incomplete IDIOT’S Guide to A330
GND SUBJECTS
GROUND
CALLOUTS
EFATO
SMOKE
FUEL LEAK
IDMM
T/OFF BRIEF
EFATO 2
ENG FAIL - CRZ
UNRELIABLE
AIRSPEED
SEP
APP BRIEF
WINDSHEAR
ALL ENG
FLAMEOUT
LVO
SEP 2
ECAM ACTION
GPWS
STALL RECOVERY
LVO CXLIST
SEP 3 – A 330
RTO
TCAS
EDTO GUIDE &
FM SETUP
NPA - MANAGED
SEP - DGR
EMER DESC
EDTO PREP &
BRIEF
NPA - SELECTED
RESERVED
EDTO
RENOMINATE
VISUAL PATTERN
V 5.6
IDMM
PROBLEM !!!
MAYDAY / PAN
CALLSIGN
NATURE OF PROBLEM
HDG/ALT/POSITION
INTENTION
SAFE
LEGAL
FEASIBLE
ECONOMICAL
FLY ,
NAV,
COMM
STABLE / IN
CTRL
5 Cs
CLEAR
OPERATIONAL
/
PROCEDURAL
C
L
E
A
R
OPERATIONAL
C
C
C
C
C
CLARIFY PROBLEM
LOOK FOR OPTIONS
EVALUATE OPTIONS
ACTION
REVIEW ACTIONS
COCKPIT CREW
CONTROLLER
CABIN
CUSTOMER
COMPANY
PROCEDURAL
PRAE
ECAM
“ECAM ACTION!”
P
R
A
E
PROCEDURAL
RECOGNITION
ACTION
EVALUATION
TYPE
INTENTION
TIME
SPECIAL
INTRO / ATTENTION
NATURE OF PROBLEM
UNDER CONTROL
SAFETY – INTENTION
INFO – TIME, WX
AFOLLL
A
F
O
L
L
L
APPROACH CxLIST
FUEL IMBALANCE
OVERWEIGHT CxLIST
LAND SLATS/FLAPS
LANDING GEAR – GRAVITY
LDG CxLIST
END.
TOC
AFOLLL:
- Approach Cx
- Fuel Imbalance
- Over weight LDG Cx
- LDG Flaps/Slats
- LDG GEAR Gravity
- LDG Cx
APPROACH BRIEF:
- NORMAL APP
- STATUS – APP PROC
To make landing run easier, it is
recommended that, in the later stage of
approach, PNF resets the rudder trim to
ZERO, upon PF request, by pushing the
RESET button.
PITCH 12.5’ then SRS
+VE CLB- GEAR UP
RUDDER TRIM 7 SEC
BETA TARGET
5 Cs
IDMM
CLEAR
- Handover CTRL
- FMGS prep.
- APP Briefing
“ ECAM ACTION
COMPLETE ”
“ CONTINUE
ECAM ”
EO ACC ALT
PUSH
ENG is considered as SECURED when
the ECAM actions of the procedures are
performed until:
1. “ENG MASTER OFF” for an eng
failure without damage
2. “AGENT 1 DISH” for an eng failure
with damage
3. Fire extinguished or “AGENT 2
DISH” for an engine fire
•
•
•
•
APPROACH
PREP:
STATUS
GREEN DOT
“ STOP ECAM ”
ALT SEL - PULL
THR LVR - MCT
•
•
•
•
“ STOP ECAM ”
CLEAN UP
“FLAPS 1”
“ CONTINUE
ECAM ”
Normal checklist
OEB
Computers RESET
RELIGHT (QRH)
“FLAPS 0”
EO ACC ALT
400 AGL
If HYD ELEC PUMP is running after an ENG FAILURE,
MEMO
displays, You may
SWITCH OFF elec. pump once in clean config.
• After a successful ENG relight, if EO CLR prompt is still
displayed, press the corresponding key. Pressing the
EO CLR key restores predictions and performance with
ALL ENG OPERATIVE.
•
“ECAM ACTION!”
“ENG FAILURE!!”
EFATO
TOC
TOC
“ENG FAILURE!!”
THR LVR – MCT
A/THR - OFF
ABNORMAL OPERATIONS
STD STRATEGY
EO LRC CEILING
VS < 500fpm
OPERATING TECHNIQUES
NUAL
Engine failure during cruise flow pattern
“ECAM ACTION”
STD & FIX SPD STRATEGY: SEL VS 500fpm
WHEN
A/THR REENGAGE
THR LVR IDLE
&
ENG START - START
1. OBSTACLE – SET
2. STD – SET 300/M.82
3. FIX SPD – 330M.82
nnected to avoid any engine thrust reduction when selecting speed according
pulling for OPEN DES to initiate the descent. With the A/THR disconnected,
controlled by the elevator when in OPEN DES.
AM actions should not be hurried, as it is important to complete the drill
there will be sufficient time to cross check all actions.
EO LRC CEILING – SET
(PROG: REC MAX = LRC CEIL
“STOP ECAM”
GY
VS < 500fpm
0.82/300 kt. The speed of M 0.82/300 kt is chosen to ensure the aircraft is
windmill engine relight in-flight envelope.
Cruise altitude, which equates to LRC with anti-icing off, is displayed on the
and should be set on the FCU. (Cruise altitude and speed are also available in
double FM failure).
than 500 ft/min, select V/S -500 ft/min and A/THR on. This is likely to occur as
pproached.
level off altitude, long-range cruise performance with one engine out may be
or Refer to FCOM/PER-OEI-GEN-10 PROCEDURE.
