EMERGENCY DESCENT
if structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering load
CABIN ALTITUDE WARNING or Rapid Depressurization
PASSENGERS SIGNS……..ON
PASS OXYGEN switch……ON
ABORTED ENGINE START
ENGINE LIMIT or SURGE or STALL
2. Thrust Lever (affected engine)…Confirm…Retard until indications stay within limits or thrust lever is closed
ENGINE FIRE or SEVERE DAMAGE or SEPARATION
To manually unlock the engine fire switch, press the override and pull
ENGINE OVERHEAT
RUNAWAY STABILIZER
Control Airplane pitch attitude manually with control column and main electric trimaran needed
4.If the runaway stops after the autopilot is disengaged
——————
5. If the runaway continues after the autopilot is disengaged
STAB TRIM CUTOUT switches (both)…CUTOUT
If the runaway continues:
Stabilizer trim wheel…Grasp & hold
LANDING CONFIGURATION
TAKE OFF CONFIGURATION
Assure correct aircraft take off configuration
WARNING HORN (INTERMITTENT) or WARNING LIGHT CABIN ALTITUDE OR TAKE OFF CONFIGURATION
If the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates in flight at an airplane flight altitude above 10,000 feet MSL
Don the oxygen mask and set the regulator 100%
Establish crew communication
Go to the CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION CHECKIST ON PAGE 2.1
If the intermittent warning horn sounds or a TAKEOFF light (if installed and operative) illuminates ON THE GROUND when advancing the thrust levers to takeoff thrust
Assure correct airplane takeoff configuration
UNCOMMANDED ROLL
AUTOPILOT(IF ENGAGED) DISENGAGE
MAINTAIN CONTROL OFTHE AIRPLANE WITH ALL AVAILABLE FLIGHT CONTROLS. IF ROLL IS UNCONTROLLABLE, IMMEDIATELY REDUCE PITCH/ANGLE OF ATTACK AND INCREASE AIRSPEED.
DO NOT ATTEMPT TO MAINTAIN ALTITUDE UNTIL CONTROL IS RECOVER
AUTOTHROTTLE(IF ENGAGE) DISENGAGE
VERIFY THRUST IS SYMMETRICAL
STALL RECOVERY
HOLD CONTROL COLUMN FIRMLY A/P A/T DISENGAGE SMOOTHLY APPLY NOSE DOWN WING LEVEL ADVANCE THRUST LEVERS AS NEEDED RETRACT SPEEDBRAKES NO CHANGE CONFIG
GPWS RECOVERY TERRAIN TERRAIN
A/P A/T DISENGAGE AGGRESSVILY APPLY MAX THRUST SIMULTANEUSLY WING LEVEL PITCH UP 20 DEG RETRACT SPEEDBRAKES IF NEEDED PITCH UP TO STICK SHAKER NO CHANGE IN CONFIG
WINDSHEAR RECOVERY
A/P DISENGAGE PUSH EITHER TOGA AGGRESSIVLY APPLY MAX THRUST A/T DISENGAGE SIMULTAN WING LEVEL PITCH 15 DEG RETRACT SPEEDBRAKES FOLLOW FD
SEVERE TURBULENCE
PAX SIGNS ON YAW DAMPER ...............ON A/T.................. DISENGAGE A/P .................................CWS ENGINE START SWTCH...FLT THRUST.................................SET