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A380 > SIMEX 01SA > Flashcards

SIMEX 01SA Flashcards

1
Q

REJECTED TAKEOFF

REASONS

A

<100KTS
ANY ECAM

> 100KTS
BE GO MINDED
FIRE ALERT OR SEV DAMAGE
SUDDEN LOSS ENG THRUST
ANY ECAM
ANY INDICATION AIRCRAFT WILL NOT FLY

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2
Q

REJECTED TAKEOFF

PROC

A

CAPT
STOP
SIMULT CLOSE THRUST LEVERS
MAX AVAIL REV THRUST

FO
MONITOR CAPT
REV GREEN
DECEL
AUTOBRAKE MONITOR
ANY AUDIO CANCEL

AIRCRAFT STOPPED
CAPT
STOW REV
PARK BRAKE ON
ALERT PA
ECAM ACTIONS ORDER

FO
ATC NOTIFY
ECAM ACTIONS

NO SPOILERS OR AUTOBRAKE FOR RTO<72Kts

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3
Q

SEV TURB IN FLT

A

MOD TURB KEEP AP AND ATHR ON

SEV TURB ECP ABN PROC
MISC SEVERE TURBULENCE IN CRUISE

ECAM PROC
MAX SPEED .85/300
MIN SPD GREEN DOT

AP ON AND ATHR OFF IF EXCESSIVE THR CHANGES

ON APP IN SEV TURB CAN DISCONNECT ATHR BUT KEEP MANAGED SPEED FOR GND SPD MINI FUNCTION

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4
Q

THUNDERSTORMS IN CRUISE

A

TO INCREASE BUFFET MARGIN CONSIDER A DESCENT BELOW OPT FL

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5
Q

RAINFALL NTENSITY LIMITS AUST

A

LAST 10 MINS

LIGHT <0.4mm

MOD 0.4mm to 1.6mm

HVY >1.6mm

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6
Q

REACTIVE WINDSHEAR

A

PRIMs DETECT

AVAIL
DURING TAKEOFF 50’ or 3 s after liftoff
LANDING 1300’ to 50’

WINDSHEAR WINDSHEAR WINDSHEAR

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7
Q

PREDICTIVE WINDSHEAR

A

DETECTS
10s BEFORE ENCOUNTER
0.5nm to 5nm IN FRONT AIRCRAFT

AVAIL
IF WX AVAIL OR OFF FOR TAKEOFF
IN FLT <1500’ AGL

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8
Q

P WS

DURING TAKEOFF ROLL TO 100KTS

A

UP TO 3nm
INHIBITED ABOVE 100KTS TO 50’

ABOVE 50’
WARNINGS CAUTIONS AND ADVISORIES AVAIL

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9
Q

REACTIVE WS

MEM ITEMS

A

BEFORE V1
IF SIGNIFICANT VARIATIONS IN AIRSPEED AND AIRSPEED TREND BELOW V1, REJECT THE TAKEOFF

AFTER V1
THR LEVERS TOGA
REACHING VR ROTATE NORMALLY
SRS ORDERS FOLLOW

WHEN AIRBORNE DURING INITIAL CLIMB OR AT LANDING
THR LEVERS AT TOGA SET OR CONFIRM
AP IF ENGAGED KEEP ON
SRS ORDERS FOLLOW

DO NOT CHANGE CONFIG UNTIL OUT OF WINDSHEAR
CAREFULLY MONITOR FLT PATH AND SPEED
RECOVER SMOOTHLY TO CLIMB WHEN OUT OF WINDSHEAR

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10
Q

POSS WS ON FINAL

A

CONSIDER FLAP 3 FOR GA PERF

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11
Q

POSS WS ON TAKEOFF

A

USE TOGA

MAINTAINS ACCEL CAPABILITY

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12
Q

GO AROUND REASONS

A

TCAS
WINDSHEAR
AIRCRAFT ON RWY
NO LANDING CLR

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13
Q

WS
RECOGNITION

A

IAS VARIATIONS 15KTS
GS VARIATIONS
VERT SPEED 500FPM
PITCH ATTIT 5 DEG
GLIDE DEV 1 DOT
HDG VAR 10 DEG
UNUSUAL ATHR ACTIVITY

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14
Q

RESPONSE TO WS WARNINGS

A

ALL REACTIVE WS MUST BE FOLLOWED

PREDICTIVE WS WHERE NO OTHER SIGNS OF POSS WS AND REACTIVE WS DO NOT NEED TO BE FOLLOWED

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15
Q

STABLE APP

LANDING CONFIG BY

A

1000’ RA

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16
Q

STABLE APP

LOWEST ALT

A

500’ RA

ALL APP IMC AND VMC

ALL NORMAL CHKLIST COMPLETE
FINAL LDG FLAP
APP PTH WITHIN TOLERANCES

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17
Q

NOT STABLE

CALL

A

<500’ RA

NORMAL CHKLIST NOT COMPLETE
FINAL LDG FLAP NOT IN POSN
SUSTAINED EXCEEDANCE OF APP TOLERANCE
PF FAILS TO CORRECT FLT PTH

ARMING GND SPOILERS, SPDBRK DEPLOYMENT OR FLAP LOAD RELIEF ARE UNSTABLE AS LDG CONFIG COMPROMISED

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18
Q

EF BELOW THR RED ALT

A

SPEED TARGET V2 to V2 + 15

SAME AS ABOVE THR RED ALT

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19
Q

EF AFTER V1

PROC

A

KEEP AIRCRAFT STRAIGHT
LOCK IN RUDDER

@VR
ROTATE NORMALLY
3 DEG PER SEC TO 10 DEG

POSITIVE CLB GEAR UP
FOLLOW SRS WHICH COMMANDS V2 to V2 + 15

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20
Q

EF AFTER V1

PROC AT 400’ RA

A

WHEN AIRCRAFT UNDER CONTROL
ECAM ACTIONS

SECURE THE ENGINE MEANS
ENG MASTER OFF NO DAMAGE
AGENT 1 DISCH WITH DAMAGE
AGENT 2 DISCH FOR FIRE

AT EO ACCEL ALT PRESS ALT

CLEAN UP
WHEN ACCEL ARROW TOUCHES GREEN DOT PULL FOR OP CLB SET MCT

THEN CONTINUE ECAM

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21
Q

EF AT CRZ

A

SET MCT
DISCONNECT ATHR ABOVE EO MAX ALT

STD
.85/ 300 PULL OP DES
VS <500 FPM USE VS 500 FPM ATHR ON

OBSTACLE
OP DES AT GREEN DOT
CLR OBSTACLE USE STD STRAT

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22
Q

ENG STALL

SYMPTOMS

A

LOUD BANGS
INSTANT LOSS THRUST
FLUCTIONS N1 N2 N3
INCREASE EGT
ENG VIBRATIONS
FLAMES INLET OR TAILPIPE

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23
Q

ENG STALL

PROC

A

FADEC DETECTS AND REQ ENG STALL ECAM

FLT CREW THRUST TO IDLE
CHECKS ENG PARAMETERS
SHUTS DOWN ENGINE IF OARAMETERS ABNORMAL

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24
Q

ENGINE VIBRATIONS

A

DEFORMATION OF BLADE
RUPTURE OR LOSS BLADE
FAN ICIING

ABN PROC ENG HI VIBRATIONS

CHK ENG PARAMETERS
USE ENG ANTI ICE

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25
Q

OEI LDG

A

REMEMBER TO CENTRE RUDDER TRIM ON FINAL
ONE UNIT WHEN DISCONNECTING

MENTION CAPT SHOULD DO LDG

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26
Q

GA SOFT

A

THRUST LEVERS TOGA THEN FLX MCT

MAN TOGA
MAN GA SOFT

TARGETS 2000FPM

ONLY AVAIL AEO
OEI MUST USE TOGA

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27
Q

GA

PROC

A

GOAROUND FLAPS
PF TOGA THEN FLX MCT
PF ROTATE 12.5 DEG 10DEG OEI
PM MONITOR
FLAPS RETRACT ONE STEP
FMA FMA
PM POSITIVE CLIMB
PF GEAR UP
PF NAV OR HDG
PM GO AROUND ALT CHECK

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28
Q

VISUAL APP PATTERN

A

ABEAM RWY
ACTIVATE APP PHASE
CHK MANAGED SPEED

DOWNWIND
SPEED GD OR BELOW
FLAPS 1

ABEAM THRESHOLD
START TIME 45 SECS +/- 1 SEC PER KT WIND

TURNING BASE
FLAPS 2
LG DOWN
SPOILERS ARMED

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29
Q

VISUAL APP PATTERN

ON BASE

A

MID BASE
BELOW VFE NEXT
FLAPS 3
BELOW VFE NEXT
FLAPS FULL

ON FINAL
500’ AIRCRAFT STABILISED WITH FLAPS FULL AT TARGET SPEED

GO AROUND
SET TOGA THR
ROTATE SRS
RETRACT FLAPS ONE STEP
POSITIVE CLIMB
GEAR UP

30
Q

LANDING

A

HAVE AIRCRAFT STABILISED
@40’
LOOK TO END AND FLARE
THR IDLE

IDLE REV
@70 KTS STOW REV

31
Q

DISCONTINUED APP

A

PF CANCEL APPROACH
SELECT LOC OR VS

32
Q

LNDING

PM CALLS

A

SPOILERS
REV GREEN
BTV
DECEL

33
Q

GLIDESLOPE INT FROM ABOVE

A

CONFIRM GS ARMED AND LOC ENGAGED
SET FCU ALT ABOVE CURRENT ALT
SELECT VS 1500FPM UP TO 2000FPM

34
Q

SUPER

A

DEP
APP
DIRECTOR
TOWER

35
Q

NADP 1

A

REDUCED THR 1000’AGL
V2 + 10-20 TO 3000’
ACCEL 3000’

36
Q

NADP 2

A

REDUCE THR 1000’AGL
GD TO 3000’
ACCEL AT 3000’

37
Q

DIVERSION APT FOR DIVERSION

A

NOT TO CAT C OR EMERG

SOME CAT B MAY HAVE RESTRICTIONS

38
Q

STANDARD DESCENT SPEEDS

A

250 < 5k

AUST
ECON/ 280-310

39
Q

APP BAN

A

ANY APP CAN BE COMMENCED REGARDLESS RVR
AT 1000’ IF CONTROLLING RVR LESS THAN MINIMA MUST NOT CONTINUE
AFTER 1000’ CAN CONTINUE TO MINIMA IF RVR BECOMES LESS THAN REQD