←I→
OBS STRATEGY
-OBS CLEARED
- EO LRC CEILING – SET &
PULL
- EO LRC SPEED – SET
- QRH - LRC ONE ENG OUT or
ONE ENG INOP CRZ TABLE
SPEED SET & PULL:
OR
Green dot
SPEED – MANAGED
QRH – LRC ONE ENG OUT
PER-N 1/4
EO CEILING
SPEED - MANAGED
AO-020 P 19/32
06 JAN 15
AFOLLL:
- Approach Cx
- Fuel Imbalance
- Over weight LDG Cx
- LDG Flaps/Slats
- LDG GEAR Gravity
- LDG Cx
APPROACH BRIEF:
- NORMAL APP
- STATUS – APP PROC
APPROACH
PREP:
IDMM
5 Cs
CLEAR
- Handover CTRL
- FMGS prep.
- APP Briefing
ENG FAIL IN CRZ
TOC
Prepares for Re-LIGHT - attempt
windmilling
“ENG FAILURE!!”
FLY
NAV
COMM
• MAINTAIN OPT
RELIGHT SPD
• RAT extended –
EMER GEN
available
• MAN FLT – ALT
LAW
• USE FPV –
remove FD flag
•
•
NO RELIGHT:
ENG MASTER SW OFF
START CHRONO
Above APU BLEED LIMIT, RELIGHT sequence can be repeated
until successful or APU BLEED
AVAIL
“ECAM ACTION”
When ECAM request:
30 sec later
Below APU BLEED LIMIT(FL 225) Refer QRH:
ALL ENG FLAMEOUT
FUEL REMAINING or
NO FUEL REMAINING
30 sec later
30 sec later
•
•
NO RELIGHT:
ENG MASTER SW OFF
START CHRONO
30 sec later & if relight unsuccessful
AFOLLL:
- Approach Cx
- Fuel Imbalance
- Over weight LDG Cx
- LDG Flaps/Slats
- LDG GEAR Gravity
- LDG Cx
APPROACH BRIEF:
- NORMAL APP
- STATUS – APP PROC
APPROACH
PREP:
IDMM
5 Cs
CLEAR
- Handover CTRL
- FMGS prep.
- APP Briefing
DUAL ENG FAIL IN CRZ
TOC
45 sec
• 25 BANK
• 400 fpm
42 sec
GEAR DOWN
F3
35 sec – F2
APP CXLIST
3 sec /100’
PF
• “AP OFF”
• “FD OFF”
• “BIRD ON”
PM
- Check
- SEL FD OFF
- SEL TRK/FPA
• ND ROSE NAV 10 nm –
cx within 2.7nm
F FULL
ATO CXLIST
LDG CXLIST
• 20 BANK
• 700-800 fpm
BEFORE TAKE OFF
• RWY HDG Set (Cx NO NAV BLUE)
• CCT ALT Set
VISUAL PATTERN
PULL
HDG
• PULL S SPEED OR
• ACTIVATE APP PHASE
• SET HDG XXX (Downwind)
TOC
ECAM
MW
PF
MC
PM
STATUS?
CLEAR
STOP ECAM
PF
PM
FLY , NAV, COMM
READ ECAM TITLE
CONSIDER:
•
•
•
•
“ECAM ACTION”
NORMAL CXLIST
OEB
ENG RELIGHT
COMPUTER RESET
5 Cs
APPROACH PREP
• Refer STATUS
• APP CxLIST
• READ ECAM TITLE
• Perform ACTION
CONTINUE ECAM
READ STATUS
CONFIRM ITEMS:
•
•
•
•
•
ENG MASTER SW
FIRE p/b
IR p/b, ADIRS
IDG
GUEARDED SW
WHEN COMPLETED
END
REMOVE STATUS?
REMOVE STATUS
ECAM ACTION
COMPLETED
CHECK
ECAM ACTION
TOC
PF
“TCAS, I HAVE
CTRL”
PF
• AP OFF
• “FDs OFF”
PF
“
TCAS, I HAVE
CTRL”
PM
• FDs OFF
• ATC “XXX
TCAS RA”
PF
PF
• “MANAGE/SEL SPD”
• “MANAGE NAV/SEL HDG”
• “FL XXX MANAGE/FL XXX
PULL
• “FDs ON”
PM
• SPD – MANAGE OR TURN
• HDG – PUSH OR SET
• ALT – TURN PUSH/PULL
PM
• FDs ON
PM
• ATC “CLEAR
OF CONFLICT”
1.
2.
AP ON
CHECK/REENGAGE FD MODES
TCAS
TCAS MODES
TA/RA mode:
• Display all intruders
• Issues TA and RA
TA ONLY mode:
• All RA are inhibited and converted into TA
• Automatically selected:
§ If WINDSHEAR, STALL, TAWS messages
(TCAS returns to TA/RA when alert over)
§ Below 900’ RA in DESC.
§ Below 1100’ RA in CLB.
• Manually selected by the crew in ENG OUT
conditions or when operating near closely spaced
runway.
TOC
INITIAL APP
INTERMEDIATE APP
FINAL APP
“APP CXLIST”
When cleared for APP
TRK FPA - SET
If GA ALT is LOWER than FAF ALT
FPA SET
1 NM
-o FLAPS 1
-S FLAPS 2
-F LG DOWN
FLAPS 3
FPA PULL
0.3NM
FLAPS FULL
GA ALT SET
IAF
FAF
NPA SELECTED
MAPt
TOC
INITIAL APP
INTERMEDIATE APP
FINAL APP
When cleared for APP
“APP CXLIST”
PF
PM
NAV ACCURACY MONITOR
(GPS PRIMARY or otherwise)
“CHECKED”
“ONE THOUSAND”
FM - VAPP Speed set at FAF..INSERT
“CHECKED”
“100 ABOVE”
FCU ALT - SET
“CONTINUE /
GA FLAPS”
“MINIMUMS”
-o FLAPS 1
-S FLAPS 2
If GA ALT is LOWER than FAF ALT
-F LG DOWN
FLAPS 3
STABLE at FAF
LDG CONFIG and at VAPP
CHECK FMA:
FLAPS FULL
GA ALT SET
IAF
FAF
NPA MANAGED
MAPt
TOC
“EMER DESC!”
