E FC4 RECURRENT TRAINING AND CHECKING A320...

A320

FLIGHT CREW TRAINING PROGRAM

RECURRENT TRAINING AND CHECKING

TABLE OF CONTENTS

E FC4 04.00

Issue 10 SEP 2012

CONTENT_EFC4

04.01 - INTRODUCTION 04.02 - TRAINING SYLLABI

TRAINING Session A CHECKING Session A TRAINING Session B CHECKING Session B TRAINING Session C CHECKING Session C TRAINING Session D CHECKING Session D TRAINING Session E CHECKING Session E

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TABLE OF CONTENTS

E FC4 04.00

Issue 10 SEP 2012

CONTENT_EFC4

THIS PAGE INTENTIONALLY LEFT BLANK

A320



INTRODUCTION

E FC4 04.01 Page 1

Issue 10 SEP 2012

INTRO_EFC4

01 - GENERAL

Airbus Recurrent Training and Checking Program is designed as a unique service for the Customer Airlines (For internal training in AIRBUS TRTO refer to the Flight Crew Training Operations Manual). The analysis supporting this recommended program has been conducted in accordance with JAR-OPS requirements for single type operation - the program is not applicable for Mixed Fleet Flying. Furthermore, this program only covers requirements for systems review and simulator recurrent training and checking. The operator remains responsible for: • Adapting this program to meet requirements of their authorities and/or to embed airline specifics • Emergency & Safety equipment training and checking • CRM refresher • Line Checks • Other refresher courses. E.g. dangerous goods The operator is also responsible for the RECURRENT TRAINING AND CHECKING FOLLOW UP in order to ensure that each pilot completes the applicable program at the required interval.

02 - COURSE DESCRIPTION The course consists of: • Aircraft systems review • Aircraft systems test - only if crew member's licence to be revalidated or renewed • One 4 hour simulator training session given by an SFI (or TRI) consisting of:

- A briefing covering technical and CRM aspects - The Full flight simulator session on level B or higher certified simulator - A debriefing covering technical and CRM aspects

• One 4 hours simulator checking session given by a TRE consisting of: - A briefing covering technical and CRM aspects - The Full flight simulator session on level B or higher certified simulator - A debriefing covering technical and CRM aspects

There are 5 different programs - (systems review and simulator sessions). The applicable program is identified by a letter - A to E - determined using the table below:

Define Applicable Program

Last Digit Current Year

0 1 2 3 4 5 6 7 8 9

Current Month

1 to 6 A C E B D A C E B D

7 to 12 B D A C E B D A C E The normal interval between 2 Recurrent Training and Checking programs is 6 months.

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INTRODUCTION

E FC4 04.01 Page 2

Issue 10 SEP 2012

INTRO_EFC4

03 - RECURRENT CBT GUIDE

SCENARIO

A B C D E

AIRCRAFT SYSTEMS

ATA 26 ATA 28 ATA 32

ATA 21 ATA 29 ATA 34 ATA 49 ATA 52

ATA 22 ATA 35

ATA 27 ATA 30 ATA 33 ATA 36 ATA 70

ATA 24 ATA 31 ATA 46

04 - SESSION PREPARATION - Recurrent training: the airport used is the generic airport called Airbus Training Airport (LFZZ). - Recurrent checking scenarios:

Events part 1: Marseille (LFML) / Lyon (LFLL) Events part 2: Lyon (LFLL) / Marseille (LFML)

A320



TRAINING SESSION A

E FC4 04.02 Page 1

Issue 10 SEP 2012

TRAINING-A_EFC4

BRIEFING ROOM Review technical: TCAS/Incapacitation Review CRM: Leadership and Teamworking SIMULATOR SETUP - FLT NBR: AIRBUS 101 POS INIT: LFZZ RWY 33 - Gate C2 V1=133 VR=133.V2=137.CONF=3 FLEX=48 WX INIT: LFZZ 26009KT 9999 F020 TCU040 28/26 Q1020 ACFT INIT CB IN VICINITY ZFWCG: 29

: ZFW: 57T

BLOCK: 8T

NOTAM: Nil MEL

: Nil

Time Total Events Part 1 PF 00.20

00.20 Transit cockpit preparation Insert route AIBAIB1 - MOU 1N DEP

if STD Crew: CM2

-

if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.10

00.30

Engine start ATA 70: Start fault, Hot Start followed by manual engine start Insert a HOT START on engine 1. After ECAM completion, restore and perform a manual engine start on engine 1. Highlight the difference of protections between AUTO and MAN. FADEC provides a passive survey of the start sequence in MAN. Review limitations.

