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CCQ A320 TO A380 COURSE

TABLE OF CONTENTS

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02.00

02.01 - INTRODUCTION

02.02 - TRAINING FOOTPRINT

02.03 - GROUND PHASE

CCQ MFTD A syllabus .............................................................Page 1CCQ MFTD 1 syllabus .............................................................Page 3CCQ MFTD 2 syllabus .............................................................Page 5CCQ MFTD 3 syllabus .............................................................Page 7

02.04 - HANDLING PHASE

CCQ FFS 1 syllabus ................................................................Page 1CCQ FFS 2 syllabus ................................................................Page 3CCQ FFS 3 syllabus .................................................................Page 5CCQ FFS 4 syllabus .................................................................Page 7


FLIGHT CREW TRAINING PROGRAM MAY 2008Issue 04

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FLIGHT CREW TRAINING PROGRAM NOV 2007Issue 03

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02.01INTRODUCTION

01 - GENERAL

A. PHILOSOPHY OF THE COURSES

This course is designed for qualified pilots to transition from the Airbus single aisle “Fly-by-Wire” aircraft (A320) to the A380 aircraft.This course only addresses the differences in procedures and handling characteristics between the base aircraft (A320) and the difference aircraft (A380).However, the ground school includes full systems study using CBT.

B. REGULATION REQUIREMENTS

They are listed in the following document :- JAR-FCL - JAR-OPS- FAR 121 - FAR 142- FAA Advisory Circular : AC 120.53- JAA / FAA / Transport Canada : Common Procedures Document

The differences between the base and the difference aircraft are published in the Operator Difference Requirement (ODR) tables approved by FAA/JAA.Airbus course is based on generic ODR tables published by the manufacturer.

C. PREREQUISITES

• Valid and current ATPL• Qualified on the base aircraft• Minimum of 3 months of operation on the base aircraft• Minimum of 150 flight hours on the base aircraft

IMPORTANT : Pilots entering this course must be highly knowledgeable on base aircraft systems.

02 - COURSE ORGANISATION

A. COURSE DESCRIPTION

a) GeneralThe CCQ training is divided into four different phases:

- Ground phase- Handling phase- Skill test - Base training or ZFTT

A welcome, which takes place before the starting of the course, includes the training center presentation, all administrative issues and the distribution of all training supports that will be used by the trainee.The reference airport used during most of the sessions is a generic airport called Airbus Training Airport.

b) Ground phaseCBT:

The aircraft systems study is progressively introduced during the first 8 days and is carried out in a classroom.


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INTRODUCTION

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The acquired knowledge will be reinforced with the use of the Maintenance and Flight Training Device (MFTD).The CBT is not defined to cover aircraft differences only: however, part of some systems is common to A320 and A380.

MFTD: The MFTD is used to reinforce the systems knowledge acquired in the CBT and to study the new SOP’s or major differences between the A320 and A380 (in normal and abnor-mal operations).Sessions are prepared by the trainee using the trainee’s booklet, FCOM, Flight Crew Training Manual (FCTM) and Procedure Data Package (PDP).Questions and answers are part of the session and will be addressed before or during the session.The PDP will be presented at the instructor discretion to either refresh the procedures common to both aircraft or to introduce new procedures related to the A380.

OIS / Performance:One full day is dedicated to Onboard Information System (OIS) presentation and to per-formance computation using the different applications.

Cabin:Doors and slides operations are conducted in a specific Cabin Trainer device.

Systems test:At the end of the ground phase the acquired knowledge will be evaluated using an elec-tronic test based on a randomized questionnaire.

c) Handling phaseThis phase conducted in the FFS is mostly dedicated to aircraft handling in Normal and Abnormal operations.All the differences listed in the approved Operator Difference Requirement (ODR) tables will be covered during this phase as well as some exercises common to both A320 and A380.

d) Skill test The skill test is defined according to the JAA requirements : for the time being, it is not a skill test that only covers the differences.

e) Base training or ZFTTAircraft training (Flight 0:45 h / pilot)ORZFTT (FFS 4:00 h / Crew)

FLIGHT CREW TRAINING PROGRAM FEB 2009Issue 05

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B. TRAINING DOCUMENTATION

DOCUMENTATION USER GUIDE A380The following documentation is given to you on the day of your arrival at the CBT room and will be used throughout the course.Training documentation is not updated therefore FCOM remains the reference

LAPTOP / DVD CONTENT

LAPTOP (HARD DISK)

-FOA (Flight Ops Applications): FOCT (Flight Ops Con-sultation Tool) and Performance Applications-WALK AROUND 3D-AIRBUS TRAINING AIRPORT JEPPESEN CHARTS

DVD1Per Aircraft / Engine / Unit

(To be given)

-STANDARD TRANSITION COURSE (Footprint) -CCQs TO A380-FAM BRIEF A380 RR TO A380 EA-FAM BRIEF A380 EA TO A380 RR-COMPUTER BASED TRAINING (CBT)-QUIZZ-PROCEDURE DATA PACKAGE (PDP)-BRIEFING GUIDES (BG)-OIS AND PERFORMANCE COURSE-CEET (CABIN EMERGENCY EXIT TRAINING)-PRE-FANS-FANS A-TCAS II COURSE-AIRBUS REFERENCE LANGUAGE (ARL)-AIRBUS OPERATIONAL EXPERTISE-FLIGHT OPERATIONS BRIEFING NOTES

DVD2VIDEO BRIEFINGS

(To be given)

-CFIT-REJECTED TAKE OFF-UPSET RECOVERY-COCKPIT DOORS

PAPER CONTENT

TRAINEE’S BOOKLET(extract of FCTP:

Flight Crew Training Program)

-RELEVANT CREW COURSE -BASE TRAINING SYLLABI-Set of 4 coloured cockpit panels

TASK SHARING AND CALLOUTS -Extracts from FCOM SOP’s and FCTM STANDARD CALLOUTS

ACTION FLOWS -"PF and PNF action flows" from PDP/FCTM

A380 JEPPESEN LEAFLET -Airbus Training Airport, Lyon Airport, Paris Orly Airport charts

Extract of QRH(Quick Reference Handbook) -SMOKE and EVACUATION procedures


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C. INSTRUCTOR BRIEFINGS

D. CRITERIA OF PROFICIENCY

1) SYSTEMS

a. Evaluation during CBT Phase :

On completion of this phase, a written multiple choice examination will be completed. The minimum level required, to be declared proficient, is determined by the Airline, but is never below 80%.

b. Unsatisfactory Examination :

Corrective action using the CBT will be determined by the instructor in coordination with Airbus Training Director. The student will then undertake a CBT examination.

2) MFTD / FFS NOTATIONS

Three boxes are used to record the overall trainee’s performance using “Trainee’s Record” file (see Page 3).They are quoted “Satisfactory”, “May need extra training” or “Unsatisfactory”

• When “Satisfactory” box is ticked:----> no specific comments are needed : “None” written indication is required. Nevertheless, comments may be made at instructor’s discretion.

• When both “Satisfactory” and “May need extra training” boxes are ticked ----> comments are required, and the following session must be assessed as :

- “Satisfactory” ----> comments must confirm improvements: OR - “Unsatisfactory”

When “Unsatisfactory” box is ticked :

----> use the specific Progress Incident Report (PIR) (see Page 9) to list and comment the trainee’s difficulties as well as the number of additional training sessions requested. It must be reported without delay to Airbus Director of Training.

Additional training sessions (see Page 10) have to be commented and use the same identification as the session involved.

Session Briefing DebriefingMFTD A No No

MFTD 1-2-3 Questions & Answers are included

FFS 1:30 0:30

Skill test 1:00 As required


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E. CRITERIA OF PROFICIENCY

1) SYSTEMS / PERFORMANCE

a. Evaluation during CBT Phase :

On completion of this phase, a written multiple choice examination will be completed. The minimum level required, to be declared proficient, is determined by the Airline, but is never below 80%.

b. Unsatisfactory Examination :

Corrective action using the CBT will be determined by the instructor in coordination with Airbus Training Director. The student will then undertake a CBT examination.

2) MFTD / FFS NOTATIONS

Three boxes are used to record the overall trainee’s performance using “Trainee’s Record” file (see Page 3).They are quoted “Satisfactory”, “May need extra training” or “Unsatisfactory”

• When “Satisfactory” box is ticked ( ) :----> no specific comments are needed : “None” written indication is required. Nevertheless, comments may be made at instructor’s discretion.

• When both “Satisfactory” and “May need extra training” boxes are ticked ----> comments are required ( ), and the following session must be assessed as :

- “Satisfactory” ----> comments must confirm improvements ( ) : OR - “Unsatisfactory”

When “Unsatisfactory” box is ticked ( ) :----> use the specific Progress Incident Report (PIR) (see ) to list and comment the trainee’s difficulties as well as the number of additional training sessions requested ( ). It must be reported without delay to Airbus Director of Training.

Additional training sessions (see Page 8) have to be commented and use the same identification as the session involved ( ).

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TRAINING FOOTPRINT

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02.02TRAINING FOOTPRINT

01 - TRAINING DEVICE TIME SHARING PER PHASE

N.B. : 1) Except when notified, the allocated time is mentioned in hour/crew2) Welcome is not part of the training footprint and is completed the day before the beginning

of ground school : all the documentation and training supports will be handled to the trainees during the welcome briefing.