DETECTION
OXY MASK ON
INTERPHONE ON
INT VOLUME
COMM
FIRST LOOP
•
•
•
•
“EMER DESC!”
ALT – TURN & PULL
HDG – TURN & PULL
SPD - PULL
PA**
• SAFE ALT
• SAFE to remove
mask
• OXY is available
• CC will b doing check
IFS/PURSOR
• POST DECOMP CX
• REPORT BACK
• INTENTION (TITS)
ANNOUNCE FMA
CHECK FMA
• SPD BRAKE - FULL
SIGN ON
ENG MODE SEL – IGN
ATC – MAYDAY CALL*
PA “EMER DESC!
EMER DESC!”
• ATC XPNDR - 7700
•
•
•
•
• ALT – FL100 or MORA
• HDG - SET
• SPEED - SET
PF
“ECAM ACTION!”
QRH – MISC –
EMER DESC
• PAX OXY ON
SECOND LOOP
• GET AREA Q
STRUCTURE DAMAGE
YES
OR
SPD/MACH
p/b PRESS
NO
VMO/MMO
ALT
v
PF
• SPD BRK RETRACT
• SPEED MANAGED
CLEAR
5 Cs
PM
CHECK
PM
PF (C concept)
PF
* Refer LIDO GEN for MAYDAY CALL content
** Refer SEP / PA Booklet for full PA content
DESC MAX 1000fpm
ROD CABIN 300fpm
EMER DESC
TOC
AVOIDANCE
TS
VIRGA
PIREP
CB
DEP
DELAY
LONGEST RW
USE WX RDR
TOGA THR
MONITOR SPD
RECOVERY
DETECTION
PF
PWS /
WINDHEAR
ALERT
WINDSHEAR,
TOGA!
“WINDSHEAR TOGA”
SET TOGA THR
FOLLOW SRS
AP may be used if engaged
PNF – Monitor and announce flt parameters
RECOVER SMOOTHLY to normal climb when out of shear
PWS
PM
ADVISORY
• Monitor FLT PATH
• ADVICE ATC
• Monitor TERRAIN and
TRACK
CAUTION
WARNING
APP
DELAY/DIVERT
LONGEST RW
USE WX RDR
FLAPS 3
MANAGE SPD/A THR
USE AP/FD
VAPP – VLS + 15
WS WARNING
*AUS phraseology:
• WINDSHEAR ESCAPE
• CLEAR OF
WINDSHEAR,
RETURNING TO…
• CLEAR OF
WINDSHEAR
DETECTION
- Both FD are removed when pitch exceed 25’ UP
- SRS guidance includes ATT protection to a max of 17.5’ UP
(22.5’ UP in case of windshear.)
WINDSHEAR
TOC
MODE 1
MODE 2
EXCESSIVE
DESC RATE
EXCESSIVE
TERRAIN
CLOSURE RATE
MODE 3
ALT LOSS
AFTER TO/GA
MODE 4
MODE 5
UNSAFE
TERRAIN CLR
NOT IN LDG
CONFIG
GPWS BASIC MODE
EXCESSIVE DEV
BELOW GS
EGPWS ALERTS
Terrain, terrain,
PULL UP
Terrain AHEAD,
PULL UP
Terrain
AHEAD
“PULL UP TOGA”
FULL BACK STICK & MAINTAIN
THR LVR TOGA
CHECK SPD BRK RETRACTED
WINGS LEVEL
ADJUST
SIMULTANEOUSLY
OBSTACLE AHEAD,
PULL UP
GPWS
Don’t SINK
FLIGHT PATH
PITCH
THRUST
CONFIG OR
INITIATE GA
Obstacle
AHEAD
Too LOW
FLAPS
TOO LOW FLAPS may lead to:
- Selecting adequate CONF.
- Modify to LDG CONF 3 on
PERF page
- Pressing FLAP MODE p/b
on GPWS panel.
TOC
ABORT!!
PF
DEPENDING ON CIRCUMSTANCES
PM
THR LVR IDLE
REV THR - MAX
REV – CX/ANN
“STOP ECAM!”
STOP ECAM ACTION
“EMER EVAC PROC”
READ & DO
DECEL – CX/ANN
CANX any MW/MC
“70 KNOTS”
AC STOPPED
EVACUATION IS NOT REQUIRED
INITIATE EVACUATION
AC TAXIABLE?
PA
REV - STOW
PRK BRK - ON
ATC – “STOPPING”3X
PA
GET EMER EVAC PRO
Attention!
This is your Captain.
Remain seated,
Attention!
This is your Captain.
EVACUATE!,
EVACUATE!
EVACUATE!
EVAC CMD p/b
ON
Remain seated.
EVAC HORN OFF
“BRAKE FAN ON”
BRK FAN ON
“ECAM ACTION!”
Initiate ECAM ACTION
AUTO EXTENSION OF GND SPOILERS
Wheel SPD >
72kts.
IF EVACUATION IS REQUIRED
SPOILERS
ARMED
ALL THR LVR IDLE
SPOILERS NOT
ARMED
REV on ONE ENG &
IDLE ON THE OTHER
ATC – inform EVAC
YES
NO
EXIT RWY &
STOP
HOLD, REQUEST
TOW TRUCK
DECIDE
“ EMER EVAC PROC
COMPLETED”
FLIGHT CREW EVACUATE
This is your CAPTAIN, remain seated.
We have aborted the take off due to (reason).
Following our safety procedures, we will be taxing
to the gate/will be towed to the gate.
We will advice you on the status of the flight later.
Please do not be alarmed as situation is well
under control.
