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TABLE OF CONTENTS

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02.00

02.01 - INTRODUCTION

02.02 - TRAINING FOOTPRINT

02.03 - GROUND PHASEMFTD A (COCKPIT AND SYSTEMS PRESENTATION)..........1MFTD B (FMS)..........................................................................3MFTD C (FMS) .........................................................................5MFTD D (SYSTEMS REVIEW).................................................7MFTD 1 (SOP) ..........................................................................9MFTD 2 (SOP) ..........................................................................11MFTD 3 (SOP) ..........................................................................13MFTD 4 (SOP) ..........................................................................15MFTD 5 (Failures) ....................................................................17MFTD 6 (Failures).....................................................................19MFTD 7 (Progress Check) ........................................................21

02.04 - HANDLING PHASEFFS 1 ........................................................................................1FFS HUD FAMILIARIZATION (HUD OPTION) .........................See LF35FFS 2 ........................................................................................3FFS 3 ........................................................................................5FFS 4 ........................................................................................7FFS 5 ........................................................................................9FFS 6 ........................................................................................11FFS 7 ........................................................................................13

02.05 - ALOFT (AIRBUS LINE ORIENTED FLIGHT TRAINING)

FLIGHT CREW TRAINING PROGRAM

FLIGHT CREW STANDARDADAPTEDFIRST TYPE RATING ON MULTI-PILOT AIRPLANE TRANSITION COURSE

FEB 2009Issue 05

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02.01INTRODUCTION

01 - GENERAL

A. PHILOSOPHY OF THE COURSES

The Flight Crew Transition Courses are based on the following three principles :

• Systematic approach to instruction,• Learning by doing,• Training to proficiency.

a. Systematic approach to instruction :

The task of training must be considered as a whole and an instruction system must be defined to achieve the training objectives. These objectives are determined by a task analysis. Methods and means necessary to implement the instruction system are cho-sen for their qualities and adaptability to the objectives.

b. Learning by doing :

Practical systems training is progressively introduced with the implementation of the Standard Operating Procedures (SOP’s), crew concept and task sharing in a close to real environment using the MFTD (Maintenance and Flight Training Device) functionality.

c. Training to proficiency :

At the end of the training program, the crew must be able of carrying out their tasks safely and efficiently, in accordance with the training objectives. Therefore, it is not pos-sible to permit a trainee to move up from one phase to the next until he has acquired the skills necessary to complete the objectives.

NOTE : CRM (Crew Resource Management) is fully integrated in the Type Rating courses.

B. PREREQUISITES

(Defined by clause 16 in aircraft purchase contract.)

In order to ensure consistent proficiency at the end of the course, minimum experience is required for entry. The prerequisites listed below are the minimum requirements specified for Airbus Training.The entry level prerequisites for the Type Rating courses are mandatory. If pilots do not meet these prerequisites, Airbus Training may provide ELT (Entry Level Training approved by Airbus Training) at Customer's request.

If the appropriate regulatory agency and/or specific airline policy demands greater or additional requirements, they will also apply as prerequisites.


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a. Captain Prerequisites

Previously qualified on JAR / FAR 25 turbojet aircraft equipped with glass cockpit tech-nology including FMS and commercial operations.

• Valid and current ATPL,• Previous command experience,• Jet experience,• Fluent in English 1,• Flight time :

- 1 500 hours as pilot,- 1 000 hours on JAR / FAR 25 aircraft,- 200 hours experience as airline, corporate or military transport pilot.

If prerequisites are not fulfilled, the trainee’s file will be studied on a case by case basis, and a training proposal will be given by Airbus Training.

b. First Officer Prerequisites :

Previously qualified on JAR / FAR 25 turbojet aircraft equipped with glass cockpit tech-nology including FMS and commercial operations.

• Valid and current CPL with IR • Jet experience• Fluent in English1,• Flight time :

- 500 hours as pilot- 300 hours on JAR/FAR 25 aircraft- 200 hours experience as airline, corporate or military transport pilot.

If prerequisites are not fulfilled, the trainee’s file will be studied on a case by case basis, and a training proposal will be given by Airbus Training.

Note: According to AMC FCL 1.261(c)For multi-pilot aeroplanes where the student pilot (captain and first officer) has morethan 500 hours MPA experience in aeroplanes of similar size and performance, BaseTraining should include at least 4 landings of which at least one should be a full stoplanding.In all other cases the student should complete at least 6 landings.

C. REGULATION REFERENCES

The course and skill test have been designed taking into account the following regulation references.- ICAO - Annex 1 Personnel licensing- French DGAC - Arrêté du 29 mars 1999 (FCL 1) modifié relatif aux licences et qualifications de membre d’équipage de conduite avion- JAR-FCL1- FAR 121- FAR 142

1. When the Trainee does not speak English or is not fluent enough to follow our Standard course he will follow the Language Adapted course (specific language adaptation).

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02 - TRANSITION COURSES AND FAMILIARIZATION COURSE DESCRIPTION

A. TRANSITION COURSES

• The Standard transition course is the basic transition course The HUD OPTION includes CBT that must be completed prior to the HUD Familiarization FFS session (after FFS 1 of standard transition course). FFS 2 to FFS 7, LVO and Skill Test are then conducted with the HUD deployed.

• The Language Adapted course is designed from the Standard course and consists of :- Projected CBT with an instructor,- Extra MFTD (Maintenance & Flight Training Device) and simulator sessions (spare sessions). TBD

NOTE : Transition courses are performed on the base aircraft.

B. FAMILIARIZATION COURSE

Same Type Rating permits the carry-over of total credit for crew qualifying from one variant of aircraft type to another, based on common cockpit and flight characteristics.It allows pilots to get a single type rating to fly all the variants of a same aircraft family,provided they performed the relevant Familiarization Course :

A380-800 RR to EA Familiarization Briefing 1:00 of CBT (ATA 70) A380-800 EA to RR Familiarization Briefing 1:00 of CBT (ATA 70)

Familiarization course is self-study training.This self-study training shall be completed before base training (if applicable). The level of knowledge will be assessed during the briefing.

03 - COURSE ORGANISATION

A. DESCRIPTION

The instruction concept applied by Airbus uses a program divided into phases.Airbus Airport is used for most of the sessions.

a. Ground phase• Welcome briefing (day 0) : general introduction presenting :

- Airbus Training Center - Course description- Airbus electronic documentation

• Airbus Procedure Pilots Interactions (APPI) module :This presentation is given on day 6 and explains that a safe and efficient flight can be achieved by a good interaction between aircraft cockpit, procedures and pilots.

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The content is :I. Airbus cockpit philosophyII. Airbus proceduresIII. Pilots : identifiy and understand some human behaviours (individual and collective)

that are likely to induce risk in operational situation.IV. Aircrat cockpit, Procedures, Pilots Interactions : illustrate how

- Airbus cockpit- Airbus procedure- Pilots

Interact in real life through operational scenario.

1. CBT (Computer Based Training)• The aircraft systems study is progressively introduced until day 8 and is carried out in a

classroom. From day 8 onwards, the trainee will continue to study the aircraft systems using the MFTD, the FCOM and if necessary CBT.The aim is to review and reinforce systems knowledge, in order to pass the systems Test on day 15.

2. MFTD (Maintenance and Flight Training Device)• The training is fully integrated which means that all the systems knowledge acquired in

the CBT is reinforced and evaluated in the MFTD using the Airbus Standard Operating Procedures : this training device (equipped with tutorial modes) allows to learn the normal and abnormal operations using task sharing and crew coordination which save precious FFS time.

• The MFTD is used: • to study and reinforce systems knowledge (MFTD A, B, C, D) • to introduce and to be proficient in SOP, systems knowledge and systems handling

(MFTD 1-7).Sessions 1 to 7 are scheduled for 4 hours.

Trainee’s session preparation :The session is prepared using:- Tutorials available in the Procedure Data Package (PDP: DVD 1)- The OIS OPS LIBRARY (FCOM and FCTM) and PERF APPLICATIONS on the laptopPDP is the support used during MFTD sessions.

Conducting the session :Each session of 4 hours includes 30 minutes of questions and answers.For each new exercise, the instructor uses a slot of this allocated time to- describe the objectives and the key points- explain how the exercise will be conducted (learning by doing)

Consequently, a session will be a succession of short briefing followed by an exercise practice.As the trainee has reviewed the tutorials before the session, the instructor conducts his session by displaying the master slide of each tutorial. This will be indicated by a "T" in the syllabus in front of the exercise.


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This master slide should be enough to conduct the exercise, but if necessary, trainees or instructor can access to any level of tutorial information for knowledge reinforce-ment.The briefings (also referred to as Q&A : Questions & Answers), and debriefings are fully integrated in each MFTD session. A debriefing will be carried out at MFTD 7 (Progress Check), according to trainee per-formanceGSI may run MFTD A, B, C and D. SFI may run all MFTD sessions.

3. OIS (On board Information System) and PERFORMANCE COURSE• One day is dedicated to performance training, and Onboard Information System (OIS)

presentation.

4. CABIN• Doors and slides operations are presented in the CBT by means of videos and in a

cabin training device.

5. SYSTEMS KNOWLEDGE AND PERFORMANCE TESTS• At the end of the Ground phase the Trainee will be evaluated on :

- Systems knowledge using an "electronic" test based on randomised questionnaire,- Aircraft performance using a "paper" test.

b. Handling phase

This phase using FFS (Full Flight Simulator) is mostly dedicated to aircraft handling in Normal and Abnormal operations. All exercises are completed in a realistic environment and allows the crew to practice Standard Operating Procedures previously learnt in the MFTD.Briefing guides (DVD 1) are used to brief FFS sessions.SFI may run all sessions.

c. ALOFT phase

A ALOFT (Airbus Line Oriented Flight Training) session is defined to summarize all the exercises learnt throughout the course and to give the trainee experience in operating the aircraft in real time scenarii.ALOFT are conducted by TRI / E

d. Skill Test phase

According to the JAR - FCL recommendations, the Skill Test syllabi have been designed in a commercial air transport environment.They consist of :• 1st part : a real time sector with some specific events.• 2nd part : additional part to deal with the remaining items to be performed by the

trainee in order to fully satisfy the JAR - FCL requirements.


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e. Base training phase

Two options are provided to the Custormer according to regulation requirements and airline request:- Aircraft Base Training (Flight = 0:45 / pilot)OR- Zero Flight Time Training (FFS ZFTT = 4:00 / crew)

Note: Before the base training, if applicable, the trainees must review the walkaround 3D located in the hard disk of the trainee’s laptop.

B. INSTRUCTOR BRIEFING

The instructor will make a briefing whose duration is stated in the table below within a reasonnable time frame before FFS session :

1. According to Trainee’s performance

C. TRAINING DOCUMENTATION

- DOCUMENTATION USER GUIDE

Briefing / debriefing duration per session :BRIEFING DEBRIEFING

- Handling FFS 1:30

At instructor's discretion1

- ALOFT FFS 1:00- Skill test FFS 1:00- Low Visibility Operations 1:00- Base Training / ZFTT 1:00


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DOCUMENTATION USER GUIDE A380The following documentation (trainee’s booklet) is given to you on the day of your arrival dur-ing the welcome briefing 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-AIRBUS TRAINING AIRPORT JEPPESEN CHARTS(For Airbus Training Centres ONLY)-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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02.01

04 - CRITERIA OF PROFICIENCY

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 :

Additional training using the CBT will be determined by the instructor in coordination with Airbus Training Director. The student will then undertake an additional CBT exami-nation.

D. MFTD AND FFS NOTATIONS

NOTE : this chapter is applicable to all Airbus Type Rating courses. The following sample is from a “Standard course”, but the way to fill a Trainee’s Record remains the same whatever is the Type Rating Course being followed.

Three boxes are used to record the overall trainee’s performance using “Trainee’s Record” file (see page 10 / page 11)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 15) 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 16) have to be commented and use the same identification as the session involved.


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INTRODUCTION

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INTRODUCTION

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TRANSITION COURSES

INTRODUCTION

Page 15A380

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02-01.fm


INTRODUCTION

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02-02.fm

STANDARD COURSE

TRAINING FOOTPRINT

Page 1A380

02.02L F2S

02.02TRAINING FOOTPRINTNG FOOTPRINT

01 - TRAINING DEVICE TIME SHARING PER PHASETotal : 24 working days (excluding low visibility operations and base training) - 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.

Trainee’s Welcome (Administration)Welcome BriefingE-doc Briefing

1:00 1:30 1:00

A. Ground phase 15 working daysAPPI (Aircraft Procedures Pilots Interactions)CBT : Aircraft systemsOIS and Performance courseCEET (Cabin Emergency Exit Training)Cabin trainer : Safety doors Systems test & debriefing Performance test & debriefing MFTD A, D session : 2 x 2 hoursMFTD B, C, 1 to 7: 9 x 4 hoursMFTD 7 debriefing : 1 x 0.5 hour

2:3038:05 5:00 1:00 1:00 4:00 2:00 4:0036:00 0:30

B. Handling phase 7 working daysBriefings & debriefings :7 x 2 hoursFFS sessions : 7 x 4 hoursHUD Option CBTFFS HUD Familiarization (option) : 1 x 2 hours

1 x 4 hours

14:0028:00 3:00

2:00 or 4:00

C. ALOFT phase 1 working dayBriefing & debriefing : 1 x 1.5 hoursFFS session : 1 x 4 hours

1:304:00

D. Skill test phase 1 working dayBriefing & debriefing : 1 x 1.5 hoursFFS session : 1 x 4 hours

1:304:00

E. Low visibility operations (Optional) 1 working dayCBTBriefing & debriefing : 1 x 1.5 hoursFFS session 1 x 3 hours or 1 x 4 hours

3:001:303:00 or 4:00

F. Base training phase 1 working dayWalk around 3D (Self Study)Aircraft flight orZFTT : FFS session : 1 x 4 hours

1:30 0:45 hour / trainee4:00


TRAINING

FEB 2009Issue 05

Recto page to be printed on yellow colour paper. -------------------------------------- Page recto à dupliquer en jaune.

02-02.fm

Page 2STANDARD COURSE

TRAINING FOOTPRINT

02.02A380 L F2S

02 - STANDARD COURSENote : To follow your course, please DO NOT respect the workstation CBT ATA numerical order but follow the ATA chapter in the same order as presented in the present footprint table.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 1 day has been completed before the next day.Day 0: Administration 1:00 - Welcome briefing: 1:30 - E-doc briefing: 1:00

Note : * HUD option: on day 17, HUD CBT module and FFS familiarization (for detailed program of FFS refer to LF35).

HUD CBT module must be studied before FFS session.

Day 1 Day 2 Day 3 Day 4 Day 5

- Intro : 0:10- Aircraft general (ATA 20) 0:20- Indicating & recording (ATA 31) 3:30- APU (ATA 49) 0:20- Lights (ATA 33) 0:30- Autoflight (ATA 22) 2:30

- Autoflight (ATA 22) 4:00- Power Plant (ATA 70) 1:20- Hydraulic system (ATA 29) 0:40

MFTD A(2:00)

- Hydraulic system (ATA 29) 0:40- Pneumatic (ATA 36) 1:00- Air conditioning (ATA 21) 2:00- Oxygen (ATA 35) 0:20

MFTD B(4:00)

- Fire & Smoke protection (ATA 26) 1:00- Electrical (ATA 24) 1:30- Doors (ATA 52) 0:30- Fuel (ATA 28) 1:00

MFTD C(4:00)

- Fuel (ATA 28) 2:30- Navigation (ATA 34) 2:30- Landing gear (ATA 32) 1:00

MFTD D(2:00)


APPI (2:30)

- Landing gear (ATA 32) 1:40- Flight Controls (ATA 27) 3:30- Operating limitations (ATA 20) 0:20

- Information system (ATA 46) 1:40- Avionics network (ATA 42) 1:00- E-logbook 0:40

OIS & PERFORMANCE

(5:00)

- Communication (ATA 23) 0:40- Ice & rain protection (ATA 30) 0:30

MFTD 1(4:00)

MFTD 2(4:00)

MFTD 3(4:00)


MFTD 4(4:00)

MFTD 5(4:00)

MFTD 6(4:00)

CEET safety presentation self

study (1:00)

- Cabin presentation (ATA 25) 0:25

MFTD 7(Progress Check)

(4:00)

Systems Test(4:00)

Performance Test

(2:00)Door Trainer

(1:00)


FFS 1 (4:00)

FFS 2* (4:00)

FFS 3 (4:00)

FFS 4 (4:00)

FFS 5 (4:00)


FFS 6 (4:00)

FFS 7(4:00)

ALOFT(4:00)

Skill Test(4:00)

Walkaround 3D

LOW VIS(4:00)


mftdA.fm

Page 1A380

02.03STANDARD COURSE

GROUND PHASE L F2S

E

E

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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GROUND PHASEL F2S



STANDARD COURSE

GROUND PHASE

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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


mftdAgd.fm

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GROUND PHASE

Page 2B02.03L F2SA380

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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GROUND PHASE

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02.03L F2SA380

Page 2C

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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Page 2D02.03L F2SA380

- 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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02.03L F2SA380

Page 2E

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

INSTR

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mftdAgd.fm

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Page 2F02.03L F2SA380


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Page 3A380


GROUND PHASE L F2S

E

E

WEATHER LFZZ 040/10 3000 OVC 010 15/10 1010 BIKF 030/10 3000 OVC 005 12/10 1010

ACTIVE / INIT

FLT NBR A/L ID 102

FROM LFZZ TO BIKF ALTN EINN

CPNY RTE AIBKEF

ALTN RTE KEFSNN

CRZ FL FL 360 CRZ TEMP -55°C

CI 90 TROPO 36090

TRIP WIND TL20

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 ATN 1N) ANTI ICE OFF PAX NUMBER : 300





VR 128 v FLEX 56 °C VR 126 v FLEX 56




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

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

1 - MFD ARCHITECTURE- MFD SYSTEM MENU- MFD GENERAL MENU BAR- USE OF KCCU AND HARD KEYS

2 - FMS INITIALIZATION- INIT - STATUS- IRS- DEPARTURE- NAVAIDS- FUEL & LOAD- T.O PERF- SEC


MFTD B (FMS) - TRAINEE 1

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GROUND PHASEL F2S

WEATHER LFZZ 040/10 3000 OVC 010 15/10 1010 BIKF 030/10 3000 OVC 005 12/10 1010

ACTIVE / INIT

FLT NBR A/L ID 102


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND TL20

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %






VR 128 v FLEX 56°C VR 126 v FLEX 56




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

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

3 - TAKE OFF4 - CLIMB (MANAGED)

- PERF : PHASES OF FLIGHT- SPEED & ALTITUDE CONSTRAINTS

5 - CRUISE- LATERAL REVISIONS- VERTICAL REVISIONS- F-PLN INFO MENU

6 - APPROACH PREPARATION- F-PLN- PERF- FUEL & LOAD- NAVAIDS- SEC


MFTD B (FMS) - TRAINEE 2

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02.0302.03


• Introduction to FMS architecture & design of interfaces.• Study and practice initialization and use of the FMS through a standard preparation

sequence.• Practice FMS functions through flight phases.