00.05 00.35 Taxi - before take-off RW 33R 00.50 Take-off: windshear (moderate) on rotation

During Climb: ATA 28 FUEL LEAK After analysis and engine shutdown procedure, leak continues. Consequently engine is restarted. Stop exercise and leak after engine restart.

During climb or cruise, ATA 22 FMGC 2 FAULT AP 2 is lost, BOTH PFD ON SAME FMGC is displayed

Radar vectors - non precision approach RW33R. During approach: PNF incapacitation Ask (private call) PNF to be incapacitated and let PF work alone for the approach and the go around

Go around - Lower ceiling or runway blocked - if required Check weather. Visual approach RW33R 01.25 Landing

00.35 Init T/O - LFZZ - RWY 24 - SID ROA 1S to join ROA - Same weather MTOW / ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=156 VR=161.V2=161. CONF=1+F FLEX=54

If STD Crew: CM1

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)

Engine failure between V1 and V2. Engine Out Contingency Procedure: At AIB/D3 or MOU/R-146 RT DCT MOU

Overweight landing procedure.

Radar vectors for ILS approach RW33R. On intercept Heading: ATA 22: AP1+2 FAULT Set ceiling below DH to force GA in IMC.

Go around.

Set visibility to 10km and ceiling OVC026. Visual approach RW33R

02.00 Landing

Notes: (1) For NON STD Crew: PF = CM1 if 2 captains or PF = CM2 if 2 F/O’s. Swap seats after the midsession break (2) RH qual Crew = 2 pilots requiring RH seat practice (TRI’s or SFI’s). Swap seats after the midsession break

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TRAINING SESSION A

E FC4 04.02 Page 2

Issue 10 SEP 2012

TRAINING-A_EFC4

Time Total Events Part 2 PF

00.15 02.15 Break

00.05

02.20

PART 2 - init holding point 33R Insert route AIBAIB1 - MOU 1N DEP Weather: LFZZ 26009KT 9999 F020 TCU040 28/26 Q1020 ZFW = 57T ZFWCG = 29 FUEL = 8T V1=133 VR=133.V2=137.CONF=3 FLEX= 48

if STD Crew : CM1

-

if NON STD

Crew : CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.30 Take-off: windshear (moderate) after rotation

During Climb ATA 26 SMOKE MAIN AVIONICS LEFT (stop after GEN1 OFF) or AIR COND SMOKE (stop after PACK2 OFF).

Radar vectors for ILS approach RWY 33R On intercept hdg: Fail AP -if required. Set FD’s OFF. Raw data approach

02.50 Landing

00.05

02.55

Init T/O RWY 24, SID ROA 1S to join ROA. Same weather MTOW - ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=156 VR=161.V2=161. CONF=1+F FLEX=54

If STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)

00.30 Engine fire and failure between V1 and V2. Engine Out Contingency Procedure: At AIB/D3 or MOU/R-146 RT DCT MOU


Radar vectors for: VOR approach RWY 33R

When RWY in sight and AP disconnect: Fail both AP’s Runway blocked: Go around one engine out

Check weather for Visual approach RW33R

03.25 Landing one engine out

00.20

03.45

Init T/O - LFZZ - RW33R Insert route PAT 33R Weather: Set RVR 0125 and ceiling OVC001 ZFW = 57T ZFWCG = 29 FUEL = 8T V1=133 VR=133.V2=137. CONF=3 FLEX= 48 CAT II/III training. 1 take-off / 1 go-around - due AutoLand Wrng light/ 1 landing