Note: If translator is required, CBT and SYSTEM TEST will be Projected CBT with instructor: the ground school duration must be adapted.

Total working days 13 working days

GROUND PHASE 8 working days

• CBT : - Aircraft systems study 30:40 - Systems test 4:00

• Cabin trainer 1:00 • OIS / Performance course 5:00• MFTD A session .................................................. 1 2:00 • MFTD 1-2-3 sessions .......................................... 3 12:00

HANDLING PHASE 4 working days

• Briefing & Debriefing (4 x 2:00)............................. 4 8:00• FFS session (4 x 4:00).......................................... 4 16:00

SKILL TEST PHASE 1 working day

• Briefing & Debriefing (1 x 1:30)............................. 1 1:30• FFS session (1 x 4:00).......................................... 1 4:00

BASE TRAINING PHASE 1 working day

• Aircraft Flight......................................................... 1 or• FFS session (ZFTT) if applicable.......................... 1

Minimum 0:45/trainee

4:00 / crew


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TRAINING FOOTPRINT

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02.02

02 - TRAINING DAILY FOOTPRINTNote: Timing is given for information: your rate of progress could be different from the standard one, however make sure that the systems study associated to one day has been completed before the next day.Day 0: Administration 1:00 - Welcome briefing: 1:30 - Electronic documentation: 1:00

Day 1 Day 2 Day 3 Day 4 Day 5

- How to use (ATA 00) 0:10- Aircraft general (ATA 20) 0:20- Indicating & Recording (ATA 31) 2:40- Auto flight(ATA 22) 3:30

- Auto flight (ATA 22) 1:00- Avionics Networks(ATA 42) 1:00 - Electrical (ATA 24) 1:20- APU (ATA 49) 0:15- Pneumatic (ATA 36) 0:50- Power plant (ATA 70) 0:55

MFTD A (2:00)

- Hydraulic system (ATA 29) 1:00- Flight Controls (ATA 27) 2:30- Landing gear (ATA 32) 2:00- Information systems (ATA 46) 1:30

- Fire and Smoke protection (ATA 26) 0:35- Lights (ATA 33) 0:25- E-logbook 0:40

OIS & Performance

(5:00)

- Fuel system (ATA 28) 3:20

MFTD 1(4:00)

Day 6 Day 7 Day 8 Day 9 Day 10

- Navigation (ATA 34) 2:20- Communication (ATA 23) 0:30- Operating limitations 0:20

MFTD 2 (4:00)

- Air conditioning / Pressurization / Ventilation (ATA 21) 1:55- Ice and Rain Protection (ATA 30) 0:20- Oxygen (ATA 35) 0:10- Cabin presentation (ATA 25) 0:25

MFTD 3 (4:00)

- Doors / Windows (ATA 52) 0:30- CEET (SAFETY) 1:00

Cabin Trainer(1:00)

System Test (4:00)

FFS 1(4:00)

FFS 2(4:00)

Day 11 Day 12 Day 13

FFS 3(4:00) FFS 4

(4:00)

Walk around 3D (1:30)

Skill Test(4:00)

Base Training (0:45 / trainee) or ZFTT (FFS : 4:00 / crew) if applicable


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02.03CCQ A320 TO A380 COURSE

GROUND PHASE L FQE

E

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WEATHER LFZZ CALM 9999 13/12 1013 LFLL CALM 9999 10/8 1013

ACTIVE / INIT

FLT NBR A/L ID 101

FROM LFZZ TO LFLL ALTN LFZZ

CPNY RTE AIBLYS

ALTN RTE LYSAIB

CRZ FL FL 110 CRZ TEMP - 7°C

CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : REFER CO ROUTE AIR COND ON (SID ONZON 1N) ANTI ICE OFF PAX NUMBER : 303

RR Trent 972 EA GP 7272

ACTIVE / PERFLFZZ 33R / GW 385 t


V1 126 TOGA V1 125 TOGA

VR 128 v FLEX 56 VR 125 v FLEX 56

V2 135 DERATED V2 132 DERATED

FLAPS 3 THS FOR FLAPS 3 THS FOR

ACTIVE / PERF ACTIVE / PERF

V1 TOGA V1 TOGA

VR FLEX VR FLEX

V2 DERATED V2 DERATED

FLAPS THS FOR FLAPS THS FOR

Time EVENTS

INIT TAKE OFF - LFZZ 33R - GW 385 tCo-route AIBLYS

REFER TO SESSION GUIDE


MFTD A (COCKPIT AND SYSTEMS PRESENTATION)

FEB 2009Issue 05

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02.03

01 - SESSION OBJECTIVE :

• To demonstrate the use of the training device.• To present a general view of the cockpit including flight instruments and major aircraft

systems controls and indications.• To present the Less Paper Cockpit philosophy

MFTD A : COCKPIT AND SYSTEMS PRESENTATION


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MFTD INITIALIZATION :• The instructor completes the MFTD set up. • INIT TAKE OFF at Airbus Airport

External power 2 and 3 : ONAPU running (APU Bleed ON)Doors closed and slides armedFMS loaded

SESSION GUIDE :NOTE :Do not explain Airbus aircraft systems but present the following according to thetrainee's aeronautical background by introducing the Airbus cockpit philosophy.Remember that, at this stage, the trainee did not study all aircraft systems.

A. TOUCHING ZONES : (IOS facilities)

Demonstrate the use of :- Push buttons and rotary knobs,- Engine master levers,- Ground spoilers,- Flaps,- External lights.

Notify the crew that it is not possible to use two touching zones at the same time.

B. COCKPIT GENERAL PRESENTATION (based on the cockpit preparation) :

- Overhead panel : Lights out philosophy / color coding / pushbuttons philosophy- Center instruments panels- Pedestal : KCCU and MFD (covered in the FMS sessions)- Glareshield : attention getters / FCU (AFS + EFIS control panels) : Highlight the wording

used by pilot which is AFS CP or EFIS CP. FCU is not used (except FCU BACKUP) and is a generic term designating the entire interface.

C. FMS :

MFD + KCCU : show only that KCCU is the unit to use for interaction on pages displayed onMFD (Multi Function Display). Explain that KCCU doesn’t interact with ECAM only ECP cando it.

D. OIS :- Less paper cockpit philosophy- FLT OPS STS- FLT OPS Menu

• T.O. PERF• LOAD SHEET• LDG PERF• IN-FLT PERF• OPS LIBRARY

- Don’t explain all the applications: this will be done during the Performance course.

MFTD A : SESSION GUIDE

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E. CDS (Control and Display System) presentation8 DUs (4 EFIS, 2 ECAM, 2 MFD)For the following demonstration use the CBT mode (Controls and Indicators) through the IOSbut do not enter in the yellow explanation boxes.

- EFISPFD : Flight parameters + memos (3 lines max) and limitations (8 lines max displaying limitations that have a direct impact on A/C flight performances)

ND : Flight navigation information + vertical display zone

- ECAME/WD : engine primary parameters + bottom part :

- Normal C/L (requested by the flight crew via the ECP)- Abnormal and emergency procedures (requested by the flight crew via the ECP)- Alerts- Limitations (left column : ALL PHASES / right column : APPR & LDG)- Memos (left column : TO and LDG memos / right column : all other memos)

SD : - Displays automatically the system page corresponding to 1 of the 12 flight phases. - Explain flight phase inhibition -

3 zones : - System display page (with MORE info on WHEEL, FUEL, STS pages)- Permanent data (TAT, SAT, ISA, time, GW, GWCG, FOB)- ATC mailbox

ECP : Explain briefly hard keys functions

1) Normal Checklist presentation :

- Select the C/L via the ECP, and perform the BEFORE START C/L- EXT PWR off- Start engines (3,4,1,2)- APU BLEED off, APU off- Select the C/L and perform the AFTER START C/L

Show :- Blue box : appears below the last completed C/L, and surrounds the next applicable one- Items detected / not detected by ECAM (preceded by a square to be ticked): blue when not completed / green when completed : Explain that any action ticked inadvertently is reversible by unticking it.

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- C/L completed indication: Color coding (blue when C/L not completed / grey when com-pleted)

- C/L RESET indication- STS indication- C/L CLEAR bar

2) Alerts procedures presentation

INIT FL 100

1. Explain alerts philosophy and procedure automatically displayed on ECAM (sensed procedure)

• Alerts levels and priority rules : advisory then levels 1,2,3 • Failure types : independent, primary, secondary• Color coding (red, amber, green, white, blue, magenta, grey)

2. Explain ABN PROC activated manually on ECAM by the crew (Not-Sensed procedures)• Associated Alert Level• Not activated : differences of color coding• When activated, transferred into the ECAM and update of STS and limitations

Note : Explain that some failures are not detected by ECAM but directly on the interface itself(eg : VHF failure displayed on RMP).

Insert the following failures in sequence without applying ECAM actions. The purpose is todemonstrate alerts levels, priority rules, failures types and color coding.

Insert ENG ENGINE VIBRATIONSExplain the advisory but do not treat the advisory (demo purpose)

Insert STEER BW STEER FAULTReview level 1 caution (color, awareness) overcoming the advisory

then

Insert ELEC GEN 1 FAULTReview level 2 caution (sound, master caution, color, independent) overcoming the level 1caution

then

Insert FIRE ENG 1 FIREReview level 3 warning (sound, master warning, color, priority, overflow) overcoming thelevel 2 cautionNote : Add an APU FIRE to highlight the priority order for the same level

Restore all systems

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Insert HYD G ENG 1 PMP A PRESS LO and apply ECAM actionsExplain :

- Color coding (blue when not done, or not validated / white when done or validated)- Blue box : surrounds the ECAM action to perform

Note : If the color coding confirms the validation of the action, the result of this action is visibleon the system display.

