MEMORY ITEMS Flashcards
ABORTED ENGINE START L R
FUEL CONTROL SWITCH AFFECTED SIDE
CUTOFF
AIRSPEED UNRELIABLE
AP DISC SW PUSH
A/THR ARM SW BOTH OFF
FD SW BOTH OFF
SET FOLLOWING GEAR UP PITCH ATTIT AND THR
FLAPS EXT 10 DEG 85% N1
FLAPS UP 4 DEG 70% N1
CABIN ALTITUDE
DON THE OXY MASKS
ESTABLISH CREW COMMS
CHECK CABIN ALT AND RATE
IF CABIN ALT UNCONTROLLABLE
PASS OXY SW PUSH TO ON AND HOLD FOR 1 SEC
WITHOUT DELAY DESCEND TO LSALT OR 10000’ WHICHEVER IS HIGHER
TO DESCEND
MOVE THR LEVERS TO IDLE
EXT SPEEDBRAKES
IF STRUCTURAL INTEGRITY IS IN DOUBT LIMIT AIRSPEED AND AVOID HIGH MAN LOADS
DESCEND VMO MMO
DUAL ENG FAIL STALL
FUEL CONTROL SW BOTH CUTOFF THEN RUN
RAM AIR TURBINE SW PUSH AND HOLD FOR 1 SEC
ENG AUTOSTART L R
FUEL CONTROL SW AFFECTED SIDE CONFIRM CUTOFF
ENG LIMIT EXCEED L R
ATHR ARM SW AFFECTED SIDE CONFIRM OFF
THR LEVER AFFECTED SIDE CONFIRM RETARD UNTIL ENG LIMIT EXCEED MSG BLANKS OR THR LEVER AT IDLE
ENG SURGE L R
ATHR ARM SW AFFECTED SIDE CONFIRM OFF
THR LEVEL AFFECTED SIDE CONFIRM RETARD UNTIL ENG SURGE MSG BLANKS OR THR LEVER AT IDLE
ENG SVR DAMAGE SEP L R
ATHR ARM SW AFFECTED SIDE CONFIRM OFF
THR LEVER AFFECTED SIDE CONFIRM IDLE
FUEL CONTROL SW AFFECTED SIDE CONFIRM CUTOFF
ENG FIRE SW AFFECTED SIDE CONFIRM PULL
FIRE ENG L R
MEM ITEMS FOR INFLT ONLY
ON GND USE CHKLIST
ATHR ARM SW AFFECTED SIDE CONFIRM OFF
THR LEVER AFFECTED SIDE CONFIRM IDLE
FUEL CONTROL SW AFFECTED SIDE CONFIRM CUTOFF
ENG FIRE SW AFFECTED SIDE CONFIRM PULL
IF FIRE ENG MSG STAYS SHOWN
ENG FIRE SW ROTATE TO STOP AND HOLD FOR 1 SEC
NOT MEM ITEM
IF AFTER 30 SECS FIRE ENG MSG STAYS SHOWN
ENG FIRE SW ROTATE TO OTHER STOP AND HOLD FOR 1 SEC
STABILIZER
STAB CUTOUT SW BOTH CUTOUT
DO NOT EXCEED THE CURRENT AIRSPEED
FD DOOR AUTO UNLOCK
FD DOOR ACCESS SEL ROTATE TO DENY AND HOLD FOR 1 SEC
APPROACH TO STALL OR STALL RECOVERY
DO AS IF ACTUAL STALL HAS OCCURRED
IMMEDIATELY DO THE FOLLOWING AT THE FIRST INDICATION OF STALL (BUFFET OR STICK SHAKER)
DO NOT USE FD
IF AP NOT ACCEPTABLE DISENGAGE
IF ATHR NOT ACCEPTABLE DISENGAGE
APPROACH TO STALL OR STALL RECOVERY
ACTIONS
PF
INITIATE THE RECOVERY
SMOOTHLY APPLY NOSE DOWN ELEVATOR TO REDUCE THE AOA UNTIL BUFFET OR STICK SHAKER STOPS
PM
MONITOR ALTITUDE AND SPEED
VERIFY ALL REQD ACTIONS HAVE BEEN DONE AND CALL-OUT ANY OMISSIONS
CALL OUT ANY TREND TOWARD TERRAIN CONTACT
PF
CONTINUE THE RECOVERY
ROLL SHORTEST DIRECTION TO WINGS LEVEL
ADVANCE THR LEVERS AS NEEDED
RETRACT SB
DO NOT CHANGE GEAR OR FLAP CONFIG
EXCEPT DURING LIFTOFF IF FLAPS ARE UP CALL FOR FLAPS 1
PM
MONITOR ALT AND SPD