02 - TRAINING TOPICS :

A. REVIEW :

Not applicable.

B. NEW EXERCICES :

• FMS ARCHITECTURE : FMS / ATC COM / SURV / FCU BKUP• FMS MENU : ACTIVE / POSITION / SEC / DATA• ACTIVE MENU : F-PLN / PERF / FUEL & LOAD / WIND / INIT• POSITION MENU • SEC MENU• DATA MENU• FMS FLIGHT PHASES• FMS REVISIONS

C. SUPPORT :

• DVD 1 : Procedure Data Package (PDP) • FCOM• FCTM

D. REFERENCES :

• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description /

Flight Planning• KCCU / Controls & Indicators

03 - SESSION PROFICIENCY CRITERIA :

• Understanding of FMS architecture and FMS functions.• Demonstrate satisfactory skill on preparation.

MFTD B (FMS) SESSION PREPARATION


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Page 4B02.03A380 L F2S

Standard crew : captain is trainee 1 and first officer is trainee 2 throughout the course (from MFTD B to FFS 7).Non standard crew : instructor determines Trainee 1 and Trainee 2 for first session, and maintains it throughout the course.

General recommandation :Use the freeze function when neededDon’t teach SOP’s during this MFTD sessionHighlight all FMA mode changes and selected / managed philosophy

INIT TAKE OFF . Cockpit prepared by instructor

1 . - Demonstrate the use of KCCU and MFD hard keys. Explain that the KCCU has 2 parts :

CCD : Cursor Control Device (trackball + wheel)KBD : Key Board

Highlight that if the CCD fails, the KBD allows any selection on MFD page via hardkeys. If the keyboard fails, the CCD allows to select any menu or field, and when a value needs to be inserted, a SOFT KEY BOARD appears to enter data.- Explain the USE of the hard key KBD: In case of partial CCD or keyboard failure, allows to display the soft keyboard without selecting the KBD switch to OFF- Present the overvall architecture of the MFD FMS, ATC COM, SURV and FCU BKUP : don’t spend time to explain this menu- Show the 4 menus without spending time on each page which will be studied progressively in an operational context :

ACTIVE : related to F-PLNPOSITION : related to aircraft position and position computationSEC : 3 secondary F-PLNDATA : data base related or pilot insertion

- Use the PERF page to explain the panels (TO,CLB,CRZ...)

2 . - Explain that the sequence of the INIT is ensured thanks to the automatic cursorjump from one field to another. This process has been designed to support the crewin initialising the F-PLN and must be used. Highlight the fact that this automatic cur-sor jump is not available on the fields that are not often used (eg. CRZ temp, tropo-pause, THR RED, ACCEL...): to recover the cursor jump, re-insert the value bydefault- INIT hard key : press- STATUS : explain the page and don’t go to FMS P/N- INIT : Do not explain all the REQUEST options- IRS : Show the option to "ALIGN ON OTHER REF"- DEPARTURE :

F-PLN review according to the electronic F-PLN (or co-route) or to the charts,using the RTE SUMMARY function

- NAVAIDSShow TUNED FOR DISPLAYShow the TUNED FOR FMS NAV : how to deselect NAVAIDS

MFTD B (FMS) SESSION GUIDE

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- FUEL & LOAD- PERF

Show all the flight phasesExplain TOGA, FLEX, DERATEDShow ARMED Modes on FMA

2 end : - SECSEC 1 : import "FROM ACTIVE"SEC 2 : import "FROM ACTIVE" and modify the runway for departure (RWY 24)

Note : During aircraft initialization, highlight the fact that messages are displayed inthe message pad at the bottom of the MFD : CLEAR INFO pb is used to clear themessages. Reinforce how to modifiy or clear a field : BACKSPACE + ENTERReinforce how to recover the cursor when a field is active : ESC

Explain interactivity between MFD, AFS - CP, EFIS - CP, PFD and ND.Explain FMA philosophy.

AFS - CP reinforce all knobs / pushbuttons

- Set FD ON: on PFD, reinforce FMA philosophy

- Show FMA- Show SPD / HDG / V/S windows dashed on AFS CP

- Set FD OFF: highlight changes• Show FMA• Show SPD / HDG / V/S windows no more dashed

EFIS CP reinforce all knobs / pushbuttons

- Set FMS F-PLN page on MFD- Set EFIS CP in plan mode, CSTR

• Scroll the F-PLN to show F-PLN color coding on the ND- PRIMARY F-PLN GREEN solid line until destination airport- Missed Approach Procedure BLUE solid line- ALTERNATE F-PLN BLUE dashed line

ATHR mode Vertical mode Lateral mode Capability Status

Active mode Active mode Active modeApproach

AP

Armed mode Armed mode Armed mode FD

Presel speed Information Minimum ATHR

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- Set FMS PERF page on MFD• Explain FMS flight phases philosophy (8 phases)• Explain that all FMS phases have an associated TAB in the PERF page,

except PREFLIGHT and DONE phases. This TAB is green when the phase is active, otherwise white

3 : - Freeze as necessary (step by step) to highlight FMA mode changes and PFD characteristic speed targets.

4 : - During Take-off and climb show the flight phase automatic swichting (PERF page)- F-PLN : demonstrate how to swap between SPD ALT and EFOB T.WIND. Explainthat lateral and vertical revisions are accessible either by a menu which opens whenclicking on a waypoint or by the menu FPLN INFO. The difference between these 2possibilities is that the revisions from the menu FPLN INFO are related to the wholeFPLN and the other to a waypoint.- Demonstrate how to insert speed or altitude constraint either from the F-PLN orfrom lateral revision at a waypoint.

5 : - At altitude capture explain FMA changes and automatic flight phase switching- Explain and use all the lateral and vertical revisions at applicable waypoints. Don’tspend too much time on lateral or vertical revisions which are not often used and willbe reviewed during IOE (Initial Operating Experience).- POSITION MONITOR : explain the content and highlight where to find the BRG / DIST TO - DIRECT TO :

- Use hard key DIR for DIRECT TO demo- Use DIRECT TO option in F-PLN for DIRECT TO ABEAM demo- Use lateral revision FROM P.POS DIRECT TO for DIRECT TO CRS IN or OUT

demo- Demonstrate OFFSET, OVERFLY (DELETE) and waypoint DELETE

Explain the " * " associated to some lateral and vertical revisions. No " * " means a submenu is available. " * " means, when clicked, direct access to the function, creating a TMPY FPLN.

Demonstrate the insert next WPT option and insert new destination : LFZZ

6 : - Approach preparation according to the predefined flow (ACTIVE, POSITION, SEC):ILS LFZZ 33R

Instructor starts the engines and initializes the aircraft ready for take-off - Initial altitude FL 70 (on AFS CP). During take off, instructor will assist the trainee with thrust setting and aircraft clean-up

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GROUND PHASE L F2S

E

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WEATHER LFZZ 330/15 9999 BKN 025 25/12 1010

ACTIVE / INIT

FLT NBR A/L ID 103

FROM LFZZ TO LFZZ ALTN LFLL

CPNY RTE -

ALTN RTE AIBLYS


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 : AIR COND ON LFZZ - MOU 1N - UM 129 - BEBIX ANTI ICE OFF UN 859 - TUGLI - MALEB - ROA -LFZZ PAX NUMBER : 303









V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

INIT TAKE OFF - LFZZ 33R - GW 385 t

1 - DATA- WAYPOINT- NAVAID- ROUTE- AIRPORT

2 - FMS INITIALIZATION- INIT - IRS- DEPARTURE- NAVAIDS- FUEL & LOAD- T.O PERF- SEC

1:00 3 - TAKE-OFF4 - CLIMB FL 1805 - CRUISE

- MANAGED SPEED- SELECTED SPEED

6 - DESCENT7 - APPROACH PREPARATION8 - ILS APPROACH

- DECELERATED- MANAGED SPEED

2:00 9 - GO AROUND


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GROUND PHASEL F2S

EWEATHER

LFZZ 150/15 9999 BKN 025 25/12 1010 LFLL 180/10 9999 OVC 030 26/11 1009

ACTIVE / INIT

FLT NBR A/L ID 103


CPNY RTE -

ALTN RTE LYSAIB


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 : AIR COND ON LFZZ - ONZON 1S - ROA - DIRBA - ANTI ICE OFF TALAR... LFLL PAX NUMBER : 302


ACTIVE / PERFLFZZ 15L / GW 385 t







V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

INIT TAKE OFF - LFZZ 15L - GW 385 t

2:15 10 - FMS INITIALIZATION- INIT

- IRS- DEPARTURE- NAVAIDS- FUEL & LOAD- T.O PERF- SEC

3:00 11 - TAKE OFF 12 - CLIMB FL12013 - CRUISE

- ND INTERACTIVITY14 - DESCENT15 - APPROACH PREPARATION16 - ILS APP LFLL 18L

- STABILIZED- SELECTED SPEED

3:30 17 - GO AROUND18 - HOLDING PATTERN19 - ENABLE ALTERNATE20 - DCT EB

IF TIME PERMITS

21 - APPROACH PREPARATION22 - RADAR VECTORS23 - ILS APP LFZZ 33R 24 - AUTOLAND


MFTD C (FMS) - TRAINEE 1

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02.03


• Practice FMS initialization• Practice FMS functions during a flight sequence with diversion to alternate airport.


A. REVIEW :

• FMS ARCHITECTURE : FMS / ATC COM / SURV / FCU BKUP• FMS MENU : ACTIVE / POSITION / SEC / DATA• ACTIVE MENU : F-PLN / PERF / FUEL & LOAD / WIND / INIT• POSITION MENU • SEC MENU• DATA MENU• SPEED / ALT CST• FMS REVISIONS

B. NEW EXERCICES :

• ND INTERACTIVITY• DESCENT• ILS APPROACH• GO AROUND• HOLDING PATTERN• ENABLE ALTERNATE• SEC FPLN• FMS REVISIONS :

- AIRWAYS- NAVAIDS DESELECTION

C. SUPPORT :

• DVD 1 : Procedure data package (PDP) • FCOM • FCTM

MFTD C (FMS) SESSION PREPARATION


mftdCgd.fm

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GROUND PHASE


D. REFERENCES :

• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description /

Flight Planning / Lateral Flight Plan• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description /

Flight Planning / Vertical flight plan• FCOM /Aircraft Systems /ATA22-AFS-Flight Management System/ System Description /

Flight Planning / Secondary Flight Plans• FCTM / Normal Operations / • FCTM / Normal Operations / ILS Approach


• Knowledge of FMS functions, MFD pages and use of KCCU.• Ability to program the FMS.

FLIGHT CREW TRAINING PROGRAMFLIGHT CREW TRAINING PROGRAM NOV 2007Issue 03

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02.03

General recommandation :Use the freeze function when neededDon’t teach SOP’s during this MFTD sessionHighlight all FMA mode changes and selected / managed philosophy

INIT TAKE OFF : Cockpit prepared by instructor

1 : - Demonstrate how to obtain data related toWAYPOINTNAVAIDROUTEAIRPORT

- Don’t insist on the PRINTER list (IOE item)

2 : Initialize the FMS using the predetermined flow (curser jump)- INIT : don’t insert a CO RTE and build the P-FLN using AIRWAYS and INSERT NEXT WPT options.- NAVAID : Deselect "ATN" VOR- SEC 1 : Insert in the INIT: LFZZ/LFLL with the CO RTE AIBLYS : modifiy the depar-ture (ONZON 1N)

4 : - After Take-off provide radar vector and altitude changes to demonstrate the following :

- Switching from CLB to OPCLB ; altitude constraint not considered- How to reengage NAV and CLB to respect altitude constraint- Final cruise altitude : FL 290 explain how to obtain ALT CRZ on FMA- Demonstrate how to select AIRWAYS in FMS revisions

5 : - Present the PERF CRZ page and explain the different cruise speeds

6 : - Start descent after the top of descent- Explain Flight phase switching : CRZ to DES- Explain speed control in Managed profile- Explain switching DES to OPDES

MFTD C (FMS) SESSION GUIDE


Instructor assists the trainees for aircraft configuration and during the Go-around

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8 : - Decelerated approach : demonstrate the following :Flight phase switching : DES to APPRExplain the 2 possibilities- automatically : overfling D point- manually : activate APPR phase. Show the field on the PERF PAGE, which isat the same position as INSERT field of other page. Insist about the importanceto read the label of the field to avoid confusion between insert and activateExplain speed target is VAPP, observe short term managed speed according tothe configurationUse of approach mode : LOC and G/S interception (FMA).0

9,17 : - Explain flight phase switching APPR to GA- Explain the FMA modes- Show that missed approach procedure changes from BLUE solid line to GREENsolid line on the ND. At the same time show that the ALTERNATE F-PLN changesfrom BLUE dotted line to BLUE solid line- Explain NAV reengagement and clean up procedure using characteristic speeds - 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)

- Explain that predictions are recovered after acceleration altitude

10 : - Initialize the FMS using the predetermined flow (curser jump)- INIT : don’t insert a CO RTE and build the P-FLN using AIRWAYS and INSERT NEXT WPT options.- NAVAID : Deselect "ATN" VOR- SEC 1 : Import from ACTIVE- SEC 2 : Import from ACTIVE and insert a quick return to LFZZ ILS 33R- PERF-CLB : Insert preselect speed 230 kts

11 : After TAKE OFF, show the target selected speed 230 kts on FMA. Explain how torecover managed speed

13 : - Explain all the ND interactivity- From the aircraft- From a waypoint- From the airport

16 : - Stabilized approach :- Select the speed according to the short term managed speed target until VAPPthen manage speed- Point out the successive configuration change at each short term target speedin order to respect "establish in full configuration and Vapp at 1000 ft AGL"

18 : - Insert Holding pattern at ARBON using the DATA BASE computation


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GROUND PHASE L F2S

E

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

ACTIVE / INIT

FLT NBR A/L ID 104


CPNY RTE AIBLYS

ALTN RTE LYSAIB


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 1S) ANTI ICE OFF PAX NUMBER : 303









V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

INIT TAKE OFF - LFZZ 15L - GW 385 tCo-route AIBLYS

REFER SESSION GUIDE

T MODE REVERSIONST GROUND SPEED MINI FUNCTION


MFTD D (SYSTEMS REVIEW)

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02.03


• To reinforce systems studied from day 1 to day 4.• To reinforce FMS system knowledge studied during CBT, MFTD B and C.

- FMS architecture: flight phases.- FMA (Flight Mode Annunciator).- Flight director - AFS control panel.- EFIS control panel

• To introduce: - Reversion modes- GROUND SPEED MINI FUNCTION for target speed in approach

MFTD D : (SYSTEMS REVIEW)


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02 - SESSION GUIDE :

Init Take Off: LFZZ 15L

Instructor sets the MFTD:• Engines OFF• EXT PWR 1, 2, 3, 4: ON• APU: OFF• DOORS: STD doors open• O2 crew supply: OFF• FMS LOADED:

LFZZ/LFLL: Use co route AIBLYS with SID ONZON 1S. Delete ONZON, delete the first ROA WPT to clear discontinuity. LFLL arrival ILS 18L. Fill the APPR page. ALTN FPLN: LFLL/LFZZ: Use co route LYSAIB. Change departure RWY 18L with SID EB 4S. Delete the discontinuity between EB and ROA.

CBT reinforcement studied during day 1 to 4Trainees perform actions requested by the instructor

Select the following SD pages using the ECP pbs

DOOR

• Highlight differences door open (door label amber) and door closed (green). Close all doors

• Arm all slides to highlight changes• Oxygen: highlight CKPT is amber because the O2 supply valve is closed (CREW SUP-

PLY pb-sw OFF). Consequently REGUL PR LO is amber due to low pressure after the supply valve. The cockpit and cabin bottle O2 pressure are indicated in green when pressure is above the minimum required to dispatch. If the pressure is below the mini-mum required to dispatch, the green value appears with an amber half frame. Do not speak about value which are customized according to airline operations.