CM1

00.05 03.50 Rejected take off + Evacuation due to inextinguishable engine fire (1) (2) See notes on previous page. RECURRENT PROGRAM COMPLETED - SEE DETAILS ON BACK PAGE (OR ATTACHMENT) DATE: ●●●●●●●●● SATISFACTORY NOT SATISFACTORY INSTRUCTOR’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●● TRAINEE’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●●

A320



CHECKING SESSION A

E FC4 04.02 Page 1

Issue 10 SEP 2012

CHECKING-A_EFC4

BRIEFING ROOM Review technical: Crosswind take-off/De-icing Review CRM: Workload Management SIMULATOR SETUP - FLT NBR: AIRBUS 102 POS INIT: LFML RWY 13L - Gate 9A V1=151 VR=151 V2=152 CONF=1+F FLEX=51 WX INIT: LOW VISIBILITY OPERATION ACFT INIT LFML 17007KT 0150 OVC001 8/7 Q1002 ZFW: 58T

:

LFLL 30006KT 0200 OVC001 6/5 Q1003 ZFWCG: 29 LFBD 2408KT 5000 OVC009 8/7 Q1004 BLOCK: 7T NOTAM: Nil MEL

: Nil

MRS Cpt 121.72GND 121.9TWR 133.65DEP 131.22MRS 123.9MRS 126.7LYS APP 136.07TWR 120.45

Time Total Events Part 1 PF JAR FCL 00.25

00.25

Transit cockpit preparation Aircraft electrically supplied - Insert route MRSLYS EOCP: AT 1600FT RT MTG. EO ACC 2000FT

if STD Crew : CM1 (1)

//

if NON STD

Crew : CM1

or CM2 (2)

1.1/1.3/1.4

00.10 00.35 Taxi - before take-off 1.5/1.6 01.00 Take-off

During climb: ATA 34 ADR 2 FAULT 2.2/3.9.1

3.4.2 During Climb: ATA 22 AUTO FLT FCU FAULT - one FCU recovered after

reset. 3.4.11

During cruise: TCAS 3.6.9 Radar vectors for ILS CAT II / III approach RWY36L 6.2 Go around 6.3 01.35 Landing CAT II / III RWY 36L 6.4

00.05

01.40

Init T/O - LFLL - RWY 36L LFLL 28015KT 6000 OVC008 15/8 Q1003 ZFW= 58T ZFWCG= 29 FUEL=7T V1=145 VR=151 V2=155 CONF=1+F FLEX=51

00.20 Engine failure then fire between V1 and V2. Engine Out Contingency Procedure: At 2300 turn left to VNE HP

2.5.2

Radar vectors for ILS approach RWY 36L. On intercept Heading: ATA 22: AP1+2 FAULT Set ceiling below DH to force GA in IMC.

3.4.8/ 3.9.3.4

Go around one engine out - AP avail after cleanup 4.3 Set ceiling at MDH + 100ft.

Radar vectors for: LOC G/S out approach RWY 36L 3.9.4

02.00 Landing one engine out 5.5 Rejected take off - ONLY for NON Standard crew 2.6

Notes: (1) If 3 hours session - Only one pilot to be checked: Pilot to be checked - CAPT or FO - performs full Part1 as PF and items marked by an asterisk in Part2 as PNF. (2) For NON STD Crew: PF = CM1 if 2 captains or PF = CM2 if 2 F/O’s. Swap seats after the midsession break

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CHECKING SESSION A

E FC4 04.02 Page 2

Issue 10 SEP 2012

CHECKING-A_EFC4

Time Total Events Part 2 PF JAR FCL (1)

00.15 02.15 Break

00.15

02.30

PART2 - init holding point RW36L Insert route LFLL - LFLL LFLL 28015KT 6000 OVC008 15/8 Q1003 ZFW 58T ZFWCG = 29 FUEL = 7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51

if STD Crew: CM2 (1)

-

if NON STD

Crew: CM1

or CM2 (2)

00.40 Take-off RWY 36L Take-off - windshear (light) after rotation

2.3 3.6.5 *

During climb ATA 32: L/G not locked up 3.4.12 *

Radar vectors for ILS approach RWY 36L On intercept hdg: ATA 22:AP & FD1+2 FAULT - Raw data approach