RTO & EVAC
TOW
TAXI
PA
REVERSER
CALLOUT:
REV GREEN NO 1
NO REVERSE NO 2
TOC
STALL RECOVERY
PF
PM
IMMEDIATE
IMMEDIATE
PF
STALL WARNING AT LIFT OFF
“STALL, I HAVE CONTROL”
NOSE DOWN
WINGS LEVEL
PM
“STALL, I HAVE CONTROL”
TOGA
15’ PITCH UP
WINGS LEVEL
SECONDARY
WHEN OUT OF STALL
THR LVR..INCREASE
SPD BRK.. CX RETRACT
FLT PATH..RECOVER
IF < FL200 AND IN CLEAN CONFIG
F1
“SPEED CHECK, F1”
STALL RECOGNITION
1. AURAL WARNING
AOA exceeds a given threshold, which depends on CONFIG & Mach No. This warning
provides sufficient margin to alert flt crew in advance of the actual stall.
2. STALL BUFFET
Airframe vibrations caused by non-stationary air-flow separation from the wing surface
when approaching AOA stall. Aural warning is set close to AOA at which the buffet starts.
STALL RECOVERY
TOC
TAKE OFF
TCAS,
I HAVE CONTROL
SET ELEC EMER CONFIG
ABORT
STALL,
I HAVE CONTROL
UNRELIABLE AIRSPEED
GO-AROUND
FLAPS
STALL,
TOGA 15’
EMERGENCY DESCENT
CANCEL
APPROACH
WINDSHEAR TOGA
EMERGENCY DESCENT
EMERGENCY DESCENT
PULLUP TOGA
UNRELIABLE
AIRSPEED
CALLOUTS
ANTISKID OFF
TOC
FUEL
LEAK – ENG/PYLON CONFIRMED
MONITOR
1.
2.
3.
4.
FOB & EFOB
DEST FUEL &
EXTRA
FOB+FU & FOB
(DEP)
FUEL FLOW &
IMBALANCE
DETECTION
1.
2.
3.
4.
5.
6.
7.
DETECTION
FOB+FU < FOB
(Eng Start) or
decreasing
VISUAL – Spray
TOTAL FUEL
qty decreasing
at an abnormal
rate
FUEL QTY in a
tank decreasing
fast
TANK
overflowing
Excessive FF
FUEL ODOUR
in cabin
PF
PM
“ADVISORY ON FUEL SYSTEM”
FLY,NAV, COMM
FUEL PG – ANALYZE
ECAM ADV – CHECK
“FUEL LEAK PROC”
FULE LEAK PROC APPLY
FUEL LEAK
LEAK NOT LOCATED
TOC
UNRELIABLE AIRSPEED
PM
PF
At or above MSA or CCT ALT
LEVEL OFF for TROUBLE SHOOTING
“UNRELIABLE
AIRSPEED”
A330/A340
QUICK REFERENCE HANDBOOK
IF REQ
AP – OFF
FD – OFF
A/THR - OFF
34.02A
ABNORMAL AND
EMERGENCY PROCEDURES
10 DEC 15
ADR CHECK PROC
Apply the UNRELIABLE SPEED INDICATION procedure.
FLT PATH IMPACTED
FLT PATH NOT IMPACTED
AP - OFF
FD - OFF
A/THR OFF
MAINTAIN
PITCH/THR
UNRELIABLE SPEED INDICATION
If the safe conduct of the flight is impacted:
AP/FD.............................................................................................................. OFF
A/THR.............................................................................................................. OFF
PITCH/THRUST
Below THRUST RED ALT...................................................................15° / TOGA
Above THRUST RED ALT and Below FL 100....................................... 10° / CLB
Above THRUST RED ALT and Above FL 100......................................... 5° / CLB
FLAPS (if CONF 0(1)(2)(3)).....................................MAINTAIN CURRENT CONF
FLAPS (if CONF FULL)...................................SELECT CONF 3 AND MAINTAIN
SPEEDBRAKES..................................................................CHECK RETRACTED
L/G..................................................................................................................... UP
When at or above MSA or Circuit Altitude: Level off for troubleshooting
PROBE/WINDOW HEAT - ON
To level off:
AP/FD............................................................................................................... OFF
A/THR............................................................................................................... OFF
SPEEDBRAKES...................................................................CHECK RETRACTED
PITCH/THRUST TABLE...............................................................................APPLY
QRH - PITCH/THR LEVEL OFF TABLE
PITCH / THRUST FOR LEVEL OFF
240 t
530 000 lb
200 t
160 t
120 t
440 000 lb
350 000 lb
260 000 lb
SLATS / FLAPS EXTENDED
ALT
< THR reduction
PITCH THR
15’ TOGA
THR red - FL100
10’
CLB
> FL100
5’
CLB
CONFIG
PF
ACTION
CONF
PITCH
3
THRUST % N1 (Resultant speed)
7.5°
70% (170 kt)
64% (155 kt)
60% (135 kt)
52% (120 kt)
2
7.5°
68% (180 kt)
62% (165 kt)
58% (145 kt)
50% (125 kt)
1+F
6.5°
66% (205 kt)
62% (185 kt)
56% (165 kt)
50% (145 kt)
1
9.5°
64% (200 kt)
60% (185 kt)
56% (165 kt)
48% (140 kt)
CLEAN
FLAP 0,1,2,3
MAINTAIN
F FULL
SELECT F 3
SPD BRK
RETRACT
GEAR
UP
“ECAM ACTION!”
THRUST % N1 (Resultant speed)
PITCH
FL
4°
at or below FL250
100
66% (280 kt)
62% (255 kt)
58% (225 kt)
50% (195 kt)
200
72% (280 kt)
68% (255 kt)
64% (225 kt)
58% (195 kt)
300
82% (300 kt)
78% (275 kt)
72% (245 kt)
66% (210 kt)
350
/
82% (270 kt)
76% (240 kt)
68% (210 kt)
400
/
/
80% (235 kt)
74% (210 kt)
3°
above
FL250
FLYING TECHNIQUE TO STABILIZE SPEED
Stabilize the altitude. When altitude is stabilized:
‐ If the pitch is above the target pitch, increase the thrust and maintain the altitude.
