synthetic flight trainer lng guide -flight …sharepoint.aag.ph/portal/downloads/synthetic flight...
TRANSCRIPT
+A320 +A330 +A340 + A380
Synthetic Flight Trainer lNG GUIDE - FLIGHT MANEUVERS
, QRH, FCTM, FOM, Instructor Support, FOBN & GTG series
THESE FLIGHT MANEUVER PROFILES ARE INTENDED FOR QUICK REFERENCE USE ONLY DURING TRAINING. DOCUMENTS OFFICIALLY
PUBLISHED BY THE AIRCRAFT MANUFACTURER AND THE OPERATOR REMAIN AS THE PRIMARY SOURCE OF INFORMATION
AIRBR 360 @
+A320 +A330 +A340 + A380 TITLE QRH Sedion/Subsedion number ---+
FCTM Section/Subsection number--+
NP - NP 4 No-eee
'---------------------------v-Aircraft family I type
tJIIer profile Flight fl'lane
;' ;'
\ Exercise page sequence
BOX BACKGROUND COLOR CODE
.,__'---*/
Normal operations
Miscellaneous 1 i.e. Special
LJ
GREEN
BLUE proceduresjopns =!!!!!!!!!!!!= Miscellaneous 2 I I "!on-normal opns, YELLOW 1. e. Go around _ _
Abnormal I AMBER I procedure
Emergency procedure
Emergency
RED
I abnormal ~t:::.JL:::IlJ\.~ procedure
~ [£} Proceed to designated exercise page, e.g "C" in this case
}
~Aircraft family/type or engine-specific variation {blue font) ,If A320: 15• NU ~
_, -" A330/A340: 12.5• NU
~ ........ " ~~
Page & Issue number r"" __ _.A '
New & old FCOM Volume reference numbers The new preceded by "• "symbol, the old by "o "
Release date DDMmm YYYY
r A.~-..... ,
f!!!e]10 Rev.s ----u • PRO - NOR - SOP - 10 o 3 .10. 20 24 Sep 20121 1
+A320 +A330 +A340 + A380 GROUND AND FLIGHT PHASES No-ese
[I] PHASE I PREFLIGHT
ACT IVED liN IT or PERF BY: key depressed
OPTIMUM SPEED
PROFILE
\.. ....._
~ TAKEOFF
SRS takeoff mode engaged and
N1 >85% EPR~1 . 25
or Grnd spd>90 kts
SRS command: • V2+10 (AEO) • V2 to fail speed
(OEI)
ACCEL ALTITUDE
THRRED ALTITUDE
[3] CLIMB
At acceleration altitude or by engagement of another vertical mode
Default profile: • 250 kts to 10,000 ft • Above FL 100: ECON CLB Speed/Macl
CLB OPCLB V/S-xxx EXP CLB (A320)
SPEED I ALnTUDE CONSTRAINT
TOP OF CLIMB
[i] [[! CRUISE DESCENT
At descent initiation (if dis!. to DEST <200nm and no step descent
AL T CRZ-"soft altitude"
ECON CRZ MACH ECON DES MACH I SPD
STEP CLIMB
llL. TCRl• ..... _ i50iool
STEP DESCENT
DES initated from CRZALT
DES OPDES V/S-xxx FPA-x.x EXP DES (A320)
Alrcr~fl must be SENTio ~n~ •HitucH. tt will nOf '"JU.fo •ny alfltud• ch•ngo by ltsoff.
TOP OF DESCENT
EARL Y / SPEED I ALTITUDE OES~ENr / CONSTRAINT
\ / JoEC ElERATEJ !
\ .'~ _ _. ....... ..... oe'tc~r I ' j
r i ..
INTERC,)T POINT BASED ON
U SPEEDIJRAJ<ES
[§] APPROACH
1) Overflying decel pseudo waypoint with NAV (or Loc•tLOC) engaged & altitude <7200 ft AGL
or 2) Manual activation
VAPP (GS mini)
Flaps retracted
Flaps 1 (slats only)
Flaps 2 I Flaps 3
Land flaps (Full or 3)
APPROACH DECELERATION
-overflying decel point or, -manual activation on MCDU
~ CLIMB (AFTER
APPR. PHASE)
Insertion of a new FL
rm1 GO AROUND
TOGA and Flap handle "I 0°
Previous approach is automatically loaded for activation/confirmation
1) VAPP or current SPD whichever is greater;
2) Green Dot at ACCELALT
Decision for a new approach or diversion
lZAJ DONE
30 seconds after landing
THRREO ALTJTUOE
1!1
,__~ _ __...,@)
_ ..... ==:...._ ~
pli110 Rev.6 o 4.92.29 24 Sep 20121 2
~A320 ~A330~A340 CD
Before T/0 settings: EFIS cntl pnl: CSTR TCAS:ABV W/wx: TILT 4° Nearby terrain:
TERR ON NO
PF
0
Set initial power
A320 CFM: 50% N1 A320 IAE : 1.05 EPR A330 PW" 1.1 EPR A330 RR: 1.1 EPR A330 GE: 50% N1 A340 CFM: 50% N1 A346 RR: 1.05 EPR
"TAKEOFF"
Start chrono
TAKEOFF 1
0
• When power stabilized, set to FLX or TOGA
• Start chronometer when takeoff roll is started
• At T/0 thrust, check: - trend arrow - yaw bar - T/0 performance active
[read boxed FMA]
0
FLX or TOGA should be achieved
before reaching 80 kts*
CM1 hand on thrust lever
Scan PFD & ENG parameters
(N1 , EGT)
------------------------------------------ (both) ---------------------------------------------------------
PNF "THRUST SET" (Callout before 80kts)
••••••••••••
80 kts
UIJi]ll Rev.14 • PRO-NOR-SOP-12 o 3.03.12 ----17 Mar2df2] 3
I+A320 +A330 •·)-A340 I TAKEOFF 2 ..
0 G) 0
PF
PNF
il Sidestick 1f2 nose down
to improve nose gear contact with runway surface till 60-80 kts* then release progressively to neutral by 1 00 kts
*CFM: 80kts PW: BOkts RR: 60kts
ND: At 80 kts ground speed & true air speed appear on upper LH side
* If tailwind or if crosswind> 20 kts PF applies full forward stick, then: 1. Sets 50% N1/1 .05 EPR (A320) 2. Rapidly increases thrust to
70% N1/1 .15 EPR (A320) 3. Progressively increases thrust to
T /0 power at 40 kts grnd speed
80 kts
••••••••••••
Connection between nosewheel steering and rudder pedals is removed and more rudder input is gradually required for crosswind correction
ND: Wind speed & direction appear on upper LH side
PF crosschecks and confirms speed on PFD
2. "CHECKED"
1. "ONE HUNDRED KNOTS"
••••••••••••
100 kts
CM1 removes hand from thrust lever
"V1"
V1
I}Uil12 Rev.lS • PRO-NOR-SOP-12 o 3.03.12 28 May 20121 4
+A320 +A330 +A340
0 0 @ VR V2 30 ft. RA
Rotate smoothly at 3°/sec RWY TRK or NAV to target pitch
A320: 12.5-15° • FD roll bar appears A330/A340: approx.12.5° then to FD SRS • Yaw bar & sidestick
Control laws indicator disappear
PF
PNF
change to flight mode
[read boxed FMA]
"ROTATE"
-.
® Positive
climb Check VSI climbing
& RA increasing
"POSITIVE CLIMB"
TAKEOFF 3
@ SRS
Managed speed A320 SRS managed speed AEO: V2+10 OEI: V2 to V2+15
A330/A340 initial climb speed: V2 to V2+20
1. "GEAR UP"
2."GEARUP"
@ 100ft RA
Autopilot available
5 seconds after liftoff,
w/minimum 100ft. RA
AP1 (or 2) on
If AP is engaged by the PNF:
"AP 1(2) ON"
@ 400ft RA
RA figure on PFD turns from amber
(large font) to green (small font)
1:1!•113 Rev.lO • PRO-NOR-SOP-12 o 3.03.12 09 Dec 20iil s
+A320 +A330 +A340
@ THRUST REDUCTION
ALTITUDE
FMA: flashing "LVR CLB" - Reduce pitch attitude - with positive speed trend:
set thrust levers to CL detent FMA: "THR CLB" Autothrust engages,
ATHR white Pack 1 (if applicable) .. .. ON
BLINKING ADVISORY
PF [read boxed FMA]
PNF .... "CHECKED"
@ ACCELERATION
ALTITUDE
(beginning of climb phase) OP CLB orCLB
Speed bug will go to value set on MCDU PERF/CLB page (normally 250 kts)
TAKEOFF4
@ @ F speed & positive speed trend:
S speed S. positive speed trend:
I I
.~ 1 ·~ "< ""''
• 0
c c
PNF:
@ 1500 ft AGL or 2 min. after T/0:
T/0 inhibit ends
Ground spoilers ... DISARM
"FLAPS ONE"
.... "SPEED CHECKED"
"FLAPS ONE"
Exterior lights ....... ... SET Pack 2 (if applicable) ... ON
"FLAPS ZERO"
.... "SPEED CHECKED"
"FLAPS ZERO"
@ AFTER T/0 CLIMB CHECKLIST
"AFTER TAKEOFF /CLIMB CHECKLIST DOWN TO THE LINE"
ljiJil14 Rev.10 • PRO-NOR-SOP-12 o 3.03.12 17 Mar 20121 6
STANDARD CALLOUTS +A320 +A330 +A340 • ACTIONS COMMANDED BY PF •
.. MANAGE SPEED II
To engage managed speed mode.