Restore all systems

Insert HYD G RSVR LEVEL LO and apply ECAM actions

Explain :- Alert types (independent, primary, secondary)- Items detected / not detected by ECAM (preceeded by a square to be ticked) : same color coding as above. Explain that any action ticked inadvertently is reversible by unticking it

- Overflow arrow- MORE indication on STS page. All the ECAM alerts which have an impact on the landing

performance are listed in the "ALERT IMPACTING LDG PERF" part of the MORE STS PAGE.The flight crew selects the applicable ECAM alert(s) in the OIS LDG PERF application to compute LDG DIST and/or VAPP.Point out that 3 indications may be displayed as applicable on the MORE page:INOP SYS REDUND,ALERTS IMPACTING LDG PERF,CANCELLED CAUTION

- Deferred procedure (ALL PHASES, or APP & LDG) : appears in the C/L menu (amber when not completed / white when completed).

Explain FAILURE PENDING INDICATIONIf an alert or ABN PROC is displayed but has not been cleared, a FAILURE PENDING mes-sage appears on the E/WD, when the crew displays a C/L (ex : APPROACH)When the C/L and the C/L menu are cleared, the alert or the not sensed ABN PROC reap-pears on the E/WD and the message disappears.

Restore all systems

Select ABN PROC BOMB ON BOARDShow the color coding when procedure is not activated (scrolling impossible)Activate the procedure and show the color coding changeHighlight the changes into the ECAM

- Deferred procedure- Limitations

Clear the procedure. Explain that the procedure is still active. Do a recall to display it.Show how to de-activate the procedure (untick). Highlight the cancellation of deferred procedure and limitations

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GROUND PHASEL FQE

E

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WEATHER LFZZ 270/10 9999 15/8 1010 LFLL 200/10 9999 18/12 1010

ACTIVE / INIT

FLT NBR A/L ID 101

FROM LFZZ TO LFZZ ALTN LFLL

CPNY RTE AIBAIB

ALTN RTE AIBLYS

CRZ FL 180 CRZ TEMP -20°C

CI 90 TROPO 36090

TRIP WIND HD 10

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : Refer to CO RTE AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER 300




V1 v TOGA V1 v TOGA

VR FLEX 56 °C VR FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

INIT TAKE OFF - LFZZ 33R - GW 385 tCo route AIBAIB

T PRELIMINARY COCKPIT PREPARATION(AIRCRAFT NOT ELECTRICALLY SUPPLIED)

T 1 - COCKPIT PREPARATIONT 2 - BEFORE STARTT 3 - ECAM : NORMAL C/LT 4 - ENGINE START - AFTER STARTT 5 - TAXI

1:00 T 6 - TAKE OFF PACKS ONT 7 - CLIMB FL 180T 8 - CRUISE : FMS EXERCISES

- INSERT NEW WPT- DELETE WPT- OVERFLY- FROM PPOS DIRECT TO- OFFSET- POSITION MONITOR- BRG / DIST TO

1:30 T 9 - DESCENT PREPARATIONT 10 - DESCENTT 11 - ILS APP LFZZ 33R (FLS)

12 - AUTOLANDT 13 - AFTER LANDINGT 14 - PARKING

2:10 T 15 - SECURING THE AIRCRAFT


MFTD 1 - TRAINEE 1

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GROUND PHASEL FQE

WEATHER

LFZZ 270/10 9999 15/8 1010

ACTIVE / INIT

FLT NBR A/L ID 101


CPNY RTE AIBAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND HD 10

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : Refer to CO RTE AIR COND OFF (SID MOU 1N) ANTI ICE OFF PAX NUMBER 300




V1 v TOGA V1 v TOGA

VR FLEX 56 °C VR FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


PRELIMINARY COCKPIT PREPARATION(AIRCRAFT NOT ELECTRICALLY SUPPLIED)16 - COCKPIT PREPARATION17 - BEFORE START18 - ENGINE START WITH EXTERNAL PNEUMATIC POWER &

CROSS BLEED19 - AFTER START20 - TAXI

3:00 21 - TAKE OFF - PACKS OFF22 - CLIMB FL 150 - ALT CONSTRAINT23 - CRUISE

- CAPT EFIS CTL PNL FAULT- HOLDING

3:25 24 - DESCENT PREPARATION25 - DESCENT

- MANAGED AND SELECTED- SPEED CONSTRAINT

26 - ILS APP - LFZZ 33RT 27 - GO AROUND

28 - MISSED APPROACH4:00 29 - DIVERSION

FREEZE

FLIGHT CREW TRAINING PROGRAM FEB 2009

MFTD 1 - TRAINEE 2

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02.0302.03

01 - SESSION OBJECTIVE :• Highlight the differences in terms of procedures through out all phases of flight in normal

operation• Apply task sharing and communication• Study and practice initialization of the FMS and review the various functions using the new

interface• Present the new systems using ECAM pages

02 - TRAINING TOPICS :

A. REVIEW

Not applicable.

B. NEW EXERCICES / REFERENCES

Standard Flight profile - SOP’s• FCOM/Procedures/Normal Procedures/Standard Operating Procedures• FCOM/Procedures/Normal Procedures/Task Sharing• FCTM/NORMAL OPERATIONS• PDP : ALL PHASES Flow pattern

FMS: Initialization - New interfaces and functions• FCOM/Procedures/Normal Procedures/Standard Operating Procedures/Cockpit

preparation/MFD FMS INITIALIZATION• FCOM/Aircraft Systems/22 - AFS-Flight Management System/System description/Flight

Planning

Normal checklists• FCOM/Procedures/Normal Procedures/Normal Checklists

Engine Start with External Pneumatic Power• FCOM/Procedures/Supplementary Procedures/Engines/Unusual Starting Procedures

Use of RMP• FCOM/Aircraft systems/23 - Communication/How to use the RMP/How to tune a frequency

FCU Backup• FCOM/Aircraft systems/22 - AFS - Flight Guidance/Abnormal Operations/FCU Backup

C. SUPPORT

• Procedure Data Package (PDP)• FCOM• FCTM* Note: In the FCTM look at procedures only and disregard the information related to handling-characteristics

03 - SESSION PROFICIENCY CRITERIA :• Understanding of the new FMS architecture and new functions• Demonstrate satisfactory knowledge and skills when applying procedures during a normal

flight profile

MFTD 1 SESSION PREPARATION


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1 :Use the ECAM ELEC page to show the electrical supply using external power and APU : Highlight the priorities- During cockpit preparation: highlight the differences in ECAM system pages (Hydraulic, Fuel, Wheel)- FMS preparation

- SURV page: check default settings Highlight that compared to the A320 Radar, EGPWS, TCAS controls are grouped

on a single panel. Show all the functions on the SURV CTL PNL and then call the MFD specific

page dedicated to SURV.- INIT hard key: press- STATUS: explain the page and don’t go to FMS P/N (Part Number)- INIT: Do not explain all the REQUEST options- IRS: Show the option to “ALIGN ON OTHER REF”- DEPARTURE:

-Demonstrate the use of TMPY F-PLN-F-PLN review according to the electronic F-PLN or to the charts

- NAVAIDS: -Show TUNED FOR DISPLAY-Show the TUNED FOR FMS NAV: how to deselect NAVAIDS

- FUEL § LOAD- PERF:

-Show all the flight phases - SEC INDEX:

-SEC 1: import “FROM ACTIVE”-SEC 2: import “FROM ACTIVE” and modify the runway for departure

Note: During aircraft initialization, highlight the fact that messages are displayed in themessage pad at the bottom of the MFD: CLEAR INFO function is used to clear themessages

- Demonstrate the use of new RMP design.

2 :Highlight the differences on the ECAM DOOR page

3 :Explain the use of the new ECAM Normal Checklist

4 :- Highlight the differences on the ECAM BLEED page- Explain the start sequence and engine parameters monitoring- For F/CTL checks show the new page but do not use controls for the check (done in FFS)

5 :- Pitch trim: explain the pitch trim setting (PFD display and Pitch trim sw)- Show the controls for Taxi cameras, Video on ECAM and OANS

MFTD 1 SESSION GUIDE

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6 :Explain the power setting (METOTS for TRENT engines)METOTS : Modified Engine Take Off Thrust Setting

7 :Show the PERF pages and highlight the differences

8 :- During FMS exercises demonstrate the access to functions through the short cutkey and through the menu at each revised waypoint

- DIRECT TO: demonstrate the four accesses and highlight the differences in CRSIN and OUT

- OFFSET: highlight the differences- Different access to BRG/DIST TO

9 :- Descent preparation: use the predefined flow (ACTIVE, POSITION and SEC)

11 :- Highlight the fact that the deceleration rate is slower than on A320: Slats / Flapsand Landing gear extension takes more time- Explain the differences on the speed scale displayed on PFD (Flaps auto exten-sion, short term managed speed)

16 :- Same full cockpit preparation - Fail the APU BLEED. Emphasize the use of MMEL on OIS- Demonstrate how to build a SEC F/PLN using SEC INIT- Demonstrate how to deselect a NAVAID

The crew has already inserted the ZFW / ZFWCG / FOB figures (refer to syllabus) inthe FMS / FUEL&LOAD pageExplain that the FQMS computes the fuel distribution to ensure a CG target for take-off of approximately 39,5% (SD page).Observe the TRIM TANK fuel quantity and note the value.