MFTD D : SESSION GUIDE

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APU• APU fire test. Explain• APU start:

• APU master sw ON reinforce auto display of APU SD: Flap moving / Flap open• APU start pb: ON reinforce GEN A/B connection amber to green parameters / APU

AVAIL on SD, on pb and on EWD memo• SD DOOR page is displayed automatically after 10"• Select APU page• Select APU bleed ON: show bleed status change and APU BLEED memo replacing APU

AVAIL on EWD• Select APU bleed OFF• Insert APU fire extinguishable: demonstrate APU automatic emergency shutdown and

automatic agent discharge. The ECAM requires actions, wait to demonstrate that if pilots do not perform ECAM actions, the system does it automatically.

• Restore. Reset systems. Restart APU.

ELEC

AC• Select EL/AC SD• Demonstrate that each EXT PWR is connected to its assigned AC bus. Show EXT PWR

memo on EWD• Demonstrate that EXT PWR has priority over APU GEN• Switch OFF EXT 1 and 4 and demonstrate

- AC 1 supplied by GEN A- AC 4 supplied by GEN B

• Switch OFF EXT 2 and 3 and demonstrate- APU GEN A supplying AC 1 and 2- APU GEN B supplying AC 3 and 4

NOTE: Remove EXT PWR one by one to highlight the SD page changes, and AVAIL green light disappears on EXT pb.

DC • Select EL/DC SD

• Observe the ELEC DC distribution• Explain TR2 B is back up to TR 2A

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BLEED • Select BLEED page• Select APU bleed ON• Highlight APU bleed supplying both packs through XBLEED valves on BLEED page. It

takes time (around 45") until hot air valves open, which is normal• Select PACK 1 OFF: demonstrate pack and hot air valves closure. Highlight the color

coding change. Show on COND page and PRESS page the changes• Select PACK 1 ON• Select BLEED SD• Select ENG START sel to IGN / START and observe automatic pack closure• Select ENG 3 master lever ON : when ENG AVAIL demonstrate automatic pack open.

Select ENG START sel to NORM• Perform a quick engine start on 1, 2 and 4• When 4 engines AVAIL, highlight APU BLEED priority on ENGINE BLEEDS• Open DOOR MAIN 1L

Highlight:• PACK 1+2 inhibited by door open when engines running• ECAM alert DOOR OPEN and MAIN 1L in amber on door page

Observe DOOR SD replaced by WHEEL SD after engine start

Highlight differences• Engines shutdown: DOOR symbol amber only• Engines running: DOOR symbol amber + DOOR name in amber

• Close the door. Alerts disappear

• Select APU BLEED OFFHighlight• XBLEED VALVES closure• ENG BLEED VALVES open. Each engine supplies its associated pack valve

• Select AC page to demonstrate engine GEN priority on APU GEN• Summary of ELEC priority: ENG GEN > EXT PWR > APU GEN

CAB PRESS

• Select PRESS page• Explain LDG ELEVN 800ft coming from FMS DESTINATION airport• Show the 4 outflow valves open on ground• Select RAM AIR ON: Observe valve open• Select ditching PB-sw ON

• Show the automatic closure of the packs and the 4 outflow valves, and the RAM AIR• Explain that this action is part of the DITCHING procedure in flight or the DE ICING

procedure on ground• Select ditching PB-sw OFF• Select RAM AIR OFF• Select APU OFF• Reset

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FMSThe purpose of this part is to reinforce FMS study, through a flight from LFZZ to LFLL.Reinforce AFS CP UNDERSTANDINGReinforce EFIS CP UNDERSTANDINGReinforce FMA on PFDReinforce FMS phases switching conditions, and associated speed management.

Initialized at take off, LFZZ 15L, aircraft ready:

Take Off to LFLL (20 minutes required) - Select FL 110• Highlight

• Each phase switching condition• All FMA changes• Speed target changes: reinforce all the managed speed changes

• Freeze position and altitude when required to highlight all these changes.• Keep simulation frozen to brief the mode reversions demo using the tutorial.

During climb, demonstrate all the lateral and vertical reversion modes except FD orders not followed.

GROUND SPEED MINI FUNCTION DEMO:• Init APP LFZZ 33R - Keep simulation frozen to brief the demo using the tutorial.

GW: 385 TWind in PERF page: 330/20The purpose is to demonstrate how the target speed changes with wind variation during approach.The exercice starts at 3700 ft from the FAF ILS 33R:1 - At 3700 ft, insert WIND 330/102 - At 3000 ft, change WIND 330/503 - At 2000 ft, change WIND 150/204 - At 1000 ft, change WIND 330/20If necessary between wind changes freeze POS/ALT to highlight the target changes.

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WEATHER LFZZ 240/10 CAVOK 13/10 1020 LFLL 270/10 CAVOK 13/10 1020

ACTIVE / INIT

FLT NBR A/L ID 105


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND TL 15

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t704 000 Ib ZFWCG 35 %





V1 v TOGA V1 v TOGA

VR FLEX VR FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

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

T 1 - USE OF TUTORIALT 2 - PRELIMINARY COCKPIT PREPARATION

(AIRCRAFT NOT ELECTRICALLY SUPPLIED)T 3 - COCKPIT PREPARATION T 4 - BEFORE START / ENG START / AFTER STARTT 5 - TAXI - BEFORE TAKE OFF T 6 - TAKE OFF PACKS ONT 7 - AFTER TAKE OFFT 8 - CLIMB FL 110


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GROUND PHASEL F2S


ACTIVE / INIT

FLT NBR A/L ID 105


CPNY RTE AIBLYS

ALTN RTE LYSAIB


CI 90 TROPO 36090

TRIP WIND HD 15

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 CO-ROUTE AIR COND ON (SID ONZON 1N) ANTI ICE OFF PAX NUMBER : 302




V1 v TOGA V1 v TOGA

VR FLEX VR FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

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

9 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT NOT ELECTRICALLY SUPPLIED)10 - COCKPIT PREPARATION11 - BEFORE START / ENG START / AFTER START12 - TAXI - BEFORE TAKE OFF 13 - TAKE OFF PACKS ON14 - AFTER TAKE OFF15 - CLIMB FL 110



NOV 2007Issue 03

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02.03


• Introduce and practice SOPs and task sharing during : - COCKPIT PREPARATION- BEFORE START / ENGINE START / AFTER START- TAXI & BEFORE TAKE OFF- TAKE OFF / AFTER TAKE OFF.- CLIMB


A. REVIEW :

• Use of FMS through a standard preparation

B. NEW EXERCICES :

• Standard operating procedures during- COCKPIT PREPARATION- BEFORE START / ENGINE START / AFTER START- TAXI & BEFORE TAKE OFF- TAKE OFF / AFTER TAKE OFF.- CLIMB

C. SUPPORT :

• DVD 1 : Procedure Data Package (PDP) • FCOM• FCTM

D. REFERENCES

• PDPNormal operationsCockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + Takeoff + Climb

• FCOMStandard flight profile - SOP's

- Procedures / Normal Procedures / Standard Operating Procedures- Procedures / Normal Procedures / Task Sharing- Procedures / Normal Procedures / Normal Checklists

Use of RMP- Aircraft Systems / 23 - Communication / How to use the RMP / How to tune a frequency

MFTD 1 (SOP) SESSION PREPARATION


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Engine start and engine operation- Aircraft systems / 70 - Engines / Ignition and Starting / Starting / Automatic Starting

Sequence- Aircraft systems / 70 - Engines / FADEC- Aircraft systems / 70 - Engines / Normal Operation

• FCTMNormal operations

- Normal Operations / General + Preliminary Cockpit Preparation + Cockpit Preparation + Before Start + Start + After Start + Taxi + Before Takeoff + Takeoff + Climb + Standard Callouts


• Demonstrate acceptable knowledge of FMS system.• Understanding of SOP’s from cockpit preparation until climb.


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USE OF TUTORIAL :T MANDATORY use of tutorial mode.

2,3 : Highlight the aircraft preparation philosophy.Preliminary cockpit preparation : mainlyperformed by the PNF and easy to memorize through 5 "boxes"

1 - POWER UP (if aircraft not electrically supplied)2 - ECAM / LOGBOOK CHECK3 - APU start4 - NSS / OIS PREPARATION. 5 - Before WALKAROUND

Cockpit preparation : performed in 2 steps- Systems checking/setting and FMS preparation (PF). Select TOGA allowing the

demo of METOTS (RR engine only)- FMS revised by PNF - Glareshield and Instruments panels checking/setting when both pilots seated - SURV page : Explain the controls and STATUS & SWITCHING pages

ELEC : Demonstrate the connection logic- Select EXT 2 : demonstrate that 1 EXT PWR unit is not enough to supply the entireelectrical network - Select EXT 3 to supply the entire network APU : Comment APU start using ECAM APU page.When APU AVAIL, call ECAM ELEC page, point out the priority logic of the EXTPWR on APU GEN.- Select EXT 1 and 4 : highlight the changesFUEL : PUMPS selection MAIN - SBY - Demo SBY - MAIN. Highlight differences

4 : Explain the automatic engine start sequence.When all engines are running, select ECAM ELEC page, to highlight the prioritychanges between engine and APU generator

5 : Explain the functionnality of TAXI camera on PFD for taxi + video selection possibil-ities on SD page.

6 : During take off, point out the following key points. FMA change after take off thrustsetting. 35 kt take off thrust sets "METOTS" on RR only Explain the evolution of ACUTE during take off : - METOTS : Modified Engine Take Off Thrust Setting (Use TOGA in order to observesignificant thrust variations)- After thrust reduction, reference changes from TOGA to GA thrust. This leads to a small change of THR. If FLEX take off THR is well below CLB THR,there will be a washout during +/- 20 sec to reach CLB THR.V1 auto callout VRPitch 12.5°SRS modeThrust reductionThrust acceleration - climb phase

MFTD 1 (SOP) SESSION GUIDE

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FEB 2009Issue 05FLIGHT CREW TRAINING PROGRAM

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MAY 2008Issue 04 FLIGHT CREW TRAINING PROGRAM


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GROUND PHASE L F2S

E

E

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ACTIVE / INIT

FLT NBR A/L ID 106


CPNY RTE AIBAIB1

ALTN RTE AIBLYS


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 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER : 350




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 33 R - GW 385 tCo-route AIBAIB1

1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT NOT ELECTRICALLY SUPPLIED)

2 - COCKPIT PREPARATION3 - BEFORE START / ENG START

AFTER START4 - TAXI - BEFORE TAKE OFF

1:20 5 - TAKE OFF PACKS ON6 - AFTER TAKE OFF7 - CLIMB FL70

T 8 - CRUISE9 - DCT ROA - HOLDING PATTERN

T 10 - APPROACH PREPARATIONT 11 - DESCENT MANAGEDT 12 - ILS APP LFZZ 33R - DECELERATED

2:00 13 - AUTOLAND (DEMO)



FEB 2009Issue 05

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GROUND PHASEL F2S


ACTIVE / INIT

FLT NBR A/L ID 106


CPNY RTE AIBAIB1

ALTN RTE AIBLYS


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 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1N) ANTI ICE OFF PAX NUMBER : 350




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


2:15 14 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT NOT ELECTRICALLY SUPPLIED)

15 - COCKPIT PREPARATION16 - BEFORE START / ENG START AFTER START17 - TAXI - BEFORE TAKE OFF

3:20 18 - TAKE OFF PACKS ON19 - AFTER TAKE OFF20 - CLIMB FL70 21 - CRUISE22 - DCT ROA - HOLDING PATTERN23 - APPROACH PREPARATION24 - DESCENT MANAGED25 - ILS APP LFZZ 33R - DECELERATED

4:00 T 26 - GO AROUND



FEB 2009Issue 05

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• Introduce and practice SOPs and task sharing during : - CLIMB- CRUISE- DESCENT- ILS APPROACH- LANDING- GO AROUND


A. REVIEW :

• Standard operating procedures during :- COCKPIT PREPARATION- BEFORE START / ENGINE START / AFTER START- TAXI and BEFORE TAKE OFF- TAKE OFF / AFTER TAKE OFF- CLIMB

B. NEW EXERCICES :

• Standard operating procedures during :- CRUISE- DESCENT- ILS APPROACH- LANDING- GO AROUND

C. SUPPORT :

• DVD 1 : Procedure Data Package (PDP) • FCOM.• FCTM



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D. REFERENCES :

• PDPNormal operationsCockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + Takeoff + Climb +Cruise + Descent + ILS Approach + Go Around + Landing


- Procedures / Normal Procedures / Standard Operating Procedures - Procedures / Normal Procedures / Task Sharing- Procedures / Normal Procedures / Normal Checklists

FMS INIT: use of SEC- Aircraft Systems / 22 - AFS - Flight Management System / Flight Planning / Secondary

Flight Plans


Engine start and engine operation- Aircraft systems / 70 - Engines /Ignition and Starting / Starting / Automatic Starting



- Normal Operations / General + Preliminary Cockpit Preparation + Cockpit Preparation + Before Start + Start + After Start + Taxi + Before Takeoff + Takeoff + Climb + Cruise + Descent Preparation + Descent + Approach + ILS Approach + Go Around + Landing + Standard Callouts


• Understanding of SOP’s from cruise phase until landing including go around phase.02.03


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2 : FMS initialization performed in the SEC 2. Import SEC 2 into SEC 1SWAP SEC 1 into active FPLN Use of RMP : explain basic functions. Scale 1 is useful. Use of RMP will be rein-forced during FFS session

12 : No radar vectors. Decelerated approach via ROA.

15 : .During FMS preparation :- Switch OFF the KCCU keyboard (KBD) in order to demonstrate the use of soft

keyboard. Fill in the INIT page. Restore- Switch OFF the KCCU Control Cursor Device (CCD) in order to demonstrate how

to fill pages with hard keyboard only - Restore.

25 : Radar vectors. Decelerated approach

26 : After 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)


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NOV 2007Issue 03 FLIGHT CREW TRAINING PROGRAM

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WEATHER LFZZ CALM 8000 OVC 015 16/11 1017 LFLL 180/10 9000 BKN 018 14/10 1016

ACTIVE / INIT

FLT NBR A/L ID 107


CPNY RTE AIBAIB1

ALTN RTE AIBLYS


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 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND OFF (SID MOU 1N) ANTI ICE OFF PAX NUMBER : 250




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)2 - COCKPIT PREPARATION3 - ENGINE START / VALVE NOT OPEN (MMEL)4 - TAXI

1:20 5 - TAKE OFF 6 - CLIMB FL 707 - DCT ROA - HOLDING PATTERN

T 8 - VOR / DME APP LFZZ 33R (FLS)1:50 9 - GO AROUND

10 - VOR / DME APP LFZZ 33R (SELECTED)2:10 11 - GO AROUND



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GROUND PHASEL F2S


ACTIVE / INIT

FLT NBR A/L ID 107


CPNY RTE

ALTN RTE AIBLYS

CRZ FL 4000 ft CRZ TEMP +5°C

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 %

NOTES RWY COND DRY AIR COND OFF ANTI ICE OFF PAX NUMBER : 250




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

INIT APP - LFZZ 24 - GW 385 t

2:25 12 - RNAV APP - LFZZ 24 (FLS)13 - GO AROUND14 - NDB APP LFZZ 33R (SELECTED)

2:50 15 - GO AROUND16 - ILS G/S INOP LFZZ 33R (FLS)

3:10 17 - GO AROUND18 - ILS APP LFZZ 33R - STABILIZED

3:30 19 - AUTOLANDT 20 - AFTER LANDINGT 21 - PARKINGT 22 - SECURING THE AIRCRAFT



MAY 2008Issue 04

STANDARD COURSE

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02.03


• Introduce and practice SOPs and task sharing during : - NON PRECISION APPROACH- AFTER LANDING- PARKING- SECURING THE AIRCRAFT


A. REVIEW :

• Standard operating procedures during :- COCKPIT PREPARATION- BEFORE START / ENGINE START / AFTER START- TAXI and BEFORE TAKE OFF- TAKE OFF / AFTER TAKE OFF- CLIMB- CRUISE- DESCENT- ILS APPROACH- LANDING- GO AROUND

B. NEW EXERCICES :

• Standard operating procedures during :- NON PRECISION APPROACH- AFTER LANDING- PARKING- SECURING THE AIRCRAFT

C. SUPPORT :




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D. REFERENCES :

• PDPNormal operationsCockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + Takeoff + Climb +Cruise + Descent + ILS Approach + Non Precision Approach +Go Around + Landing + Park-ing / Securing the Aircraft




Engine start and engine operation- Aircraft systems / 70 - Engines /Ignition and Starting / Starting / Automatic Starting


Engine Start Valve Manual Operation- Procedures / Supplementary Procedures / Engines / Unusual Engine Starting Procedures

• Master Minimum Equipment List (MMEL)- MMEL Items / 80 - Engine Start / 11- Start System / 80 - 11 -01 Engine Start Valve


- Normal Operations / General + Preliminary Cockpit Preparation + Cockpit Preparation + Before Start + Start + After Start + Taxi + Before Takeoff + Takeoff + Climb + Cruise + Descent Preparation + Descent + Approach + ILS Approach + Non Precision Approach + Go Around + Landing + Parking + Standard Callouts

Use of MMEL- Normal Operations / Flight Preparation / MEL


• Standard knowledge and understanding of non precision approaches.• Ability to program and use FMS through different flight phases.• Standard knowledge of normal SOP’s, task sharing and callouts.


STANDARD COURSE

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3 : Emphasize MMEL consultation. Dispatch with start valve inoperative on engine 3 toperform a manual start valve operation

10,14: On the IOS, insert GPS PRIMARY lost to get F-APP + RAW. Then, on the POSI-TION monitor MFD page, insert RNP less than EPU to get NAV ACCU LOW & FLS:RAW only.

16 : Fail G/S. Demonstrate how to deselect G/S in FMS, in order to fly this approach in LOC - F/GSBefore go around, freeze at MDA-50 ft to demonstrate "DISCONNECT AP FORLDG" message on PFD


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WEATHER LFZZ CALM 8000 OVC 015 16/11 1017 BIKF 180/20 7000 BKN 038 6/2 1016

ACTIVE / INIT

FLT NBR A/L ID 108


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND HD 20

ACTIVE FUEL & LOAD

GW 423 t930 600 Ib FOB 83 t

182 600 Ib

ZFW 340 t748 000 Ib ZFWCG 33,9 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND OFF (SID ATN 1N) ANTI ICE OFF PAX NUMBER : 250




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 33 R - GW 423 tCo-route AIBKEF

1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)2 - COCKPIT PREPARATION

1:30 3 - TAXI4 - TAKE OFF - PACKS OFF5 - CLIMB MANAGED - SELECTED

T 6 - FUEL TRANSFER7 - NORMAL CRUISE FL 3108 - RETURN TO DEPARTURE

2:00 T 9 - JETTISON 10 - APP PREPARATION11 - DESCENT MANAGED - SELECTED

T 12 - ILS G/S FROM ABOVE LFZZ 33R2:20 13 - AUTOLAND



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GROUND PHASEL F2S


ACTIVE / INIT

FLT NBR A/L ID 108


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 300 TROPO 36090

TRIP WIND HD 20

ACTIVE FUEL & LOAD

GW 423 t930 600 Ib FOB 83 t

182 600 Ib

ZFW 340 t748 000 Ib ZFWCG 33,9 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND OFF (SID ATN 1N) ANTI ICE OFF PAX NUMBER : 250




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS


2:35 14 - TAKE OFF - PACKS OFF15 - CLIMB MANAGED - SELECTED FL 120 16 - DIVERSION TO LFLL

3:00 17 - DESCENT PREPARATION18 - DESCENT MANAGED - SELECTED19 - OVERWEIGHT LANDING PROCEDURE (NO JETTISON)20 - ILS APP LFLL 18L

3:30 21 - AUTOLAND22 - AFTER LANDING23 - PARKING24 - SECURING THE AIRCRAFT



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• Introduce and practice SOPs and task sharing during : - FUEL JETTISON- OVERWEIGHT LANDING PROCEDURE- DIVERSION


A. REVIEW :

• Standard operating procedures during :- COCKPIT PREPARATION- BEFORE START / ENGINE START / AFTER START- TAXI and BEFORE TAKE OFF- TAKE OFF / AFTER TAKE OFF- CLIMB- CRUISE- DESCENT- ILS APPROACH- LANDING- AFTER LANDING- GO AROUND- PARKING - SECURING THE AIRCRAFT

B. NEW EXERCICES :

• Standard operating procedures during :- FUEL TRANSFER- FUEL JETTISON- DIVERSION- OVERWEIGHT LANDING PROCEDURE

C. SUPPORT :




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D. REFERENCES :

• PDPNormal operationsCockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + Takeoff + Climb +Cruise + Descent + ILS Approach + Go Around + Landing + Parking / Securing the Aircraft

Abnormal operationsFuel Jettison




Weight and Balance- Limitations / Weight and Center of Gravity Limits- Performance / Load Control / Weights + CGs

Auto ground transfer- Aircraft Systems / 28 - Fuel / Controls and Indicators / REFUEL/GROUND TRANSFER

PANEL- Procedures / Abnormal and Emergency Procedures / 28 - Fuel / FUEL AUTO GND XFR COMPLETED

- Procedures / Abnormal and Emergency Procedures / 28 - Fuel / FUEL CG OUT OF RANGE

Engine start and engine operation- Aircraft systems / 70 - Engines /Ignition and Starting / Starting / Automatic Starting Sequence

- Aircraft systems / 70 - Engines / FADEC- Aircraft systems / 70 - Engines / Normal Operation

Fuel Transfer- Aircraft systems / 28 - Fuel / System Description / Transfer System

Fuel Jettison- Procedures / Abnormal and Emergency Procedures / 28 - Fuel Jettison- Procedures / Not - Sensed Procedures (ABN PROC) / Fuel Jettison

Diversion- Aircraft Systems / 22 - AFS - Flight Management System / System Description Flight Planning / Lateral Flight Plan Revisions / Alternate

- Aircraft Systems / 22 - AFS - Flight Management System / Controls and Indicators / MFD - FMS pages / Alternate page


STANDARD COURSE

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Overweight Landing Procedure- Procedures / Not - Sensed Procedures (ABN PROC) / Miscellaneous


- Normal Operations / General + Preliminary Cockpit Preparation + Cockpit Preparation + Before Start + Start + After Start + Taxi + Before Takeoff + Takeoff + Climb + Cruise + Descent Preparation + Descent + Approach + ILS Approach + Go Around + Landing + Parking + Standard Callouts

Abnormal operations- ABNORMAL OPERATIONS / Miscellaneous / Overweight Landing


• Standard knowledge and understanding of FMS architecture.• Ability to program and use FMS through different flight phases.• Standard knowledge of normal SOP’S, task sharing and call outs.


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2 : 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= 345 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:

• 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= 340 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= 340 TZFWCG= 38%


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3

2(end):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.

5 : During CLIMB to FL 310.FMS exercices : - CLB CSTR- MACH CSTR (0.80) at OKRIX- ALT CRUISE CHANGE 310 instead of 360

6 : Explain the main transfers, the load alleviation transfers and the CG control transferduring climb and cruise. Use PDP CRUISE.

8 : In cruise to KEF, demonstrate predictive GPS function, and how to deselect GPSsatellite and GPS.To return to departure, select LFZZ as ALTN in ALTERNATE menu of FPLN INFO.Then use the enable ALTN function to activate it.

9 : Explain the philosophy for jettison.- If it is urgent to land, the crew consider the overweight landing procedure.

This procedure includes the consideration of jettison.- If it is not urgent to land, the crew does not usually consider the overweight landing

procedure and wants first to Jettison. In this case, they use the jettison procedure.Perform the jettison procedure after the activation of the not sensed jettison proce-dure. Explain that fuel can be jettisoned except fuel from the feed tanks.Rate is approximately 150 t per hour (2.5 t per minute).Explain the JTSN GW field in the active / FUEL & LOAD pageExplain the AUTO RCL function.

17 : Urgent landing due to medical problem with a passenger. LFZZ CLOSED diversionto LFLL.

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WEATHER LFZZ 020/10 5000 OVC 005 05/03 1012

ACTIVE / INIT

FLT NBR A/L ID 201


CPNY RTE AIBAIB1

ALTN RTE AIBLYS


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 %

NOTES RWY COND WET FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1N) ANTI ICE ON PAX NUMBER : 272




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

INIT FL 100 - LFZZ 33 R - GW 385 tCo-route AIBAIB1

T 1 - ECAM MANAGEMENT2 - FUEL TK 2 MAIN PMP FAULT3 - PACK 1 OVHT4 - HYD G RSVR LEVEL LO - RESTORE


1:15 5 - TAKE OFFT 6 - ENGINE FAIL - NO DAMAGE

7 - ENGINE RELIGHT8 - ENG 4 ATHR FAULT - RESTORE

INIT FL 350 - GW 540 t - ZFW 320 t - FOB 220 tCo-route AIBAIB

1:35 9 - ENGINE FAIL T 10 - ONE ENGINE OUT OPERATIONS- RESTORE

2:15 T 11 - FUEL LEAK (ON ENGINE)- RESTORE


MFTD 5 (FAILURES) - TRAINEE 1

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GROUND PHASEL F2S

WEATHER LFZZ 020/10 5000 OVC 005 05/03 1012

ACTIVE / INIT

FLT NBR A/L ID 201


CPNY RTE AIBAIB1

ALTN RTE AIBLYS


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 %

NOTES RWY COND WET FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1N) ANTI ICE ON PAX NUMBER : 272




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


2:30 12 - TAKE OFF13 - ENG FAIL - NO DAMAGE14 - ENGINE RELIGHT 15 - CLIMB FL 7016 - HYD G + Y RSVR LEVEL LO17 - ILS APP - LFZZ 33R

3:20 18 - GO AROUND - RESTORE

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

3:25 19 - TAKE OFF - CLIMB 4000 ftT 20 - FLAPS LOCKED AT RETRACTION

21 - ENG 1 ATHR FAULT IN DOWNWIND22 - ILS APP - G/S INOP - LFZZ 33R - (FLS)

3:50 23 - GO AROUND - RESTORE



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02.03


Study of : • ECAM MANAGEMENT• ENGINE FAILURE and RELIGHT PROCEDURE• FUEL LEAK• DUAL HYDRAULIC FAILURE• FLAPS FAILURE


A. REVIEW :

• STANDARD OPERATING PROCEDURES

B. NEW EXERCICES :

• ECAM MANAGEMENT• ENGINE FAILURE and RELIGHT• DUAL HYDRAULIC FAILURE• FUEL LEAK• FLAPS FAILURE

C. SUPPORT :


MFTD 5 (FAILURES) SESSION PREPARATION


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D. REFERENCES

• PDPNormal OperationsTakeoff + Climb + Cruise + Descent + ILS Approach + Go Around

Abnormal Operations- ECAM Management- Engine failure after V1- Engine failure in cruise- Fuel leak- Slats / Flaps failure cases



ECAM Procedures- Aircraft Systems / 31 - Indicating/Recording / ECAM / How to Handle ECAM Procedures

Eng fail- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG FAIL- Procedures / Not - Sensed Procedures (ABN PROC) / ENG RELIGHT IN FLT

Performance- Performance / In-flight /One Engine Inoperative

Fuel leak- Procedures / Abnormal and Emergency Procedures / 28 - Fuel / FUEL LEAK DETECTED- Procedures / Not - Sensed Procedures (ABN PROC) / FUEL LEAK

• FCTMNormal operationsNormal Operations / Takeoff + Climb + Cruise + Descent Preparation + Descent + Approach +ILS Approach + Go Around + Standard Callouts

Abnormal operations- Operational philosophy / ECAM- ABNORMAL OPERATIONS / Operating techniques / Engine Failure After V1 + Engin

Failure During Initial Climb + Engine Failure during cruise- ABNORMAL OPERATIONS / Hydraulic / G + Y Hydraulic Failures- ABNORMAL OPERATIONS / Flight Controls / Abnormal Flaps and/or Slats Configuration


• Understanding of ECAM philosophy and application of ECAM procedure.


STANDARD COURSE

GROUND PHASE

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02.03

1 : 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

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)

ECAM system management : Insert ENG 1 FIRE and perform ECAM actions. Follow the tutorial to explain the management of the ECAM alertRestore

6 : Insert ENG 3 failure No damage when A/P ON

7 : When relight is successful, explain the deactivation of the not sensed ENGINERELIGHT PROC. Reinforce the philosophy : when the condition which has initiatedthe activation of a not sensed PROC has disappeared, deactivate the procedure.

8 : Insert ENG 4 A/THR failure. Demonstrate that A/THR is available and drives engine1, 2 and 3 while engine 4 thrust has to be manually controlled via THR LVR 4.Restore.

MFTD 5 (FAILURES) SESSION GUIDE

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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11 : Insert a fuel leak of 1000 kg/min on FEED TANK 1 to trigger "FUEL LEAKDETECTED" (consider leak from engine) which takes around 3 minutes. On IOS donot clear malfunction but select a leak of 0 kg/min.After analyse and engine shutdown, consider leak stopped.Consequently engine is kept shutdown.

13 : Insert Engine 2 failure. No damage when AP : ON

16 : Insert simultaneously HYD GREEN RSVR LEVEL LO and YELLOW RSVR LEVELLO

20 : Insert FLAPS LOCKED between Flaps 3 and 1 position - Highlight the max speeddisplayed on ECAM. Explain that the VFE on PFD is the VFE of the actual conf andnot linked with the flaps lever position

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GROUND PHASE L F2S

E

E

WEATHER LFZZ 280/10 2000 OVC 010 -20/-21 1000

ACTIVE / INIT

FLT NBR A/L ID 202


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 150 TROPO 36090

TRIP WIND TL 20

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t 704 000 Ib ZFWCG 35 %

NOTES RWY COND SNOW FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1W) ANTI ICE ON PAX NUMBER : 402


ACTIVE / PERFLFZZ 24 / GW 385 t


V1 v TOGA V1 v TOGA

VR FLEX °C VR FLEX


FLAPS OPT THS FOR FLAPS OPT THS FOR


V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

INIT TAKE OFF - LFZZ 24 - GW 385 tCo-route AIBKEF

1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICAL SUPPLIED)2 - COCKPIT PREPARATION3 - BEFORE START / ENG START / HOT START4 - AFTER START5 - TAXI - BEFORE TAKEOFF

0:50 6 - TAKE OFF7 - ENGINE FAIL - DAMAGE 8 - RADAR VECTORS

T 9 - VOR DME APP - ONE ENGINE OUT - LFZZ 33R (FLS)

1:15 10 - GO-AROUND - RESTORE11 - AFS + EFIS CTL PNL FAULT

T 12 - NDB APP (DOWN TO MDA) - LFZZ 33R (FLS) - RESTORE

INIT FL 350 - GW 385 t Co-route AIBAIB

1:40 T 13 - EMERGENCY DESCENT FL 100 / MORA - RESTORE

INIT FL 350 - GW 385 t Co-route AIBAIB

14 - EXCESS CAB ALT2:05 15 - EMERGENCY DESCENT

FL 100 / MORA - RESTORE



FEB 2009Issue 05

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GROUND PHASEL F2S

WEATHER LFZZ 280/10 2000 OVC 010 -20/-21 1000

ACTIVE / INIT

FLT NBR A/L ID 202


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 150 TROPO 36090

TRIP WIND TL 20

ACTIVE FUEL & LOAD

GW 385 t847 000 Ib FOB 65 t

143 000 Ib

ZFW 320 t 704 000 Ib ZFWCG 35 %

NOTES RWY COND SNOW FPLN : refer CO-ROUTE AIR COND ON (SID MOU 1W) ANTI ICE ON PAX NUMBER : 502




V1 v TOGA V1 v TOGA

VR FLEX °C VR FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS

INIT TAKE OFF - LFZZ 24 - GW 385 tCo-route AIBKEF

2:20 16 - TAKE OFF17 - CLIMB 4000 ft18 - ENG FAIL - DAMAGE19 - RADAR VECTORS

T 20 - VOR DME APP - ONE ENGINE OUT - LFZZ 33R (FLS)21 - GO AROUND ONE ENGINE OUT - RESTORE

INIT FL 350 - GW 385 t - Co-route AIBAIB

2:50 T 22 - CDS RECONFIGURATION DEMO23 - EMERGENCY DESCENT FL 100 / MORA - RESTORE

INIT FL 350 - GW 500 t - ZFW 350 t - FOB 150tCo-route AIBAIB

3:20 24 - CABIN PRESSURIZATION LEAK25 - EMERGENCY DESCENT FL 100 / MORA - RESTORE


3:30 T 26 - SMOKE AVIONICS SMOKE (LEFT) FL 100 / MORA - RESTORE


3:45 27 - BOMB ON BOARD (BRIEFING ONLY)



FEB 2009Issue 05

STANDARD COURSE

GROUND PHASE

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Study of : • ENGINE START FAULT• MANUAL ENGINE START• CABIN PRESSURIZATION PROBLEM• CDS FAILURE / RECONFIGURATION• AUTO FLIGHT SYSTEM FAILURE• EMERGENCY DESCENT• AVIONICS SMOKE


A. REVIEW :

• STANDARD OPERATING PROCEDURES• ENGINE FAILURE AND RELIGHT

B. NEW EXERCICES :

• MANUAL ENGINE START• CDS FAILURE / RECONFIGURATION• AUTO FLIGHT SYSTEM FAILURE• EXCESS CAB ALT / CABIN PRESSURIZATION LEAK• EMERGENCY DESCENT• AVIONICS SMOKE

C. SUPPORT :


MFTD 6 (FAILURES) SESSION PREPARATION


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STANDARD COURSE

GROUND PHASE

Page 20B02.03A380 L F2S

D. REFERENCES

• PDPNormal OperationsCockpit Preparation + Before Start / After Start + Taxi / Before Takeoff + Takeoff + Climb +Cruise + Descent + ILS Approach + Non Precision Approach +Go Around

Abnormal Operations- Engine failure after V1- CDS Reconfiguration- Emergency Descent- SMOKE Procedure



ECAM Procedures- Aircraft Systems / 31 - Indicating/Recording / ECAM / How to Handle ECAM Procedures

Engine start fault- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG START FAULT

Manual engine start- Procedures / Supplementary Procedures / Engines / Unusual starting procedures

Eng fail- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG FAIL- Procedures / Not - Sensed Procedures (ABN PROC) / ENG RELIGHT IN FLT

FCU Back up- Procedures / Abnormal and Emergency Procedures / 22- Auto flight / AUTO FLT AFS

CTL PNL FAULT- Procedures / Abnormal and Emergency Procedures / 31- Indicating/Recording / CDS CPT

(EFIS) CTL PNL FAULT

Emergency descent- Procedures / Abnormal and Emergency Procedures / 21 - Pressurisation / CAB PRESS

EXCESS CAB ALT- Procedures / Not - Sensed Procedures (ABN PROC) / Emergency procedures

CDS Failure- Procedures / Abnormal and Emergency Procedures / 31 - Indicating/Recording / CDS

Smoke- Procedures / Abnormal and Emergency Procedures / 26 - Fire and smoke protection /

SMOKE MAIN AVNCS SMOKE

FLIGHT CREW TRAINING PROGRAM Issue 03 NOV 2007

STANDARD COURSE

GROUND PHASE

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• FCTMNormal operationsNormal operations / Cockpit Preparation + Before Start / After Start + Taxi / Before Takeoff +Takeoff + Climb + Cruise + Decent Preparation + Descent + Approach + ILS Approach + NonPrecision Approach + Go Around + Standard callouts

Abnormal operations- Operational philosophy / ECAM- ABNORMAL OPERATIONS / Operating techniques / Engine Failure After V1 + Engine

Failure During Initial Climb - ABNORMAL OPERATIONS / Fire Protection / SMOKE/FUMES- ABNORMAL OPERATIONS / Miscellaneous / EMERGENCY DESCENT- ABNORMAL OPERATIONS / Auto flight / AUTO FLT AFS/EFIS CTL PNL FAULT- ABNORMAL OPERATIONS / Miscellaneous / Bomb on Board

• QRH- SMOKE procedures


• Demonstrate comprehensive knowledge of aircraft systems operation, use of ECAM and appropriate procedure.

• Understanding and application of crew coordination under malfunctions conditions.


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Page 20D02.03A380 L F2S

02.03

2 : FMS preparation with KBD OFF on KCCU 2 in order to practice FMS preparationwith CCD and SOFT KEYBOARD.When FMS preparation completed, restore

3 : Insert a HOT START on engine 4. When ECAM actions completed, restore, performa manual engine start on engine 4. Then perform a manual start on Engine 1 withhot start to highlight the difference of protections between AUTO and MAN. Restoreand perform a quick start through IOS panel.

9,12,20: FLS approach in cold weather conditions. Explain that the FLS profile takes intoaccount the temperature corrections (use tutorial NPA flown with FLS function,COLD WEATHER).

11 : For training purpose, on MFD FCU BACKUP page, select manually AFS and EFISBACKUP.

13,23: When Q and A with Tutorial completed, trainees perform an emergency descentwithout failure. Trainees should select the ABN Not-Sensed PROC : EMERDESCENT to update the ECAM limitations.

14 : Insert EXCESS CAB ALT. (EXPLOSIVE DECOMPRESSION).

22 : Perform the DEMO by switching OFF the DU’s instead of inserting failure. Proceedstep by step, to demonstrate the auto reconf, and then the manual one, via theRECONF P/B. After the demo, insert a CAPT PFD CDS unit fault. When ECAMactions completed, restore.

24 : Insert CABIN PRESS DOOR LEAK 1L with a leak rate of 1500 ft/min

26 : Insert SMOKE MAIN AVNCS SMOKE (LEFT). The flight crew performs ECAM actions (immediate actions) and reverts to QRH asper ECAM procedure. Freeze when EMER ELEC considerRestore.

27 : Brief the "BOMB ON BOARD" procedure using the FCOM. Then for demo activatethe not sensed "BOMB ON BOARD" procedure for display only. Do not perform actions.

MFTD 6 (FAILURES) SESSION GUIDE

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GROUND PHASE L F2S

E

E.

WEATHER LFZZ 030/12 3000 OVC 006 30/20 1011 LFPO 060/10 4000 OVC 800 28/26 1012

ACTIVE / INIT

FLT NBR A/L ID 203


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 150 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 390 t858 000 Ib FOB 90 t

198 000 Ib

ZFW 300 t660 000 Ib ZFWCG 35 %





V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

QUESTIONS & ANSWERS


1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)2 - COCKPIT PREPARATION3 - BEFORE START 4 - ENG START5 - AFTER START6 - TAXI - BEFORE TAKEOFF

1:00 7 - TAKE OFF8 - AFTER TAKE OFF9 - CLIMB

10 - CRUISE11 - PACKS 1 + 2 FAULT12 - DIVERSION - LFPO

1:40 13 - ILS APP - G/S INOP - LFPO 06 (FLS)14 - GO AROUND15 - ILS APP - LFPO 06

2:00 16 - AUTOLAND 17 - AFTER LANDING18 - PARKING - TAIL PIPE FIRE


MFTD 7 (Progress Check) - TRAINEE 1

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GROUND PHASEL F2S

EWEATHER

LFPO 060/10 4000 OVC 800 28/26 1011

ACTIVE / INIT

FLT NBR A/L ID 203

FROM LFPO TO BIKF ALTN EINN

CPNY RTE ORYKEF

ALTN RTE KEFSNN


CI 150 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 390 t858 000 Ib FOB 90 t

198 000 Ib

ZFW 300 t660 000 Ib ZFWCG 35 %

NOTES RWY COND DRY FPLN : refer CO-ROUTE AIR COND ON (SID ATREX 1V) ANTI ICE OFF PAX NUMBER : 301


ACTIVE / PERFLFPO 06 / GW 390 t

ACTIVE / PERFLFPO 06 / GW 390 t

V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Time EVENTS

INIT TAKE OFF - LFPO 06 - GW 390 tCo-route ORYKEF

2:15 19 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)20 - COCKPIT PREPARATION21 - BEFORE START 22 - ENG START23 - AFTER START24 - TAXI - BEFORE TAKEOFF

3:15 25 - TAKEOFF26 - AFTER TAKEOFF27 - ENGINE FAILURE28 - RETURN TO DEPARTURE29 - RADAR VECTORS

3:35 30 - VOR DME APP ONE ENGINE OUT LFPO 06 (SELECTED)31 - GO AROUND - ONE ENGINE OUT32 - RADAR VECTORS33 - ILS APP - ONE ENGINE OUT - LFPO 06

3:55 34 - AUTOLAND ONE ENGINE OUT35 - AFTER LANDING36 - PARKING 37 - SECURING THE AIRCRAFT


MFTD 7 (Progress Check) - TRAINEE 2

Issue 05 FEB 2009

STANDARD COURSE

GROUND PHASE

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• Check trainee’s ability to carry out normal and abnormal operations according to standard requirements.


A. REVIEW :

• STANDARD OPERATING PROCEDURES• ECAM PHILOSOPHY AND ECAM MANAGEMENT

B. NEW EXERCICES :

• NIL

C. SUPPORT :



The application of normal standard operating procedures and the management of abnormalprocedure are of standard level or above, which means "Ready for next phase" (FFS).

MFTD 7 (Progress Check) SESSION PREPARATION

FLIGHT CREW TRAINING PROGRAM Issue 04 MAY 2008

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STANDARD COURSE

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Page 22B02.03A380 L F2S

02.03

2 : Give the crew a slot for departure.

3 : LOADSHEET last minute change : ZFW : 305 tZFWCG : 37 % If flight crew decision is to perform a fuel auto ground transfer, give a new slot fordeparture. Therefore, due to time constraint, flight crew will compute a new load-sheet on the OIS with updated figures, instead of performing a fuel transfer.

7 : During line up, change clearance to Heading 310 4000 ftWhen airborne reaching 4000 ft, resume navigation on SID.

10 : Final cruise FL 340.Request predictions (TIME / DIST) to FL 340.

11 : At BRY, Insert PACK 1 OVHT and PACK 2 FAULT. When PACKS OFF, insert PACK1 FAULT. Explain that with PACKS OFF, the cabin depressurization rate is less than1000 ft / min. Descent and diversion to LFPO, fail G/S of ILS RWY 06.Clearance is MLN FL 60 then radar vectors for LOC APP RWY 06 (G/S INOP)

15 : Cancel G/S ILS 06 failureRADAR VECTORS for ILS APP RWY 06

18 : During engine shutdown, ground mechanics indicates a tail pipe fire on engine 2.Flight crew performs the Not-Sensed TAIL PIPE FIRE procedure.

20 : Insert HYD G ENG 1 PUMP A PRESS LO. Dispatch with MMEL.

24 : RWY change for take off 08 due to runway obstruction on runway 06

27 : Insert engine 4 OIL QTY at 0 to trigger ENG 4 OIL PRESS LO, which leads the crewto shutdown the engine.

30 : Due to ILS 06 FAILURE, radar vectors for VOR DME RWY 06.For training purpose, approach in selected mode.

31 : GO AROUND ordered by ATC due to RWY incursion

33 : Cancel ILS 06 failureRadar vectors for ILS approach RWY 06

MFTD 7 (Progress Check) SESSION GUIDE

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FLIGHT CREW TRAINING PROGRAM Issue 05 FEB 2009

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HANDLING PHASE L F2S

E

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WEATHERLFZZ 330/10 9999 SCT 025 20/10 1010LFLL CALM 5000 OVC 008 20/10 1010

ACTIVE / INIT

FLT NBR A/L ID 201


CPNY RTE AIBLYS

ALTN RTE LYSAIB


CI 90 TROPO 36090

TRIP WIND HD 15

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID ONZON 1N) AIR COND ON PAX NUMBER : 100 ANTI ICE OFF




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Tim

e EVENTS

AP

FD

ATH

R T

RK

-FPA

HU

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INIT GATE A 1 - LFZZ 33R GW 385 t Co-route AIBLYS


2 - COCKPIT PREPARATION3 - ENG START / AFTER START4 - TAXI

0:50 5 - TAKE OFF v v6 - SID - CLIMB FL 120 v v v7 - STUDY OF NORMAL LAW (15’) v8 - SIDE STICK PRIORITY DEMO (5’) v v9 - DES-STAR v v

10 - ILS APP LFLL 18L v v11 - LANDING

1:35 INIT HOLDING POINT- LFZZ 33RGW 385 tCo-route PAT 33 R

12 - TAKE OFF v v13 - CLIMB 4000 FT v v14 - PATTERN 33R v v15 - VISUAL APP v v16 - LANDING

1:50

INIT HOLDING POINT - LFZZ 33RGW 385 tCo-route PAT 33 R

17 - TAKE OFF v v18 - CLIMB 2300 FT v v19 - VISUAL PATTERN v v20 - GO AROUND v v21 - CLIMB 2300 FT v v22 - VISUAL PATTERN v23 - LANDING24 - AFTER LANDING


FFS 1 - TRAINEE 1

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HANDLING PHASEL F2S

EWEATHER

LFZZ 330/10 9999 SCT 025 20/10 1010LFLL CALM 5000 OVC 008 20/10 1010

ACTIVE / INIT

FLT NBR A/L ID 201


CPNY RTE AIBLYS

ALTN RTE LYSAIB


CI 90 TROPO 36090

TRIP WIND HD 15

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb

ZFWCG 35 %





V1 TOGA V1 TOGA

VR v FLEX VR v FLEX




V1 TOGA V1 TOGA

VR FLEX VR FLEX



Tim

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AP

FD

ATH

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RK

-FPA

HU

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2:25 INIT HOLDING POINT- LFZZ 33RGW 385 tCo-route AIBLYS

25 - TAKE OFF v v26 - SID - CLIMB FL 120 - TCAS EVENT v v v27 - DES - STAR v v28 - ILS APP LFLL 18L v v29 - LANDING

2:55 INIT HOLDING POINT- LFZZ 33R GW 385 tCo-route PAT 33 R

30 - TAKE OFF v v31 - CLIMB 4000 FT v v32 - PATTERN 33R v v33 - VISUAL APP v v34 - LANDING

3:10 INIT HOLDING POINT- LFZZ 33RGW 385 tCo-route PAT 33 R

35 - TAKE OFF v v36 - CLIMB 2300 FT v v37 - VISUAL PATTERN v v38 - GO AROUND v v39 - CLIMB 2300 FT v v40 - VISUAL PATTERN v41 - LANDING42 - AFTER LANDING43 - TAXI44 - PARKING - GATE A1

3:45 45 - SECURING THE AIRCRAFT


FFS 1 - TRAINEE 2

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

ffs1gd.fm


02.04


• Practice cockpit preparation (real environment).• Introduction to aircraft handling characteristics.• Introduction to "Normal Law" - Envelope protections.• Practice visual pattern, go around and landing.


A. REVIEW :

• Cockpit preparation using aircraft equipments in a real environment.

B. NEW EXERCISES :

• TAKE OFF • NORMAL LAW - PROTECTIONS• SIDE STICK PRIORITY• VISUAL PATTERN• TCAS EVENT• GO AROUND• LANDING

C. SUPPORT :

• DVD 1 : FFS briefing guides• FCOM • FCTM

D. REFERENCES

• BRIEFING GUIDESTaxi + Takeoff + Landing + Normal Law + Visual Pattern + Velocity Vector + TCAS

Standard flight profile - SOP's- Procedures / Normal Procedures / Standard Operating Procedures- Procedures / Normal Procedures / Task Sharing- Procedures / Normal Procedures / Normal Checklists

Normal Law- Aircraft systems / 27 - Flight Controls / Flight Control System / Normal Law

Protections- Aircraft systems / 22 - 27 - Flight Envelope / Operating Speeds + Protections

FFS 1 SESSION PREPARATION


STANDARD COURSE

HANDLING PHASE


ffs1gd.fm

Side stick priority and indications- Aircraft systems / 27 - Flight Controls / Controls and Indicators / Side Sticks + Side Stick

Priority + Side Stick Indication on PFD- Aircraft systems / 22 - AFS - Flight Guidance / Controls and Indicators / Sidestick- Aircraft systems / 25 - Equipment / Cockpit / Cockpit Seats

TCAS Event- Procedures / Non ECAM Procedures / 34 - Navigation / SURV Traffic Advisory Alert +

Resolution Advisory Alerts

• FCTM

Handling in normal operations- Normal Operations / Taxi + Before Takeoff + Takeoff + Climb+ Descent Preparation +

Descent + Approach + ILS Approach + Visual Approach + Landing + Go Around + After Landing + Parking + Standard Callouts

Taxi roll, steering and braking- Normal Operations / Taxi

Takeoff roll and rotation technique- Normal Operations / Takeoff

Landing: flare, callout, derotation, rollout, braking- Normal Operations / Landing

Normal Law and Protections- Operational Philosophy / Flight Controls / Laws + Protections

Side Stick and Priority P/B- Operational Philosophy / Flight Controls / System characteristics

Velocity Vector- Supplementary Information / Flight References


• Understanding of Normal Law protections.• Ability to handle the aircraft in Normal Law.• Ability to apply correct take off and landing techniques.


STANDARD COURSE

HANDLING PHASE

ffs1gd.fm



02.04

DAY VISUAL (Select visibility 25 km)

2 : - 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, flashing lights)- 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.

4 : Aircraft component location : use components visualization menu in the IOSrepositionning function page to display on visual : gears, engines, wing tips position

7 : VV design- Explain that whatever the size and the color, VV indicates always the same thing /the track (TRK) and the flight path angle (FPA).- The message to be adressed about size and color is :

• Size means FD status• small : FD ON follow FD • big : FD OFF follow VV

• Color means • black = HDG / VS • green = TRK / FPA

Flight control law demonstration performed by each trainee:- Level flight: Speed 280 kts - AP OFF

• Disconnect the A/THR: check that the standard procedure is applied• Remove the FD, select TRK / FPA: explain relationship between Flight Path

Angle and pitch attitude- Stability in pitch

• Level flight: Increase and decrease speed by 40 kts: explain stability in pitch (auto trim)

• Repeat the same exercise using FPA ±3° keeping the same thrust setting- Stability in roll

• Turn with 30° bank angle: explain roll stability and turn coordination • Increase to 45° bank angle: stability is lost and need for side stick inputs to

maintain bank angle and level flight• Release the side stick: explain bank angle back to 33° and need for small

back pressure to regain the altitude

FFS 1 SESSION GUIDE

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Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE


ffs1gd.fm

7(end): ProtectionsTrainee 1 performs all the protections exercices in clean configuration.Trainee 2 performs only the high angle of attack protection in landing configuration. AP OFF - FD OFF - TRK / FPA - A/THR OFF

- Roll: speed around 280 kts • Ask the pilot to practice 45° bank angle turns• Ask the pilot to increase bank angle to the maximum (67°) (green dashes)• Emphasize that the max bank angle corresponds to the max G load (2.5 G),

displayed on SD

- Pitch: speed around 280kts• Apply progressively maximum full up side stick deflection • Emphasize maximum pitch up to 30° (green dashes) reduced to 25° at low

speed• Alpha floor could engage due to high angle of attack protection• Repeat the same demonstration for maximum full down side stick deflection

(maximum 15° pitch down): do not engage high speed protection and resume normal flight

- High speed: speed around 280kts - LEVEL FLIGHT

• Set FPA -3° and release the side stick• Observe pitch up demand at VMO+10 / MMO + .02• Recover speed to 320kts and apply full forward side stick• Mention that the speed can increase up to VD-10 / MD -.02M but pitch up

demand still applies with maximum side stick deflection• Apply maximum bank angle (limited to 45°)• And then release the side stick to demonstrate spiral stability

- High angle of attack Disconnect A/THR

• Reduce speed below VLS side stick free: demonstrate pitch down to maintain speed above alpha PROT

• At α PROT the auto trim ceases• Between α PROT and α MAX, α FLOOR engages: disconnect it• Explain that with full back side stick aircraft reaches α MAX but does not stall• Demonstrate the maximum bank angle (45°)• Restore VAPP. and establish the aircraft on a 3° FPA in descent: ask the pilot

to practice an emergency pull up (Maximum deflection in pitch and roll)

Re-engage appropriate modes for automation after recovery

9,27 : When reaching DME ARC, trainee disconnects AP, to fly manually following FDorders.

10,28 : Stabilized approach to allow the trainee to feel the aircraft configuration changeswhile manually flying.

11,29 : Reinforce flare technique before landing

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14,32 : Freeze position in downwind. Trainees set FD OFF. Insert 25 kt crosswind left thenright to notice the impact on the VV position. Then remove crosswind and unfreeze.

22,40 : ATHR OFF in downwind to fly in manual thrust.Highlight the management of thrust with ACUTE. Manual adjustment of ACUTE onall engines to target value is sensitive : 1% of N1 = about 5% of ACUTE

26 : TCAS event : select scenario 9 (reversed V/S) when levelled off at FL 120.