SPEED .. PULL SPEED KNOTS"
To engage a selected mode or target. SPD knob is pulled and turned.
A.T r---l,\\.10'----, VIS I <!9' 20000 0 +2Soo - .. '"' 0 - .., ..., 0
1=1 1=1 Q >«:,\" b"' .... .. ~ ~ ~ ~fiHlf'ftL OII
[d liiiil liiiil L.J ® l.!!!.J
n ~ l~fJ•lll Rev.2 • PRO-NOR-SOP-90 o 3.03.90 ... 19-bec 20111 7
+A320 +A330 +A340
I AP/FD/ATHR engagement status]
Maintaining 250 knots,
3000 feet
Heading 228 [ND. ATC instructions]
PF/PNF DUTIES TRANSFER • TURNOVER OF CONTROL •
TRANSFER OF CONTROL (example)
I :f}•l 14 Rev .1 • PRO-NOR -SOP-90 cJ 3.03. 90 -----20 i5&20fl] 1 o
+A320 +A330 +A340
.. THV001 .. -+ I FROH
UTC SPO/ALT
C335 BRG394' 1 I BIG07t. 1927 250/ 2500 I
C27 9 • a C27 3 • 9. 0. u DEST UTC DIST EFOB I
EGLL27R 1932 1 5 4. 1
··=r:.J F-PLN • Lateral:
STAR/Transition I Approach/Landing runway /GA/ Alternate flight plan
• Vertical: Altitude & speed constraints/winds
Compare with approach chart
PERF APPR • Insert wx (A TIS) • DH for CAT II/III or
MDA for other types of approach
• Landing config
~ RADIO NAV
VOR!/FREQ FREQ/VDR2
CRS CRS
l LS /FREQ CHA '1/ HLS
CRS SLOPE CRS - . -
ADF! / FREQ FREQ/AOF2
'
RAD NAV • Manually tune required &
available nav frequencies • Check ILS ident/frequency
/course • Check idents on ND (VOR
& ADF) and PFD (ILS)
PERF GA Check: • Thrust reduction altitude • Acceerationl altitude
APPROACH PREPARATION • MCDU •
NP-NP N0-100
~ THV001 ~
CRZ OPT R E C HA X -----
I <REPORT VDEV= FT I UPDATE AT
BRG /DIST I TO
I PREDICTIVE <GPS REQUIRED ACCUR ESTIMATED ~
NH
·~J •. ;·.J PROG • Insert VOR DME or landing
runway threshold
• For VOR DME check BRG/DIST (accuracy check)
FUEL PRED Check: • Estimated landing weight • EFOB • Extra fuel to evaluate holding
possibilities at destination
•••••••••••••••••••••••••••••••••• • • : .
~ C-l fl ®® .,. '-'''l" llfl!
® ® ® ® .;;-c ~,, -.- oJ (jill .· ... 1,., ._I :' I J -" ... _ .. ,,
A B c D m Key pad flow:
. rl . ~ ~ ~ ~
•• • • •• • • • •• • ••••••• • •• • • • ••• • •• ••
.·· · ·· ·o6·. a······· ····. : I L • ••••• • ••••• • ••••••
... NON-PREC APP: \ : -- ~ : : 1700' :
. . : I : • • • • •••••••••••••••••••• •
~ FROM SEC H ~
BIG UTC SPD/ALT :
2336 I 4800 ~ C335 8RG334' 7
BIG07t. 2 3 4 0 250/ 2 62 0 r~ TRK289• 1 ~
(DECEL) 2340 250/ 2 3 a 0 ft 6 ••
CI27L 2 3 41 137/ 2980 [''< C27 9 • 3-3.0. "' FI27L 2 343 · I 1400 .,
DEST UTC D I 5 T E F 0 8 :~ EGLL27L 2329 2 1 4.0 j
t.!. ·.'
SEC F-PLN • Same approach (backup) • Another STAR • Parallel, opposite or
intersecting runway • Circling approach • Diversion I alternate airport • Another type of approach
• Enter VAPP
at FAF
• . . . •. <RETVRN ~· : . ~ .
• •••••••••••••••• • •• •
[iJJi]ll Rev.4 • PRO-NOR-SOP-16 • PRO-NOR-SOP-SRP-01-60 o 3.06.XX _u___ 28 May20f2] 11
+A320 +A330 +A340
''1 "' ) • -" (.All AP1•1 1X1Ai. HOI
.,... A,'T'I\Q
LS pb ON for ILS & LOC approaches
LS pb OFF for other approaches
ILS Approach
NAVIGATION ACCURACY ND
PF I PNF GPS PRIMARY
NAV ACCUR HIGH ARC or ROSE NAV NAV ACCUR LOW and with NAVAID raw data
NAV ACCURACY check 5 1 NM GPS PRIMARY LOST and NAV ACCUR LOW and ARC or ROSE NAV
NAV ACCURACY check > 1 NM ROSE ILS or ROSE ILS
GPS PRIMARY LOST and with NAVAID Aircraft flying within unrel iable radio raw data
NAVAID area - -- ------------------- ----
APPROACH PREPARATION • FCU PFD ND •
~P-NP NO~lOO
•
AP/FD mode
NAV
NON-PREC:TRK/FPA
NON-PREC: Arm LOC for LOC only approach
THV001 HAX ~ CRZ OP T REC
~ <REPORT 'JOEV •
F T Jl UPDATE AT
ORO / OIST Ill PRE DICT IVE
<GPS
I I
REQ UIRE D ACCUR ES IIHATEO
"" ~
NAVIGATION ACCURACY
GPS PRIMARY NAV ACCUR HIGH
NAV ACCUR LOW and NAV ACCURACY check 5 1 NM
GPS PRIMARY LOST and
ArmAPPR for managed approach
NON-PREC Set FPA at least 1 nm before FAF
... , , A.P2
'"" MOoto A.'n<lt
- - - -- - - - - - - --- - - -- ---
Approach NO AP/FD mode guidance PF PNF
NAV-FPA or Managed" ** ARC or ROSE NAV * APP·NAV/ or Wiltl NAVAID raw data FINAL selected ***
HOG or TRK NAV ACCUR LOW and ARC or ROSE
HDG or TRK
NAV ACCURACY check NAV or ROSE > 1 NM Selected ROSE VOR "* VOR ** TRK-FPA
GPS PRIMARY LOST and With NAVAID aircraft flying wtthin unreliable raw data
radio NAVAID area -------- --------------------- --
(*) For VOR approaches, one flight crew may select ROSE VOR. (**) For LOC approaches, select ROSE ILS. (***) Managed vertical guidance can be used, provided that the approach coding in
the navigation database was validated.
(4(•112 Issue 1 • PRO-NOR-SOP-16 • PRO-NOR.:SOP:SRP:-o-:1.:6o-o~.-06.XX___ 10 Dec 20111 12
+A320 +A330 ~-)-A340 I INITIAL & INTERMEDIATE APPROACH NP-NP
N0-100
:·· ·FM·· ~~~· ·~~~·~~~·~~·~·h~~·k ..... ...... .......................................... .. .................... 1 \ Select flying reference (attitude or bird) \ ! • Track/FPA for visual and non-precision approaches ' ! • HeadingNS for ILS approach
L.~~~~y~~~ .. ~P.P.~?~~.~ .. P..~~~.~ ............................................ ....................... .. ... ,
' IAF
DECEL POINT Approximately 15 n.m.
from touchdown
ll...
