MEMORY ITEMS Flashcards by Paul Bond

ABORTED ENGINE START L R

FUEL CONTROL SWITCH AFFECTED SIDE
CUTOFF

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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

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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

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DUAL ENG FAIL STALL

FUEL CONTROL SW BOTH CUTOFF THEN RUN
RAM AIR TURBINE SW PUSH AND HOLD FOR 1 SEC

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ENG AUTOSTART L R

FUEL CONTROL SW AFFECTED SIDE CONFIRM CUTOFF

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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

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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

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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

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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

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STABILIZER

STAB CUTOUT SW BOTH CUTOUT
DO NOT EXCEED THE CURRENT AIRSPEED

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FD DOOR AUTO UNLOCK

FD DOOR ACCESS SEL ROTATE TO DENY AND HOLD FOR 1 SEC

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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

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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

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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

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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

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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

RCB
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

RCB 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