‐ If the pitch is below the target pitch, decrease the thrust and maintain the altitude.
Refer QRH when instructed by ECAM
MAS MSN 1209 9M-MTA
FLY THE GREEN
MCDU – GPS ALT
VSI removed
BUSS (AOA & SFCC)
ALT BY GPS
UNREALIABLE AIRSPEED
TOC
1
2
3
4
DATA page 2
STORED WAYPOINTS
ENTER EEP,ETP,EXP
LAT/LONG
FLT PLN
1L –FIX INFO
ENTER REF FIX
NEXT FIX
CX with PLN MODE
SEC F-PLN
Insert EEP/ETP in
SEQUENCE
NEW DEST from ETP
NEW RTE to ALTN
Set S100 @ETP
GET PERF DATA
GET ETP FUEL
ETP FUEL + ZFW =
GW over ETP
(
ARROW)
EDTO GUIDE
BEFORE EEP
AC STATUS
•
FUEL STATUS
•
EDTO ALT STATUS
CHECK WX, NOTAMS,
CHARTS
CTC ODC, REQ NEW
EA OR RENOMINATE
EA MANUALLY
CHECK FUEL
SATISFY
CRITERIA
• REROUTE TO NON
EDTO / DIVERT
• ADVISE ODC
YES
NO
SATISFY
CRITERIA
NO
YES
CONTINUE EDTO
BRIEFING
EDTO GUIDE & FM SETUP
TOC
1
2
WEATHER
MAN
NOTAMS
MACHINE
AOI
ENVIRONMENT
TERRAIN / AIRSPACE
ALTN
ROUTING
MME
SECOND FPLN
DIRECT
3
OBS
FUEL RESERVE
6
AIRWAYS
STD
FIX
PERF DATA
4
5
TERRAIN
DECIDE STRATEGY
SPC BRIEF
CEILING
PER N 1/4
PER N 1/4
FCOM PER OEI CRT FIX SPD
or PRO SPO 40A-60 P1/12
SPEED
GREEN DOT
PER N 3/4
330/M0.82
CRITICAL FUEL VS ETP FUEL & DESTINATION EFOB
UNABLE TO CTC ATC
ENG FAIL/FIRE
DEPRESS
CARGO SMOKE/FIRE
SPECIAL CONSIDERATION – ELECTRICAL FAILURE
DIVERSION IS REQUIRED IN CASE OF:
1. ONLY ONE GENERATOR (EITHER ONE IDG, APU GEN
OR EMER GEN) REMAINING AVAILABLE FOLLOWING
A MULTIPLE FAILURES.
2. ONLY ONE MAIN GENERATOR (EITHER ONE IDG OR
APU GEN) REMAINING AVAILABLE AND GREEN
HYDRAULIC CIRCUIT LOW LEVEL OR LOW PRESSURE
OR OVERHEAT.
EDTO PREPARATION & BRIEF
TOC
CHANGE OF ALTERNATE /
RENOMINATION
1
2
3
EEP
From ETOPS
PLOTTING CHART
ETP
FM – DATA –
EQUITIME POINT
EXP
From ETOPS
PLOTTING CHART
Get DIST to
& 2nd ALT
1st ALT
Get ETP location
ALONG TRACK
Get ETA & FUEL at
ETP
Get fuel required
PRO SPO 40A60 P12/14
MINUS
1 ENG BURNOFF to
ALT using FCOM
1 ENG BURNOFF to
ALT using FM
SEC FPLN – insert
ETP LOCATION
SET new DEST at SEC
FPLN
Insert S100 at ETP
+ 30%
PER OEI GEN 05 P2/2
Get EFOB @ 1st ALT
SEC FPLN change
DESC SPD to .82/320
ACARS TO ODC (FREE TEXT MSG):
• REQ NEW EA
• REQ EEP, ETP, EXP COORDINATES
AND EDTO CRITICAL FUEL
• REQ WX AND NOTAM UPDATE
EDTO - RENOMINATE
TOC
NOTE
PF
PM
“CHECK”
350 RA
FMA “LAND”
“LAND”
200 RA
For NO DH
“CONTINUE”
DH +100
“CHECK”
40 RA
FMA ‘FLARE”
30 RA
FMA “THR IDLE”
DH
“CHECK”
PROCEDURES
NORMAL PROCEDURES
A330/A340
FLIGHT CREW
SYSTEMS RELATED PROCEDURES
- FMS
TD
“CHECK”
OPERATING MANUALFMA “ROLLOUT”
70 KTS
FAILURES AND ASSOCIATED ACTIONS BELOW 1000 FT
DURING AN ILS CAT II OR GLS
CAT I APPROACH
Ident.: PRO-NOR-SRP-01-70-00002526.0001001 / 12 FEB 13
Applicable to: ALL
“CHECK”
DH
VIS
TDZ RVR
CAT I
200
800 M 550 M
CAT II
100
“100 ABOVE”
CAT III A
“FLARE / NO FLARE”
CAT III B
MID RVR RO RVR
-
-
350 M
125 M
ADV
50
200 M
125 M
ADV
NO DH / 0
75 M
75 M
ADV
WIND
LIMITS:
H 35
X 20
T 10
“NO IDLE”
“MINIMUMS”
“ROLLOUT /
A330/A340
FLIGHT
CREW
NO
ROLLOUT”
OPERATING MANUAL
PROCEDURES
PROCEDURES
NORMAL PROCEDURES
NORMAL PROCEDURES
A330/A340
SYSTEMS RELATED PROCEDURES - FMS
“70 KNOTS_
SYSTEMS RELATED PROCEDURES - FMS
FLIGHT CREW
OPERATING MANUAL
FAILURES AND ASSOCIATED ACTIONS BELOW 1000 FT FOR CAT III APPROACH WITH DH
FAILURES AND ASSOCIATED ACTIONS BELOW
1000 FT FOR CAT III APPROACH WITHOUT DH
Ident.: PRO-NOR-SRP-01-70-00002528.0001001 / 09 OCT 12
Applicable to: ALL
Ident.: PRO-NOR-SRP-01-70-00002527.0001001 / 09 OCT 12
Applicable to: ALL
LVO
TOC
DH
VIS
CAT I
200
800 M 550 M
CAT II
100
CAT III A
CAT III B
LVO GUIDE
CREW QUALIFICATION
CHECKED
AIRCRAFT STATUS
CHECKED
DEST & ALT WX
CHECKED
AIRFIELD LVOP
CHECKED
MINIMA
…....... SET
350 RA
CREW TASKS
REVIEWED
200 RA
SEAT & LIGHTING
OPTIMUM /
SET
DOWNGRADING / APP
BAN
REVIEWED
PRACTICE AUTOLAND IN CAT 1 ILS OR
LVO NOT ENFORCED:
• ILS sensitive areas are not protected
• CAT 1 minima must be applied
• Optional – advise ATC
POST FLIGHT:
• MR 1 – FOR INFO, AUTOLAND CAT
II/III XXXX RW XX
SUCCESSFUL/UNSUCCESFUL
• PERSONAL LOGBOOK – RECORD
AUTOLAND FOR RECENCY RECORD
TDZ RVR
MID RVR RO RVR
-
-
350 M
125 M
ADV
50
200 M
125 M
ADV
NO DH / 0
75 M
75 M
ADV
NOTE
PF
PM
FMA “LAND”
“LAND”
“CHECK”
For NO DH
“CONTINUE”
DH +100
40 RA
FMA ‘FLARE”
30 RA
FMA “THR IDLE”
“CHECK”
“100 ABOVE”
“CHECK”
“FLARE / NO FLARE”
“NO IDLE”
DH
TD
FMA “ROLLOUT”
70 KTS
•
•
WIND
LIMITS:
H 35
X 20
T 10
“MINIMUMS”
PF
“CHECK”
“ROLLOUT /
NO ROLLOUT”
VISUAL REFERENCE
“CHECK”
“70 KNOTS_
SUFFICIENT
INSUFFICIENT
“CONTINUE”
“GA FLAPS”
SYS DOWNGRADING – NOT LOWER THAN 1000
APP BAN – OM (or equivalent) OR SPECIFIC AIRPORT
LVOP WHICHEVER LIMITING.