The FQMS normally receives (via the avionics system) approx every 10 min anupdated ZFWCG sent by the airline operations via DATALINK (the ground engineermay also update it using the OMT (laptop located at the rear of the cockpit)), in orderto ensure proper fuel distribution (especially quantity in the trim tank) and finalGWCG target of 39,5%

Then, give the trainees a LOADSHEET last minute change:ZFW= 325 TZFWCG= 37%Note: Do not change the figures on the IOS to ensure that the current fuel dis-tribution will not change.

The crew inserts the new figures in the FMS / ACTIVE / FUEL&LOAD page.Observe that the current fuel distribution does not change. Therefore the FQMScomputes a new GWCG according to the updated ZFW / ZFWCG inserted by thecrew in the FMS.The crew checks that the updated GWCG is within operational limits:


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• If YES:

The crew will request an updated LOADSHEET.For demonstration, the crew will use the LOADSHEET application on the OIS:inserts the updated figures above (use the trip fuel displayed on the FUEL & LOADpage). The crew will change the TRIM TANK value to the actual one checked on SD(using the TRIM TANK ADJUSTMENT field), then compute.The TOCG result must be crosschecked versus the FQMS computation (GWCG onSD). If the difference is within 1%, the CM1 signs the LOADSHEET.If the difference is above 1%, investigate the causes (wrong figures insertion, wrongfuel distribution, FQMS failure….).

• If NO:

To demonstrate GWCG out of operational limits, the instructor inserts on the IOSthe new initial figures (make sure that the crew does not change the figures onthe FMS FUEL & LOAD page to allow the fuel to be redistributed):ZFW= 320 TZFWCG= 32%FOB= 83 TGive the crew an updated LOADSHEET: The loading set up has changed:New figures to be inserted by the crew in the FMS:ZFW= 320 TZFWCG= 38%

Observe the updated GWCG on SD: above 44% and amber.The crew must consider using the AUTO GND XFR procedureThe crew pushes the AUTO GND XFR pb-sw on the OVHD MAINTENANCE panel:Observe on the FUEL SD, the FWD transfer done by the FQMS to obtain a GWCGof 39,5%. The FQMS will automatic stop the GND XFR when the GWCG 39,5% isreached.

Due to time constraint (give a new slot for departure), stop the exercise as soon asthe GWCG has turned green or around 41% of GWCG. Explain that it should takeapprox 17 min for the fuel to be transferred forward in the feed tanks, in this case.The transfer rate is approx 600kg per min.The crew should crosscheck on the OIS the FQMS computation obtained at the endof the AUTO GND XFR. Crosscheck the TOCG (OIS) versus the GWCG (SD): If the difference is within 1%, the CM1 signs the LOADSHEET.If the difference is above 1%, investigate the causes.

22 :Demonstrate how to insert an ALT constraint using the menu at a revised waypointor inserting the constraint directly in the F/PLN

23 :Insert FCU 1 FAULT to get CAPT EFIS CTL PNL: demonstrate the use of FCUbackup: restore after demonstration

25 :Demonstrate how to insert a SPEED constraint at a revised waypoint or at a definedaltitude

26 :Demonstrate FD display in TRACK/FPA and VV

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27 :Select the PERF page and explain the differences compared to the A320: differentphases of flight in go aroundAfter the GA acceleration altitude:- Explain that the FMS recovers prediction and vertical managed profile after the

acceleration altitude (CLB, ALT CRZ, DES are available during the missedapproach procedure).

- Explain that the CRZ FL is automatically updated and is the higher of: • the value selected in the AFS - CP or • the higher value of the FPLN (MAP + previous approach)

29 :Demonstrate how to activate (SWAP) a SEC F/PLN after a missed approach proce-dure

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WEATHER LFZZ 360/10 9999 15/10 1010 LFLL 270/08 9999 14/10 1010

ACTIVE / INIT

FLT NBR A/L ID 102


CPNY RTE AIBAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND HD 030

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 34 %

NOTES RWY COND DRY FPLN : Refer to CO RTE AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER : 285


ACTIVE / PERFLFZZ 33R /GW 385 t


V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


PRELIMINARY COCKPIT PREPARATION(AIRCRAFT ELECTRICALLY SUPPLIED)1 - COCKPIT PREPARATION2 - BEFORE START3 - ENGINE START - START FAULT4 - AFTER START5 - TAXI

0:55 6 - TAKE-OFF - PACKS ON7 - CLIMB FL 180 : FMS EXERCICES

-TIME MARKER - FIX INFO - CLOSEST AIRPORT

T 8 - CDS RECONFIGURATIONT 9 - ECAM PHILOSOPHY / MANAGEMENT

1:40 10 - DIVERSION11 - ENGINE FIRE - RESTORE12 - DESCENT PREPARATION13 - DESCENT

T 14 - VOR-DME APP (FLS) - LFLL 18R2:10 15 - MISSED APPROACH

FREEZE


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WEATHER LFZZ 360/10 2000 BKN 008 5/2 998 BIKF 200/05 9999 -10/-15 1000

ACTIVE / INIT

FLT NBR A/L ID 102

FROM LFZZ TO BIKF ALTN EINN

CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 35500

TRIP WIND TL 090

ACTIVE FUEL & LOAD

GW 450 t990 000 Ib FOB 130 t

286 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND WET FPLN : Refer to CO RTE AIR COND OFF (SID ATN 1E) ANTI ICE ON PAX NUMBER : 250


ACTIVE / PERFLFZZ 06 / GW 450 t

ACTIVE / PERFLFZZ 06/ GW 450 t

V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

INIT TAKE OFF - LFZZ 06 - GW 450 tCo route AIBKEF

PRELIMINARY COCKPIT PREPARATION(AIRCRAFT ELECTRICALLY SUPPLIED)16 - COCKPIT PREPARATION17 - TAXI

2:40 18 - TAKE-OFF - PACKS OFF19 - CLIMB FL 31020 - SYSTEMS REVIEW21 - FMS EXERCICES - INTERACTIVITY WITH ND - REVIEW DIRECT TO - CMS - STEP ALT22 - ECAM MANAGEMENT - NOT SENSED PROCEDURES

T 23 - FUEL LEAK - RESTORE3:25 24 - RETURN TO DEPARTURE

T 25 - FUEL JETTISON26 - OVERWEIGHT LANDING27 - DESCENT PREPARATION28 - DESCENT29 - LOC APP (FLS) - LFZZ 33R30 - MISSED APPROACH31 - FMC B + C FAULT

FREEZE


MFTD 2 - TRAINEE 2

FEB 2009Issue 05


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02.0302.03


• Practice SOP’s using proper callouts and cross checks• Highlight the differences in failure handling using the new ECAM procedures• Study the Non Precision Approaches using the FLS function (if not retrofitted on A320)• Study and practice new FMS functions


A. REVIEW

• FMS initialization - New interfaces and functions• SOP: Normal Operations - TASK Sharing

B. EXERCICES / REFERENCES

OIT: Use of Take-off performance and MEL applications·• FCTM/NORMAL OPERATIONS/Flight Preparation/MELENGINE START FAULT• FCOM/Procedures/Abnormal and Emergency Procedures/70-Engines/ENG START FAULTECAM Procedures: new philosophy• FCTM/OPERATIONAL PHILOSOPHY/ECAM• PDP: ECAM PHILOSOPHYCDS reconfiguration• FCOM/Aircraft Systems/31-Indicating-Recording/CDS/Abnormal Operations• FCOM/Procedures/Abnormal and Emergency Procedures/31-Indicating-Recording/CDS

FAULTFUEL LEAK• FCOM/Aircraft Systems/28-fuel/Abnormal Operations/Fuel leak Detection• FCOM/Procedures/Abnormal and Emergency Procedures/28-Fuel/FUEL LEAK

DETECTED• FCOM/Procedures/Abnormal and Emergency Procedures/70-Engines/ENG FUEL LEAKBRAKES: system review• FCOM/ Procedures/Abnormal and Emergency Procedures/32-Landing Gear/BRAKES

FAULTFMS: FMC FAULT• FCOM/Aircraft Systems/22-AFS-Flight Management/Abnormal Operations/ FMC FAULT·

FCOM/Procedures/Abnormal and Emergency Procedures/22-Flight Management System/AUTOFLT FMC FAULT and AUTO FLT FMS FAULT

Non Precision Approach using FLS• FCOM/Procedures/Normal Procedures/Standard Operating Procedures/Non Precision

Approach• FCTM/Normal Operations/Non Precision Approach• PDP/Non Precision Approach



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C. SUPPORT

• Procedure Data Package (PDP)• FCOM• FCTM

* Note: In the FCTM look at procedures only and disregard the information related to handling-characteristics

03 - SESSION PROFICIENCY CRITERIA :

• Ability to carry out all normal tasks according to SOP’s• Demonstrate an acceptable knowledge and user skill of the new FMS interface• Demonstrate satisfactory knowledge of the new ECAM procedures



GROUND PHASE

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1 :- Use of OIS for aircraft loading and performance computation- MMEL item SEC 3 INOPERATIVE

3 :Insert ENG START (4) FAULT due to EGT OVERLIMIT. When ECAM actions completed, restore, perform a manual engine start on engine 4.Then, perform a manual start on engine 1 with hot start to highlight the difference ofprotections between AUTO and MAN. Restore and perform a quick start through IOSpanel.

7 : Highlight fuel transfer after take-off (load alleviation)

8 :- Highlight the differences between the A320 and the A380- PFD / ND transfer and Automatic reconfigurations (loss of PFD or EWD) are identical- Demonstrate the use of hard key to recover FMS pages: Fail the MFD CAPT side and push PERF to recover the PERF page on ND- Call the fuel page : explain fuel transfer according to the actual situation

9 :ECAM system philosophy review and introduction of management

The instructor leads the demo by following this scenario :

Dot not perform any ECAM actions

After each failure insertion, instructor highlights on EWD and PFD- Priority between alerts in a same level- Priority between alerts in different levels- Priority between limitations on PFD- Memos on PFD- Deferred procedure and limitations : Approach deferred proc is inserted chronolog-

ically before approach check list, because the deferred actions to perform canmodifiy the STATUS and the briefing. Consequently, the approach C/L which referto STS and briefing is the last protection about aircraft status awareness.

- STATUS

Restore


Insert N1 vibration on ENG 1 (Advisory): use of FCOM to look for ECAM advisory

Insert BRAKES ALTN BRK FAULT (level 1)

Insert ELEC BAT 1 FAULT (level 2-Master Caution + SC)

Insert HYD G RSVR LEVEL LO (level 2-Master Caution + SC)

Insert ENGINE 1 FIRE (level 3-Master Warning + CRC)

Insert LEFT MAIN AVIONICS SMOKE (level 3 - Master Warning + CRC)

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- Insert a FUEL FEED TK 1 MAIN+STBY PUMPS FAULT and perform ECAM actions.

Explain the flow before completing all ECAM actions Complete ECAM actions explaining the use of tick and clear bar Show the MORE FUEL page Restore

- Insert HYD G RSVR LEVEL LO and perform ECAM actions Demonstrate when and how to use DEFERRED PROC Explain the LIMITATIONS on PFD and ECAM Show STATUS MORE page Use of OIS / Laptop for landing performance computation Restore

10 :- Diversion to LFLL: use the ENABLE ALTERNATE function- Proceed DIRECT TO TALAR for a VOR-DME 18R

16 :- Initialize the aircraft on Runway 06: engines running- Use of OIS for performance computation- Insert flight parameters in the FMS

20 : - BRAKES ALTN BRAKES FAULT- BRAKES EMER BRAKES FAULT- CAB PRESS AUTO CTL FAULTHighlight the differences with the A320: explain braking reconfiguration and differences in CAB ALT control

22 :- Freeze aircraft position for this demonstration - Demonstrate how to access to the NOT SENSED PROCEDURES using the ABNPROC pb on the ECP and show the list of procedures Activate the not sensed L/G LDG with Abnormal WING & BODY L/Gs : Explain thatthere are a few procedures whose management is different. Those PROC are displayed until landing, disregarding normal C/L (e.g. LANDINGWITH 2 ENGs INOP ABN PROC)

23 :- Insert a fuel leak (1000 kg/minute) - FUEL LEAK DETECTED is triggered: compareFuel at departure with fuel used + FOB and complete ECAM actions

1st scenario- Leak is coming from the engine : after engine shut down, do not reset the failure butinsert 0 kg/min2d scenario- Leak is coming from the feed tank- Do not play this scenario but explain the difference to the traineeRestore

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24 :- Proceed DIRECT TO MOU – MOU 1B Arrival – LOC Approach 33R- Use speed up function if required

25 : - To accelerate the fuel jettison, use fuel tank distribution on the IOS and set XFRand TRIM TKS to 0 in order to keep FEED TANKS FULL only. Stop at GW 420 t.

29 : Fail the G/S and brief the crew that he must deselect the G/S

31 :- Fail FMC B: Demonstrate that FMC C is taking over- Fail FMC C : Demonstrate FMS SOURCE switchingRestore

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WEATHER LFZZ 020/15 9999 -20/-21 1025 LFLL 010/15 9999 -20/-21 1025

ACTIVE / INIT

FLT NBR A/L ID 103


CPNY RTE AIBAIB

ALTN RTE AIBLYS

CRZ FL 120 CRZ TEMP 0°C

CI 90 TROPO 36090

TRIP WIND HD 25

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND COMPACTED SNOW FPLN : Refer to CORTE AIR COND ON (SID MOU 1N) ANTI ICE ENG ON PAX NUMBER 280




V1 TOGA V1 TOGA

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V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


PRELIMINARY COCKPIT PREPARATION(AIRCRAFT ELECTRICALLY SUPPLIED)1 - COCKPIT PREPARATION2 - BEFORE START3 - ENGINE START4 - AFTER START5 - TAXI

0:40 T 6 - TAKE-OFF - ENGINE FAILURE - NO DAMAGE7 - ENGINE RELIGHT8 - CLIMB FL 1209 - AFS CTL PNL FAULT - RESTORE

T 10 - AIR COND SMOKE - RESTORE1:25 11 - HYD G + Y SYS PRESS LO

12 - DESCENT PREPARATION13 - DESCENT14 - ILS APP - LFZZ 33R15 - MISSED APPROACH AT 500 ft - RESTORE

2:10 16 - VOR-DME APP (FLS) - LFZZ 33R FREEZE AT MDA


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FEB 2009Issue 05

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GROUND PHASEL FQE

WEATHER LFZZ 020/15 9999 -20/-21 1025 LFLL 010/15 9999 -20/-21 1025

ACTIVE / INIT

FLT NBR A/L ID 103


CPNY RTE AIBAIB

ALTN RTE AIBLYS

CRZ FL 120 CRZ TEMP 0°C

CI 90 TROPO 36090

TRIP WIND HD 25

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND COMPACTED SNOW FPLN : Refer to CORTE AIR COND ON (SID MOU 1N) ANTI ICE ENG ON PAX NUMBER 280




V1 TOGA V1 TOGA

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V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


17 - COCKPIT PREPARATION18 - TAKE-OFF - ENGINE FAILURE - RESTORE19 - CLIMB FL 12020 - MAIN AVIONICS SMOKE - RESTORE

3:00 21 - AFS CTL PNL FAULT22 - DESCENT PREPARATION23 - DESCENT 24 - ILS APP - LFZZ 33R - RESTORE

3:25 25 - MISSED APPROACHT 26 - SLATS LOCKED

3:45 27 - NDB APP (FLS) - LFZZ 33RFREEZE AT 500 FT

INIT GATE

28 - AFTER LANDING29 - PARKING (TAIL PIPE FIRE)30 - SECURING THE AIRCRAFT


MFTD 3 - TRAINEE 1

FEB 2009Issue 05


GROUND PHASE

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02.0302.03

01 - SESSION OBJECTIVE

• To highlight the differences in abnormal procedures using the new ECAM procedures• To practice SOP’s using proper call outs and cross checks• To review new FMS functions

02 - TRAINING TOPICS

A. REVIEW

• FMS initialization• SOP: Normal operations• ECAM procedures: new philosophy• FCU Backup

B. EXERCISES / REFERENCES

ENGINE FAILURE• FCOM/Procedures/Abnormal and Emergency Procedures/70-Engines/ENG FAIL• PDP: ENGINE OUT AFTER TAKE-OFF

ENGINE RELIGHT• FCOM/Procedures/Abnormal and Emergency Procedures/70-Engines/ENG RELIGHT IN

FLIGHT

G+Y SYS PRESS LO• FCOM/Procedures/Abnormal and Emergency Procedures/29-Hydraulic/G+Y SYS PRESS

LO• FCTM/Abnormal Operations/Hydraulic/G+Y Hydraulic Failures• PDP: DUAL HYDRAULIC FAILURE

AIR COND SMOKE• FCOM/Procedures/Abnormal and Emergency Procedures/26-Fire and Smoke Protection/

SMOKE-FUMES AVIONICS SMOKE• FCTM/ABNORMAL OPERATIONS/Fire Protection/Smoke-Fumes

AVIONIC SMOKE• FCOM/Procedures/Abnormal and Emergency Procedures/26-Fire and Smoke/L(R)

AVIONICS SMOKE

SLATS LOCKED• FCOM/Procedures/Abnormal and Emergency Procedures/27-Slats-Flaps/ SLATS LOCKED

and SLATS FAULT

ENGINE TAIL PIPE FIRE• FCOM/Procedures/Abnormal and Emergency Procedures/70-Engines/TAIL PIPE FIRE



mftd3gd.fm


GROUND PHASE


C. SUPPORT

• Procedure data package (PDP)• FCOM• FCTM

* Note: in the FCTM look at procedures only and disregard information related to handlingcharacteristics

03 – SESSION PROFICIENCY CRITERIA

• Demonstrate proficiency in FMS use• Demonstrate ability to manage failures using the new ECAM interface• Demonstrate ability to carry out all normal tasks according to SOP’s



