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+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 AIRB R 360 @

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Page 1: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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 @

Page 2: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 3: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 4: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

~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

Page 5: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

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

Page 6: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 7: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 8: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

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

Page 9: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 10: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 11: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

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+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

Page 13: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

Page 14: Synthetic Flight Trainer lNG GUIDE -FLIGHT …sharepoint.aag.ph/portal/Downloads/Synthetic Flight Trainer.pdf · +A320 +A330 +A340 + A380 Synthetic Flight Trainer lNG GUIDE -FLIGHT

+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

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+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

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+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

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+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

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+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.

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+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

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+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

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+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

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+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

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+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

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+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)

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+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

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+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

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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

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+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

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+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

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+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

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+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

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+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

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+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

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+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

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+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)

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+ @ 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

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+ @ 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

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+ ® 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

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+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

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........

+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

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+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

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+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

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+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

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+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

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+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

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+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

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+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

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+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

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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

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+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