
TAKEOFF - “REJECT”
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.

+ If after V1:
TAKEOFF - “CONTINUE”

“WINDSHEAR TOGA”

THR LEVERS - TOGA

REACHING VR - ROTATE

SRS ORDERS - FOLLOW
If necessary, the flight crew may pull the sidestick fully back.
Note: 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.

> = Airborne, initial climb or landing:

“WINDSHEAR TOGA”

THR LEVERS - TOGA

AP - KEEP ON (if engaged)

SRS ORDERS - FOLLOW
If necessary the flight crew may pull the sidestick fully back.
Notes:
1. Autopilot disengages when below 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 & SPEED.

RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR.