SIMEX 01SA Flashcards

(70 cards)

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
OEI LDG
REMEMBER TO CENTRE RUDDER TRIM ON FINAL ONE UNIT WHEN DISCONNECTING MENTION CAPT SHOULD DO LDG
26
GA SOFT
THRUST LEVERS TOGA THEN FLX MCT MAN TOGA MAN GA SOFT TARGETS 2000FPM ONLY AVAIL AEO OEI MUST USE TOGA
27
GA PROC
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
28
VISUAL APP PATTERN
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
29
VISUAL APP PATTERN ON BASE
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
LANDING
HAVE AIRCRAFT STABILISED @40’ LOOK TO END AND FLARE THR IDLE IDLE REV @70 KTS STOW REV
31
DISCONTINUED APP
PF CANCEL APPROACH SELECT LOC OR VS
32
LNDING PM CALLS
SPOILERS REV GREEN BTV DECEL
33
GLIDESLOPE INT FROM ABOVE
CONFIRM GS ARMED AND LOC ENGAGED SET FCU ALT ABOVE CURRENT ALT SELECT VS 1500FPM UP TO 2000FPM
34
SUPER
DEP APP DIRECTOR TOWER
35
NADP 1
REDUCED THR 1000’AGL V2 + 10-20 TO 3000’ ACCEL 3000’
36
NADP 2
REDUCE THR 1000’AGL GD TO 3000’ ACCEL AT 3000’
37
DIVERSION APT FOR DIVERSION
NOT TO CAT C OR EMERG SOME CAT B MAY HAVE RESTRICTIONS
38
STANDARD DESCENT SPEEDS
250 < 5k AUST ECON/ 280-310
39
APP BAN
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
RATES OF DESCENT
5000-3000’ AGL LESS THAN CURRENT ALT IN FPM 3000-1000’ MAX 2000 FPM
41
INTERCEPTION VERT APP PTH
BY FAF OR FAP IF INSTRU APP REQD IF NOT REQD BY 1000’AGL
42
TOLERANCES ALL APPs
DESCENT RATE 1000FPM VASI PAPI ANY SIG VARIATION CENTRELINE ANY SIG VAR AIRSPEED -5 to +10 THRUST ENERGY CORRECT
43
TOELRANCES INSTRU APP
ILS LLZ LDA 1/2 DOT DME ARC +/- 2NM RNAV 0.3nm
44
INSTRU PROC CALLS
OM HEIGHT CHECKED 100 ABOVE MINIMA VISUAL CONTINUE MINIMA NO CONTACT GO AROUND FLAPS EARLY VISUAL CALL CONTINUE OR STANDARD PROCs
45
TARGET TDZ
1000’-2000’ BEYOND THRESHOLD
46
LANDING IDLE REV WHEN MUST FULL REV BE SEL
DECEL NOT AS EXPECTED FAILURE AFFECTS LDG DIST PERF LONG TOUCHDOWN UNEXPECTED TWC
47
CAPTAIN NON ROUTINE BRIEF
NITS NATURE OF EMERG PROBLEM INTENTIONS TIME AVAIL SPECIAL CONSIDERATIONS OR REQUIREMENTS
48
RA CALLS
TCAS RA UNABLE TCAS RA CLEAR OF CONFLICT RETURNING TO FL CLEAR OF CONFLICT FL RESUMED
49
WINDSHEAR EMERG DESCENT RADIO CALLS
WINDSHEAR ESCAPE EMERGENCY DESCENT
50
TAKEOFF ALTERNATE
CAT A OR B THAT IS AVAIL AND TWO HOURS FLT TIME OEI DIST 800NM AT OR ABOVE LDG MINIMA +/- 30MINS
51
OQD NEW PROC
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
TAKEOFF DATA WHEN TO RECALC
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
LETS COME TOGETHER
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
TAKEOFF BRIEFING
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
BEFORE START CLR
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
AT START CLR
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
ENGINE START
``` 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
AFTER START
``` 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
TAXI
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
BEFORE TAKEOFF
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
TAKEOFF
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
AFTER TAKEOFF
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
DESCENT NOTES
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
CONFIGURING FOR APP
``` 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
MANUAL LANDING
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
AFTER LANDING
``` 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
TAKEOFF DATA PM CHECKS
XCHK AVIONICS RWY IDENT INTERSECTION EO ACCEL ALT
68
CONTENT PERF DATA CROSSCHECK
RWY IDENT TAKEOFF SHIFT V SPDS TAKEOFF THRUST FLAPS PACKS ANTI ICE EO ACCEL ALT
69
PAVEMENT FAILURE
DEMONSTRATE USE IPAD RECALC TAKEOFF DATA REBRIEF PERF DATA PM XCHK AVIONICS AND VERIFY RWY, INT AND EO ACCEL ALT
70
REJECTED LANDING
VERY LATE MAY HAVE WHEELS TOUCH CAN ALWAYS GA UNTIL REV THR SEL