40
Q

RATES OF DESCENT

A

5000-3000’ AGL LESS THAN CURRENT ALT IN FPM
3000-1000’ MAX 2000 FPM

41
Q

INTERCEPTION VERT APP PTH

A

BY FAF OR FAP IF INSTRU APP REQD

IF NOT REQD BY 1000’AGL

42
Q

TOLERANCES ALL APPs

A

DESCENT RATE 1000FPM
VASI PAPI ANY SIG VARIATION
CENTRELINE ANY SIG VAR
AIRSPEED -5 to +10
THRUST ENERGY CORRECT

43
Q

TOELRANCES INSTRU APP

A

ILS LLZ LDA 1/2 DOT
DME ARC +/- 2NM
RNAV 0.3nm

44
Q

INSTRU PROC CALLS

A

OM HEIGHT CHECKED
100 ABOVE
MINIMA VISUAL CONTINUE
MINIMA NO CONTACT GO AROUND FLAPS

EARLY VISUAL CALL
CONTINUE
OR STANDARD PROCs

45
Q

TARGET TDZ

A

1000’-2000’ BEYOND THRESHOLD

46
Q

LANDING IDLE REV WHEN MUST FULL REV BE SEL

A

DECEL NOT AS EXPECTED
FAILURE AFFECTS LDG DIST PERF
LONG TOUCHDOWN
UNEXPECTED TWC

47
Q

CAPTAIN NON ROUTINE BRIEF

A

NITS

NATURE OF EMERG PROBLEM
INTENTIONS
TIME AVAIL
SPECIAL CONSIDERATIONS OR REQUIREMENTS

48
Q

RA CALLS

A

TCAS RA
UNABLE TCAS RA
CLEAR OF CONFLICT RETURNING TO FL
CLEAR OF CONFLICT FL RESUMED

49
Q

WINDSHEAR
EMERG DESCENT RADIO CALLS

A

WINDSHEAR ESCAPE
EMERGENCY DESCENT

50
Q

TAKEOFF ALTERNATE

A

CAT A OR B THAT IS AVAIL
AND
TWO HOURS FLT TIME OEI

DIST 800NM

AT OR ABOVE LDG MINIMA +/- 30MINS

51
Q

OQD NEW PROC

A

APU START
WAIT UNTIL APU FLAP POSN ON SD PAGE IS OPEN BEFORE START

ALSO
WHEN STARTING ENGINES WAIT 3 SECS BETWEEN EACH ENG MASTER LEVER

52
Q

TAKEOFF DATA
WHEN TO RECALC

A

INCREASE TOW
TOGA OR FLX <300m STOP MARGIN FOR ANY ADVERSE CHANGE

> 300m STOP MARGIN
HWC DECREASE 5KTS
ANY INCREASE TWC
OAT 2 DEG INCREASE
QNH REDUCES BY 2 hPa

THEN XCHK WITH AVIONICS

53
Q

LETS COME TOGETHER

A

WHEN BOTH CREW MEMBERS SEATED

PF AND PM ARE THE SAME

LOUDPSPEAKER KNOB SET
BARO REF SET
EFIS CP SET
AFS CP PF CHECK PM CROSSCHECK

LATERAL CONSOLE

PF PM SAME

OXY MASK TEST
EFB MOUNT CHECK
PFD CHECK
ND CHECK

54
Q

TAKEOFF BRIEFING

A

PF PM
FUEL ON BOARD CHECK

PM
SQWK SET CHECK

PF
TAKEOFF BRIEFING PERFORM

PF PM
FUEL QTY CHECK

PF
BEFORE START CL
PM
DOWN TO THE LINE

55
Q

BEFORE START CLR

A

PM
HF CHECK

BOTH
FINAL LOAD SHEET CHECK
FOB TRIM TK CHECK

ZFW ZFWCG CHECK REVISE
PAX NUMBER CHECK REVISE
LOADSHEET MACTOW VS ECAM GWCG CROSSCHECK

IF DIFF <1% NO CHANGE
>1% AUTO GND XFR PBSW ON
IF TAKEOFF COND CHANGE

BOTH
OIS FINAL TO PERF DATA RECOMPUTE

PF
FMS TO DATA REVISE

PM
OIS FINAL TO PERF DATA XCHK W AVIONICS

BOTH
SEATING POSN ADJUST

PF
FMS PERF
PM
FMS F PLN

PM
APU CHECK AVAIL
EXT PWR CHECK AVAIL
EXT PWR DISCONNECTION REQUEST
LP GND CARTS CHECK DISCONNECTED
APU BLEED SW ON

PF
BEFORE START CL DOWN TO THE LINE
CONFIRM COMPLETE
PM

DOWN TO THE LINE
CONFIRM COMPLETE

56
Q

AT START CLR

A

PM
PUSHBACK STARTUP CLR OBTAIN

PM
BEACON ON

BOTH
WINDOWS AND DOORS CHECK CLOSED
SLIDES ARMED
TAXI VIDEO ON

PF
ACCU PRESS CHECK

BOTH
SURV DEFAULT SETTINGS SEL

PF
THR LEVERS IDLE
NW STEER DISC CHECK DISPLAYED
PARK BRK HANDLE AS REQD

PF
BEFORE START CL BELOW THE LINE
PM
BEFORE START CHECKLIST COMPLETE

PUSHBACK COMPLETE
PARK BRK ON
L AND R PRESS IND CHECK

57
Q

ENGINE START

A 
PF
THRUST LEVERS IDLE
ENG START SEL IGN START
ENG 1 and 2 START ANNOUNCE
ENG MASTER 1 then 2 ON
ENG IDLE PARAMETERS CHECK
REPEAT FOR ENG 3 and 4
58
Q

AFTER START

A 
PF
ENG START SEL NORM
APU BLEED AS REQD
ENG ANTI ICE AS REQD
APU NOT REQD
APU MASTER SW OFF
PM
ONCE PF ENG START SEL THEN
GND SPLRS ARM
RUDDER TRIM ZERO
FLAPS SET
PITCH TRIM CHECK
BOTH
ECAM STATUS
PM
CHECK
PF
CROSSCHECKED