VERIFY ALL ACTIONS CALL OMISSIONS
CALL ANY TREND TOWARDS TERRAIN
SET FLAP AS DIRECTED
PF
COMPLETE THE RECOVERY
CHECK AIRSPEED AND ADJ THR
ESTABLISH PITCH ATTIT
RETURN TO DESIRED FLT PATH
REENGAGE AP AND ATHR IF DESIRED
PM
MONITOR ALT AND SPD
VERIFY AND CALL OMISSIONS
CALL ANY TREND TOWARD TERRAIN
REJECTED TAKEOFF
REASONS
BEFORE 80 KTS
MASTER CAUTION
SYS FAILURE
UNUSUAL NOISE OR VIBRATION
TYRE FAILURE
ABNORMALLY SLOW ACCEL
TAKEOFF CONFIG
FIRE OR FIRE WARNING
ENG FAIL
PWS
AIRPLANE UNSAFE UNABLE TO FLY
> 80 KTS
FIRE OR FIRE WARNING
ENG FAIL
PWS
AIRPLANE UNSAFE UNABLE TO FLY
DURING TAKEOFF CREW MEMBER WHO OBSERVES NON NORMAL SITUATION CALLS IT OUT AS CLEAR AS POSSIBLE
REJECTED TAKEOFF
ACTIONS
CALL STOP
CAPT
CLOSE THR LEVERS
DISENGAGE ATHR
AND
MAX MANUAL BRAKING OR VERIFY RTO BRAKING
IF AUTOBRAKE MSG NEED MANUAL BRAKING
APPLY REV THR TO MAX AMOUNT CONSISTENT WITH CONDS
VERIFY SB ARE EXTENDED
CONTINUE MAX BRAKING UNTIL CERTAIN AIRPLANE CAN STOP ON RWY
WHEN STOPPING ASSURED
REV THR LEVERS TO REACH REV IDLE BY TAXI SPD
AT REV IDLE STOW REV
FO VERIFY
THR LEVERS CLOSED
ATHR DISENGAGED
MAX BRAKE APPLIED
REV THR APPLIED
SPEEDBRAKES UP
REVERERS NORMAL
AUTOBRAKES
CALL ANY OMISSIONS
60 KTS
COMMUNICATE REJECT DECISION TO TOWER AND CABIN AS SOON AS PRACTICAL
REJECTED TAKEOFF
AFTER AIRPLANE STOPPED
ACTIONS
NNC
BRAKE COOLING SCHEDULE
CONSIDER:
WHEEL PLUGS MELTING
NEED TO CLEAR RWY
REQ FOR REMOTE PARKING
WIND DIRECTION INCASE OF FIRE
ALERTING FIRE EQUIP
NOT SETTING PARK BRAKE UNLESS PAX EVAC NEEDED
ADVISING GND CREW HOT BRAKES
ADVISING PAX OF NEED TO REMAIN SEATED OR EVAC
GPWS
CAUTION
PF
CORRECT FLT PATH OR AIRPLANE CONFIG
GPWS
WARNING
PULL UP
OBSTACLE PULL UP
TERRAIN TERRAIN PULL UP
PF
DISCONNECT AP
DISCONNECT ATHR
AGGRESSIVELY MAX THRUST
SIMULT ROLL WINGS LEVEL AND ROTATE TO PITCH ATTIT 20 DEG
VERIFY SB RETRACTED
IF TERR STILL A THREAT CONTINUE ROTATION UP TO PLI OR STICK SHAKER OR INITIAL BUFFET
PM
ASSURE MAX THR
VERIFY ACTIONS CALL OMISSIONS
PF
DO NOT CHANGE GEAR OR FLAP UNTIL TERRAIN SEP IS ASSURED
MONITOR RADIO ALT FOR SUSTAINED OR INCREASING TERRAIN SEP
WHEN CLEAR OF TERRAIN SLOWLY DECREASE PITCH ATTIT AND ACCEL
PM
MONITOR VERT SPD AND ALT RADIO ALT FOR TERR CLR AND BARO ALT FOR MINIMUM SAFE ALT
CALL ANY TREND TOWARD TERRAIN
AFTER RECOVERY THE AIRPLANE POSN TOGETHER WITH MSA OR LSALT MUST BE CROSSCHECKED
GPWS
WARNING
NOTES
DO NOT USE FD
IF POSITIVE VISUAL VERIFICATION IS MADE THAT NO OBSTACLE OR TERR HAZARD EXISTS WHEN FLYING UNDER DAYLIGHT VMC COND PRIOR TO TERR OR OBSTACLE WARNING ALERT MAY BE REGARDED AS
CAUTIONARY AND APP CONTINUED