GROUND PHASE

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1 :- Use OIS / laptop for performance calculation- Switch off the KBD to demonstrate the use of soft keyboard and restore after a few

insertions

6 :- Insert engine failure with no damage at 200 ft AGL

9,21 : - Trainee 2: - Show the AFS CP Back up page and all the associated functions- Demonstrate scroll wheel use and restore: flying demonstration will take place dur-

ing the second part of the session.- Trainee 1:- Insert FCU 1 + 2 fault to trigger CAPT AFS CP FAULT. Explain that CAPT and F/O

EFIS CP are also lost in this case.- Keep the failure until the end of the missed approach- Provide radar vectors to the crew in order to allow them to practice the use of FCU

back up

10 : - Cabin crew warns the flight crew that smoke is coming from the AIR COND outletsin the Main and Upper cabin (specific smell: oil burnt)

- The instructor warns the crew that there is also smoke in the cockpit- Flight crew applies SMOKE / FUMES ABN PROC if the visibility in the cockpit is

sufficient and ECAM is available or refer to the QRH.- Stress communications between cabin crew and cockpit- No change when PACK 1 is selected to OFF- When PACK 2 is selected to OFF (after 2 minutes) insert ENGINE 3 - OIL PRESS

LO - With PACK 2 OFF Cabin crew will advise the crew that smoke starts to disappear

from the Main and Upper cabin and the instructor informs the crew that smoke isremoved from the Cockpit

11 :- Highlight the differences compared to the A320- Aircraft is in Alternate law but the AP and the ATHR are available- Call the ECAM F/CTL page and show which surfaces are controlled by the EBHA

or EHA- Flaps are lost: the handling characteristics will be seen in the FFS- Approach can be flown with the AP down to 500 ft- Call the WHEEL page : explain the Landing Gear gravity extension- Braking with antiskid is available and NWS is available but slow

16,27: - FLS approach in cold weather conditions. Explain that the FLS profile takes intoaccount the temperature corrections (use of tutorial NPA flown with FLS function,COLD WEATHER)

17 : - Instructor prepares the aircraft for take-off

18 : - Insert engine failure with damage at 200 ft AGL

19 . - Restore after ECAM actions completed and restart the engine


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20 : - Insert a L MAIN AVNCS SMOKE and tell the crew that a little bit of smoke is comingfrom Pedestal panel

- The crew will apply the ECAM procedure and then refer to QRH.- Cancel the failure when GEN 3 and 4 have been selected to OFF and tell the crew

that the smoke disappears- Explain the remaining of the procedure if the smoke was still present

26 :- During missed approach, insert a slats locked (by wing tip break) during slatsretraction between Conf 1 and Conf 0

29 :- During engine shut down warn the crew that flames are coming out from the Engine2. Show where to find the Tail pipe fire procedure (No differences from the A320).

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HANDLING PHASEL FQE

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WEATHER LFZZ 310/10 CAVOK 20/12 1010

ACTIVE / INIT

FLT NBR A/L ID 101


CPNY RTE AIBAIB

ALTN RTE AIBLYS

CRZ FL FL 180 CRZ TEMP -20°C

CI 90 TROPO 36090

TRIP WIND HD 20

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : Refer to Co-route AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER 450




V1 TOGA V1 TOGA

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V1 TOGA V1 TOGA

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Time EVENTS

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INIT GATE A1 - LFZZ 33R - GW 385 tCo route AIBAIB

PRELIMINARY COCKPIT PREPARATION(AIRCRAFT NOT ELECTRICALLY SUPPLIED)1 - COCKPIT PREPARATION2 - ENGINE START3 - AFTER START4 - TAXI5 - TAKE OFF v v6 - CLIMB FL 140 v v v7 - AIRWORK v8 - DESCENT v v v9 - ILS APP - LFZZ 33R v v

1:30 10 - LANDING

INIT HOLDING 1000 FT - LFZZ 33R - GW 385 t

11 - FINAL APPROACHES v2:00 12 - LANDINGS

INIT HOLDING LFZZ 33R - GW 385tWIND 240/25

13 - TAKE OFF - CROSSWIND v v14 - VISUAL PATTERN v v15 - REJECTED LANDING v v16 - VISUAL PATTERN v v

2:15 17 - LANDING - CROSSWIND


FFS 1 - TRAINEE 1

FEB 2009Issue 05

A380


HANDLING PHASEL FQE

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WEATHER

LFZZ 310/10 CAVOK 20/12 1010

ACTIVE / INIT

FLT NBR A/L ID 101


CPNY RTE AIBAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND HD 20

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : Refer to Co-route AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER 450




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX





V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

AP

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2:25 INIT HOLDING POINT - LFZZ 33R - GW 385t Co route AIBAIB

18 - TAXI19 - TAKE-OFF v v20 - CLIMB FL 140 v v v21 - AIRWORK v22 - DESCENT v v v23 - ILS APP - LFZZ 33R v v

03:05 24 - LANDING

INIT APPROACH 1000 FT - LFZZ 33RGW 385 t

25 - FINAL APPROACHES v03:35 26 - VISUAL PATTERN v

INIT TAKE OFF LFZZ 33R - GW 385 tWIND 240/25

27 - TAKE OFF - CROSSWIND v v28 - VISUAL PATTERN v v29 - REJECTED LANDING v v30 - VISUAL PATTERN v v

03:50 31 - LANDING - CROSSWIND32 - TAXI TO THE GATE33 - PARKING 34 - SECURING THE AIRCRAFT


FFS 1 - TRAINEE 2

FEB 2009Issue 05


HANDLING PHASE

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02.0302.03


• To handle the A380 in normal, alternate and direct law using experience from the A320• To practice SOP’s applicable to the A380• To review specific changes in panels and controls during cockpit preparation


A. REVIEW

• SOP’s - Task sharing• FMS: initialization and use during all flight phases• Use of OIS / LAPTOP for take-off performance computation


Use of ETACS• FCOM/Aircraft Systems/31-Indicating-Recording/Video/Description/External and Taxing Aid

Camera System

Use of OANS• FCTM/NORMAL OPERATIONS/Taxi/Onboard Airport Navigation System• FCOM/Aircraft Systems/34-Navigation/Airport Navigation

Taxi • Briefing guide: Taxi • FCOM/Standard Operating Procedures/Taxi

Take-off: handling technique• Briefing guide: Take-off• FCTM/NORMAL OPERATIONS/Take-off

Landing: handling technique• Briefing guide: Landing• FCTM/NORMAL OPERATIONS/Landing

Rejected landing• FCTM/NORMAL OPERATIONS/Go around/Rejected landing

C. SUPPORT

• Briefing Guides• Procedure Data Package (PDP)• FCOM• FCTM

FFS 1 SESSION PREPARATION


ffs1gd.fm


HANDLING PHASE



• Ability to carry out normal task in accordance with SOP’s• Ability to handle the aircraft within standard criteria of flight accuracy• Ability to apply correct take-off and landing technique in cross wind conditions



HANDLING PHASE

ffs1gd.fm


1 :- Presentation of equipments that are not available in the MFTD- Show the location of the A380 simulator instructor guide- Safety equipments (fire extinguishers, escape ropes, torch)- Seat adjustment, lights- Laptop installation- Oxygen masks- Audio : hand mike, headset, RMP, ACP, PTT- Use of taxi camera, airport navigation- First FFS handling characteristics review (NWS, taxi, brake check, flight controlcheck, take off side stick position, rotation technique)

Reinforce frequency insertion procedure : 2 possibilities1) Insert all the digit and enter : e.g. : 118.0 or2) If you insert only 18 without validating it, the field is still active. Explain the following risk : If the pilot wants to enter another frequency (eg : 135.0),and enters 35, the result will be 118.35 which is not expected.

- Demonstrate the use of OIS for performance computation

4,32 :- Demonstrate the use of ETACS- Use simulator facilities to show the position of the landing gear, engines and wing tips- Use of Onboard Airport Navigation System to follow the taxi clearance

6,20 :Practice FMS during climb- Place / Bearing / Distance- Place - Bearing / Place - Bearing- DIRECT TO on ND

7,21 :- FD off with the VV on- Practice some steep turns and low speed flight- Highlight the fact that the handling characteristics are similar to the A320- Protections are identical: no need for demonstration however ask the pilot to perform an emergency pull up with maximum bank angle- Use DIRECT LAW function on IOS: reduce speed to green dot and establish the aircraft in landing configuration, then clean up the aircraft: practice use of TRIM switch

11,25 : Five different Approaches for each trainee- INIT 1000 ft Approach: FD on, ATHR on - INIT 1000 ft Approach: FD off, VV on, ATHR on- INIT 1000 ft Approach: FD on, ATHR on - Wind 250/15 kts- INIT 8 NM - 2NM Left: FD off, VV on, ATHR on - Wind 060/10 kts- INIT 12 NM: FD on, ATHR on, 6000 - OVC 600 - 010/20 gust 5, turbulence 20%

15,29 : Rejected landing below 100 feetAfter go around insert wind 240/10.