PF
NW STEER DISC CHECK NOT DISPLAYED
READY FOR DISCONNECT ANNOUNCE

BOTH
FLT CONTROLS CHECK

PF
AFTER START CL
PM
AFTER START CL COMPLETE

59
Q

TAXI

A

PM
TAXI CLR OBTAIN

BOTH
TAXI PB EFIS AS REQD
ND RANGE ZOOM AS APPROP

PF
EXTERIOR LTS SET
PARK BRK HANDLE OFF
THRUST LEVERS AS REQD
BRAKES PRESS

PM
LH RH BRK PRESSURE CHECK ZERO
ATC CLR CONFIRM

IF TAKEOFF COND CHANGED

BOTH
OIS FINAL TO PERF DATA RECOMPUTE

PM
FMS TO DATA REVISE

PF
OIS FINAL TO PERF DATA XCHK AVIONICS

PM
FLAPS LEVER AS APPROP
F PLN SID TRANS REVISE OR CHECK
INITIAL CLB LMT SPD LMT REVISE CHECK
AFS CP SET
FD CHECK ON

BOTH
PFD ND CHECK
PF FMS PERF PM FMS F PLN

PF
TAKEOFF BRF CONFIRM

BOTH
EFIS CP AS REQD

PM
RTO ARM
ATC CODE CONFIRM SET
TO CONFIG TEST
TO MEMO CHK NO BLUE

BOTH
CABIN REPORT RECEIVE

PF
BEFORE TAKEOFF CL
PM
DOWN TO THE LINE

60
Q

BEFORE TAKEOFF

A

PM
LINEUP CLR OBTAIN

BOTH
TAKEOFF RUNWAY CONFIRM

BOTH
APP PATH CLR TFC

PF
STROBE ON
PM
PACKS 1 + 2 AS REQD

EFIS CP
TAXI PB OFF
ND AND MODE RANGE AS REQD

TCAS TA RA PM
SLIDING TABLE STOWED

PF
BEFORE TAKEOFF CL BELOW THE LINE
PM
BEFORE TAKEOFF CL COMPLETE

61
Q

TAKEOFF

A

PM
TAKEOFF CLR OBTAIN

PF
EXTERIOR LTS SET
TAKEOFF ANNOUNCE
THR 30%
BRAKES RELEASE
THRUST LEVELR FLX OR TOGA

PM
CHRONO START

PF
DIRECTIONAL CONTROL USE RUDDER

PM
PFD ND MONITOR
TAKEOFF THRUST CHECK

BELOW 80KTS
PM
THRUST SET ANNOUNCE
PFD ENG IND MONITOR

AT 100KTS
PM
ONE HUNDRED KNOTS ANNOUNCE
PF
CROSSCHECK

V1
PM MONITOR OR ANNOUNCE

VR
PM 
ROTATION ORDER
PF
ROTATION PERFORM
POSITIVE CLB
PM
POSITIVE CLIMB ANNOUNCE
PF
LG UP ORDER
PM
LG UP
PF
AP AS REQD

THR RED ALT

PF
THRUST LEVERS CL
PM
PACKS 1 and 2 ON IF APPLICABLE

AT F SPD
PF
FLAPS 1 ORDER
PM
FLAPS 1 SELECT
AT S SPD
PF
FLAPS ZERO ORDER
PM
FLAPS ZERO SELECT
GND SPLRS DISARM
EXT LTS SET
62
Q

AFTER TAKEOFF

A

IF APU USED DURING TAKEOFF

PM
APU BLEED OFF
APU MASTER OFF

IF TAKEOFF TA ONLY
PM
TA PB TA RA
ANTI ICE AS REQD

PF
AFTER TAKEOFF CL
PM
AFTER TAKEOFF CL COMPLETE

63
Q

DESCENT NOTES

A

AT T/D
PF
ALT KNOB PUSH

ATC REQ EARLY DESCENT
PF
USE DES MODE
WILL USE 1000FPM TO INT DES PATH

ATC DELAYS DESCENT
T/D REACHED message PFD MFD
DES MODE MANAGED SPEED WHEN CLEARED

MANAGING THE DESCENT
TO INCREASE ROD
USE SELECTED SPEED
KEEP FAST UNTIL ALT* LOSE SPEED IN LEVEL OFF

BELOW PROFILE
SELECTED SPEED AND VS

OP DES
SPEED BRAKES INCREASE ROD

IN DES MODE
ON PROFILE ATC NEEDS HIGHER ROD DO NOT USE SB AS A/THR WILL ADD THRUST TO MAINTAIN PROFILE. USE OP DES AND SB