3.9.3.1 3.4.8 *

03.10 Crosswind Landing 5.3 *

00.05

03.15

INIT T/O - LFLL - RWY 36L Same weather ZFW 58T ZFWCG=29 FUEL = 7T V1=145 VR=151 V2=155 CONF=1+F FLEX=51

00.35 Engine fire and failure between V1 and V2. Engine out Contingency Procedure: At 2300 turn left to VNE HP

2.3 2.5.2

Radar vectors for ILS approach RWY 36L. On intercept Heading: ATA 22: AP1+2 FAULT Set ceiling below DH to force GA.

3.4.8 3.9.3.4


Radar vectors for: VOR approach RWY 36R 3.9.4

03.50 Landing one engine out 5.5

00.05

03.55

Init T/O - LFLL - RWY36L LFLL 34007KT 0125 OVC001 8/7 Q1002 ZFW 58T ZFWCG = 29 FUEL + 7T V1=159 VR=159 V2=160 CONF=1+F FLEX = 52

*

00.05 04.00

Rejected take off due to unextinguishable engine fire 2.6 3.6.1 *

(1) (2) See notes on previous page. JAR-FCL references to fill JAR FCL FORM 1.240 1.1/1.3/1.4/1.5/1.6/2.2/2.3/2.5.2/2.6/3.4.2/3.4.8/3.4.11/3.4.12/3.6.1/3.6.5/3.6.9/3.9.1/3.9.3.1/3.9.3.4/3.9.4/4.3/5.3/5.5/6.1/6.2/ 6.3/6.4. RECURRENT PROGRAM COMPLETED - SEE DETAILS ON BACK PAGE (OR ATTACHMENT) DATE: ●●●●●●●●● SATISFACTORY NOT SATISFACTORY INSTRUCTOR’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●● TRAINEE’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●●

A320



TRAINING SESSION B

E FC4 04.02 Page 1

Issue 10 SEP 2012

TRAINING-B_EFC4

BRIEFING ROOM Review technical: Crosswind take-off/ Windshear recovery Review CRM: Workload Management SIMULATOR SETUP - FLT NBR: AIRBUS 101 POS INIT

: LFZZ RWY 33 - Gate C2 V1=132.VR=132.V2=136. CONF=3 FLEX=46

WX INIT: LFZZ 26018KT 9999 FEW030 SCT045 20/16 Q998 ACFT INIT ZFWCG: 29

: ZFW: 58T

BLOCK: 7T

NOTAM: Nil MEL

: Nil



if STD Crew: CM2

-

if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.10

00.30

Engine start ATA 70: Start valve stuck closed. Insert “START VALVE fault CLOSED”. Emphasize the MMEL consultation. Dispatch with the start valve inoperative on the corresponding engine and perform the manual start valve operation.


ATA 34 F/O ATT disagree (pitch) Warning will be triggered after a discrepancy of 5°. The CHECK ATT message will flash for 9sec then remains steady on both PFD

During cruise, ATA 29 HYD system overheat: Insert an overheat on GREEN system and keep the overheat till landing

Radar vectors - non precision approach RW33R. During approach: Windshear ahead Insert a predictive windshear about 2 miles on final


00.35 Init T/O - LFZZ - RWY 24 - SID ROA 1S to join ROA - Same weather MTOW / ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=162.VR=165.V2=165. CONF=1+F FLEX= 53

If STD Crew: CM1

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)




Go around.