TCAS TA
PF
LOOK FOR TFC USING TFC DISPLAY AS A GUIDE CALL OUT ANY CONFLICTING TFC
IF TFC SIGHTED MANOEUVRE IF NEEDED
TCAS RA
EXCEPT IN LANDING CONFIG
DESCEND RA BELOW 1000’ AGL SHOULD NOT BE FOLLOWED
PF
IF MANOEVERING REQD DISENGAGE AP AND ATHR
SMOOTHLY ADJ PITCH AND THR TO SATISFY RA COMMAND
FOLLOW PLANNED LATERAL FLT PATH UNLESS VISUAL CONTACT WITH CONFLICTING TFC REQ OTHER ACTION
ATTEMPT TO ESTABLISH VISUAL CONTACT CALL OUT CONFLICTING TFC
TCAS RA
CLIMB RA IN LANDING CONFIG
PF
DISENGAGE AP AND ATHR
ADV THR LEVERS FWD TO ENSURE MAX THR ATTAINED CALL FLAPS 20
SMOOTHLY ADJ PITCH TO SATISFY RA COMMAND
FOLLOW PLANNED LATERAL PATH UNLESS VISUAL CONTACT WITH CONFLICTING TFC REQ OTHER ACTIONS
PM
VERIFY MAX THR SET FLAP 20
VERIFY POSITIVE RATE ON ALT AND CALL POSITIVE RATE
PF
VERIFY POSITIVE RATENOF CLIMB ON ALT AND CALL GEAR UP
PM
SET GEAR UP
PF
ATTEMPT TO EST VIS CONTACT CALL OUT ANY CONFLICTING TFC
UPSET RECOVERY
DEFINITION
HISTORICALLY
PITCH GREATER THAN 25 DEG NOSE UP
PITCH GREATER THAN 10 DEG NOSE DN
BANK ANGLE GREATER THAN 45 DEG
LESS THAN ABOVE BUT INAPPROP FOR THE CONDS
NOW
CONSIDERED ANY TIME AN AIRPLANE IS DIVERTING FROM INTENDED AIRPLANE STATE.
NOSE HIGH RECOVERY
PF
RECOGNISE AND CONFIRM
DISCONNECT AP AND ATHR
RECOVER
APPLY NOSE DOWN ELEV APPLY AS MUCH ELEV AS NEEDED TO OBTAIN A NOSE DOWN PITCH RATE
APPLY APPROP NOSE DOWN STAB TRIM
REDUCE THR
ROLL ADJ BANK ANGLE TO OBTAIN NOSE DOWN PITCH RATE
PM
CALL OUT ATTITUDE SPD AND ALTITUDE
VERIFY ALL ACTIONS AND CALL OMISSIONS
PF
COMPLETE RECOVERY
WHEN APP HORIZON ROLL WINGS LEVEL
CHECK SPD AND THR
ESTABLISH PITCH ATTITUDE
NOSE LOW RECOVERY
PF
RECOGNISE AND CONFIRM
DISCONNECT AP AND ATHR
RECOVER
RECOVER FROM STALL IF NEEDED
ROLL IN SHORTEST DIRECTION TO WINGS LEVEL IF BANK ANGLE MORE THAN 90 DEG UNLOAD AND ROLL
PM
CALL OUT ATTITUDE SPD AND ALTITUDE THROUGHOUT RECOVERY
VERIFY ALL ACTIONS CALL OMISSIONS
PF
COMPLETE RECOVERY
APPLY NOSE UP ELEVATOR
APPLY NOSE UP TRIM IF NEEDED
ADJ THR AND DRAG IF NEEDED
WINDSHEAR WARNING
PWS ON TAKEOFF
MONITOR RADAR DISPLAY
PF MANOUVRE AS REQD TO AVOID
PWS DURING TAKEOFF ROLL
WINDSHEAR AHEAD WINDSHEAR AHEAD
PRIOIR TO V1 REJECT
AFTER V1 PERFORM WINDSHEAR ESCAPE MAN
WINDSHEAR DURING TAKEOFF ROLL
PRIOR V1 MAY NOT BE SUFF RWY TO STOP IF RTO INITIATED AT V1
AT VR ROTATE NORMAL RATE TO 15 DEG PITCH ATTIT
AIRBORNE WS ESCAPE MAN
IF WS ENCOUNTERED NEAR NORMAL ROTATION SPD AND AIRSPD SUDDENLY DECREASES MAY NOT BE SUFF RWY TO ACCEL BACK TO NORMAL TAKEOFF SPD. IF INSUFF RWY TO STOP ROTATE 2000’ BEFORE END RWY IS AIRSPD LOW.