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CI 90 TROPO 36090

TRIP WIND HD 15

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID MOU 1N) AIR COND ON PAX NUMBER : 250 ANTI ICE OFF




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2 - COCKPIT PREPARATION v3 - ENG START / AFTER START v4 - TAXI v

1:00 5 - TAKE OFF - CROSSWIND - INCAPACITATION

v v v

6 - SID - CLIMB FL 120 - TCAS EVENT v v v v7 - DES - STAR v v v v8 - LOC APP - LFZZ 33R (FLS) v v v v v9 - REJECTED LANDING v v v

10 - VOR DME - LFZZ 33R (FLS) v v v v11 - LANDING - CROSSWIND v

1:40 INIT HOLDING POINT- LFZZ 33R GW 385 t - WIND 050/15 Co-route PAT 33R

12 - TAKE OFF - PREDICTIVE WINDSHEAR WINDSHEAR

v v v

13 - CLIMB 4000 FT v v v14 - PATTERN 33R v v v15 - ILS APP RAW DATA - LFZZ 33R v v v

2:00 16 - LANDING v

INIT APP - LFZZ 33R GW 385 t

17 - ILS RAW DATA - LFZZ 33R v v v18 - HIGH ENERGY GO AROUND - CLEAN UP - FREEZE

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CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID 1B) AIR COND ON PAX NUMBER : 250 ANTI ICE OFF




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19 - TAKE OFF - CROSSWIND v v v20 - CLIMB 4000 FT v v v v21 - PATTERN 33R v v v v22 - DOWNWIND - TCAS EVENT v v v v23 - VOR DME APP - LFZZ 33R (SELECTED)

v v v v v

24 - HIGH ENERGY GO AROUND v v v25 - NDB APP - LFZZ 33R (FLS) v v v v26 - LANDING - CROSSWIND v

3:00 INIT HOLDING POINT- LFZZ 33R GW 385 t - CAVOKCo-route PAT 33R

27 - TAKE OFF - CROSSWIND v v v28 - CLIMB 2300 FT v v v29 - VISUAL PATTERN v v v30 - REJECTED LANDING v v v31 - VISUAL PATTERN v v v32 - LANDING - CROSSWIND v

3:20 INIT HOLDING POINT - LFZZ 33R - GW 385 t - WIND 050/15 - 8000 - OVC 008 Co-route PAT 33R

33 - TAKE OFF - WINDSHEAR v v v34 - CLIMB 4000 FT v v v v35 - PATTERN 33R v v v v36 - ILS APP RAW DATA - LFZZ 33R v v v37 - GO AROUND - INCAPACITATION v v v

INIT APP- LFZZ 33R GW 385 t

3:45 38 - ILS APP RAW DATA - LFZZ 33R v v v39 - LANDING LFZZ 33R v40 - AFTER LANDING v41 - TAXI - GATE A1 v42 - PARKING v

3:55 43 - SECURING THE AIRCRAFT v


FFS 2 - TRAINEE 1

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

ffs2gd.fm


02.04


Practice :• Cockpit preparation (real environment).• Non precision approaches and ILS RAW DATA.• Windshear recovery techniques at Takeoff.• Takeoff and Landing with crosswind.


A. REVIEW :

• Cockpit preparation using aircraft equipments in a real environment.• Visual pattern.• ILS approach.• Go around procedure.

B. NEW EXERCISES :

• TAKE OFF WITH CROSSWIND• PREDICTIVE WINDSHEAR - WINDSHEAR (TAKE OFF)• ILS RAW DATA• NON PRECISION APPROACH• CREW INCAPACITATION• LANDING WITH CROSSWIND

C. SUPPORT :




ffs2gd.fm

STANDARD COURSE

HANDLING PHASE


D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + Crosswind takeoff + Incapacitation + Windshear + ILS RAW DATA + Visual Pattern + Velocity Vector + TCAS

• FCOM


Crew Incapacitation- Procedures / Non ECAM Procedures / Miscellaneous

TCAS Event- Procedures / Non ECAM Procedures / 34 - Navigation / SURV Traffic Advisory Alert +

Resolution Advisory Alerts

Windshear- Procedures / Supplementary Procedures / Adverse Weather / Operations in windshear - Downburst conditions

- Procedures / Non ECAM Procedures / 34 - Navigation / SURV MONITOR RADAR DIS-PLAY + WINDSHEAR AHEAD WINDSHEAR AHEAD + GO AROUND WINDSHEAR AHEAD + WINDSHEAR, WINDSHEAR, WINDSHEAR

• FCTM

Handling in normal operations- Normal Operations / Taxi + Before Takeoff + Takeoff + Climb + Descent Preparation + Descent + Approach + Non Precision Approach + ILS Raw Data Approach + Landing + Go Around + Standard Callouts

Taxi roll, steering and braking- Normal Operations / Taxi

Takeoff roll and rotation technique- Normal Operations / Takeoff

Landing: flare, callout, derotation, rollout, braking- Normal Operations / Landing


Crew Incapacitation- Abnormal Operations / Miscellaneous


STANDARD COURSE

HANDLING PHASE

ffs2gd.fm



• Apply good crew coordination and task sharing.• Proper use of automation.• Confirm the ability to :

- Handle the aircraft safely.- Perform Non precision approaches.- Perform ILS raw data.- Take off and landing in crosswind conditions


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HANDLING PHASE



DAY VISUAL

TRAINEE 2

4 : Demonstrate FMS Take Off shift function. Line up via B2 with a shift of 170 meters.

5 : Trainee 2 incapacitation :At 100 ft the trainee 2 set an unusual high pitch attitude and holds the stick control.Emphasize the latching condition on Trainee 1 side (more than 30 sec.).Back to normal crew position when incapacitation procedure completed and aircraftin clean configuration.

6 : TCAS : Select scenario 10 : " RA crossing flight path ".

8 : Fail IANR G/S.

9 : Reject landing at 50 ft.

12 : On environment page select microburst to activate predictive windshear at take off.Cancel predictive windshear, then insert windshear on rotation for recovery technique.

18 : In CONF1 and when Go Around altitude set, initiate a Go Around and perform standard missed approach procedure.The idea is to insure that trainees are able to cope with a well above MDA GOAROUND, with rapid FMA changes.

TRAINEE 1

22 : TCAS event : Select scenario 6 (maintain V/S).

24 : When on final, conf 2 or 3, initiate a go around before 1000 ft AGL and provide radarvectoring with a climb to 3700 ft QNH.After aircraft is clean, resume climb to MSA.The idea is to insure that trainees are able to cope with a well above MDA GOAROUND, with rapid FMA changes.

30 : Reject landing at 50 ft.

33 : Insert windshear after rotation.

37 : Trainee 1 incapacitation :During go around, trainee 1 faints, then trainee 2 takes control.End of exercice when incapacitation procedure completed and aircraft in clean configuration.

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CI 90 TROPO 36090

TRIP WIND TL 15

ACTIVE FUEL & LOAD

GW 569 t1 232 000 lb FOB 209 t

440 000 lb

ZFW 360 t792 000 lb ZFWCG 35 %

NOTES NIGHT VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID MOU 1W) AIR COND OFF PAX NUMBER : 500 ANTI ICE OFF


ACTIVE / PERFLFZZ 24 / MTOW 569 t


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INIT GATE A1 - LFZZ 24 MTOW 569 t Co route AIBKEF - NIGHT VISUAL

1 - PRELIMINARY COCKPIT PREPARATION APU BLEED FAULT (AIRCRAFT NOT ELECTRICALLY SUPPLIED)2 - COCKPIT PREPARATION3 - ENG START WITH EXT PNEUMATIC

POWER4 - TAXI

0:50 5 - TAKE OFF - PACKS OFF - ARS DEMO v v6 - SID - CLIMB FL 120 - TCAS EVENT v v v7 - CRUISE - DIVERSION TO LFZZ v v v

1:10 8 - DES - STAR v v v9 - LOC APP OVERWEIGHT - LFZZ 33R

(FLS) - AES DEMOv v v v

10 - PREDICTIVE WINDSHEAR / WINDSHEAR ON APP v v

1:30 11 - GO AROUND v v12 - ILS APP - LFZZ 33R v v v v13 - OVERWEIGHT LANDING

1:50 INIT HOLDING POINT - LFZZ 24GW 385t - ZFW 320 t - FOB 65 t310/25 - 25 km - SCT 030 - NIGHT VISUAL

14 - TAKE OFF - CROSSWIND - DEMO FLRS

v v

15 - CLIMB 2300 FT v v16 - VISUAL PATTERN v v17 - LOW ENERGY WARNING v18 - LANDING CROSSWIND19 - 180° ON RUNWAY 60 m WIDTH

2:00 INIT APP - LFZZ 33 RGW 385 tNIGHT VISUAL

20 - ILS APP LFZZ 33R - G/S FROM ABOVE

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21 - GPWS BASIC MODE DEMO RECOVERY PROC

v v v

22 - GO AROUND - AFTER T/OFF C/L v v


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CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND TL 15

ACTIVE FUEL & LOAD

GW 569 t1232000 lb FOB 209 t

440 000 lb

ZFW 360 t792 000 lb ZFWCG 35 %

NOTES NIGHT VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID MOU 1W) AIR COND OFF PAX NUMBER : 500 ANTI ICE OFF




V1 v TOGA V1 v TOGA

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2:25 INIT HOLDING POINT- LFZZ 24MTOW 569 t Co-route AIBKEF - NIGHT VISUAL

23 - TAKE OFF - PACKS OFF v v24 - SID - CLIMB FL 120 - REVERSION MODE v v v25 - RETURN TO DEPARTURE v v v26 - LOC (BACK CRS) DME - LFZZ 15L v v v v27 - WINDSHEAR ON APP v v

2:55 28 - GO AROUND v v29 - ILS APP - LFZZ 33R v v v v30 - OVERWEIGHT LANDING

3:15 INIT HOLDING POINT- LFZZ 24GW 385t - ZFW 320 t - FOB 65 t310/25 - 25 km - SCT 030 - NIGHT VISUAL

31 - TAKE OFF - CROSSWIND v v v32 - CLIMB 2300 FT v v v33 - VISUAL PATTERN v v34 - LANDING CROSSWIND v35 - 180° ON RUNWAY 60m WIDTH v

3:30 INIT HOLDING POINT- LFZZ 24 GW 385t - 310/25 - 25 km - SCT 030 NIGHT VISUAL

36 - TAKE OFF - CROSSWIND WINDSHEAR

v v

37 - CLIMB 2300 FT v v v38 - VISUAL PATTERN v v39 - LANDING CROSSWIND v v40 - TAXI v41 - APU FIRE42 - EMER EVAC


FFS 3 - TRAINEE 2

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

ffs3gd.fm


02.04


Practice • Decision making (CRM).• Unusual engine start / engine start with EXT PNEU PWR• Heavy weight operations.• Non precision Approaches.• Windshear recovery technique in approach.• 180° TURN on RWY 60m width• GPWS recovery technique


A. REVIEW :

• Non precision approach.• Go around procedure.• Take off and landing with crosswind.• TCAS

B. NEW EXERCISES :

• UNUSUAL ENGINE START / ENGINE START WITH EXT PNEU PWR• PREDICTIVE WINDSHEAR - WINDSHEAR (LANDING)• AUTO RETRACTION / EXTENSION SYSTEM • REVERSION MODE (FD orders not followed)• LOW ENERGY WARNING• FLAPS LOAD RELIEF• 180° TURN ON RWY 60M WIDTH• G/S FROM ABOVE• GPWS• EMER EVACUATION

C. SUPPORT :




ffs3gd.fm

STANDARD COURSE

HANDLING PHASE


D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + Crosswind takeoff + Slats - Flaps protections + Windshear + Visual Pattern + Velocity Vector + Low energy warning + Glide slope from above + Taws + Mode Reversions + TCAS + Emergency evacuation



Engine start with EXT Pneumatic power- Procedures / Supplementary Procedures / Engines / Unusual starting procedures

180 degree turn on 60 meter wide runway- Procedures / Normal Procedures / Standard Operating Procedures / Taxi

Auto extension/retraction system, FLRS- Aircraft systems / 27 Flight Controls / Slats/Flaps / Configurations / Slats/Flaps Extension/Retraction

Low energy warning- Aircraft systems / 22 - 27 - Flight Envelope / Protections / Low Energy Warning

Windshear- Procedures / Supplementary Procedures / Adverse Weather / Operations in windshear - Downburst conditions

- Procedures / Non ECAM Procedures / 34 - Navigation / SURV MONITOR RADAR DIS-PLAY + WINDSHEAR AHEAD WINDSHEAR AHEAD + GO AROUND WINDSHEAR AHEAD + WINDSHEAR, WINDSHEAR, WINDSHEAR

Taws- Procedures / Non ECAM Procedures / 34 - Navigation / SURV

TCAS Event- Procedures / Non ECAM Procedures / 34 - Navigation / SURV Traffic Advisory Alert + Resolution Advisory Alerts

Overweight landing- Procedures / Not - Sensed Procedures / Miscellaneous

APU Fire- Procedures / Abnormal and Emergency Procedures / 26 - Fire and Smoke Protection / APU FIRE

• Master Minimum Equipment List (MMEL)- MMEL Entries / ECAM Alert / AIR / APU BLEED FAULT


STANDARD COURSE

HANDLING PHASE

ffs3gd.fm


• FCTM

Handling in normal operations- Normal Operations / Taxi + Before Takeoff + Takeoff + Climb + ILS Raw Data Approach +

Landing + Go Around + Standard Callouts

180 Deg Turn - Normal Operations / Taxi

Takeoff at heavy weight- Normal Operations / Takeoff / Takeoff at heavy weight

ILS glide slope from above- Normal Operations / ILS Approach / Final Approach / Glide Slope Interception From Above


Use of MMEL- Normal Operations / Flight Preparation / MEL

Overweight Landing- Abnormal operations / Miscellaneous

Emergency Evacuation- Abnormal operations / Operating Techniques

• QRH- EVACUATION


• Assess crew coordination and task sharing.• Handling : Flight within the below listed criteria should not be achieved at the

expense of smooth and good coordination :Speed : + 10 / - 5 ktsHeading : ± 5°Tracking : ± 5°Altitude : ± 100 ftAll phases must be handled safely.

• At this stage, the trainee must be able to start Abnormal and Emergency procedures study.


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STANDARD COURSE

HANDLING PHASE


02.04

NIGHT VISUAL

TRAINEE 1

1 : Insert APU Bleed fault, before APU Bleed ON selected by flight crew. Dispatch withMMEL

5 : When in CONF 1 + F, observe flap autoretraction at 212 kt, and change on PFD : 1 + F to 1

6 : TCAS : Select scenario 10 (crossing flight path).

7 : Passing FL 70 : Call from the cabin :- A pregnant passenger is ready to give birth to her fourth child,- There is no doctor, nor midwife on board,- If the crew doesn't react, advise that 80% of the passengers start to strongly protest

against the Captain decision to continue to destination. Overweight landing procedure due to urgency

9 : Fail IANR G/S. In approach, select CONF 1; reduce speed below 205 kt to activatethe automatic extension system (AES). Observe that flaps will extend to 1 + F.

10 : On environment page, select microburst to activate predictive windshear onapproach. When the message "WINDSHEAR AHEAD" is displayed cancelmicroburst and select moderate windshear for recovery technique.

14 : Demo FLRS : At acceleration altitude, reduce the pitch to increase IAS to VFE + 2,5 kt, observe FLAP LOAD RELIEF and RELIEF displayed on lower PFD.Continue to accelerate in order to exceed VFE ; observe no further retraction andoverspeed warning. Increase pitch to 15° and point out FLAP reextension at VFE - 2,5 kt. Fly FD to retract Slats / Flaps

17 : A/THR Off : Start final turn in level flight to trigger the "SPEED, SPEED, SPEED"warning.

20 : Delay G/S interception for G/S from above exercise

21 : When the trainee has completed the G/S from above procedure and rearmed the G/S, the instructor requests to disarm the G/S to demonstrate the GPWS warnings.The purpose is to perform the recovery procedure when "PULL UP" is triggered.

TRAINEE 2

24 : Demo of reversion mode : FD orders not followed.

25 : Passenger has a heart attack. Overweight procedure due to urgency.

38 : A/THR OFF in downwind to fly in manual thrust.