At 2500 feet RA Crew monitors radio altimeter
If auto callout inoperative,
PNF: "RADIO ALTIMETER ALIVE"
' IAF
@l•l13 Rev.3 • PRO-NOR-SOP-18/19 • PRO-NOR-SOP-SRP-01-60 o 3.06.XX 09 Dec 20111 13
+A320 +A330 +A340 + A380
INITIAL APPROACH
FM nav accuracy check
\,
I DECEL point I ®
INTERMEDIATE APPROACH
Approximately 15 n.m. from touchdown
ILS APPROACH 1
DECELERATED
NP-NP NO-lee
LOCALIZER CAPTURE
IAF 0
Cleared for the approach " \, ~ ... &~~ ~ • "~~ .. ~~
I LOG* I ----------~~ ~~--.. &~~
FAF
Activate approach or "FLAPS ONE'"' Press APPR push button "LOG STAR" set Green Dot speed Engage 2nd autopilot
PF Read FMA change, i.e. "ACTIVATE "LOG BLUE, G.S. BLUE"
APPROACH PHASE" Monitor LOG & GS capture
.... "APPROACH .... "SPEED CHECKED" ..,. "CHECKED" PHASE ACTIVATED" Confirm position, .... "CHECKED"
PNF then "FLAPS ONE" Monitor LOG & GS capture
[f{•l21 Rev.3 • PRO- NOR - SOP-18 e ·PRO-NOR-SOP- SRP-01 - 70 o 3.03.18 ·· ·a96eC:.2bll l 14
+A320 +A330 +A340 + A380 ILS APPROACH 2
I LOC I
GIS ' ................................................ ~ GS intercept below 2000 ft .
i.e. at 1500 ft AGL: One dot below GS, PF: "FLAPS 2"
Check or set F speed
PF "GS STAR"
To minimize flap wear, extend flaps at VFE-15kts when possible
"GA ALTITUDE FEET SET'
PNF ... "CHECK"
Speed < VFE, "FLAPS TWO"
DECELERATED
... "SPEED CHECKED" Confirm position, then "FLAPS TWO"
NP-NP No-1ee
Speed< VFE, "FLAPS THREE"
... "SPEED CHECKED" Confirm position, then "FLAPS THREE"
[il•l22 Rev.S .- - PRO-NOR-SOP-18 • PRO-NOR-SOP-SRP-01-70 o 3.03.18 19 Ma{2o:CL] 15
+A320 +A330 +A340 + A380 ILS APPROACH 3
Speed < VFE, "FLAPS FULL"
PF Check or set VAPP CM1: Obtain cabin report Advise cabin crew
-> "SPEED CHECKED" Confirm position,
PNF then "FLAPS FULL"
•Gts
~ ~
"LANDING CHECKLIST"
->Read Landing C/L
"LANDING CHECKLIST COMPI FTF"
DECELERATED
2. "CHECKED"
Check approach stabilized
1. "ONE THOUSAND" Check maximum parameters: A340-600: VIS 1000fpm V/S 1200fpm lAS +10/-5 knots
2."CHECKED"
1. "ONE HUNDRED ABOVE"
Bank 7° A ,...--A320 A3301A340 ...__ ___ ___ A_3_8_0 _ _ _ ____
LOC 1j. dot 500 ft: LOC & GS 1 dot LOC 1j. dot GS 1 dot 300 ft: LOC ~dot GS 1 dot GS 1 dot Pitch : Pitch: Pitch: NU+10° NU+10° NU+12deg{below400RA) ND -2.5° ND 0° ND -3 deg
VAPP stable Landing config
*1000 ft min IMC 500 ft min VMC or as restricted
by operator policy or air regulations
100 above MDA
2. Visual contact:
NP-NP No-1ee
No visual contact:
"CONTINUE" "GO AROUND -FLAPS"
1. "MINIMUM"
I MDA -,
' Sf I
• PRO-NOR - SOP-18 • PRO-NOR-SOP-SRP-01-70 o 3.03.18 26Dec2012l 16
+A320 +A330 +A340
INITIAL APPROACH
NON PRECISION APPROACH 1 NP-NP N0-120
INTERMEDIATE APPROACH
FM oav accuracy check Appm<imately 15 nm [IJGl Set VAPP speed at FAF fmm to"'hdown ~
""" . - ... • ' ' ' ' ... JII ___ IIII!I• IAF
PF
PNF
DECEL point
®
Activate approach or Set Green Dot speed
"ACTIVATE APPROACH PHASE"
"APPROACH PHASE ACTIVATED"
At Green dot
"FLAPS ONE""
-> "SPEED CHECKED" Confirm position, then "FLAPS ONE"
At S speed
Speed< VFE, "FLAPS TWO"
When Flaps 2
"GEAR DOWN"
-> Autot5raKe: as requlreci
When UG down, below VFE NEXT
Speed< VFE, "FLAPS THREE"
-> "SPEED CHECKED" UG lever down -> "SPEED CHECKED" Confirm position, Arm ground spoliers Confirm position, then "FLAPS TWO" Rwy turnoff & taxi lights-ON then "FLAPS THREE"
"GEAR DOWN" ECAM Wheel page: check
tl§ltlll Rev~3 • PRO-NOR-SOP-19 • PRO-NOR-SOP-SRP-01-70 o 3.03.19 30 May 20121 22
+A320 +A330 +A340
PF "CONTINUE"
PNF
CD
"PITCH, PITCH" if the pitch angle~ 1 o• "BANK. BANK" if bank angle ~7"
0 0 TOUCHDOWN
REV MAX
~----I- '
LANDING
Reversers and Ground spoilers} Check
Deceleration announce
0 CHECK
FWD PANEL
il a
• If no spoilers, call out "NO SPOILERS" Check Wheel SO page If no spoilers: PF THR LEVERS IDLE or REV DETENT
REV MAX Press brake pedals
~ •• "REVERSE GREEN"
~
or "NO REVERSE ENGINE or "NO REVERSE"
... "DECEL" or "NO DECEL" - monitored by DECEL light, feel of deceleration and PFD speed trend arrow
THR LVRS - FWD IDLE
"70 KNOTS"
0 70 KTS
~
'!1•111 Issuel -- -- . PRO-SOP-22 D 3.03.22 .. ----m 30 May 20fL) 27
+A320 +A330 +A340
PF THR LVRS - FWD IDLE
PNF
® TAXI SPEED
~ ~:::r
AUTO BRK - DISENGAGE
@ BEFORE 20 KTS
~
AFTER LANDING
m
IA1 GND. SPLRS ~ -Disarm
Signal for PNF to execute after landing procedure
"AFTER LANDING CHECKLIST"
[3 .. ·
m Eng mode :
selector m ~ttl
.Jjr ,m ..... l.i.l.i
Silent check: "AFTER LANDING CHECKLIST COMPLETE"
®
k I.
+A320 +A330 +A340 I ELECTRIC EMERGENCY CONFIGURATION
r ...................................... r~· ·d·i·~ ti·~-9~i~h .. b.~t~~~ ·Al:L .. EN·ci· ·FLAME.6u:r·& ·E ·LE·C' ·EME.RG.caN·F·iG'~··········· ................. ! - check engine parameters- i.e. oil pressure :
· ...................................................................... .......... ......................... ........................ ............................................ ..................... ..... ... ....... .................. .. :································ .. ················ .. ··············· .. ········"······················"·· ······ .. ··········· ·· .. ···· .. ··· ····················· ··· ···· ·············································""''''''''''''' ''·:
r .. ~~~~~~~~·;·;~·~~~~;~~·;;~·~; ·~~~~~~·~~~ ... j LH seat pi lot: RH seat pilot:
1. Cancel master warning 2. Switch dome lights & storm lights on 3. Set Track/FPA - FDs off (to regain track
index on PFD) 4. Perform Emergency Communications
Procedure 5. Perform ECAM actions
• Push VHF1 transmission key (this may default to OFF during power loss) .
• Declare emergency - through A TC or "blind" transmission on 121.5 ("MAYDAY'?
·Transmit: - altitude and heading - approximate position
. - intention : ................... .............. ............................................................................. .... ...... :
: ........ ....... ..... ..... ............ ............ .. ........... ... ..... ....... ................. .. .............................. ..... ... ...... ......... ...... ................. .... .. .. ...... .. .......... ............ ....... .. ......... :
'\.... \i.... - ,..
..-...-.-.-.. -.-.................... . ······~ \, J~~~~~~ ....... ~
For APU start, FL 250 or lower
Refer to QRH ABN-24
A330/A340: In view when Land Recovery activated {
•• .... . . . . . . .......... .................. , APPROACH PREPARATION:
• QRH FPE-SPD for green dot speed (2nd table all engines operative)
- for weight use ZFW+remaining fuel - get Conf1/Conf2/Conf3NLS speeds+5
l..._
_ flap lever position for landing QRH ABN-24 • QRH ABN-80 - obtain: }
- delta Vref Summary _ landing distance factor
• QRH FPE-IFL- multiply landing distance Conf full by landing distance factor from QRH ABN-80
If~ Ill Rev.9 -- u u _u___ • PRO-ABN-24 o 3.02.24 25 Apr 2009] 44
+A320 +A330 +A340 LANDING WITH SLATS OR FLAPS JAMMED ABN-27 A0-027
0 INITIAL APPROACH • Use selected speed (AfT ON) On non-maneuvering flight: • Select VFE NEXT, reduce speed
& change configuration until landing config is achieved
0 FINAL APPROACH • Do not use AlP below 500ft AGL • MED autobrake recommended (FCTM)
NO SLATS NO FLAPS • More maneuvering distance required • Set flap handle to Config 1
to arm Go Around mode • More attention required with speed contro • Prepare for possible hot brakes
d' g area if Request 11?1 '~s required additional tl~~e preparation
to comPlete
0
0 • Select flaps 2. If flaps do not extend
accelerate to green dot and select flaps 1
• Determine landing configuration:
QRH
CD SLATS OR FLAPS JAMMED • Speed select ·Go to VFE NEXT-5kts (::::200 kts)
A3301A340:
If no flaps and no slats available: QRH ABN-27.03 No flaps no slats landing
1. Landing config I Vapp I Ldg dist.factor: .. ABN-80 2. Vapp determination ...... ............ .... .. .. ...... ABN-80 3. Landing distance! : .. .. ............ .. .............. ... PE-IFL 4. Landing with slats or flaps jammed: .. ...... ABN-27
.; ., , .; , ,
...... ,...