02.00 Landing


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TRAINING SESSION B

E FC4 04.02 Page 2

Issue 10 SEP 2012

TRAINING-B_EFC4


00.15 02.15 Break

00.05

02.20

PART 2 - init holding point 33R Insert route AIBAIB1 - MOU 1N DEP Weather: LFZZ 26018KT 9999 FEW030 SCT045 20/16 Q998 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=132.VR=132.V2=136.CONF=3 FLEX= 46

if STD Crew : CM1

-

if NON STD

Crew : CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)


During Climb ATA 24 ELEC EMER CONFIG


02.50 Landing

00.05

02.55

Init T/O RWY 24, SID ROA 1S to join ROA. Same weather MTOW - ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=162.VR=165.V2=165. CONF=1+F FLEX=53

If STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)




When RWY in sight and AP disconnected: Fail both AP’s Runway blocked: Go around one engine out



00.20

03.45

Init T/O - LFZZ - RW33R Insert route PAT 33R Weather: Set Wind 260/5, RVR 0125 and ceiling OVC001 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=132.VR=132.V2=136. CONF=3 FLEX= 46 CAT II/III training. 1 take-off / 1 go-around - due Auto Land Wrng light/ 1 landing

CM1


A320



CHECKING SESSION B

E FC4 04.02 Page 1

Issue 10 SEP 2012

CHECKING-B_EFC4

BRIEFING ROOM Review technical: Contaminated take-off/Windshear recovery Review CRM: Problem Solving & Decision making SIMULATOR SETUP - FLT NBR: AIRBUS 102 POS INIT: LFML RWY 13L - Gate 9A V1=151 VR=151 V2=152 CONF=1+F FLEX=51 WX INIT: LOW VISIBILITY OPERATION ACFT INIT LFML 17007KT 0150 OVC001 8/7 Q1002 ZFW: 58T

:


: Nil



00.25



//

if NON STD

Crew : CM1

or CM2 (2)

1.1/1.3/1.4


During climb: ATA 21 VENT BLOWER FAULT (remove when Blower overridden) 2.2/3.9.1

3.4.1 During Climb: ATA 29 GREEN RSVR LOW LEVEL 3.4.5 During cruise: TCAS 3.6.9 Radar vectors for ILS CAT II / III approach RWY36L 6.2 Go around 6.3 01.35 Landing CAT II / III RWY 36L 6.4

00.05

01.40

Init T/O - LFLL - RWY 36L LFLL 28015KT 6000 OVC008 15/8 Q1003 ZFW= 58T ZFWCG= 29 FUEL=7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51


2.5.2


3.4.8/ 3.9.3.4





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CHECKING SESSION B

E FC4 04.02 Page 2

Issue 10 SEP 2012

CHECKING-B_EFC4


00.15 02.15 Break

00.15

02.30

PART 2 - init holding point RW36L Insert route LFLL - LFLL LFLL 28015KT 6000 OVC008 15/8 Q1003 ZFW 58T ZFWCG = 29 FUEL = 7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51


-

if NON STD

Crew: CM1

or CM2 (2)


2.3 3.6.5 *

During climb ATA 27 FLAPS locked at retraction between 1 and 2 3.4.13 *


3.9.3.1 3.4.8 *


00.05

03.15

INIT T/O - LFLL - RWY 36L Same weather ZFW 58T ZFWCG=29 FUEL = 7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51

00.35 Engine fire and failure between V1 and V2. Engine Out Contingency Procedure: At 2300 turn left to VNE HP

2.3 2.5.2


3.4.8 3.9.3.4




00.05

03.55

Init T/O - LFLL - RWY 36L LFLL 34007KT 0125 OVC001 8/7 Q1002 ZFW 58T ZFWCG = 29 FUEL + 7T V1=159 VR=159 V2=160 CONF=1+F FLEX = 52

*

00.05 04.00



A320



TRAINING SESSION C

E FC4 04.02 Page 1

Issue 10 SEP 2012

TRAINING-C_EFC4

BRIEFING ROOM Review technical: De-icing / Contaminated Runway Review CRM: Communication SIMULATOR SETUP - FLT NBR: AIRBUS 101 POS INIT: LFZZ RWY 33 - Holding Gate C2 V1=118.VR=125.V2=129.CONF=3 FLEX=TOGA WX INIT: LFZZ 27005KT 1500 SNSH OVC008 M1/M3 Q1005 ACFT INIT Slush 1/4” (6.3mm), RWY CONTA ZFWCG: 29