AT 10000’
LDG LT ON
WING LT ON
AT NIGHT LOGO ON

PRESS LS FOR
ILS GLS
USING FLS FUNCTION

64
Q

CONFIGURING FOR APP

A 
PF
F PLN SEQUENCING ADJUST
ACTIVATE APP PHASE
PM
APP PHASE ACTIVATED

PF
MANAGED SPEED CHECK
FLT PATH MONITOR
SPEED BRAKES AS REQD

PM
GPS PRIMARY LOST
NAV ACCURACY MONITOR

APP GD
PF
FLAPS 1 ORDER
PM
FLAPS ONE SEL
TA PB TA TA RA
2500’ AGL MINIMUM
PF
FLAPS 2 ORDER
PM
FLAPS 2 SEL
AFTER FLAPS 2 SEL AT 2000’AGL MINIMUM
PF
L/G DOWN ORDER
PM
L/G DOWN
AUTO BRK CONFIRM
GND SPLRS ARM
EXT LGTS SET
SEATBELTS ON
AFTER LG DN SEL
PF
FLAPS 3 ORDER
PM
FLAPS 3 SEL
WHEEL SD PG SEL
PF
FLAPS FULL ORDER
PM
FLAPS FULL SEL
A/THR CHECK SPEED MODE OR OFF

BOTH
SLIDING TABLE STOWED

PM
L/G MEMO NO BLUE

PF
LANDING CL
PM
LANDING CL COMPLETE
FLT PARAMETERS MONITOR
65
Q

MANUAL LANDING

A

PF
AP OFF

AROUND 40’ RA
PF
FLARE PERFORM
THRUST LEVERS IDLE
PM
ATTITUDE MONITOR
AT TOUCHDOWN
PF
ALL REV LEVERS PULL
DIRECTIONAL CONTROL ENSURE
PM
GND SPLRS EXTENDED CHECK ANNOUNCE
REVERSERS CHECK ANNOUNCE

IF AB SEL
PM
AUTO BRK CHECK ANNOUNCE

DECEL
PM
CHECK ANNOUNCE

AT 70KTS
PM
SEVENTY KNOTS ANNOUNCE
PF
ALL REVERSER LEVERS IDLE

AT TAXI SPEED
PF
ALL REVERSER LEVERS STOW
AUTO BRK DISARM

66
Q

AFTER LANDING

A 
PF
GND SPLR DISARM
EXT LTS SET
PM
FLAPS RETRACT
APU START
ENG START SEL NORM
ANTI ICE AS REQD

BOTH
ND RANGE ZOOM AS APPROP
TAXI PB AS REQD
WX PB CHECK OFF

PM
FLT NBR REENTER
BRAKE TEMP MONITOR

PF
AFTER LDG CL
PM
AFTER LDG CL COMPLETE

67
Q

TAKEOFF DATA
PM CHECKS

A

XCHK AVIONICS
RWY IDENT
INTERSECTION
EO ACCEL ALT

68
Q

CONTENT PERF DATA CROSSCHECK

A

RWY IDENT
TAKEOFF SHIFT
V SPDS
TAKEOFF THRUST
FLAPS
PACKS
ANTI ICE
EO ACCEL ALT

69
Q

PAVEMENT FAILURE

A

DEMONSTRATE USE IPAD
RECALC TAKEOFF DATA
REBRIEF PERF DATA
PM XCHK AVIONICS AND VERIFY RWY, INT AND EO ACCEL ALT

70
Q

REJECTED LANDING

A

VERY LATE
MAY HAVE WHEELS TOUCH
CAN ALWAYS GA UNTIL REV THR SEL

A380 (45 decks)

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