.;
, """'"
LANDING
MISSED APPROACH PROCEDURE
QRH ABN-27
• For no flaps, Tailstrike possibility due pitch high
• Monitor tire speed
.. . lfJllO Rev.l2 • PRO-ABN-27 o 3.02.10 09 Jun 20121 46
+A320 +A330 +A340 DUAL HYDRAULIC FAILURE
Ref" FCTM 03.029
@ Set up FMGS for arrival Approach briefing* (see paragraph 3b below) Approach checklist (QRH) Advise ATC, ready to commence approach Advise company & cabin crew, give ETA for landing preparation Exit hold
@ * APPROACH BRIEFING ITEMS: • use of selected speeds on FCU • type of approach (precision/non-precision) • managed or selected; Vapp selected • approach config & flap lever posn • early landing configuration & long stabilized approach • when to extend landing gear (gravity extension -use QRH) • tailstrike awareness • landing/braking/steering • go around procedure: callout/aircraft configlspeed
~ CD
QRH
G+B summary .. .... .. .. .... .. . . ... . .. . . . . .. ABN-29 B+Y summary .... ............. ... .... ...... l G+Y summary .......... .. .. .............. .. Ldg config I Vapp /ldg distance .. . ABN-80 VLS config full & VAPP ......... ..... . Landing distance ... .. ... ... .. ........... ..... FPE-IFL Landing w/ slats or flaps jammed .... ABN-27 Landing gravity extension ........... .. .. ABN-32
Enter VAPP on the MCDU perf appr page Read Ldg w/ S/F Jammed & Ldg Grav.Ext.
C/L notes during prep. , to be skipped when performing C/L
Refer to FCOM PRO-ABN-29 for further info
DUAL HYDRAULIC FAILURE
AlP loss - take over manually Observe max speed/mach # Maneuver with care FD & ATHR still available -Alternate law protection may be lost
Advise ATC, declare emergency (LAND ASAP red)
Check weather-destination/alternate Activate SEC or APPR as required Advise cabin crew/passengers Advise company
B+Y G+B G+Y Maneuver with care Alternate Law;
protection lost
Maneuver with care Maneuver with care Alternate Law;
protection lost
IJflif- Rev.13 • PRO-ABN-29 o 3.02.29 09 Dec 20111 47
+A320 +A330 +A340
APPROACH Cat I only Landing gravity extension
B+Y: Slats & flaps slow G+B: Slats jammed I flaps slow G+Y: Slats slow/ flaps jammed
0 Slats slow
LANDING No nosewheel steering B+Y: Braking normal
DUAL HYDRAULIC FAILURE
A320
• G+B & G+ Y: Fit controls AL T LAW; DIRECT LAW when gears are extended • G+B:
- Autobrake inoperative - Extend ldg gr @ 200 kts to improve controllability on single elevator - disconnect AfT for better pitch control during approach & go around
• G+Y: - stabilizer frozen - Autobrake inop. - pitch trim lost
A330/A340 B+Y syst. low press.: FCOM PRO-ABN-29
- loss of pitch trim G+B syst. low press.: FCOM PRO-ABN-29 • Maximum brake pressure 1000 psi I call out pressure in
increments of 10 - PNF to monitor brake pressure during landing roll
• Minimize use of rudder during turns; use ailerons to minimize use of hydraulic pressure
G+Y syst. low press.: FCOM PRO-ABN-29
Any G system failure: request towing eqpmnt (NW steering failure) Missed approach procedure for
abnormal contig : QRH ABN-27
,. ,. ,. , , ,. ..,.,.
, ,. GO AROUND No gear retraction For circuit,G+B & G+Y:
Maintain slats/flaps config For diversion:
G+B: Select clean config G+Y: If flaps zero: Select clean config
If flaps >0: Maintain slats/flaps config
G+Y: Aircraft sluggish - Direct law
Rev.14 n- - n-n- • PRO-ABN-29 o 3.02.29 09 Dec 20111 48
+A320 +A330 +A340 ONE ENGINE OUT IN CRUISE PHASE
ording to engine-out strategy*
1. Check on Progress Page: EO MAX ALT
2. Advise ATC 3. Use QRH:
Engine out maximum altitude Gross flight pathdescent at gro Cruise at LRC speed In cruise quick check LR ..... .. .
/ {
~ 'after PNF has advised ATC \ : ........... .......................... ......................... .. .... .. ... ... ............................................................ .. ... ........... .. ...................... ........................................ .
,.,...
Notes:
* ENGINE-OUT STRATEGIES: FCOM
Standard ------------------------------- PER-OEI-GEN-1 0 Obstacle ----------------------------------- PER-OEI-GEN-15 Fixed speed (ETOPS-A320/A330) --- PER-OEI-GEN-20 2nd engine failure (A340) ---------------- PER-TEl
~
1-ArrHRj l disconnect
~
• Performance Cruise page appears with "EO CLR" prompt and displays the level-off altitude with descent and cruise at green dot speed (obstacle strategy)
• Progress page displays "EO MAX AL T". If the aircraft is above EO MAX AL T, the target speed is the long-range engine-out cruise speed at EO MAX AL T
• The autopilot will track the target speed in open descent mode • Disconnect the A/THR during the initial descent to prevent it from setting idle thrust.
Upon reaching the FCU-selected altitude or whenever normal descent is resumed , re-engage A/THR
• DES mode is not available above EO MAX AL T • For A340: In case of a 2nd engine failure descend at green dot speed, thrust at MGT
..... .,.. ,.,.
FPE-OEI A0-027
1Jli130 Rev.9 • PRO-ABN-70 o 3.06.XX: 09 Dec 20111
+A320 +A330 +A340
® Check FMA
m I I
ONE ENGINE OUT IN CRUISE PHASE
el> r,9e; f>'~Oj ·~\)l>e
~'IJ.,~\ ~e~ ~'<..~
I3H4Isl o -o o
ECAM actions
[2] I I
1l" . [!] , Act1ve engines:
A/THR CL to MCT
disconnect
FPE-OEI A0-027
lifl•13i--1ssue 1 • PRO-ABN-70 o 3.06.XX - ---- --------23 Jul 2012)
+A320 +A330 +A340 ® GO AROUND PROCEDURE ~ .-"
WITH ONE ENGINE INOPERATIVE [j'J§)=(§f?X§)
CD MISSED APPROACH:
PF:
Thrust levers-TOGA "GO AROUND- FLAPS" Check HDGNS mode (if TRK/FPA previously selected) Pitch 10- 12.5" up Center (3 target Call out FMA:
"TOGA (SRS) GA TRK AL T"
"GEAR UP" "MANAGE NAV" (if missed approach
procedure in nav database) or "HEADING PULL"
At EO acceleration altitude, level off & follow flap retraction schedule
PNF:
Check TOGA thrust is set Retract flaps one step up Start chrono Check heading knob, switch to HDGNS
and check FDs on
Verify FMA - "CHECK" "POSITIVE CLIMB"
Retract gears, "GEAR UP" Push heading knob to engage NAV mode
or pull to engage HOG mode
Inform ATC
0 Select NAV or HOG mode as applicable Level off at engine out acceleration altitude Accelerate to green dot At F speed, "FLAPS ONE" At S speed, "FLAPS ZERO" At green dot -
Open Climb Thrust lever MCT After takeoff checklist
~--·'~~~- ..... ------.....
ALTITUDE CAPTURE: I "* In the event of low altitude capture with engine failure while in AL T* mode, monitor the speed carefully as there is no low speed protection in AL T *mode. ' __,
~~
~
ENGINE OUT ACCELERATION ALTITUDE
0 1 . Check weather condition 2. Check fuel status using fuel used information
( FOB indication may not be accurate during climb or go around)
3. Announce intention: a. Diversion-enable alternate b. Immediate reland-activate approach
4. Advise ATC
When time permits:
5. Coordinate with cabin crew 6. Advise passengers (PA) 7. Advise company
lifl•l16 Rev.ll • PRO-ABN-10 o 3.02.10 09 Dec 20111
+A320 +A330 +A340 ALL ENGINES FLAMEOUT WITH FUEL REMAINING
r----------------------1 ...................... ....... ................... ....... ............ ........... ........... ......................... ... ............ ...... .......................................... ................................... .......... ~ I I
. PF: PNF: \ 1 EMERGENCY COMMUNICATIONS PROCEDURE ~ I
1. Take control (PFD & NO display 1. Silence horn (cancel ~ast.warning) ! 1 • Push VHF1 transmission key (this may available only on the left) 2. Switch storm & dome lights on ! I default to OFF during power loss).