FFS 1 SESSION GUIDE

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HANDLING PHASEL FQE

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WEATHER LFZZ 270/15 6000 BKN 008 3/1 998 BIKF 280/10 CAVOK -10 / -12 1007

ACTIVE / INIT

FLT NBR A/L ID 102


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 37100

TRIP WIND HD 070

ACTIVE FUEL & LOAD

GW 569 t 1 232 000 Ib FOB 219 t

462 000 Ib

ZFW 350 t770 000 Ib ZFWCG 36 %

NOTES RWY COND WET FPLN : Refer to Co-route AIR COND OFF DEP : ATC Clearance ANTI ICE ON PAX NUMBER : 500




V1 v TOGA V1 v TOGA

VR FLEX VR FLEX


FLAPS OPT THS FOR FLAPS OPT THS FOR







Time EVENTS

AP

FD

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RK

-FPA

INIT GATE A1 - LFZZ 24 - GW 569 tCo route AIBKEF

1 - COCKPIT PREPARATION2 - ENGINE START3 - AFTER START4 - TAXI

00:45 5 - TAKE OFF (MTOW) v v6 - CLIMB FL 100 v v v7 - RETURN TO DEPARTURE v v v8 - ILS APP (RAW DATA) - LFZZ 33R v v9 - GO AROUND -MISSED APP v v

10 - LOC APP (G/S INOP) - LFZZ 33R v v11 - LANDING (OVERWEIGHT)

01:45 12 - 180° ON RUNWAY

INIT HOLDING POINT LFZZ 33R - GW 385 tZFW 320 t - FOB 65 t290/12 6000 BKN 012 Co route PAT 33R

13 - TAKE OFF - WINDSHEAR v v14 - ADR 1 + 2 + 3 FAULT v15 - ILS APP - LFZZ 33R - DIRECT LAW v

02:10 16 - LANDING


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HANDLING PHASEL FQE

WEATHER

LFZZ 270/15 6000 BKN 008 3/1 998 BIKF 280/15 CAVOK -10 / -12 1007

ACTIVE / INIT

FLT NBR A/L ID 102


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 37100

TRIP WIND HD 070

ACTIVE FUEL & LOAD

GW 569 t 1 232 000 Ib FOB 219 t

462 000 Ib

ZFW 350 t770 000 Ib ZFWCG 36 %

NOTES RWY COND WET FPLN : Refer to Co-route AIR COND OFF DEP : ATC Clearance ANTI ICE ON PAX NUMBER : 500




V1 v TOGA V1 TOGA

VR FLEX VR FLEX


FLAPS OPT THS FOR FLAPS OPT THS FOR







Time EVENTS

AP

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INIT HOLDING POINT LFZZ 24 - GW 569 tCo route AIBKEF

2:25 17 - TAKE OFF (MTOW) - PACKS OFF v v18 - CLIMB FL100 v v v19 - RETURN TO DEPARTURE v v v20 - ILS APP (RAW DATA) - LFZZ 33R v v21 - GO AROUND - MISSED APP v v22 - VOR-DME APP (FLS) - LFZZ 33R v v23 - LANDING - OVERWEIGHT

03:25 24 - 180° ON RUNWAY

INIT HOLDING POINT LFZZ 33R - GW 385 tZFW 320 t - FOB 65 t290/12 6000 BKN 012 Co route AIBAIB1

25 - TAKE OFF - WINDSHEAR v v26 - NAV ALL AIR DATA DISAGREE v27 - ILS APP - LFZZ 33R - DIRECT LAW v

3:50 28 - LANDING

INIT TAKE OFF LFZZ 24 - GW 569 t

29 - TAKE OFF - REJECTED v v


FFS 2 - TRAINEE 1

FEB 2009Issue 05


HANDLING PHASE

ffs2gd.fm


02.0302.03


- To practice MTOW and overweight landing- To practice rejected take-off- To practice new functions specific to the A380: NPA approaches using FLS- To practice Back Up Speed in Direct law


A. REVIEW

• SOP’s - Task sharing• Non Precision Approach using FLS• Take-off and landing techniques


Max Take-off weight• FCTM/NORMAL OPERATIONS/Take-off/Take-off at heavy weight

Taxi - 180° turn on 60 m runway• Briefing guide: Taxi - 180° turn on 60 m runway• FCOM/Standard Operating Procedures/Taxi/180° turn on 60 m wide runway

Overweight landing• FCOM/Procedures/Abnormal and Emergency Procedures/80-Miscellaneous/

OVERWEIGHT LDG• FCOM/Procedures/Not Sensed Procedures/Miscellaneous/OVERWEIGHT LDG

ADR1+2+3 FAULT - Backup Speed Scale• FCOM/Procedures/Abnormal and Emergency Procedures/34-Navigation/Unreliable Speed

Indication• FCOM/Procedures/Abnormal and Emergency Procedures/34-Navigation/ADR1+2+3FAULT• FCOM/Aircraft Systems/31-Indicating - Recording/EFIS/PFD/Backup Scales• Briefing guide: BACK UP SPEED SCALE (BUSS)

C. SUPPORT

• Briefing guides• Procedure Data Package (PDP)• FCTM• FCOM


• Ability to fly the aircraft in direct law using back up speed scale• Demonstrate proficiency in normal manoeuvers: take-off, approach and landing• Demonstrate proficiency in FMS use and NPA approaches using FLS



ffs2gd.fm


HANDLING PHASE


1 : Explain that the flight is planned with landing weight far above MLW for training pur-pose (Take-off at MTOW consideration)

4,17 :Clearance for departure: RWY heading to 2000 ft - Right turn to intercept ATN 240°radial inbound.On the OANS, demonstrate the use of FLAGS to identify the taxi clearance.

5,17 :New feature on PFD speed scale for Flaps auto retraction

6 :- Insert weather cells to demonstrate the use of the Radar

7,19 :- In order to return to departure choose between the following - PACK 1 + 2 OVERHEAT at 9000 ft - Window crack (No diagnostic possible) - Medical emergency- Decrease GW to 440t - Cancel runway: wet- Return to departure: Radar vectors for ILS 33R- Notify the crew that he is not having enough time for jettison due to problems withpassengers (behavior, sickness, riot …)- Demonstrate the Flaps auto extension at 205 kts

8 :- Fail G/S at 800 ft

12,24 :- Vacate on runway 24 to make the 180° on a 60 m width runway

13,25 :- Insert windshear after rotation (light)- On Resets /Freezes page activate the crash inhibit function

14 : In downwind, when aircraft is cleaned up, set 3 ADR OFF for BUSS demonstrationWeather : CAVOK

20 : Decrease ceiling at 200 ft and fail ILS at 400 ft

26 : In downwind, when aircraft is cleaned up, set ADR 2 + 3 OFF. Then, 1 minute later,insert CAPT L+R PITOT BLOCKEDWeather : CAVOK

29 :- INIT Take-off 33R• 1st rejected take-off: 50 kts (engine failure)• 2d rejected take-off: V1 - 15 kts (engine fire)

Note: Circling approaches will be performed under specific airline requirement (if approved by thelocal Authority): in this case an additional 30 minutes will be required to complete the session.

FFS 2 SESSION GUIDE

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HANDLING PHASEL FQE

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WEATHER LFZZ 350/10 8000 OVC 008 15/12 1002

ACTIVE / INIT

FLT NBR A/L ID 103


CPNY RTE PAT 33R

ALTN RTE AIB LYS

CRZ FL 4000 ft CRZ TEMP +8°C

CI 90 TROPO 36090

TRIP WIND N/A

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %

NOTES RWY COND DRY DEP : N/A AIR COND ON (SID 1B) ANTI ICE OFF PAX NUMBER : N/A













FLAPS OPT1+F

THS FOR FLAPS OPT2

THS FOR

Time EVENTS

AP

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INIT HOLDING POINT - LFZZ 33R - GW 385 tEngines running - NIGHT VISUALCo route PAT 33R

1 - TAXI2 - TAKE OFF - ENGINE FAILURE v v3 - RADAR VECTORS v v v4 - ILS APP - LFZZ 33R v v

00:45 5 - LANDING - ONE ENG OUT

INIT TAKE OFF LFZZ 24 - GW 500 tZFW 350 t - FOB 150 t - DAY VISUAL330/10 SID MOU 1W

6 - TAKE OFF - ENGINE FAILURE v v7 - RADAR VECTORS v v v8 - RNAV APP (FLS) - LFZZ 24 v v v9 - GO AROUND v v v

10 - RADAR VECTORS v v v11 - ILS APP - LFZZ 33R v v

1:35 12 - LANDING - TWO ENGINES OUT

INIT BASE LEG - LFZZ 33R

13 - RADAR VECTORS v v14 - VISUAL APP - LFZZ 33R v v


If time permits: Exercises at trainee and instructor discretion


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HANDLING PHASEL FQE

WEATHER

LFZZ 350/10 8000 OVC 008 15/12 1002

ACTIVE / INIT

FLT NBR A/L ID 103


CPNY RTE PAT 33R

ALTN RTE AIB LYS


CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %














FLAPS OPT1+F

THS FOR FLAPS OPT2

THS FOR

Time EVENTS

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2:05 INIT HOLDING POINT - LFZZ 33R - GW 385 tCo route PAT 33R - NIGHT VISUAL

16 - TAKE OFF - ENGINE FAILURE v v17 - CLIMB 4000 ft v v v18 - ILS APP - LFZZ 33R - ONE ENG OUT v v19 - LANDING

INIT TAKE OFF LFZZ 24 - GW 500 tZFW 350 t - FOB 150 t - DAY VISUAL330/10SID MOU 1W

2:30 20 - TAKE OFF - ENGINE FAILURE v v21 - RADAR VECTORS v v v22 - RNAV APP (FLS) - LFZZ 24 v v v23 - GO AROUND v v v24 - RADAR VECTORS v v v25 - ILS APP - LFZZ 33R v v