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CPNY RTE AIBLYS

ALTN RTE LYSAIB


CI 90 TROPO 36090

TRIP WIND HD 15

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %





V1 TOGA V1 TOGA

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INIT HOLDING POINT - LFZZ 33R GW 385tCo-route AIBLYS

1 - TAKE OFF - WINDSHEAR v v v2 - CLIMB FL 110 v v v v3 - ALTERNATE LAW DEMO

DIRECT LAW DEMO BACKUP MODULE DEMO

v v

4 - STALL RECOVERY v0:50 5 - HYD G + Y RSVR LVL LO v v v v

6 - DES - STAR v v v v7 - ILS APP - LFLL 36L - ALTN LAW v v v8 - LANDING v9 - TAXI v

1:25 INIT HOLDING POINT - LFLL 36 L GW 385 t Co-route LYSAIB

10 - TAKE OFF v v v v11 - CLIMB FL 120 v12 - ALL GEN FAULT v v13 - EMER ELEC CONFIGURATION v v14 - DES - STAR v15 - ILS APP - LFZZ 06 - DIRECT LAW v v16 - LANDING v


FFS 4 - TRAINEE 1

Issue 05 FEB 2009

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HANDLING PHASEL F2S

WEATHER LFZZ 350/10 6000 OVC 010 30/10 1020 LFLL 350/10 6000 OVC 012 30/10 1020

ACTIVE / INIT

FLT NBR A/L ID 204

FROM LFLL TO LFZZ ALTN LFLL

CPNY RTE LYSAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND HD 15

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND DRY (SID EB) AIR COND ON PAX NUMBER : 350 ANTI ICE OFF


ACTIVE / PERFLFLL 36L GW 385 t


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2:20 INIT HOLDING POINT - LFLL 36 L GW 385 t Co-route LYSAIB

17 - TAKE OFF v v v18 - CLIMB FL 120 v v v v19 - CRUISE v v v v20 - FUEL LEAK (ON FEED TANK) v v v v21 - DES - STAR v v v v22 - RELIGHT IN FLIGHT v v v v23 - FLAPS SYS 1+2 FAULT v v v24 - ILS APP - LFZZ 33R - ALTN LAW v v v25 - LANDING v

3:00 INIT TAKE OFF - LFZZ 33R - GW 385 t Co-route AIBAIB1

26 - TAKE OFF v v v27 - CLIMB 3000’ v v v v28 - EGPWS DEMO - RECOVERY PROC v v v v29 - PRIM 1+2+3 FAULT v v v

3:20 30 - ILS APP - LFZZ 33R - DIRECT LAW v v31 - LANDING v

IF TRAINEE 2 CAPTAIN

INIT APP - LFZZ 06GW 385 t

32 - ILS APP - LFZZ 06 - IN ELECTRICAL EMERGENCY CONFIGURATION

v v

33 - LANDING v


FFS 4 - TRAINEE 2

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

ffs4gd.fm


02.04


• Demonstration of FCTL alternate and direct laws.• Demonstration of backup modulePractice :• Stall recovery• Dual hydraulic failure event.• Emergency electrical configuration event.• Approach and landing in alternate and direct law.• EGPWS recovery technique.


A. REVIEW :

• WINDSHEAR RECOVERY TECHNIQUE• FUEL LEAK

B. NEW EXERCISES :

• F/CTL RECONFIGURATION LAWS• STALL RECOVERY• HYD G + Y RSVR LVL LO • EMERGENCY ELECTRICAL CONFIGURATION• EGPWS• FLAPS LOCKED (BEFORE EXTENSION)• ILS APP in ALTERNATE / DIRECT LAW

C. SUPPORT :




ffs4gd.fm

STANDARD COURSE

HANDLING PHASE


D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + Windshear + Reconfiguration Law + Stall Recovery + Slats - Flaps protections + Velocity Vector + Taws



Windshear- Procedures / Supplementary Procedures / Adverse Weather / Operations in windshear -

Downburst conditions- Procedures / Non ECAM Procedures / 34 - Navigation / SURV MONITOR RADAR DIS-

PLAY + WINDSHEAR AHEAD WINDSHEAR AHEAD + GO AROUND WINDSHEAR AHEAD + WINDSHEAR, WINDSHEAR, WINDSHEAR

Reconfiguration Control Laws- Aircraft Systems / 27 - Flight Controls / Flight Control System / Reconfiguration Control

Laws

Dual hydraulic failure- Procedures / Abnormal and Emergency procedures / 29 - Hydraulic / G + Y SYS PRESS

LO

Emer Elec Config- Procedures / Abnormal and Emergency procedures / 24 - Electrical / EMER ELC CONFIG

Fuel leak- Procedures / Abnormal and Emergency procedures / 28 - Fuel / Fuel leak

Slats / Flaps Fault- Procedures / Abnormal and Emergency procedures / 27 - Slats/Flaps / FLAP SYS 1 + 2

FAULT

All PRIM failure- Procedures / Abnormal and Emergency procedures / 27 - Flight Controls / PRIM 1+2+3

FAULT

Taws- Procedures / Non ECAM Procedures / 34 - Navigation / SURV


STANDARD COURSE

HANDLING PHASE

ffs4gd.fm


• FCTM

Handling in normal operations- Normal Operations / Taxi + Before Takeoff + Takeoff + Climb + ILS Raw Data Approach +

Landing + Standard Callouts


Abnormal operations- Operational philosophy / Flight Control / Laws / Alternate Law + Direct Law + Indications

Dual Hydraulic Failure- Abnormal operations / Hydraulic

Emer Elec Config- Abnormal operations / Electrical

Abnormal Flaps and/or Slats Configuration- Abnormal operations / Flight Controls


• Ability to handle the aircraft in alternate and direct Law.• Apply good crew coordination and task sharing during abnormal operations, using ECAM

and OIS applications.


ffs4gd.fm

STANDARD COURSE

HANDLING PHASE


02.04

DAY VISUAL

TRAINEE 1

INIT HOLDING POINT: Cockpit preparation performed by instructor.

1 : Insert moderate windshear on rotation.

3 : - Use FCTL ALTN / DIRECT / BACK UP module / demo menu to perform theses exercises.- No failure inserted during these demo.- Do not explain in details the different laws.- Reinforce the following points:ALTN LAW progressive degradation impacting handling and protectionIMPORTANT: Whatever the ALT LAW active, the ECAM always displays FCTL protection lost, even if some protections remain available.DIRECT LAW: Use of manual pitch trimBACKUP Module: Aircraft controlable on the 3 axis through sidestick and rudder

4 : STALL recovery in ALTN law performed by each trainee.- in clean configuration.

• in turn : trainee 1• wings level : trainee 2

- in landing configuration.• in turn : trainee 2• wings level : trainee 1

Note : reinforce that in turn VLS is not "G loaded"

5 : Insert simultaneously HYD G + Y RSVR LEVEL LO

9 : Demonstrate NWS in alternate mode, to vacate the runway only.

14 : Arrival VIA ROA.

TRAINEE 2

20 : Insert a fuel leak of 1000 kg/min on FEED TANK 1 to trigger "Fuel leak detected"(which takes around 3 minutes).After analize and engine shutdown, consider leak continues consequently engine isrelighted.

23 : Insert failure before slats / flaps configuration.

28 : Set CAVOK"After ROA heading 250°, maintain 3000 ft".Explain to your trainees that for training purpose they don’t change the aircraft trajectory in spite of terrain ahead caution and warning in order to trigger the "PULLUP" and to perform the recovery procedure at "PULL UP".

32 : If TRAINEE 2 CAPTAIN : Trainee 2 changes from right to left seat : Instructor configurates the aircraft in elec-trical emergency configuration with gear and flaps extended before releasing thesimulation.

FFS 4 SESSION GUIDE

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E

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WEATHER LFZZ CALM 6000 OVC 008 15/10 1000

ACTIVE / INIT

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CPNY RTE PAT 33R

ALTN RTE AIBLYS

CRZ FL 4000 ft CRZ TEMP 0°C

CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY and NIGHT VISUAL FPLN : refer CO-ROUTE RWY COND WET (SID 1B) AIR COND ON PAX NUMBER : 200 ANTI ICE OFF




V1 TOGA V1 TOGA

VR v FLEX VR v FLEX





V1 145 v TOGA V1 146 v TOGA

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INIT HOLDING POINT APU RUNNING - LFZZ 33 R - GW 385 t - DAY VISUALCo-Route PAT 33R

1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)

2 - COCKPIT PREPARATION3 - ENGINE START / AFTER START4 - TAXI5 - TAKE OFF v v6 - ONE ENGINE OUT FAMILARIZATION

0:45 INIT HOLDING POINT - LFZZ 33 R

GW 385 t - DAY VISUALCo-Route PAT 33R

7 - TAKE OFF ENGINE FAIL AT VR v v8 - RELIGHT v v

1:00 INIT HOLDING POINT - LFZZ 33 R

GW 385 t - DAY VISUALCo-Route PAT 33R

9 - TAKE OFF ENGINE FIRE AT V2 v v10 - CLIMB 4000 FT v v v11 - RADAR VECTORS v v v12 - ILS APP - ONE ENGINE OUT - LFZZ 33 R

v v

13 - LANDING - ONE ENGINE OUT

1:25 INIT TAKE OFF - LFZZ 06MTOW 569 t - ZFW 360 t FOB 209 t - RADAR VECTORS - NIGHT VISUAL

14 - TAKE OFF ENGINE STALL AFTER V1

v v v

15 - CLIMB 4000 FT v v v v16 - RADAR VECTORS v v v v17 - OVERWEIGHT LANDING PROCEDURE v v v v18 - ILS APP - ONE ENGINE OUT - LFZZ 33R v v v v v19 - OVERWEIGHT LANDING ONE ENGINE OUT

v

1:55 INIT TAKE OFF - LFZZ 06MTOW 569 t - NIGHT VISUALRADAR VECTORS

20 - TAKE OFF ENGINE FIRE BEFORE V1 v v v21 - REJECTED TAKE OFF v

2:05 22 - EMER EVAC


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HANDLING PHASEL F2S

WEATHER LFZZ CALM 6000 OVC 008 15/10 1000

ACTIVE / INIT

FLT NBR A/L ID 205


CPNY RTE PAT 33R

ALTN RTE AIBLYS

CRZ FL FL 70 CRZ TEMP 0°C

CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY and NIGHT VISUAL FPLN : refer CO-ROUTE RWY COND WET (SID 1B) AIR COND ON PAX NUMBER : 200 ANTI ICE OFF




V1 TOGA V1 TOGA

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2:20 INIT HOLDING POINT - LFZZ 33R - GW 385 t - DAY VISUALCo-Route PAT 33R

23 - TAKE OFF ENGINE FAIL AT VR v v24 - RELIGHT UNSUCCESSFUL v v v

2:40 INIT HOLDING POINT - LFZZ 33RGW 385 t - DAY VISUALCo-Route PAT 33R

25 - TAKE OFF ENGINE FIRE AT V2 v v26 - CLIMB 4000 FT v v v27 - RADAR VECTORS v v v28 - ILS APP - ONE ENGINE OUT LFZZ 33 R

v v

29 - LANDING - ONE ENGINE OUT

3:10 INIT TAKE OFF - LFZZ 06 - MTOW 569 t - ZFW 360 t FOB 209 tRADAR VECTORS- NIGHT VISUAL

30 - TAKE OFF ENGINE STALL AFTER V1 v v v31 - CLIMB 4000 FT v v v v32 - RADAR VECTORS v v v v33 - OVERWEIGHT LANDING PROCEDURE v v v v34 - ILS APP - ONE ENGINE OUT LFZZ 33R

v v v v v

35 - OVERWEIGHT LANDING ONE ENGINE OUT

v

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36 - TAKE OFF ENGINE FIRE BEFORE V1 v v v37 - REJECTED TAKE OFF v38 - EMER EVAC


FFS 5 - TRAINEE 1

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

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Page 10A02.04A380 L F2S

02.04


Practice :• TAKE OFF and LANDING with engine failure.• TAKE OFF with engine failure at MTOW.• LANDING with engine failure in overweight.• REJECTED TAKE OFF.


A. REVIEW :

• OVERWEIGHT LANDING

B. NEW EXERCISES :

• ENGINE FAILURE• ENGINE RELIGHT• REJECTED TAKE OFF• EMER EVACUATION

C. SUPPORT :


D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + One Engine Out + Rejected Takeoff + Emergency evacuation

• FCOM


Engine Failure After V1 - Continued Takeoff- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG FAIL- Procedures / Abnormal and Emergency Procedures / Operating Techniques

Engine Stall- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG STALL

Engine Relight- Procedures / Not - Sensed Procedures (ABN PROC) / ENG



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Engine Fire- Procedures / Abnormal and Emergency Procedures / 26 - Fire and Smoke Protection /

ENG FIRE

Overweight landing- Procedures / Not - Sensed Procedures / Miscellaneous

Rejected Takeoff- Procedures / Abnormal and Emergency Procedures / Operating Techniques

Emergency Evacuation- Procedures / Not - Sensed Procedures (ABN PROC) / Emergency Procedures

• FCTM

Handling in normal operations- Normal Operations / Taxi + Before Takeoff + Takeoff + Climb + ILS Approach + Landing +

Standard Callouts

Takeoff at heavy weight- Normal Operations / Takeoff / Takeoff at heavy weight

Engine Failure After V1 - One Engine Inoperative Landing- Abnormal operations / Operating Techniques

Overweight Landing- Abnormal operations / Miscellaneous

Rejected Takeoff + Emergency Evacuation- Abnormal operations / Operating Techniques

• QRH- EVACUATION


• Ability to perform take off and landing ONE ENG OUT.• Acceptable engine out procedure knowledge.


STANDARD COURSE

HANDLING PHASE

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02.04

DAY / NIGHT VISUAL

6 : TRAINEE 2 / TRAINEE 1 Freeze POS and ALT at 500 ft after take off.SRS commands satisfied, wings level, side stick released, feet off rudder pedals.Select F/CTL page. Select IDLE thrust on one engine.Adjust pitch attitude to that required by SRS (the current speed or V2, whichever isgreater up to V2 + 15 kt).Hands off: observe response of FBW system. Stabilized bank angle 7~9°, spoilersand ailerons deployed, rudder pedals feedback, flying the pitch as adjusted before.Side slip index is blue now and displays the BETA TARGET.Fly the aircraft. Use continuous rudder input to center the BETA TARGET.Trim out the foot load and observe the flight controls status on F/CTL page.Repeat up to proficiency.Transfer the controls to Trainee 1 and repeat exercises.

7 : Insert engine 1 fail no damage. Restore to relight the engine.

9 : Insert simultaneously engine 4 fire 2nd agent discharge and engine 4 fail damage.

14,30 : Verify Δ V1 / Vr 10 Kt minimum. Insert stall at V1 + 2 Kt and flame out damage at Vron engine 1.

17,33 : Inform the crew that a passenger requires an immediate medical assistance. Crewperfoms overweight landing procedure and initiates the jettison.For training purpose, the instructor reduces the landing weight to 420t.

18,34 : ILS 06 U/S

23,24 : Insert engine 4 fail no damage. Insert an engine start fault EGT overlimit on engine 4.In order to interrupt the relight procedure and highlight the FADEC limited protectionin flight.

25 : Insert simultaneously engine 1 fire 1st agent discharge and engine 1 fail damage noN1.

FFS 5 SESSION GUIDE

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Issue 03 NOV 2007

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E

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WEATHER LFZZ 270/10 9999 OVC 015 20/10 998

ACTIVE / INIT

FLT NBR A/L ID 206


CPNY RTE AIBAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND WET (SID MOU 1N) AIR COND ON PAX NUMBER : 310 ANTI ICE OFF




V1 TOGA V1 TOGA

VR v FLEX °C VR v FLEX


FLAPS 3 THS FOR FLAPS THS FOR


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INIT HOLDING POINT- LFZZ 33R GW 385 tCo route AIBAIB

1 - TAKE OFF v v v2 - CLIMB FL 350 - TCAS EVENT v v v3 - FCU BACKUP v v v4 - FMS 1 + 2 FAULT - Restore v v v5 - CRUISE FL 350 v v v6 - DOOR LEAK v v v7 - EMERGENCY DESCENT

1:00 INIT FL 350 GW 385 tCo-route AIBAIB

8 - ALL ENGINE FLAME OUT v v9 - FL 100 RELIGHT ENGINE 1,2,3 v v v v

10 - RADAR VECTORS v v v v

1:4011 - ILS APP ONE ENGINE OUT LFZZ 33R

v v v

12 - GO AROUND ONE ENGINE OUT v v v13 - RADAR VECTORS - DOWNWIND v v v14 - TWO ENGINES OUT v v v15 - ILS APP - TWO ENGINES OUT LFZZ 33 R

v v v

16 - LANDING TWO ENGINES OUT v

2:00 INIT HOLDING POINT - LFZZ 33RGW 385 tCo-route PAT 33R

17 - TAKE OFF ENGINE FAILURE BEFORE V1

v v v

18 - REJECTED TAKE OFF v


FFS 6 - TRAINEE 1

Issue 05 FEB 2009

ffs6.fm

Page 12A380


HANDLING PHASEL F2S

WEATHER LFZZ 270/10 9999 OVC 015 20/10 998

ACTIVE / INIT

FLT NBR A/L ID 206


CPNY RTE AIBAIB

ALTN RTE AIBLYS


CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW 385 t847 000 lb FOB 65 t

143 000 lb

ZFW 320 t704 000 lb ZFWCG 35 %

NOTES DAY VISUAL FPLN : refer CO-ROUTE RWY COND WET (SID MOU 1N) AIR COND ON PAX NUMBER : 310 ANTI ICE OFF




V1 TOGA V1 TOGA

VR v FLEX °C VR v FLEX


FLAPS 3 THS FOR FLAPS THS FOR


V1 TOGA V1 TOGA

VR FLEX °C VR FLEX



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2:20 INIT HOLDING POINT- LFZZ 33R GW 385 t Co-route AIBAIB

19 - TAKE OFF20 - CLIMB FL 120 - TCAS EVENT v v v21 - LEFT MAIN AVIONICS SMOKE v v v22 - RETURN TO DEPARTURE - RESTORE v v v23 - RADAR VECTORS v v v24 - BACKUP SPEED SCALE DEMO v25 - ILS APP - LFZZ 33R - DIRECT LAW v26 - LANDING

2:55 INIT FL 350 GW 385 t Co-route AIBAIB

27 - DOOR OPEN v v v v28 - EMER DESCENT v v v v

3:05 29 - FL 150 - ENGINE FAILURE v v v v30 - RADAR VECTORS v v v v31 - ILS APP ONE ENGINE OUT LFZZ 33 R

v v v v v

32 - GO AROUND ONE ENGINE OUT v v v33 - RADAR VECTORS - DOWNWIND v v v34 - TWO ENGINES OUT v v v35 - ILS APP - TWO ENGINES OUT LFZZ 33 R

v v v


3:50 INIT HOLDING POINT - LFZZ 33RGW 385 t Co-route PAT 33R

37 - TAKE OFF ENGINE FIRE BEFORE V1 v v v38 - REJECTED TAKE OFF v39 - EMER EVAC


FFS 6 - TRAINEE 2

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

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Page 12A02.04A380 L F2S

02.04 <


Practice :• One engine out landing.• Two engines out landing.• Rejected take off.• All engines flame out. • Avionics smoke• Back Up Speed Scale (BUSS)