LVO GUIDE
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TOC
SEP GENERAL:
1. Pilot incap : to request assistance, flight crew must announce .... CCIC, report to
flight deck
2. When there is a tear in the raft, REPAIR CLAMP to be used to prevent air from
escaping
3. Dangerous goods : after confiscating the dangerous goods from pasenger, store it
in a safe place and maintain communication with flight crew thorugh out the
flight
4. Lithium battery fire : water or non flammable liquid is required to Cool the device
(to prevent re-ignition)
5. A passenger attempts force entry into the flight deck. Cabin crew must use the
interphone and discreetly alert the flight crew with the phrase ROMEO ROMEO
6. After the flight crew makes the post decompression announcement Cabin crew to
obtain the nearest oxygen bottle and check all areas
7. Fire fighting policy : the second crew member at the scene will be the
Communicato
8. Post Decompression : Cabin crew shall obtain the nearest oxygen bottle
and...check all areas for crew & passenger, and render first aid if required.
9. Intruder attempting to enter the flight deck..flight crew must Use P.A to alert cabin
crew with the code “ROMEO ROMEO”
10. Ground Air Visual code : During daylight, to indicate that they have understood the
ground signal code, they will : Rock the aircraft wings to acknowledge the code
11. Prepared Emergency : the commander shall brief the CCIC on :
a. Type of emergency
b. Time available for cabin prepation
c. Any other special instructions
12. Dangerous goods : After confiscating the dangerous goods from passenger, Store
it in a safe place & maintain communication with flight crew throughout the
flight.
13. Landing Procedure : on descent when passing 10’000 feet above aerodrome level
(AAL), pilot shall switch on the fasten seat belt (FSB) sign. If the FSB has been on
due to weather, pilot shall : Select the FSB sign to OFF and ON again, to indicate
that the aircraft is passing this attitude
14. In the event of a fire, information that is required when reporting to the flight crew are
: Location, type, source, severity and actions taken to fight the fire
TOC
15. No person shall smoke in any compartment of a malaysian aircraft : Yes,
including electronic cigarettes
16. The spare lithium batteries cabin be carried on board and it...Must be in
carry-on baggage
17. Dangerous goods : if restricted articles are carried onboard, crew shall :
Confiscate and keep the article in a safe place if unable to surrender
it to the airport authorities
18. Ditching : After passengers have boarded the rafts : Board and
separate the slideraft, and rescue any survivors who are still in the
water
19. Prepared emergency : The P.A system is unserviceable, the brace
order will be given by : Flashing the ‘Fasten Seatbelt’ sign, 30
seconds before impact
20. Before commencing the post decompression duties, cabin crew shall
wait for : Commander’s announcement stating that the aircraft is at
safe level
21. To prevent from frostbite when in extreme cold weather : Keep warm
and dry, move your limbs and excercise face muscles
22. When in the open sea on board a raft, “Look Outs” must be continuous ...
Scan the horizon for crafts, birds, seaweed and land
23. Flight deck intruder alert procedure : Any suspicious character or
security breach, cabin crew are to adopt ....Agressive Actions through
Teamwork
24. If restricted articles are carried onboard, crew shall .... confiscate and
keep the articles in a safe place if unable to surrender to airport
authorities
25. Smoking of Electronic Cigarette is prohibited...recharging of this
device is also prohibited and it must be securely kept in the carryon baggage
26. E-cigarettes : smoking and recharging of these devices on board the
aircraft is...strictly prohibited
27. P.E.D fire or smoke : if smoke is coming from the overhead bin, but the
device is not visible....Remove other baggage from the overhead bin
to access the affected bag, identify the item and douse device in
water
SEP A330 specific:
1. To switch the aural indication for emergency evacuation signalling system : press
the “EVAC RESET” switch at FAP and AAP’s
2. When smoke detector is unserviceable, the affected toilet must be blocked and
rendered in-op
3. To separate the slide raft from the aircraft; first pull disconnection handle.then
pull the manual release handle located in a POUCH (keyword for the answer)
to release the mooring line.if the mooring line is not released,use the knife
to cut.
