Memoralis Flashcards
Ground Incident (AOM 1.02.10 P2)
CAPTAIN:
-If an immediate evacuation is not required I will PA, “REMAIN SEATED, REMAIN SEATED”.
-If urgent contact with the In-Charge is required, I will PA, “IN-CHARGE FLIGHT ATTENDANT CALL (OR REPORT TO) THE FLIGHT DECK”.
-If an evacuation is required I will call,
“CHECKLIST, PASSENGER EVACUATION”.
FIRST OFFICER:
I will read the Passenger Evacuation checklist.
Passenger Evacuation (AOM 1.02.10 P3)
Captain:
“Checklist, Passenger Evacuation”
Engine Fire/Failure/Severe Damage/Separation At or Above V1 (AOM 1.02.10 P5)
PF:
In the event of an Engine Fire or Failure after V1, I will continue the take-off and rotate at VR.
PM:
I will call “ENGINE FIRE” or “ENGINE FAILURE” and cancel any warnings. When established in a definite climb I will call “POSITIVE RATE”.
PF:
I will call “GEAR UP.”
PM:
I will select the gear up.
PF:
When stabilized in a climb above 400’ AGL at a minimum of V2, I will ensure or call “LNAV” or “Heading Select”. If Fire or Severe Damage, I will call “ENGINE FIRE DRILL”.
PM:
I will ensure or select LNAV or Heading Select, disengage Autothrottle if engaged, and call “CONFIRM #1 (#2) THRUST LEVER”
PF:
“CLOSE”
PM:
“CONFIRM #1 (#2) ENGINE START lever”
PF:
“CUTOFF”
PM:
“CONFIRM #1 (#2) ENGINE FIRE SWITCH”
PF:
“PULL”
PM:
If the Engine Fire switch or Engine Overheat light remains illuminated, I will discharge the bottle and call “LEFT (RIGHT) BOTTLE DISCHARGED LIGHT ON”. I will call “FIRE OUT” or “30 SECONDS UP”. If the Engine Fire switch or Engine Overheat light remains illuminated, I will discharge the second bottle and call “RIGHT (LEFT) BOTTLE DISCHARGED LIGHT ON”
PF:
At Engine out Acceleration height I will call for Flap retraction on schedule
PM:
I will retract the flaps
PF:
When the flaps are selected up and airspeed is at Flaps up maneuvering speed, I will call (or
select) “LEVEL CHANGE, MAX CONTINUOUS THRUST”
PM:
I will ensure or select Level Change (LVL CHG) and set Max Continuous Thrust
PF:
I will call “CHECKLIST, ENGINE FAILURE” or “CHECKLIST, ENGINE FIRE or ENGINE SEVERE DAMAGE or
SEPARATION”
PM:
I will read and action the appropriate Checklist
Engine Inoperative Cruise/Driftdown (AOM 1.02.10 P8)
PF:
“DISENGAGE AUTOTHROTTLE”, “SET MAX CONTINUOUS THRUST”
PM:
Disengage autothrottle, Select CON thrust in FMC, Manually set Maximum Continuous Thrust
PF:
Adjust trim as required. Confirm that the thrust mode changes to CON and the thrust is set to MCT. Request ENG OUT to be selected on the ECON CRZ page
PM:
On ECON CRZ Page, select ENG OUT, select Failed ENG.
Determine drift down requirement and advise PF. Set the Maximum Engine Out Altitude in the MCP Altitude Window. Set the Engine Out Target Airspeed in the MCP IAS Window
PF:
Slow to Engine Out Target Airspeed, select LVL CHG
PM:
All exterior lights on and advise ATC
PF:
Initiate turn if required and call “CHECKLIST ENGINE FAILURE.” At altitude capture, determine optimum
cruise altitude. Manually adjust thrust to maintain the
ENG OUT speed. Proceed to land at nearest suitable
airport
PM:
Read and action the checklist
Rapid Depressurization and Emergency Descent (AOM 1.02.10 P12)
Captain:
In the event of a rapid depressurization I will assume control, ensure the Autopilot is engaged and call “RAPID DEPRESSURIZATION DRILL”. I will don my oxygen mask and call “CAPTAIN ON OXYGEN”
First Officer:
I will don my oxygen mask and call “FIRST OFFICER ON OXYGEN”
Captain:
I will select the FASTEN BELTS ON. I will PA “ATTENTION - FLIGHT ATTENDANTS SECURE THE CABIN, PASSENGERS TAKE YOUR SEATS”
First Officer:
I will select the Pressurization mode selector to MAN, Select the Outflow VALVE switch to CLOSE until indication shows fully closed. I will check the Cabin Altitude and Rate and call “CABIN OK” or “CABIN UNCONTROLLABLE”
Captain:
If the cabin is uncontrollable I will call, “EMERGENCY DESCENT”, Set the lowest safe altitude or 10,000 ft,
whichever is higher, Initiate a turn if required, Select LVL CHG, Ensure the Thrust Levers are closed, Extend the Speedbrakes, Set VMO/MMO in the speed window
First Officer:
I will Select the Pass Oxygen switch to ON, Ensure FASTEN BELTS selected ON, Select the Landing Lights ON, Advise ATC, Squawk 7700, I will PA: “ATTENTION, PUT ON YOUR OXYGEN MASKS IMMEDIATELY”
Captain:
I will call,“CHECKLIST, CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION”
First Officer:
I will silently read the checklist
Captain:
At 2000 ft above target altitude I will reduce the
airspeed and 1000 ft above, slowly retract the Speedbrakes
First Officer:
Once leveled off I will PA, “IN-CHARGE FLIGHT ATTENDANT CALL (OR REPORT TO) THE FLIGHT DECK”
Traffic Avoidance TA (AOM 1.02.10 P17)
PF and PM:
Look for traffic and use traffic display as guide. Call out any conflicting traffic
PF:
If traffic is sighted, maneuver if needed
Traffic Avoidance RA (AOM 1.02.10 P17)
PF:
Autopilot off, Autothrottle off. Pitch and thrust to satisfy RA command. Follow lateral command, unless visual contact requires other action
PM:
Verify PF actions.