A. REVIEW :

• FCU AFS CTL PNL FAULT• ENGINE FAILURE• ENGINE RELIGHT• TCAS• REJECTED TAKE OFF• EMERGENCY DESCENT• AVIONICS SMOKE• EMER EVACUATION

B. NEW EXERCISES:

• BACK UP SPEED SCALE (BUSS)• ALL ENGINES FLAME OUT• FMS 1 + 2 FAULT• TWO ENGINES OUT APPROACH & LANDING

C. SUPPORT :




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HANDLING PHASE

Page 12B02.04A380 L F2S

D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + TCAS + All Engines Out + Two Engines Out + Back Up Speed Scale (BUSS) + FMS 1+2 FAULT + Landing + Rejected Takeoff + Emergency evacuation



FCU Back Up- Procedures / Abnormal and Emergency Procedures / 31 - Indicating/Recording / CDS

CPT + F/O EFIS CTL PNL FAULT- Procedures / Abnormal and Emergency Procedures / 22 - Flight Guidance / AUTO FLT

AFS CTL PNL FAULT

FMS 1 + 2 Fault- Procedures / Abnormal and Emergency Procedures / 22 - Flight Management

Emergency Descent- Procedures / Abnormal and Emergency Procedures / 21 - Pressurisation / CAB PRESS

EXCESS CAB ALT

All Engines Flame Out- Procedures / Abnormal and Emergency Procedures / 70 - Engines

Left Main Avionics Smoke- Procedures / Abnormal and Emergency Procedures / 26 - Fire and Smoke Protection

ADR failure + unreliable speed- Procedures / Abnormal and Emergency Procedures / 34 - Navigation / ADR 1+2+3 FAULT

+ ALL AIR DATA DISAGREE + UNRELIABLE AIRSPEED INDICATION

BUSS- Aircraft System / 34 - Navigation / ADIRS / System Description / ADR Monitoring +

Backup Speed and Altitude Scale

Landing with 2 Engines Inoperative (on the same wing)- Procedures / Not - Sensed Procedures (ABN PROC) / ENG

Engine Relight in Flight- Procedures / Not - Sensed Procedures (ABN PROC) / ENG




STANDARD COURSE

HANDLING PHASE

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Page 12C02.04A380 L F2S

• FCTM


Standard Callouts

FMS 1+2 Fault - Abnormal operations / Auto Flight

FCU Back Up- Abnormal operations / Auto Flight

Emergency Descent- Abnormal operations / Miscellaneous

All Engines Flame Out- Abnormal operations / Power Plant

Flying the Back Up Speed Scale- Abnormal operations / Navigation

Smoke / Fumes - Abnormal operations / Fire Protection

Engine Failure- Abnormal operations / Operating Techniques / Engine Failure during Cruise + One Engine

Inoperative Go Around + One Engine Inoperative Landing + Two Engine Inoperatvie Landing


• QRH- EVACUATION- SMOKE / FUMES


• Ability to perform approach, landing and go around with one engine out.• Ability to perform approach and landing with two engines out.• Satisfactory engine out procedure knowledge.• Good knowledge and understanding of unreliable speed indication event and satisfactory

application of the BUSS.


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Page 12D02.04A380 L F2S

02.04

DAY VISUAL

TRAINEE 1

INIT HOLDING POINT: Cockpit preparation performed by instructor.

2, 3, 4 : During climb to FL 350. - Simulate SMOKE coming FROM FCU PANEL

• Demonstrate how to switch OFF FCU (LEFT KNOB). Highlight use of FCU backup. Restore

- Insert FMC A+B+C FAULT to trigger FMS 1+2 FAULT. Explain that :• FOR NAVIGATION : Show the different items of the SFD and SND menu.

- Insert on the SND 2 or 3 waypoints (MOU and ROA for example) and AIB asa 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.

Restore.

6 : Insert cabin door leak (rate 2500 ft/min). Restore.

7 : Insert CAB PRESS - EXPLOSIVE DECOMPRESSION.

8 : Insert ENG 1 FAIL NO DAMAGE ENG 2 FAIL NO DAMAGE ENG 3 FAIL NO DAMAGE ENG 4 FAIL DAMAGE

Ditching and forced landing procedure which are not performed in the simulator willbe reviewed during the briefing only.

9 : Keep engine failed to apply relight procedure in windmilling until FL 200 where theAPU is started.When APU BLEED on, cancel engine failure on engine 1 and 2 to allow relight onengine 1 and 2.When the first engine is relit, ALL ENG FLAME OUT alert disappears. Continue tentative of relights on engine 3 by selecting the ENG RELIGHT ABNPROC as requested by ECAM. Cancel engine 3 failure to allow engine 3 relight butkeep engine 4 failed to continue the approach with one engine inoperative. Restore electrical emergency configuration. Reset all systems and ADIRS quickalignment to recover normal law, but keep engine 4 shutdown.

13 : In downwind, insert 2nd engine failure on engine 3.

17 : Insert ENG 3 N1 OVER LIMIT

FFS 6 SESSION GUIDE

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STANDARD COURSE

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TRAINEE 2

21 : Insert LEFT MAIN AVNCS SMOKE. When GEN 1 + 2 OFF, smoke still detected inthe bay. Continue procedure. When Gen 3 + 4 OFF, smoke stops in the AVNCS BAY.

24 : Set 3 ADR OFF for BUSS demo. Explain that the lower part of the green band is thetarget to fly before extending S/F configuration. The higher part the target to retract.When configurated, target to fly is the middle of the green band.

27 : Insert FWD CARGO DOOR NOT CLOSED + CAB PRESS EXCESS CAB ALT inorder to simulate cargo door loss. .

29 : Passing FL 150, insert engine 3 OIL PRESS LO in order to shutdown the engine

33 : In downwind, insert 2nd engine failure with damage on engine 4.

37 : Insert an engine fire not extinguishable.

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E

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WEATHER LFZZ 270/15 3000 SN OVC 009 -2/-4 1019 BIKF 320/18 2000 SN OVC 008 -10/-3 1013

ACTIVE / INIT

FLT NBR A/L ID 207


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW - FOB -

ZFW 300 t777 000 lb ZFWCG 35 %

NOTES DAY VISUAL (down to night) RWY COND COMPACTED SNOW FOR TAKE OFF AND WET FOR LANDING FPLN : refer CO-ROUTE AIR COND ON (SID ATN 1N) ANTI ICE ENG + WING ON PAX NUMBER: 450


ACTIVE / PERFLFZZ 33R / MTOW


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INIT HOLDING POINT- LFZZ 33R - MTOW Co-route AIBKEF

1 - PRELIMINARY COCKPIT PREPARATION (AIRCRAFT ELECTRICALLY SUPPLIED)

v

2 - COCKPIT PREPARATION v3 - ENG START / AFTER START v4 - TAXI v

0:40 5 - TAKE OFF v v v6 - ENGINE FAIL AFTER V1 v v v7 - JETTISON v8 - NDB APP ONE ENGINE OUT

LFZZ 33R (SELECTED) v v v v1:00 9 - GO AROUND ONE ENGINE OUT v v v

10 - RADAR VECTORS - DOWNWIND v v v11 - ILS APP - LFZZ 33 R TWO ENGINES OUT

v v v


1:40

INIT HOLDING POINT - LFZZ 24 MTOW 569 t - ZFW 360 t - FOB 209 tCo-route AIBAIB1RR Trent 972 V1 : 126 - VR : 150 - V2 : 158 - TOGAEA GP 7272 V1 : 154 - VR : 171 - V2 : 175 - Flex 30

13 - TAKE OFF ENGINE FAILURE BEFORE V1 v v v14 - REJECTED TAKE OFF v


FFS 7 - TRAINEE 2

Issue 05 FEB 2009

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Page 14A380


HANDLING PHASEL F2S

WEATHER LFZZ 270/15 3000 SN OVC 009 -2/-4 1019 BIKF 320/18 2000 SN OVC 008 -10/-3 1013

ACTIVE / INIT

FLT NBR A/L ID 207


CPNY RTE AIBKEF

ALTN RTE KEFSNN


CI 90 TROPO 36090

TRIP WIND -

ACTIVE FUEL & LOAD

GW - FOB -

ZFW 300 t777 000 lb ZFWCG 35 %

NOTES DAY VISUAL (down to night) FPLN : refer CO-ROUTE RWY COND COMPACTED SNOW FOR TAKE OFF AND WET FOR LANDING AIR COND ON (SID ATN 1N) ANTI ICE ENG + WING ON PAX NUMBER: 450




V1 v TOGA V1 v TOGA

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2:05 INIT HOLDING POINT - LFZZ 33R - MTOWCo-route AIBKEF

15 - TAKE OFF v v v16 - ENGINE FAIL AFTER V1 v v v17 - JETTISON v v v18 - VOR DME APP ONE ENGINE OUT - LFZZ 33 R (FLS) v v v

2:30 19 - GO AROUND ONE ENG OUT v v v20 - RADAR VECTORS - DOWNWIND v v v21 - ILS APP - LFZZ 33 R TWO ENGINES OUT

v v v


2:50 INIT TAKE OFF - LFZZ 24 MTOW 569 t - ZFW 360 t - FOB 209 tCo-route AIBAIB1RR Trent 972 V1 : 126 - VR : 150 - V2 : 158 - TOGAEA GP 7272V1 : 126 - VR : 150 - V2 : 158 -

23 - TAKE OFF - ENGINE FAILURE BEFORE V1 - INCAPACITATION

v v v

24 - REJECTED TAKE OFF v

3:00 INIT FL 350 GW 385 t - ZFW 320 t - FOB 65tCo-route AIBAIB

25 - AIR COND SMOKE v v v v26 - SMOKE / FUMES REMOVAL v v v v27 - DES - RADAR VECTORS v v v v28 - BACKUP SPEED SCALE DEMO v v29 - ILS APP - LFZZ 33R - DIRECT LAW v

3:45 30 - LANDING31 - EMER EVAC


FFS 7 - TRAINEE 1

Issue 05 FEB 2009

STANDARD COURSE

HANDLING PHASE

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Page 14A02.04A380 L F2S

02.04


• Practice one engine out take off / go around.• Practice two engines out landing.• Familiarize and practice Back Up Speed Scale (BUSS).• Crew incapacitation.• Practice AIR COND SMOKE and SMOKE FUMES REMOVAL procedures


A. REVIEW :

• EMERGENCY DESCENT• ENGINE FAILURE• CREW INCAPACITATION• JETTISON• BACK UP SPEED SCALE (BUSS)• TWO ENGINES OUT• REJECTED TAKE OFF• EMER EVACUATION

B. NEW EXERCISES :

• AIR COND SMOKE - SMOKE FUMES REMOVAL

C. SUPPORT :

• DVD 1 : FFS briefing guides• FCOM• FCTM



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Page 14B02.04A380 L F2S

D. REFERENCES :

• BRIEFING GUIDESTaxi + Takeoff + 2 Engines Out + Back Up Speed Scale (BUSS) + Landing + Rejected Takeoff + Emergency evacuation

• FCOM


Engine Failure After V1 - Continued Takeoff- Procedures / Abnormal and Emergency Procedures / 70 - Engines / ENG FAIL- Procedures / Abnormal and Emergency Procedures / Operating Techniques

Fuel Jettison - Procedures / Not - Sensed Procedures (ABN PROC) / Fuel

ADR failure + unreliable speed- Procedures / Abnormal and Emergency Procedures / 34 - Navigation / ADR 1+2+3 FAULT

+ ALL AIR DATA DISAGREE + UNRELIABLE AIRSPEED INDICATION

BUSS- Aircraft System / 34 - Navigation / ADIRS / System Description / ADR Monitoring +

Backup Speed and Altitude Scale

Landing with 2 Engines Inoperative (on the same wing)- Procedures / Not - Sensed Procedures (ABN PROC) / ENG


Crew Incapacitation- Procedures / Non ECAM Procedures / Miscellaneous


• FCTM


Standard Callouts

Emergency Descent- Abnormal operations / Miscellaneous


STANDARD COURSE

HANDLING PHASE

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Flying the Back Up Speed Scale- Abnormal operations / Navigation

Engine Failure- Abnormal operations / Operating Techniques / Engine Failure during Cruise + One Engine

Inoperative Go Around + Two Engine Inoperatvie Landing


Crew Incapacitation- Abnormal Operations / Miscellaneous

• QRH- EVACUATION- SMOKE / FUMES


• Good knowledge and understanding of unreliable speed indication event and satisfactory application of the BUSS.

• The application of normal standard operating procedures and FMS initialisation and abnormal procedures in all flight phases is of standard level or above.


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02.04

DAY VISUAL

Start session with date 1st June at 16.30 factor 1 inserted on IOS to induce progressive day tonight flight

TRAINEE 2

INIT HOLDING POINT LFZZ 33R: Let the trainees compute the MTOW.

6 : Insert engine fail damage + turbine over heat on engine 1.

7,17 : Speed up jettisoning from IOS to reach GW below MLW

10,20 : In downwind, insert 2nd engine failure on the same wing and adjust visibility 8 km / ceiling 1500’ AGL when reaching pattern altitude.

13 : Insert engine 1 fail at 50 kt

TRAINEE 1

23 : Select SMOKE GENERATOR "ON" in the simulator control menu, in order to preheat. (10 min) the generator for the AIR COND SMOKE exercise.Insert engine 1 fail damage.When engine failed no reaction of trainee 1 who is incapacitated.Trainee 2 takes over and performs the RTO.

25 : Call from the purser "Smoke in the cabin coming from OUTLETS".Flight crew applies SMOKE / FUMES ABN PROC if the visibility in the cockpit is sufficient and ECAM is available or refer to the QRH.After 1 minute insert AIR COND SMOKE, to generate smoke in the cockpit.Dense smoke in the cockpit : Crew apply SMOKE / FUMES REMOVAL and descentto FL 100.Cancel AIR COND SMOKE when PACKS 1 + 2 OFF. SMOKE GENERATORSTOPS. Radar Vectors

28 : In downwind, set 3 ADR OFF for BUSS demo. Explain that the lower part of theGREEN BAND is the target to fly before extending S/F configuration. The higher partthe target to retract. When configurated, target to fly is the middle of the green band.

31 : Insert an APU fire not extinguishable when runway vacated.

FFS 7 SESSION GUIDE

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02.05

02.05LOFT SYLLABI

The Airbus Line Oriented Flight Training (ALOFT) session is intended to provide crews with opportunities to enhance their understanding of the A380 and to apply Crew Resource Management principles to simulated regular airline flight.Scenarios are intended to produce a busy environment, but should never overload the crew. In many cases, there is no single 'right' answer but, using their skills and knowledge, the crew should be able to reach a successful conclusion to each scenario. Alternative solutions may provide useful, constructive post-flight discussion.Relative simple failures are introduced during the flight to enable the session objectives to be met.

To make ALOFT as valuable and realistic as possible, flight documentation (files available in the “INST SUP FLIGHT” menu on Airbus People server) is provided by the instructor to the trainees before the briefing. The flight briefing will begin 1 hour before the scheduled simulator start time and will take 15-20 minutes. Thereafter the crew will have some time to study the documentation and, for example, decide on the required fuel load, etc. The take-off time for the flight is considered to be 30 minutes after the simulator session starts.

ALOFT scenario routing is :

- Trainee 1 : Paris-Charles de Gaulle / New-York Kennedy (LFPG / KJFK)- Trainee 2 : London-Heathrow / New-York Kennedy (EGLL / KJFK)


ALOFT

Issue 03 NOV 2007

02-05.fm


ALOFT SYLLABI

02.05A380

02.05



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ALOFT SYLLABI

Page 1A380

02.05

02.05LOFT SYLLABI

The Airbus Line Oriented Flight Training (ALOFT) session is intended to provide crews with opportunities to enhance their understanding of the A380 and to apply Crew Resource Management principles to simulated regular airline flight.Scenarios are intended to produce a busy environment, but should never overload the crew. In many cases, there is no single 'right' answer but, using their skills and knowledge, the crew should be able to reach a successful conclusion to each scenario. Alternative solutions may provide useful, constructive post-flight discussion.Relative simple failures are introduced during the flight to enable the session objectives to be met.

To make ALOFT as valuable and realistic as possible, flight documentation (files available in the “INST SUP FLIGHT” menu on Airbus People server) is provided by the instructor to the trainees before the briefing. The flight briefing will begin 1 hour before the scheduled simulator start time and will take 15-20 minutes. Thereafter the crew will have some time to study the documentation and, for example, decide on the required fuel load, etc. The take-off time for the flight is considered to be 30 minutes after the simulator session starts.

ALOFT scenario routing is :

- Trainee 1 : Paris-Charles de Gaulle / New-York Kennedy (LFPG / KJFK)- Trainee 2 : London-Heathrow / New-York Kennedy (EGLL / KJFK)


ALOFT

Issue 03 NOV 2007

02-05.fm


ALOFT SYLLABI

02.05A380

02.05



Documents

elearning.onurair.com.trelearning.onurair.com.tr/webcmi/data/.../XAY09301/A380_FTCP/LF2S… · 02-00.fm FLIGHT CREW TRANSITION COURSE TABLE OF CONTENTS Page 1 A380 02.00 L F2S 02.00