HIGHER THAN NORMAL ATTITUDES MAY BE REQD TO LIFTOFF IN REMAINING RWY. ENSURE MAX THR SET
GO AROUND WINDSHEAR AHEAD
WS ESCAPE MAN OR AT PILOTS DISCRETION NORMAL GA
INDICATIONS
OF AIRPLANE IN WINDSHEAR
WINDSHEAR WARNING
WINDSHEAR WINDSHEAR WINDSHEAR
OR UNACCEPTABLE FLT PATH DEVIATIONS
BELOW 1000’ AGL
15 KTS IAS
500 FPM VERT SPD
5 DEG PITCH
1 DOT G/S
UNUSUAL THR LEVER POSN FOR SIGNIFICANT PERIOD OF TIME
WINDSHEAR ESCAPE MANOUVRE
MANUAL FLT
PF
DISCONNECT AP
PUSH EITHER TOGA SW
AGRESSIVELY MAX THR
DISCONNECT ATHR
SIMULT ROLL WINGS LEVEL ROTATE 15 DEG
VERIFY SB RETRACTED
FOLLOW TOGA GUIDANCE
PM
VERIFY MAX THR
VERIFY ALL ACTIONS CALL OMISSIONS
AUTOMATIC FLT
PF
PUSH EITHER TOGA SW
VERIFY TOGA FMA
VERIFY GA THR
VERIFY SB RETRACTED
MONITOR SYS PERF
PM
VERIFY GA THR
VERIFY ALL ACTIONS CALL OMISSIONS
MANUAL OR AUTO FLT
PF
DO NOT CHANGE CONFIG
MAINTAIN WINGS LEVEL MAX CLB GRADIENT UNLESS TURN OBST CLR
MONITOR VERT SPD AND ALT
DO NOT ATTEMPT TO REGAIN LOST AIRSPD UNTIL WS NO LONGER FACTOR
PM
MONITOR VERT SPD AND ALT
CALL ANY TREND TOWARDS TERRAIN
RECOGNISING A STALL
STICK SHAKER
BUFFET THAT CAN BE HEAVY AT TIMES
LACK OF PITCH AUTHORITY
LACK OF ROLL CONTROL
INABILITY TO STOP A DESCENT
IF AIRPLANE STALLED FIRST RECOVER FROM STALL BY APPLYING AND MAINTAINING NOSE DOWN ELEV UNTIL STALL RECOVERY IS COMPLETE AND STICK SHAKER STOPS
ILS GLS PRM BREAKOUT MAN
PF
DISC AP AND IMMEDIATELY TURN TO BREAKOUT HEADING
IF REQD INITIATE A CLIMB OR DESCENT
PM
TURN BOTH FD OFF
SET BREAKOUT HDG MCP
SET BREAKOUT ALT ON MCP
AS SOON AS PRACTICABLE
PM
ACKNOWLEDGE ATC
SEL PM FD ON
SEL HDG SEL AND VS OR FLCH
WHEN SEL MODES ON PM FD
PF FD ON
AFTER ACFT ON BREAKOUT HDG
RE ENGAGE AP AS REQD
PF CALL FOR FLAP AND GR AS REQD
IF DESCENT REQD MAX 1000 FPM
FOLLOW ANY TCAS RA MUST COMPLY WITH TURN UNLESS PIC DEEMS SAFETY A PROHIBITING FACTOR