4. Doors 3L & 3R are equipped with : single line ESCAPE SLIDES
5. To arm the cabin door :
a. remove the safety pin,
b. move slide arming lever to the ARMED position,
c. close the plastic cover and stow the safety pin
d. verify arming lever is aligned to the side arm placard.
6. If the door is not properly closed and locked : the locking indications will show
“UNLOCKED”with `RED” background
7. The evacuation procedure when evacuationing from the flight deck sliding
windows are : open the window, remove the knotted rope from the stowage
and throw it out of the window and evacuat
8. Freighter : while on duty in the MDCC, cabin occupants must : carry and keep
the OXYGEN BOTTLE within reach
9. Freighter : commander shall notify all cabin occupants thru p.a system: phase of
descent and preparation for landing
10. Freighter : pre-flight check of the portable oxygen cylinder with full face mask is
the : pressure gauge needle to be within the red band and the full face mask
is connected to the Outlet Assembly
11. Freighter : in case of smoke detected in MDCC : Make PA announcement to
inform all cabin occupants to return to their seat and put their oxygen mask
12. Freighter : in case of smoke is detected in the LDCC, the ventilation system will
be shut off and the depressurization process initiated
13. Recommended technique to evacuate through the sliding window is by Sitting on
the windowsill with upper body outside and the lower body to the ground
TOC
14. To preflight check for the doors when instructed, ensure that The door
pressure gauge and slide pressure gauge are in the GREEN zone
15. To Disarm the cabin doors : Remove Safety Pin from the stowage,
select the lever to the ‘disarm’ position and insert the safety pin
16. In a ditching situation cabin crew at Door 3 shall : Block exit and
redirect passengers to the usable exits
17. Door 1, 2 and 4 are equipped with : Double Lane Sliderafts
18. When smoke detector is activated, ACP at the affected area will flash in :
AMBER
19. The emergency evacuation signalling can be activated from the :
Overhead panel in the flight deck & FAP in the cabin
20. Freighter : Cabin evacuation devices are – Slide raft, which is installed
at each cabin door
21. Freighter : Prior to departure, the co-pilot is responsible to ARM the
cabin door
22. Flight deck sliding windows are equipped with Knotted escape ropes
for use when there is a need to escape
23. Smoke detectors are installed in all lavatories to Detect Smoke
24. In an emergency operation, if the slide fails to deploy automatically ...
Pull the RED MANUAL INFLATION HANDLE to inflate it
automatically
25. When the door is disarmed and the warning light at the observation
window flashes RED : Cabin crew shall report to the Commander as
differential pressure is present
26. The purpose of the emergency evacuation signalling system is to : Alert
the cabin crew to start passenger evacuation
27. Freighter : Entry into MDCC is not permitted..for taxi, takeoff and
landing
28. To open te cabin doors 1,2 and 4 in an emergency
CRASHLAND....Ensure that the door is ARMED and rapidly lift the
door control handle up and release
TOC
SEP A330 specific:
29. The purpose of the flight deck sliding window is for the flight crew to .... Evacuate
when access to the cabin is not possible or obstructed in an evacuation
30. To operate door 3 L/R in an emergency...
a. lift the door Control Handle cover
b. lift door Control Handle rapidly fully up
c. release handle
31. When the lavatory smoke detector is triggered, the visual warnings at the FAP,
AAPs and AIPs are .... i)at the FAP, CIDS caution lights comes on, affected
lavatory displayed on the smoke detection page and SMOKE RESET button
becomes RED ii) AAP – ‘SMOKE LAV’ light comes ON iii) AIP – RED light
comes ON indication location of the smoke
32. Freighter : Access to cargo compartment is prohobited during ... Taxi, Take off
and Landing
33. The primary exit in a CRASHLAND situation are...Doors 1, 2 & 4
34. In a Ditching situation doors 3 Left/Right are to be opened....As secondary exits
– in the armed mode
35. To reset the aural warning from the smoke detector when it is
activated....Press the ‘Smoke Reset’ pushbutton at FAP or the affected
AAP
36. When in the emergency evacuation signalling system is activated,
Primary crew shall....Comply with the evacuation command and
proceed to assess the situation
37. The Primary exits in a CRASHLAND situation are ...Doors 1, 2 & 4
38. When smoke detector is inoperative, the indicators in the cabin are.....the
CIDS caution light comes ON at the FAP, respective position name is
displayed in the amber and a message on the control pad stating
SENSOR INOP/NO DATA AVAILABLE
39. To preflight check for the doors when instructed, ensure that ....te door
pressure gauge n slide gauge are in the Green Zone
40. Upon pressing the ‘EVAC RESET’ pushbutton...Visual and aural warning
is cancelled (with FAP diagram)
DGR:
1. In the case of a spill of known or suspected dangerous goods in powder form :
a. Leave everything undisturbed, do not use fire agent or water
b. Cover area with polyethylene or other plastic bags and blankets, keep
area isolated until after landing
c. All of the above
2. What is the risk of this DG – DICHLOROMETHANE to the aircraft? :
Contamination with either toxic solids or liquids
3. DG UN2722 : the risk posed to the occupants of the aircraft : Eye, nose and
throat irritation, skin damage on contact. Other risk is either low or none at
all
4. Section 1.5 – DG bearing ‘Cargo Aircraft Only’ are required to be accessible
inflight except : Class 3, 6, 7 and 9
5. In case of any incidents, landing as soon as possible should be considered?
a. Because of the possible disastrous consequence of a DG incident
b. Because DG incidents may develop very critical stage with time and
severely restrict operational flexibility
c. BOTH of the answers are correct
6. To verify a DG incident, for the drill code you will refer to? Table 4-2 or 4-3 and 41 of the ERG
7. UN 3258 : what is the risk of this DG substance to the aircraft? Drill letter ‘L’ –
additional risk of the substance is either low or none at all
8. What is the UN number of this DG – BUTYRIC ANHYDRIDE? UN 2937 \ UN 2739
9. What is the drill code for this DG – CHLOROPICRIN? 6L
10. What additional Risk posed by a DG substance with the drill letter ‘X’? Oxidizer
11. Table to refer once you have acquired the drill code : Table 4-1 for appropriate
action to take in response to the incident
12. A general consideration in the event of spillage of a known DG in powder form :
The spillage should not be covered with a fire agent or even diluted with
water but instead covered with blankets / polyethylene bags and left
undisturbed
13. The inherent and additional risk of this DG – HEXACHLOROPHENE : It is toxic
and may be fatal if inhaled, ingested or absorbed by the skin. Other risk are
low or none
14. Aircraft emergency response drills : Drill no 4 – what is the risk to occupants?
Smoke, fumes and heat; and as indicated by the drill letter(s)
TOC
15. Aircraft emergency response drill : Drill no 11 _ what is the firefighting
procedure involved? All agent according to availability. No water on
“Y” drill letter
16. DG leakages in the underfloor cargo compartment, you must : Don the
quick donning mask and consider turning off non essential
electrics
17. What is the additional risk posedby a DG substance with drill letter “F”?
Flammable
18. What is the inherent risk posed by this DG substance –
DICHLOROMETHANE? Toxic, maybe fatal if inhaled, ingested or
absorbed by skin
19. Aircraft emergency response drills : with drill letter “H”, what is the
additional risk involved? Highly ignitiable
20. What is the additional risk posedby a DG substance with drill letter “P”?
Toxic
21. If a chemical substance is identified by a proper shipping name or
number in an incident and you are unable to respond appropriately :
Helpful information can be obtained from national chemical DATA
BANKS by a phone patch procedure
22. DG with a “CARGO AIRCRAFT ONLY” label (CAO) with the exception of
classes 6, 7, 9 and 3 of packing group :
a. Are not required to be accessible inflight
b. It is not stated in the ERG (emergency Response Guidance for
aircraft incidents involving DG)
c. Are REQUIRED to be accessible inflight ß this is the
answer !!! refer under section 1.5 in the ERG.this question is
similar to number 4 question..only confusing.
23. What is the drill code for this DG – AMINOPYRIDINES? 6L
24. What is the UN number for this DG – EPIBROMOHYDRIN? UN 2558
25. Aircraft cargo compartments are generally classified into : 5 Classes
26. What will be the spill or leak procedure for this dangerous goods – LEAD
CYNIDE UN 1620.... Use 100% oxygen, establish and maintain
maximum ventilation and donot touch without Gloves
27. What is the drill code for this DG – ETHYLDICHLOROSILANE? 4HW
1.
2.
3.
4.
5.
6.
PERF:
TO RWY
TO Config.
FLX/TOGA (MCDU)
V1/VR/V2 (PFD)
Trans ALT
THR RED /ACC ALT /
EO ACC ALT
TAXI:
1. EFB Version
2. Route
3. Special Proc.
FLT PLAN:
1. MSA/MEA/MGA/CRZ
ALT
2. Assigned ALT/FL
(BLUE)
3. FLT Plan RTE
- SID (MCDU)
- PLAN (ND)
INIT B:
1. BLOCK fuel
2. EZFW/ETOW
3. Extra/Time
RAD NAV:
ND
TAKEOFF BRIEF
T.E.M
MISC:
1. Ac type
2. Data validity
1.
2.
3.
4.
ABNORMAL OPS:
EOSID/RETURN
Secondary FP
Weight (LDG)
Special Proc.
Standard Company Procedures and Callouts. Monitor engine and flight instruments. If a malfunction occurs
before V1, call out SYSTEM and CONDITION. If I decide to reject the take-off, I will announce 'ABORT', and
carry out the manoeuvre. Monitor my actions and callout any omissions. If a malfunction occurs at or after V1,
the take-off will continue and there shall be no actions below 400ft AFE.”
For Right Hand Seat sector, any malfunction before V1, I will do the Reject manoeuvre and you will revert to
support duties. If a malfunction occurs at or after V1, the take-off will continue, and you will continue flying the
aircraft until I announce, 'I HAVE CONTROL', at which point you shall hand over controls and revert to support
duties."
Should you have any doubts on the safety of the flight, do not hesitate to bring it to my attention immediately
TOC
TAKE OFF BRIEF
FLT PLAN:
1. Missed APP
2. Diversion
SEC F/PLAN:
1. Alternate
plan
1.
2.
3.
4.
LANDING:
CHARTS
- RWY info
& lights
- Exit & Taxi
- LDG PERF
TAIL strike
Autobrakes
Reverses
APPROACH BRIEF
RAD NAV
PERF :
1. APP
-MDA/DH/
FLAPS/Trans/
VAPP
2. GA
- THR RED
- ACC
- EO ACC
PERF:
1. TOD
2. Des
SPD
TAXI ROUTE
APPROACH BRIEF
T.E.M
MISC:
1. Ac type
FUEL PRED:
1. Extra
Fuel /
Time
FLT PLAN (ND):
1. CHARTS
- MORA/STAR/MEA
- ALT & SPD
constrains
- Holding
2. APP TYPE
PROG:
GPS
PRIMARY
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