PM & PF:
Attempt to establish visual contact and call out any conflicting traffic
Traffic Avoidance RA Landing Config (AOM 1.02.10 P18)
PF:
Autopilot off, autothrottle off. Advance throttle to maximum thrust and call flap 15. Pitch to RA command, Follow lateral command, unless visual contact requires other action.
PM:
Verify max thrust and select flap 15. When in climb, call positive rate.
PF:
Gear up.
PM:
Select gear up.
PF/PM:
Attempt to establish visual contact. Call out any conflicting traffic.
Nose High Recovery (1.02.10 P23)
PF/PM:
Recognize and confirm the situation
PF:
Disengage autopilot and autothrottle, apply as much as full nose-down elevator, apply appropriate nose down stabilizer trim, reduce thrust, roll to obtain a nose down pitch rate.
Complete the recovery:
When approaching the horizon, roll to wings level, check airspeed and adjust thrust, establish pitch attitude
PM:
Call out attitude, airspeed and altitude throughout the recovery, verify all required actions have been completed and call out any omissions
Nose Low Recovery (1.02.10 P23)
PF/PM:
Recognize and confirm the situation
PF:
Disengage autopilot and autothrottle, recover from stall, if required, roll in shortest direction to wings level (unload and roll if bank angle is more than 90 degrees.)
Recover to level flight:
Apply nose up elevator, apply nose up trim, if required, adjust thrust and drag as required.
GPWS Caution (1.02.10 P24)
PF/PM:
Correct the flight path, airplane configuration, or airspeed
GPWS Warning (P1.02.10 P24)
PF:
“FIREWALL”, disengage autopilot, disengage autothrottle, aggressively apply maximum thrust, simultaneously roll wings level and rotate to an initial pitch attitude of 20°, retract speedbrakes. If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
PM:
Assure maximum thrust, verify all required actions have been completed and call out any omissions.
PF:
Do not change gear or flap configuration until terrain separation is assured, monitor radio altimeter for sustained or increasing terrain separation. When clear of terrain, slowly decrease pitch attitude and accelerate.
PM:
Monitor vertical speed and altitude (radio altitude for terrain clearance and barometric altitude for a minimum safe altitude.) Call out any trend toward terrain contact.
In-Air Overrun Warning (1.02.10 P25)
PF/PM:
Execute go-around.
On-Ground Overrun Warning (1.02.10 P26)
PF:
Simultaneously close the thrust levers and apply maximum manual wheel brakes, verify speed brakes are deployed or raise the SPEED BRAKE lever, apply reverse thrust up to the maximum amount consistent with conditions, continue maximum braking until certain the airplane can stop on the runway
PM:
Verify actions as follows:
Thrust levers closed, maximum brakes applied, verify SPEED BRAKE lever and call “SPEEDBRAKES UP.” or “NO SPEEDBRAKES”, call “REVERSE GREEN” or “NO REVERSE NUMBER 1” (or 2), as appropriate”. Call out omitted action items.
PF:
When stopping is assured:
Start movement of the reverse thrust levers to reach the reverse idle detent before taxi speed, move
the reverse thrust levers to full down.
PM:
Call 60 knots
Approach to Stall Recovery or Stall Recovery (1.02.10 P27)
PF:
“STALL” and :
*Initiate the recovery:
*Hold the control column firmly.
*Disengage autopilot and autothrottle.
*Smoothly apply nose down elevator to reduce the angle of attack until buffet or stick shaker stops. Nose down stabilizer trim may be needed.
PM:
*Monitor altitude and airspeed.
*Verify all required actions have been done and call out any omissions.
*Call out any trend toward terrain contact.
PF:
*Roll in the shortest direction to wings level if needed.
*Advance thrust levers as needed.
*Retract the speedbrakes.
*Do not change gear or flap configuration, except during liftoff, if flaps are up, call for flaps 1.
PM:
*Monitor altitude and airspeed.
*Verify all required actions have been done and call out any omissions.
*Call out any trend toward terrain contact.
*Set the FLAP lever as directed.
PF/PM:
WHEN CONTROL OF FLIGHT PATH IS REGAINED AND GROUND CONTACT IS NOT A FACTOR:
PF:
*Check airspeed and adjust thrust as needed.
*Establish pitch attitude.
*Return to the desired flight path.
*Re-engage the autopilot and autothrottle if desired.
PM:
*Monitor altitude and airspeed.
*Verify all required actions have been done and call out any omissions.
*Call out any trend toward terrain contact.