2. Command "Track FPA" 3. Set track/FPA . . ! I • Distress: "Mayday, mayday, mayday" 3. Turn left or right, direction depending 4. Seat belt s1gns on; extenor lights on j 1 • Urgency: "Pan pan, pan pan, pan pan"
on terrain, nearby traffic, heading towards 5. Perform Emergency · · alternate airport, fly parallel 25 n.m. Communications Procedure
4. Descend at optimum relight speed 6. Perform QRH ABN-70 procedure - initially 300/M.82 or 2 degrees
nose down pitch attitude 5. Command "QRH actions" after ATC
has been informed
~- •••••••••••••••••••••••••••• • •••••••••••• • 0 •• ••••••••••• • •••••• • ••• • •• 0 • • •• ••• • ••••••••••••• • •••••• •• •• • •••••••••• • • • • • •• 0 •••• ••• •••••• •••• ••••• • •• • • • •••• •• •• • ••••• • •••••••• •• ••••••• • •••• • ••••••••• • 0 •••••• •• • •••• • •••••••••
[ ' ' ' ''''~' ' '"'''' ' "' ' '""'"''"'' ' ''~"' ' " ' '''''' ' "' ' ""' ''' "''''''' ' "''"''"''''''' ' '''' ' ' ' '""' ''' "'''''''''" ' ' "''''' ''' '' '' '' " ' " '''''''''' ' '''''' ' ' ' ''"''''''''''''"''' ~ PF: ~ PNF: ~ \ 6. Inform cabin crew & -'....._ j. 7. Continue QRH procedure \ ! passengers of situation ~ 8. Clear ECAM warnings; check STATUS !
j 7. Inform company ! ............. ........... .. ............................. .. ............................................... .. ......................................... .. ............................................ ........... ................... :
• COMMUNICATIONS Transponder code 7700 121.5 MHz, 243.0 MHz - aeronautical emergency 500 KHz, 2182 KHz - international distress 8364 KHz - swvival craft - through A TC or "blind" transmission
·Transmit: - Aircraft identification - Nature of the distress - Intention -Position - Flight level/altitude -Heading
m41 Rev.l4 • PRO-ABN-70 D 3.02.70/5 --- 10 Dec2o1TJ
I I I I
+A320 +A330 +A340 ALL ENGINES FLAMEOUT WITH FUEL REMAINING
,. ,
' ,
,. ,
.~.N.G..IN!; .. R..~. !,..lG.HT. .G.ON$J.P..~.R.AT.lQN$ ........ .................................. . r·· · ·· ·~~; · · · · · ···· · ··· ·· ·· ··· · ·· · · · ·· · ·· · ···· · · ··· · · · ·· · · · ··· ·· ········ ·· ···· ·· ···· ............. .................. ... ....... .. ...... P.NF·:··········· ·········· ..................... ................................. ~ • Guaranteed rel ight envelope:
= ~ : QRHABN-70 6. Inform cabin crew &
8. Perform QRH ABN-70 procedure ·
passengers of situation 7. Inform company of situation ! FL checkpoints:
~ ...... .... ... ............ ......................... ..... ............................. ....... .. ....... ......... ................... ..... ......... ....................................................... .. .. ... .... ......... ..... i ..,. FL 250 - start APU
-- ------------ ------ ------- -----------Windmilling start phase (300 knots)
engine master start sequence:
:J~Yl~h~ P,o-,ocoo~ ii ~:\¥! ~-~li" (':::"] G G ~ J ~ cycle C:J - -- ---
mll5ll D a ~
'----- -- ---- -------- -- ---------- --- --- ---- -- --- -- --- --- ------- --- ----- --- --- -
' \ I
I I
... ' I
I
..,. FL 200 - APU bleed on; reduce glide to optimum speed: A320: Green dot A330: 230kts then green dot } Option, to bring Green A340: 250kts then green dot dot in view on PFD
..,. FL 150 - ram air on
..,. FL 100 - oxygen masks off
! ... ~-~-~~--~-~.s.~t.i~~ - ~~-~. i ~-~~ - ~~~~~-~~i-~-~-: ... ~.?.~ .......... ...................... ..... ......... .... .
.,...,_
L!.-~ ~~ ........ ~ .................. ~-
Notes:
', Engine master switches ON one at a time, then OFF
I I
I • PRESSURIZATION: Cabin altitude will rise due to shutdown of ale packs - monitor this due ---------------- ----------------------- to the possibility of having to use 02 masks
• INDICA T/NG SYSTEM: To view upper ECAM cancel button has to be pressed continuously • AUTOFLIGHT: NP and NT have disengaged - restore upon recovery of electrical power • ELECTRICAL: Emergency generator will cut in automatically powered by the RAT and can
only be reset on the ground. During approach press Land Recovery button. • FLIGHT CONTROLS (A330/A340) :
- Ailerons are preset upward. Observe flight domain limitations in QRH ABN-27 Eleverator Redundancy Lost procedure
114•142 Rev.l6 • PRO-ABN-70 o 3.02.70/5 - ------- t7Mar 2bT21
+A320 +A330 +A340 EMERGENCY DESCENT - INITIAL
r;:;-J \ "EMERGENCY ~;f))) CMl: Announce DESCENT"
Check FMA
~ I I
el>. ~ \ t::~'9e; fll.l!J.'~Oj i~~l>.e
~~c ~e ~
I A6ll As I A41
liD Establish
communications
I I Extend
r;;;, ·nspeedbrakes
~~~
~
lg:!t]ll Rev.2 -.PRO-ABN-80 0 3.02.80 nn ______ 21Mayn26121
+A320 +A330 +A340 EMERGENCY DESCENT - INITIAL
P.P.I .... ······m·o · • •••••••••• . ..... ....
Pax02 masks-ON
- ••••• .t,.c •• '#if.
Signs I \ • '• '• • • •'6 'f( J-
ON ~· ~ •• .f. • •• 17 ~ . . ,~
• ••• ~0 .. ~ . . ""' • •• '& •• •• i" • •• . ' . • • • • • • • • .•. ..
• l. •
I I • •• I f ·• • i • · ··~ ,, 1' ':. + I I • • •
• • I+
.-0 I Ignition -0~ ~ m
•• •• •• ' .. •· •
G Establish
communications
• • • • • • • • •
II •
AdviseATC
li:lt112 Rev.3 ----------ePRO-AB-N=So o 3.02.80 - - -- -- 21 MaY2012I
+A320 +A330 +A340 EMERGENCY DESCENT - INITIAL
If cabin pressurization loss is deemed uncontrollable: CM1 - announce "EMERGENCY DESCENT"
,.,_ <E r·s~th··~~i~t~; ... .. .................. ... ............. .. .................... ,
I 1. CREW 02 MASKS ON
' 2. ESTABLISH COMMUNICATIONS - , ~·:·~~o.~· ~Oo~~to ~~~ PF: ~ PNF:
3. AL T selector knob - turn CCW & pull 4. HDG selector knob -determine direction
(Lor R- due to traffic, terrain, etc.), turn & pull 5. SPD/MACH knob - PULL /Jush SPD/MACH pushbutton 6. Check FMA: ITHR IDLE loP DES II HDG I 7. Speed brake -deploy (initially Y2 to avoid sudden pitch up,
then gradually to FULL) 8. Command "ECAM action" after completion of immediate actions
3. Seat beiUNo smoking signs - ON 4. All external lights - ON 5. Ignition - ON 6. Transponder - squawk 7700 7. Check MEA, inform ATC
"Mayday (3X), (aircraft ident) rapid decompression, descending on heading _ will call back for our intentions."
~
(after RH seat pilot has called ATC) 8. If cabin altitude>14 000 feet: Pax 02- MAN ON 9.
10. 11.
ALT- select FL 100 initially or MSA w/c ever is higher, then as required by ATC HDG - fine-tune as required Speed - determine if high or low speed descent required * ~
····· ···· ·························· ··· ·· ·· ·· ········· ····················· ··· ·················· ··································································· ···························································· ··· ··························································· ··························· ···················· ··•
* DESCENT SPEED ASSESSMENT
NO STRUCTURAL DAMAGE: High speed descent possible Pull speed knob and select VMOIMMO
STRUCTURAL DAMAGE ASSUMED: Pull speed knob and maintain current lAS Adjust lAS during descent as required
TURBULENCE If turbulent air encountered reduce to turbulence penetration speed if necessary
Qush Speed/Mach 0/b
o display speed mode djust speed during escent as required
l]illl13 Rev.l4 • PRO-ABN-80 o 3.02.80 ... u--·27.May 2oi21
+A320 +A330 +A340 EMERGENCY DESCENT
RECOVERY & LANDING PREPARATION
VERIFY
- ~ i DESCENT • DESCENT i . . . ~ STABILIZED: •... STABILIZED ! : .
PF: •.. PNF: ••
12. Advise A TC of position • • • and intention • • •
13. Inform cabin crew and • • • passengers of the situation • • •
8. Review QRH ABN-80
. 14. Contact company or relay situation • • • .
;·:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::~.!~·~·::::::::::::::::::::::::::::::::::::::::::::::::::::::::::::.! .. .. .... ............... .. .............................................. .... ... ......... ..................... .. ........ .. .. ...... .. ......... .. .......... .. .................... .
[ APPROACHING TARGET ALTITUDE: •... APPROACHING TARGET ALTITUDE: : ... : PF: • •• : . PNF: i ••• ~ 15.1000 feet above target altitude: retract speed brakes •... 9. Call out approaching 14000 feet l 16. 500 feet above target altitude: set target or managed speed •... ' 10. Call out 2000, 1000 and 500 feet before target altitude l 17. At target altitude announce: " Passengers & crew remove masks" • • ' 11 . Review QRH and reset systems as required j 18. Check cabin situation l 19. Reset systems (QRH) CRUISE: Refer to QRH FPE-CAB In flight performance ! -............._ FCOM PRO-SP0-20 Flight w/o Cabin Pressurization ............................................................... ......................... ........................................................... ............................................................................ ........