: ZFW: 58T

BLOCK: 7T

NOTAM: Nil MEL

: Nil



if STD Crew: CM2

-

if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.10

00.30

Engine start ATA 70: Start fault, Hung start followed by manual engine start. Insert a HUNG START on engine 1 due to low air pressure. After ECAM completion, restore and perform a manual engine start on engine 1. Highlight the difference of protections between AUTO and MAN. FADEC provides a passive monitoring of the start sequence in MAN. Review limitations


During Climb: ATA 34 BLOCKED PITOT ON CM1 Blocked PITOT: insert failure on CM1 during climb. IAS, TAS and MACH indications on CAPT PFD are not reliable, Airspeed on CAPT side is frozen as long as the aircraft stays in level flight and increases/decreases if aircraft climbs/descends

During Approach: ATA 27 SLATS LOCKED Insert the SLATS LOCKED just before reaching Conf 1

Radar vectors - non precision approach RW33R. During approach: Destabilized approach. Keep the trainee high or fast (e.g. 170 kt to the OM) in approach and introduce some tailwind. Being not established at 1000ft, the trainee must go around


00.35 Init T/O - LFZZ - RWY 24 - SID ROA 1S to join ROA - Same weather MTOW / ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=127.VR=138.V2=140. CONF=1+F. FLEX= TOGA

If STD Crew: CM1

-

if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM2 (2)




Go around.


02.00 Landing


A320



TRAINING SESSION C

E FC4 04.02 Page 2

Issue 10 SEP 2012

TRAINING-C_EFC4


00.15 02.15 Break

00.05

02.20

PART 2 - init holding point 33R Insert route AIBAIB1 - MOU 1N DEP Weather: LFZZ 27005KT 1500 SNSH OVC008 M1/M3 Q1005 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=118.VR=125.V2=129.CONF=3. FLEX= TOGA

if STD Crew : CM1

-

if NON STD

Crew : CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)


During Climb ATA 32 ATA 29 DUAL HYD FAILURE (G+Y).

Radar vectors for ILS approach RWY 33R On intercept heading: Fail AP -if required. Set FD’s OFF. Raw data approach

02.50 Landing

00.05

02.55

Init T/O RWY 24, SID ROA 1S to join ROA. Same weather MTOW - ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=127.VR=138.V2=140. CONF=1+F. FLEX= TOGA

If STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)







00.20

03.45

Init T/O - LFZZ - RW33R Insert route PAT 33R Weather: Set RVR 0125 and ceiling OVC001 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=118.VR=125.V2=129. CONF=3. FLEX= TOGA CAT II/III training. 1 take-off / 1 go-around - due Auto Land Warning / 1 landing

CM1


A320



CHECKING SESSION C

E FC4 04.02 Page 1

Issue 10 SEP 2012

CHECKING-C_EFC4

BRIEFING ROOM Review technical: TCAS/Emergency descent Review CRM: Leadership and Teamworking SIMULATOR SETUP - FLT NBR: AIRBUS 102 POS INIT: LFML RWY 13L - Gate 9A V1=151 VR=151 V2=152 CONF=1+F FLEX=51 WX INIT: LOW VISIBILITY OPERATION ACFT INIT LFML 17007KT 0150 OVC001 8/7 Q1002 ZFW: 58T

:


: Nil



00.25



//

if NON STD

Crew : CM1

or CM2 (2)

1.1/1.3/1.4


During climb: ATA 21 CAB PR2.2/3.9.1

3.4.1 SYS 1 FAULT During Climb: ATA 32 LGCIU 1 FAULT 3.4.6 During cruise: TCAS 3.6.9 Radar vectors for ILS CAT II / III approach RWY36L 6.2 Go around 6.3 01.35 Landing CAT II / III RWY 36L 6.4

00.05

01.40



2.5.2


3.4.8/ 3.9.3.4





A320



CHECKING SESSION C

E FC4 04.02 Page 2

Issue 10 SEP 2012

CHECKING-C_EFC4


00.15 02.15 Break

00.15

02.30



-

if NON STD

Crew: CM1

or CM2 (2)