3:20 26 - LANDING - TWO ENGINES OUT v

INIT BASE LEG - LFZZ 33R

27 - RADAR VECTORS v v28 - ILS APP - LFZZ 33R v v


INIT TAKE OFF - LFZZ 06 - GW 500 tZFW 350 t - FOB 150 tRR TRENT 972 : Conf 3 - V1:144 - VR: 160 - V2: 165 - Flex 44° CEA GP 7272 : Conf 3 - V1:143 - VR: 159 - V2:164 - Flex 44° C

30 - TAKE OFF - REJECTED v v

INIT TAKE OFF - LFZZ 06 - GW 500 t

31 - TAKE OFF - REJECTED v v32 - REJECTED TAKE OFF

3:50 33 - EMERGENCY EVACUATION

If time permits: Exercises at trainee and instructor discretion


FFS 3 - TRAINEE 1

FEB 2009Issue 05


HANDLING PHASE

ffs3gd.fm


02.0302.03


• To practice the engine failure on A380 highlighting the fact that the procedure is similar• To practice approach and landing with two engines inoperative on the same wing• To practice the on ground emergency evacuation


A. REVIEW

• SOP’s - Task sharing• Non Precision Approach using FLS• Rejected Take-off

B. NEW EXERCISES / REFERENCES

Engine Failure during Take-off• FCOM/Procedures/Abnormal and Emergency procedures/70-Engines/ENG FAIL

Approach with two engines out• FCOM/Procedures/Abnormal and Emergency procedures/70-Engines/LDG WITH 2 ENGs

INOP ON THE SAME WING

EMERGENCY EVACUATION• FCOM/Procedures/Abnormal and Emergency procedures/80-Miscellaneous/EMER EVAC

C. SUPPORT


03 - SESSION PROFICIENCY CRITERIA

• Demonstrate the ability to perform all exercises, using the correct procedures and techniques in accordance with SOP's

• Demonstrate the ability to perform a one / two engine out approach and landing• Demonstrate the ability to perform an emergency evacuation using good crew coordination



ffs3gd.fm


HANDLING PHASE


INIT HOLDING POINT:- The instructor will prepare the aircraft and the crew will prepare the FMS- Aircraft will be given to the trainee in Take-off configuration ready for the BeforeTake-off checklist

2,16 :- Night environment for this traffic pattern- Insert an engine flame out (with damage) at 30 feet- Highlight the fact that the engine out profile is the same as the one for A320

6,20 :- LFZZ to LFZZ with MOU 1W Departure- Insert an engine flame out (with damage) after V1

8,22 :- Insert weather CATII

10,24 :- Decrease GW to 380t- Weather: CAVOK - 310/10 kts- Clearance : maintain speed 250 kts to highlight the engine relight with windmilling.- Insert an engine failure with no damage (second engine on the same wing). Relight is unsuccessful (insert EGT overlimit)

INIT BASE LEG :- INIT 8NM - 2NM Left or right- Slew altitude to 3200 ft- All ECAM actions and procedure have been completed- Select V/S: 700 ft/mn to stay on the G/S until LOC interception (with APPR modearmed)

13,27 :- Assist the crew for LOC and G/S interception

30 :- Rejected take-off at 70 kts (engine failure)

31 :- Rejected Take-off at V1-15kts (non extinguishable fire)

Note: The session allows extra time and some exercises can be repeated at instructor / traineediscretion.

FFS 3 SESSION GUIDE

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HANDLING PHASEL FQE

E

E

WEATHER LFZZ 300/10 8000 OVC 010 20/16 1010

ACTIVE / INIT

FLT NBR A/L ID 104


CPNY RTE PAT 33R

ALTN RTE AIBLYS


CI 90 TROPO 36900

TRIP WIND N/A

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %





V1 TOGA V1 TOGA

VR v FLEX VR v FLEX





V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

AP

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INIT GATE A1 - LFZZ 33R - GW 385 tCo route PAT 33R

1 - COCKPIT PREPARATION2 - ENGINE START3 - AFTER START4 - TAXI5 - TAKE OFF v v6 - CLIMB TO 4000 ft v v v7 - FLAPS SYS 1 + 2 FAULT v v v8 - VOR - DME APP (FLS) - LFZZ 33R v v v v

1:15 9 - LANDING - NO FLAPS

INIT HOLDING POINT - LFZZ 33R - GW 385 tCAVOK - 060/20

10 - TAKE OFF - CROSSWIND v v11 - VISUAL PATTERN v v

1:30 12 - LANDING - CROSSWIND

INIT HOLDING POINT - LFZZ 33R - GW 385 t300/15 OVC 008Co route AIBAIB 1 - SID MOU 1N

13 - TAKE OFF v v14 - CLIMB FL 80 v v v15 - ALL GENERATORS FAULT v16 - DESCENT v17 - ILS APP (RAW DATA) - LFZZ 33R v

2:05 18 - LANDING


FFS 4 - TRAINEE 1

FEB 2009Issue 05

ffs4.fm

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HANDLING PHASEL FQE

WEATHER

LFZZ 300/10 8000 OVC 010 20/16 1010

ACTIVE / INIT

FLT NBR A/L ID 104


CPNY RTE PAT 33R

ALTN RTE AIBLYS


CI 90 TROPO 36900

TRIP WIND N/A

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %





V1 TOGA V1 TOGA

VR v FLEX VR v FLEX









Time EVENTS

AP

FD

ATH

R T

RK

-FPA

2:15 INIT HOLDING POINT LFZZ 33R - GW 385 t - Co route PAT 33R

19 - TAKE OFF v v20 - CLIMB TO 4000 FT v v v21 - FLAPS LOCKED (WING TIP BRAKES) v v v22 - NDB APP (FLS) - LFZZ 33R v v v v

2:40 23 - LANDING - NO FLAPS

INIT HOLDING POINT LFZZ 33R - GW 385 t CO Route AIBAIB1

24 - TAKE OFF v v25 - CLIMB FL 70 v v v26 - FMS 1 + 2 FAULT v v v27 - DESCENT v v v28 - ILS APP (RAW DATA) - LFZZ 33R v

3:15 29 - LANDING

INIT HOLDING POINT LFZZ 33R - GW 385 t CAVOK - 240/20

30 - TAKE OFF - CROSSWIND v v31 - VISUAL PATTERN v v32 - LANDING - CROSSWIND

IF 2 CAPT: INIT APPROACH - LFZZ 33R

33 - ILS APPROACH (EMER ELEC CONF) v34 - LANDING

3:30 INIT TAKE OFF LFZZ 06 - GW 500 t ZFW 350 t - FOB 150 t

35 - TAKE OFF - ENGINE FIRE v v36 - REJECTED TAKE OFF37 - EMERGENCY EVACUATION


FFS 4 - TRAINEE 2

FEB 2009Issue 05


HANDLING PHASE

ffs4gd.fm


02.0302.03


• To operate the aircraft in normal and abnormal situations according to SOP’s• To practice no flaps approach and landing• To practice emergency electrical configuration including approach and landing in direct law


A. REVIEW

• SOP’s - Task sharing• Non Precision Approach using FLS• Rejected Take-off

B. NEW EXERCISES / REFERENCES

ELEC emergency configuration• FCOM/ABNORMAL OPERATIONS/Electrical/Emergency Electrical Configuration• FCOM/Procedures/Abnormal and Emergency Procedures/24-Electrical/ELEC EMER

CONFIG

Landing with Flaps locked• FCOM/Procedures/Abnormal and Emergency procedures/27-Slats-Flaps/FLAPS LOCKED

and FLAPS SYS 1+2 FAULT

FMS 1+2 FAULT• FCOM/Procedures/Abnormal and Emergency procedures/22-Flight Management System/

FMS 1+2 FAULT• FCOM/Aircraft Systems/34-Navigation/Standby Instruments

C. SUPPORT


03 - SESSION PROFICIENCY CRITERIA

• Demonstrate the ability to perform all exercises, using the correct procedures and techniques in accordance with SOP's

• Understanding of all new A380 features• The trainee is proficient in all exercises listed for the issuance of the type rating



ffs4gd.fm


HANDLING PHASE


1 :- Departure under MEL: FLAPS SYS 1 FAULT

7 :- Insert FLAPS SYS 2 FAULT after Flaps retraction

IF 2 CAPT :- INIT APPROACH at 12 NM: do not reset the all generators failure

21 :- Insert flaps locked by wingtips brakes when flaps are below 1

INIT HOLDING POINT 33R :- F/PLN: 33R - MOU 1N - MBY - ROA - ILS 33R

26 : - At 4000 ft insert FMC C FAULT: use of reset procedure- FL 70: insert FMC A+B FAULT

• FOR NAVIGATION : Show the different items of the SFD and SND menu.- Insert on the SND 2 or 3 waypoints (MBY: 109.6 - N4632.5 / E00330.0 and ROA for example) and AIB as a fix. - Explain that you can insert a FIX in the SND and a different one in the SFD.- Make a Direct TO using the LS / D . Explain that this pb has 2 functions: 1 - DIR TO on SND, 2 - Display of LS scale on SFD.- Explain the MODE pb.

• FOR NAVAID TUNING : Demonstrate how to insert navaid frequencies and courses on RMP STBY RAD NAV.

35 :- Runway 06- Rejected take-off at V1 - 15 kts

FFS 4 SESSION GUIDE

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