Note: • Manually deploy passenger oxygen masks only when cabin altitude exceeds 14,000 feet • Cabin 02 generators can supply pure oxygen under positive pressure for 22 minutes • With cockpit 02 diluter set to Normal, 02 supply is at least 15 minutes • Oxygen supply can be extended by selecting 02 mask diluter selector to N position • When descent is established and time permits, check the outflow valve position on the
cabin pressure ECAM page: - if closed, pressurization is uncontrollable - if not closed, and differential pressure is positive, select manual control and set the VIS
• During descent there will be an ECAM warning "CABIN PRESS SAFETY VALVE OPEN" -clear the warnina- ECAM actions disolaved (decreased VIS) cannot be aoolied
• To expedite descent, landing gear may be extended rA320 below FL 250 -reduce speed to VLONLE first lt\3301A340 below FL 210
• A3301A340: An ECAM "Pack 2 fault" message merely calls for a computer reset - reset CPC 2 (QRH ABN-80.21)
• During descent below 10,000 feet, maintain a maximum descent rate of 1000 fpm for passenger & crew comfort due to the unpressurized cabin.
toggle switch to full down (FCOM PRO-SP0-20)
,.,_
r··~~~-~·;~~·-~~-~~~~~~;;~·~~-~·~~~·ss~~·;~~~··~·~ ·~·G·~~;·· ... j • TOD=Aititude x 6; descend at approximately 500 fpm
: ................................................... .................................... ................................ ... ........... :
QW114 Rev.12 • PRO-ABN-80 o 3.02.80 uu27MaYib121
+A320 +A330 +A340 @ ENGINE FAILURE AFTER Vl • CONTINUED TAKEOFF •
) ))) (1)
After V1: "ENGINE FAILURE" CM1 : "GO!"
Note: PNF to call out engine failure without identifying which engine has failed
••
0 p target will appear after liftoff
PF: Set p target to neutral w/ rudder When able, set rudder trim Control heading with bank angle
PNF: Inform ATC
PF option: If Flex T/0 used, consider applying TOGA power for climb performance. Increased thrust may cause directional difficulties at light weight & low speed
Setting TOGA thrust when out of SRS mode with slats extended will trigger the GO AROUND mode.
Takeoff thrust (FLEX or TOGA) must be kept until Green Dot spedd is reached, limited to 10 minutes (5 minutes under (FAR)
On DERATED takeoff (operator option), do not use TOGA thrust if speed is below Fin CONF 2 or CONF 3.
0 VR Rotate to 12.5° NU
After liftoff, follow SRS Control direction with rudder
Note: Rotation rate is lower due to reduced power. Acceleration is also reduced.
~~ .. .
~ / D
E'@=®W)
0 Positive climb & increasing RA:
"GEAR UP" Note: With cycling of gear doors drag
will momentarily increase. Adjust pitch to minimize speed loss.
lifl•l11- Rev.26 • PRO-ABN-10 o 3.02.10 02 Jul 20111 49
+A320 +A330 +A340
0 Priority must be given to the control of aircraft trajectory.
Once the PF has stabilized the flight path , at a minimum of 400 feet AGL the PNF confirms the failure and the PF commands "ECAM ACTION".
. -~ .
" -. -10--10 ~
-:~ ·-. .. 10--=--10 __ <>_·_·_
Note: RA figure changes from large amber font to smaller green font at 400 feet RA
PF: Retard thrust lever PNF: Switch off engine master
ECAM actions can be stopped at any time on PF request for trajectory, configuration and other essential PNF assistance
There must be no movement of: • thrust lever • engine master switch • fire push button
without confirmation from PF & PNF
® ENGINE FAILURE AFTER Vl §} ~
• AGL;::: 100 FEET • ~~ -~~ . {f[Q)of&J§)
CD
0 With 100 feet minimum RA & aircraft stabilized, PF may use AP to reduce workload
' If turn is required: "PULL HEADING _ .. Follow AP or FD order With no AP/FD, limit bank to 15°
up to F, S Green dot
->Bank angle is limited to15o up to [maneuvering speed -10 kts] -> then linear increase to 25° up to [maneuvering speed - 3 kts] -> 25° above {maneuvering speed - 3 kts]
1Jli112 Rev.28 • PRO-ABN-10 o 3.02.10 20 Nov 20121 50
+A320 +A330 +A340
0 Priority must be given to the control of aircraft trajectory.
Once the PF has stabilized the flight path, at a minimum of 400 feet AGL the PNF confirms the failure and the PF commands "ECAM ACTION".
- v
~ , 1o-=-1o ' ~<
.. --:f -- '•
10---10 ·..:_!::._
Note: RA figure changes from large amber font to smaller green font at 400 feet RA
PF: Retard thrust lever PNF: Switch off engine master
ECAM actions can be stopped at any time on PF request for trajectory, configuration and other essential PNF assistance
There must be no movement of: • thrust lever • engine master switch • fire push button
without confirmation from PF & PNF
® ENGINE FAILURE AFTER Vl • AGL ~ 100 FEET •
CD
® With 100 feet minimum RA & aircraft stabilized, PF may use AP to reduce workload
' If turn is required: "PULL HEADING _ " Follow AP or FD order With no AP/FD, limit bank to 15°
up to F, S Green dot
->Bank angle is limited to15o up to (maneuvering speed -10 kts] -> then linear increase to 25° up to [maneuvering speed - 3 kts] -> 25° above (maneuvering speed - 3 kts]
§] ----/]i§)o@~
lfi•Jf2 Rev.28 • PRO - ABN - 10 o 3.02.10 20 UNnv?nnl
+A320 +A330 +A340 © ENGINE FAILURE AFTER Vl ~ _,.
• ACCELERATION & CLEANUP • /][p)c(§fg§)
The flight crew should secure the engine before initiating acceleration. An engine is considered as secured when the ECAM actions of the procedures are performed until:
PF: "F SPEED - FLAPS 1" • "ENG MASTER OFF" for an engine
failure without damage [:;\ "S SPEED - FLAPS 0"
• "AGENT 1 DISCH" for an engine failure with damage
When conditions are met, PNF to announce:
\V When flaps at 0:
• Fire extinguished or "AGENT 2 DISCH" for an engine fire . "ENGINE SECURED"
------~ .... ---· ~
~ 0
ENGINE OUT ACCELERATION AL Tl TUDE
® At 100 feet before acceleration altitude (approximately1 0% of VSI):
A320: "PUSH TO LEVEL OFF" A330/A340: "ALTITUDE HOLD"
"CONTINUE ECAM"
When flaps at 0, f3 target reverts to sideslip indicator
~ ~
0 • If further altitude change is
required . set target altitude
• Approaching green dot (speed trend arrow touches green dot) or approach config:
• Pull or push altitude knob • Thrust lever to MGT
(select OP CLB before setting MCT, or else power will reduce to maintain green dot speed)
Approaching engine out acceleration altitude:
Pitch attitude & rudder requirement will reduce Cleanup to flaps zero
"STOP ECAM" - or, if making an immediate reland: Maintain flaps 1 (option) "ACTIVATE APROACH"
'{}$If the decision has been taken to delay the acceleration, the flight crew must not exceed the engine out maximum acceleration altitude.
The engine out maximum acceleration altitude corresponds to the maximum altitude that can be achieved with one engine out and the other engine(s) operating at takeoff thrust within the maximum time limit
(JAR: 10 minutes; FAA 5 minutes)
The altitude can be obtained from the LPC NG & from RTOW charts.
•••••••••••••••••••••••••••••••••••••••••••••••••• NOTE:
Consider engine damaged if: - loud noise I explosion was detected - high engine vibration prior to flameout - repeated or uncontrollable engine stalls - abnormal engine indications on ECAM (e.g. N1 or N2 near zero
In any of these cases do not attempt engine relight ~ ........................•.......................• :
IJ1il13 Rev.25 • PRO-ABN - 19 o 3.92.19 22Janu2of3)
+ @ ENGINE FAILURE AFTER Vl m;m '~ +A320 +A330 A340 • COMPLETION OF ECAM ACTIONS • B@o@?JID
,.,.
G) When ECAM on Status page:
PNF: "STATUS PAGE" PF: "STANDBY STATUS, AFTER TAKEOFF/CLIMB CHECKLIST" PNF: Read checklist PF: "READ STATUS" PNF: Review Status page PF: "REMOVE STATUS" PNF: After clearing status page
"ECAM ACTIONS COMPLETED"
\ ~~ 0
~······················································ • If engine not considered damaged & CM1 decides to attempt a relight:
• complete all ECAM actions • accompish After Takeoff/Climb checklist to the line • ensure gear and flaps retracted • establish safe flight path • consider engine relight reaching the STATUS page
Engine relight in flight: QRH ABN-70 •••••••••••••••••••••••••••••••••••••••••••••••••••••••
1. Check weather at origin/dest.lalternate 2. CM1 announce intention 3. Advise ATC 4. Coordinate with cabin crew 5. Advise passengers (PA} 6. Advise company
lfl•l14 Rev.23 • PRO- ABN - 10 o 3. 02.10 17 Mar 20121
+ @ ENGINE FAILURE AFTER Vl §I _.-+A320 +A330 A340 • COMPLETION OF ECAM ACTIONS • B@c~
.,.,..