2.3 3.6.5 *

During climb ATA 26 FWD (AFT) CARGO SMOKE 3.6.1 *


3.9.3.1 3.4.8 *


00.05

03.15

INIT T/O - LFLL - RWY 36L Same weather ZFW 58T ZFWCG=29 FUEL = 7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51


2.3 2.5.2


3.4.8 3.9.3.4




00.05

03.55


*

00.05 04.00


(1) (2) See notes on previous page. JAR-FCL references to fill JAR FCL FORM 1.240 1.1/1.3/1.4/1.5/1.6/2.2/2.3/2.5.2/2.6/3.4.1/3.4.6/3.4.8/3.6.1/3.6.5/3.6.9/3.9.1/3.9.3.1/3.9.3.4/3.9.4/4.3/5.3/5.5/6.1/6.2/6.3/6.4. RECURRENT PROGRAM COMPLETED - SEE DETAILS ON BACK PAGE (OR ATTACHMENT) DATE: ●●●●●●●●● SATISFACTORY NOT SATISFACTORY INSTRUCTOR’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●● TRAINEE’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●●

A320



TRAINING SESSION D

E FC4 04.02 Page 1

Issue 10 SEP 2012

TRAINING-D_EFC4

BRIEFING ROOM Review technical: Rejected Landing/Early Go-around Review CRM: Leadership and Team working SIMULATOR SETUP - FLT NBR: AIRBUS 101 POS INIT: LFZZ RWY 33 - Gate C2 V1=132.VR=132.V2=136. CONF=3 FLEX=47 WX INIT: LFZZ 28017G25KT 9999 BKN025 OV040 15/13 Q995 ACFT INIT CB IN VICINITY ZFWCG: 29

: ZFW 58T

BLOCK: 7T

NOTAM: Nil MEL

: Nil


00.20 00.20

Transit cockpit preparation Insert route AIBAIB1 - MOU 1N DEP

if STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.10

00.30

ATA 49: APU fault / Engine start with ground pneumatic power Insert APU fault during preparation. Emphasize the MMEL consultation. Dispatch with APU inoperative.

00.05 00.35 Taxi - before take-off RW 33R

00.50 Take-off: windshear (moderate) on rotation

During climb: ATA 21 CABIN DUCT OVHT

During climb or cruise, ATA 27 flight control ELEV G SERVO JAM LEFT

Radar vectors - non precision approach RW33R. ATA 34 NAV IR1 FAULT - RW Blocked at 2000 FT

Go around - Lower ceiling or runway blocked - if required

Check weather. Visual approach RW33R

01.25 Landing

00.35 Init T/O - LFZZ - RWY 24 - SID ROA 1S to join ROA - Same weather MTOW / ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=163 VR=165.V2=166. CONF=1+F FLEX= 53

If STD Crew: CM1

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)




Go around.


02.00 Landing


A320



TRAINING SESSION D

E FC4 04.02 Page 2

Issue 10 SEP 2012

TRAINING-D_EFC4


00.15 02.15 Break

00.05

02.20

PART 2 - init holding point 33R - APU REPAIRED Insert route AIBAIB1 - MOU 1N DEP Weather: LFZZ 28017G25KT 9999 BKN025 OV040 15/13 Q995 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=132.VR=132.V2=136.CONF=3 FLEX= 47

if STD Crew : CM1

-

if NON STD

Crew : CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.30 Take-off: wind shear (moderate) after rotation

During Climb INIT FL 350. ATA 70: all ENG flame out followed by 1 ENG out app.


02.50 Landing

00.05

02.55

Init T/O RWY 24, SID ROA 1S to join ROA. Same weather MTOW - ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=163.VR=165.V2=166. CONF=1+F.FLEX=53

If STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)







00.20

03.45

Init T/O - LFZZ - RW33R Insert route PAT 33R Weather: Set Wind 280/10, RVR 0125 and ceiling OVC001 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=132.VR=132.V2=136. CONF=3 FLEX= 47 CAT II/III training. 1 take-off / 1 go-around - due Auto Land warning / 1 landing