G) When ECAM on Status page:
PNF: "STATUS PAGE" PF: "STANDBY STATUS, AFTER TAKEOFF/CLIMB CHECKLIST" PNF: Read checklist · PF: "READ STATUS" PNF: Review Status page PF: "REMOVE STATUS" PNF: After clearing status page
"ECAM ACTIONS COMPLETED"
~ .,~ 0
~······················································ • If engine not considered damaged & CM1 decides to attempt a relight:
• complete all ECAM actions • accompish After Takeoff/Climb checklist to the line • ensure gear and flaps retracted • establish safe flight path • consider engine relight reaching the STATUS page
Engine relight in flight: QRH ABN-70 •••••••••••••••••••••••••••••••••••••••••••••••••••••••
1. Check weather at origin/dest./alternate 2. CM1 announce intention 3. Advise ATC 4. Coordinate with cabin crew 5. Advise passengers (PA) 6. Advise company
ifl•l14 Rev.23 j PRO-ABN-10 o 3. 02.10 ) 17 Mar 20121
+ ® IMMEDIATE LANDING FOLLOWING ~ +A320 +A330 A340 ENGINE FAILURE ON TAKEOFF · ~-
PF:
1. "ACTIVATE APPROACH PHASE, CONTINUE ECAM"
4. "STANDBY STATUS, AFTER T/0 CLIMB CHECKLIST"
6. "CONTINUE STATUS"
8. "REMOVE STATUS"
0 PNF:
2. SO page cues (options, may be done after ECAM actions are completed):
A320 & A330 : At ELEC page, APU master on A330 & A340: At flaps 3 reminder-highlight CONF3 on MCDU PERF page (A320 CONF FULL}
3. At status page:"ST ATUS"
5. Read After T/0 climb checklist
.. "AFTER TAKEOFF/CLIMB CHECKLIST COMPLETED"
7. Review status page
9. Clear Status page _,. "ECAM ACTIONS COMPLETED" _,. _,. Start APU (for A320/A330,
optional on A340)
~
_,-' _,.
0
_,. _,. ~
Check if QRH overweight landing checklist required QRH ABN 80.06
~ A320/A330:
Set up FMGS for arrival
PF conduct approach briefing then, "APPROACH CHECKLIST"
PNF: When APU AVAIL, bleed on For landing configuration,
refer to QRH ABN-80.01 Approach with One Engine Inoperative
0 Runway in sight: PF-"ZERO MY TRIM AT _ FEET"
~ ~
lfi•JlS Rev.22 JPR.O:ABNU.:.fO CJ 3.02.=10 5--u--------~· 22 Jan 20131
+A320 +A330 +A340
Z2 Engine failure procedure - RPLL 06
CAAP Skill Test Part 2
1. Maintain runway track
2. At 500 feet turn right 240° magnetic heading
3. At 1500 feet AGL level off and accelerate
4. Follow ATC instructions
........
+A320 +A330 +A340 CAAP Skill Test Part 2 ~.·,..........00@--r-.· D _ ___.
Z2 Engine failure procedure - RPLL 06
1. Maintain runway track
2. At 500 feet turn right 240° magnetic heading
3. At 1500 feet AGL level off and accelerate
4. Follow ATC instructions
lmJ14 R-ev.i • PRO-ABN-xx o 3.02.10 - --n 22 Novl 2e121
+A320 +A330 +A340
Y'SEAIR ) DG Engine failure procedure - RPLL 06
CAAP Skill Test Part 2
1.Ciimb on 061 o heading. 2.At 800 feet turn righot to MIA VOR
3. Hold over MIA VOR 113.8 inbound 243°, left turn
~
[]tjU) ...
l~fl•l13 Rev.l .. -~---- ---- ) PRO-ABN::x)( o 3.02.19 J 07 Jul2012l
+A320 +A330 +A340
i;PEEBU PACIFIC Sl Engine failure procedure - RPLL 06
6. An option to hold over Tara may be requested to complete the necessary procedures
CAAP Skill Test Part 2 . @JiW _.......,.
1. Declare an Emergency at the earliest possible time. 2.Turn right heading 150° within 5 nautical miles
3. Accelerate to single engine altitude & clean up
4. Climb to 3000 heet QNH
5. At 3,000 QNH turn right to Tara and request ATC vectors
~
l~f!•lll Rev.l JPRO=A:sN-=-ii-0-3.02.10 -- T 07 Jul2012l
+A320 +A330 +A340
• . •
' .
~~~; -~ :.~~?: ··~~-. ~~'·. ,~ ';:;·,
-', !.'- •~ -~ .!rn : ,.,. ... :;,~ - . ·.n
/ · ,,.,..~ · ~ - ~ -~
-~ 1•r1m.
~ '" - 1 .. 1 H J m-=- G ~· Lt& . ... ~ ..,. ~:: ..
Note chanr~O of nA color from amber to grocn at 400 fool
ECAM 1
DETECTION First pilot who notices:
Master Caution/Warning .. RESET Title of failure ........ .. ANNOUNCE
PF: Fly and Navigate
If failure occurred just after takeoff, no action until 400ft AGL with
safe flight path established
At or above 400ft AGL with safe flight path established: PF order: " .. I have control and communications - ECAM action"
••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• : PF is in charge of all communications until : • •
:. ~If. 9l.t.~~. sR!-).'Y!. ?_q.f!9.'!.~. h~'f~ .i?.f!.f!!?. ~9!!?P.~f!!~?. ~
If the aircraft is not equipped with the OEB reminder function*, the crew should review the applicable OEB(s) before starting any ECAM actions
~ OEB ~ I * FCOM DSC-31-27 -.• ... tV.•I · •• t u ... . lf,.Mio
li(:I•l91 Rev.B • PRO-ABN-01/80 • DSC-31 o 3.02.10 27 May 2012) 63
+A320 +A330 +A340 ECAM 2
PF: PNF ECAM actions ................ PERFORM Request .... CLEAR [name of system]
Confirm ... CLEAR [name of system]
To be repeated for each failure displayed on the ECAM
BOTH PILOTS SHOULD CONFIRM IRREVERSIBLE I GUARDED ACTIONS
6 AGfMI ENG 1 AGEN1'2
l rl:!;]~~~ ~ TEST 0 FIRE 01 00
If a system page is displayed on the lower ECAM screen:
PF: PNF System page displayed ........... ANALYZE
~:::: ~ 1., .. .. 1·w .. ., •• ) Request .......... CLEAR [name of system]? System display .............................. CLEAR
Confirm ... CLEAR [name of system]
li:I•192. Rev.4 • PRO-ABN-01/80 • DSC-31 o 3.02.10 27 May 20121 64
+A320 +A330 +A340
When STATUS page appears
3 Read STATUS page
TAT •17 •c r- IGH SAT •11 ·c I 16 11 15
ECAM 3
QRH NCL.CJ
I GAif!BUS 'I n ~~.~ .. - -~ ~-~ , .•.. ,
-· - .. ~1·-· Jl ·-- -- = .._
~r,o- -- __ , """'" ... WRPMnto.1.AI ,_ -'""""""" Tti[)I.Tl ........
"""'-"'
""""' ;:~
Normal 1 I checklist
sn eon-- -., .Ofll
""""' t.t'Ve( t
5'ft!Xl"
""""' ""'"'
~
QRH 80.14/15
, ~- .... ___ u~ r----- ........ LA.. 1
so.1fl L~ QIOQENCYPAOCXOtMI:t ~·1
c=~- fltMVI(JI - T I ...., • ...,._......,.~ ••otMtlr*""~v-. h()pp:oilor
ur-n--~"•""'~"..,...""flf••~ .......... -~-- .... ........,._ ... _..._.IOIII'NI_flll __ _ ==..._..w_,_,. .,..,...,ew•-..-••.,...,._,..
C t ~~-2 1 ompu er -- ~~ ~~-·-reset _
[ .......... ---- ........ 1 - ~~0~~ I
- --~ ~&~~
LDG DOS1' PROC -·· APPl. Y If required, obtain VAPP I ECAM 4) & actual landing distance
fiCAEAIED FUB.. CUN8U1W"
QRH FPE-FPF
!Afl~ -~~-- 00 F\JfJ. IEIW.TY FACTOAS.ICAM Alfln' TMll 1
Refer to the FUEL PENALTY FACTORS/ECAM ALERT TABLE in order to assess the impact of the failure on the fuel consumption after any ECAM alert that: U Displays the line INCREASED FUEL CONSUMP in the STATUS SO page, or n Displays Flight Control Surfaces in the INOP SYS, or u Impacts the Landing Gears or Landing Gear Doors retraction (when extended).
1]5Ii193 Rev.S • PRO-ABN-91/89 • DSC-31 o 3.02.10 - -- u---2 0 Nov2.5TIJ 65
+A320 +A330 +A340 + A380 ECAM4
Use the RCAM to assess the braking action
IC FUOHT PBIFOIIMo\Na:
RUNWAY CONDITION ASSESSMENT MATRIX FOR LANDING
2 Determine V REF
1
$ AIR:=l II I'UOKI' IUIUIUNCE l ~~M I ...,.o118M'J&,.,. IOW.Ytl
VAPP DETERMINATION WITH FAIWRE
r;-..,;-:-~, • / Nf/IE.I •IJWt~
I - -. .. -~~.;..-~ -~-------=:l
+
Compute Approactr ..... G'orrection, vAPP
& Landing Distance Correction
• WAPPRCCA• til t~~ CMWIIM..,... ....,_lUG QMI..IM) .. .., •..-oc.
•• ,..,(lOA .. . ,..........,~
...... ...._~ ..... ~0...--
,., ... ,....,.....ut.,........,....,... .. .,...v,., ..... ...... II!Mofi_.~.,M"'OQIIIVI'¥ti:M~.....,..,.,.....,. .NIA .. .._..,...r~ta..nlfW!Io..ndhl.....,...,...._WM. H...., .. .._ ................
3 Locate: 1) Aircraft system 2) Braking action 3) Failure title 4) Flap lever position
for landing Obtain 11VReF
IN fliGHT P£AFORIIAtcE
5 Calculate the Landing Distance
lj'W194 Rev.4 • PRO-ABN-80 o 3 . 02 . 80 15Nov 2cn2J 66
+A320 +A330+A340
(!) IF TIME PERMITS ...
CheckQRH &FCOM
Crew briefing
.:::=:.~:":- ~·: ~
~ .. ·~ l rE!J-11 ~\ ~- .. !..!.!. til,.. •c
r.r:~ r;r:~ I'"' ....... l r~' l 'g' l laJ , ,1 ~ ,
10-~--?U :~ • Jtoo-~ .. -,.so • 3 :
. S-EAT Bt:lTS ·~ : NO S!.IOKINO llANU />!jAJ> .................. ............
~~~ "' ····· JJ
SfATUS
MlPI , . ,,.,,. ,, , ,lX)I ,U
.Wtll'fiOC..._ Int LO I't ----:l'J"'').f CJ,Kf W' 1
1JA: C.l t ......... . .. . . . CI!
-4/G . . ... .. ... .,. IIIN'tYiltl'llt -uc Cf'III I:'CIIO' • •• •• , ... KICI' -tte•ru .... .. ...... . .• ,.., W I CII..f UII!UII
~tlltlf:Oit lil'l R ),.W.U
z:r: ''=tl ·~\~,
STAl US
M.t vt .. .... . . .. .. 2'() 1.1'
~ , .. , '"" I.MtlU. SPUtl• Jot ' L lllV lf'l•l
""""'' -... ,... ~-,OD;C~
CN \U(I)fo:~
~ IIPft't«WIII. II'tt i O Jioll r~ ---:trlD.eOUtf fN" r lot l U
1lJ,f iC..[( ~ .. ...... .CJ. ; I"UUh)t~
'(." , .... . ..... .. toWn D:ne L lllY 'i.JICft i'«MJJ. . . . . .. . .. IXf .,., 1..M ~ 111 .. ... . . ....... 1 lA =-= t
(AI 1M.' ..... ... ~(Allf!O.
tiN l.t l ' M.L'
u: ~ ·~ :f 1
Ml llRA
JJ-,,.(OCI ~:9!:t~·-~1
ECAM 5
SLATS I FLAPS
~ .... •·· .. ~ &
LANDt<GGEAA
llliF."' n RUDDER
TRIM
~
• Approach checklist [!:~~~ _WAL,.CClOOA£1 ~
"" """'- Jl ·- - ·--IITOII
~- COiol-~---···· C<llnlOI
GOA r94 .-.: <XMH5. AU4"'l0 ~<XD KNS <~t•1fo . "" _ ill !WI ~ ~ • 1\A ~ ~I QIA.'Itl1Y ( t'il fl _ SfTMr-Q
'>11710 IOt"AfA. .... ,,. .. ........ """"' ..._, t.ll .... • lil.l 4~ Fffi)()Jf ""'"' "'11._.,.. """"'I
' IIQAJ AIJIC.IAn_, ___ ,_ ~A>"' 'C.AUI&W t fV"'
Other checklists as required
$ AIIlBUS
LOO COIIF .... ~ :I
~ tAl
ABNORIIAL AND ENEAOENCY PROCEOURf.S
OVERWEIGHT LANDING
ABNORMAL AND EIWIGENCY PIIOCEDURES
HYO II • Y SY! lO 'fl SIJMMoUIY
~~~~~~ ABNORMAL AND M RG[ljCY PIIOC EDURES
tU C UIEA COHJIQ SUI&UAY
""' ""' "1.111\.AW PfiOHOSl Cfl.'f CAPT IInDT A.'() a.ol HeATED IU( L : Cl'A Tit lJI'AIS.Aat: co .. : .,..,, ,n;, ,.,ltlrf, HAY: 1.'1 Y!Jff i.O P'JH~ I •• MUt,.,.~l~
1 ~4.02 y,l#'f/411
... l.'OKT
[.-ntoat t I ... I ~ I • I R I W i eo l tc i .. I ':'Z I 't ) -. 1 r;o..- ' ~ · ru• 1 n• r ·~· 1 ~ 1 .... , ... 1 •• I 111 1 * 1 .... 1
lij:lt]9S Rev) • PRO- ABN -91/80 • DSC - 31 o 3.02.10 mn n. n--28 May 20f2) 67
+A320 +A330 +A340 + A380
.. • • • • • • • • • • • •• • • • • • • ••• • ••• .. , .. ,
lit. •••
• FMGS preparation • Briefing • Approach checklist • Entry to holding
~ CAAP Skill Test Part 1 [@)r:l§f!lf§)
Wind shear •••••••••••••••••••••••••••••••••••••••••••••••••••
ALTITUDE
• Height Generally .... . ... .. ........ ...... .. .... .... .. . ± 100 feet • Starting a go-around at decision height ... + 50 feet I -0 feet • Minimum descent height/ altitude ............ + 50 feet I -0 feet • Tracking on radio aids .... ... .. .................... ± s· • Precision approach .. ......... ... .. .......... ......... Half scale deflection,
azimuth & glide path
HEADING
• All engines operating ±50 • With simulated engine failure ± 10°
SPEED
• All engines operating .. ............... ............... ± 5 knots • With simulated engine failure ......... .. ........ .. + 10 knots / -5 knots
• •••••••••••••••••••••••••••••••••••••••••••••••••••
Failure: Loss of dual FMGS
or dual FCU
Medical emergency or airport closure
Dlc~ +A320 +A330 +A340 + A380 ECAM4 ,__.
1 Use the RCAM to assess the braking action
~!!!!'l! IN FUOHT PERFORMANCE
RUNWAY CONDITION ASSESSMENT MATRIX FOR LANDING
2 Determine VREF
~RBUSL IHl.GHT~RFORMAICE ~~ oacc,....&_ 30W.Y1Z
I VAPP DETERMINATION WITH FAIWRE I
W-fTI ..., t\UCOUJ~W(W.
[ v.,..\ltl:f:, •f.Yfllll' · A.fl'f"lt~
Compute Approactr--"G.cfrrection,VAPP & Landing Distance Correction
3 Locate: 1) Aircraft system 2) Braking action 3) Failure title 4) Flap lever position
for landing Obtain 6 VREF
IN FUGKT PERFORMANCE
5 Calculate the Landing Distance
Mt .... ,...~...., .................. ..,...._._v,.,..IM ....,.. .. ~~~"ii"'V~-~ ...... ~ WKIA•~WitNSI'rJ~afhl .... ~WM. do"'l ... ,., .................... ..,......
lji:!t)94Rev.4 • PRO-ABN-80 o 3. 02.80 1Sul'i6v2012l
+A320 +A330 +A340 + A380
... • • • • • • • • • • • ••••••• • ••• • ••• •• •• •• # lit. ~ ••
• FMGS preparation • Briefing • Approach checklist • Entry to holding
CAAP Skill Test Part 1 ~ !J:@o~
Wind shear •••••••••••••••••••••••••••••••••••••••••••••••••••
ALTITUDE
• Height Generally .. ... .. . ... .... ..... ... .. . . .. .. ...... ± 100 feet • Starting a go~around at decision height ... + 50 feet I -0 feet • Minimum descent heighV altitude ... .. ... .... + 50 feet I -0 feet • Tracking on radio aids ... ... .. ... ........... ... .... ± 5° • Precision approach ....................... ............ Half scale deflection,
azimuth & glide path
HEADING
• All engines operating ....... .. • With simulated engine failure
SPEED
±50 ± 10°
• All engines operating ...... .. ......... ..... .... ...... ± 5 knots • With simulated engine failure ............ ........ . + 10 knots I -5 knots
• •••••••••••••••••••••••••••••••••••••••••••••••••••
Failure: Loss of dual FMGS
or dual FCU
Medical emergency or airport closure
t;f!•]lO Rev.l ) PRO-ABN-xx o 3.02.10 ;--------- 19Dec2012l