CM1


A320



CHECKING SESSION D

E FC4 04.02 Page 1

Issue 10 SEP 2012

CHECKING-D_EFC4

BRIEFING ROOM Review technical: RTO/Incapacitation Review CRM: Situation Awareness SIMULATOR SETUP - FLT NBR: AIRBUS 102 POS INIT: LFML RWY 13L - Gate 9A V1=151 VR=151 V2=152 CONF=1+F FLEX= 51 WX INIT: LOW VISIBILITY OPERATION ACFT INIT LFML 17007KT 0150 OVC001 8/7 Q1002 ZFW: 58T

:


: Nil



00.25



//

if NON STD

Crew : CM1

or CM2 (2)

1.1/1.3/1.4


During climb: ATA 21 AUTO FLT2.2/3.9.1 3.4.11 A/THR OFF

During Climb: ATA 36 AIR L 3.4.1 (R) WING or ENG 1(2) BLEED LEAK During cruise: TCAS 3.6.9 Radar vectors for ILS CAT II / III approach RWY36L 6.2 Go around 6.3 01.35 Landing CAT II / III RWY 36L 6.4

00.05

01.40

Init T/O - LFLL - RWY 36L LFLL 28015KT 6000 OVC008 15/8 Q1003 ZFW= 58T ZFWCG= 29 FUEL=7T V1=145 VR=151 V2=155 CONF=1+F FLEX= 51


2.5.2


3.4.8/ 3.9.3.4





A320



CHECKING SESSION D

E FC4 04.02 Page 2

Issue 10 SEP 2012

CHECKING-D_EFC4


00.15 02.15 Break

00.15

02.30



-

if NON STD

Crew: CM1

or CM2 (2)


2.3 3.6.5 *

During climb ATA 26 smoke cargo smoke aft 3.6.2 *


3.9.3.1 3.4.8 *


00.05

03.15


00.35 Engine fire and failure between V1 and V2. Engine out Contingency Procedure: At 2300 turn left to VNE HP

2.3 2.5.2


3.4.8 3.9.3.4




00.05

03.55


*

00.05 04.00



A320



TRAINING SESSION E

E FC4 04.02 Page 1

Issue 10 SEP 2012

TRAINING-E_EFC4

BRIEFING ROOM Review technical: RTO/Emergency descent Review CRM: Situation Awareness SIMULATOR SETUP - FLT NBR: AIRBUS 101 POS INIT: LFZZ RWY 33 - Gate C2 V1=134.VR=136.V2=140. CONF=3. FLEX=47 WX INIT: LFZZ 28009KT 4000 RA FEW008 OVC025 7/5 Q1015 ACFT INIT ZFWCG: 29

: ZFW: 58T

BLOCK: 7T

NOTAM: Nil MEL

: Nil


00.20 00.20

Transit cockpit preparation Insert route AIBAIB1 - MOU 1N DEP

if STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)

00.10 00.30

Engine start ATA 70: ENG START VALVE MANUAL OPERATION Start valve fails to open ENG 1

00.05 00.35 Taxi - before take-off RW 33R

00.50 Take-off: windshear (moderate) on rotation

During climb: ATA 70 ENG 1 THR LEVER FAULT Insert ENG 1 THR LEVER FAULT before flaps retraction. If slats are extended the last valid lever position is selected by the FADEC until slats retraction. At next slats retraction CLB value is automatically selected by the FADEC until slats or landing gear extension. At this time idle is automatically selected and frozen by FADEC.

During climb or cruise, ATA 24 ELEV AC ESS BUS FAULT

Radar vectors - non precision approach RW33R.

Go around - Lower ceiling or runway blocked - if required

Check weather. Visual approach RW33R

01.25 Landing

00.35 Init T/O - LFZZ - RWY 24 - SID ROA 1S to join ROA - Same weather MTOW / ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=153.VR=162.V2=162. CONF=1+F FLEX=54

If STD Crew: CM1

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)




Go around.


02.00 Landing


A320



TRAINING SESSION E

E FC4 04.02 Page 2

Issue 10 SEP 2012

TRAINING-E_EFC4


00.15 02.15 Break

00.05

02.20

PART 2 - init holding point 33R Insert route AIBAIB1 - MOU 1N DEP Weather: LFZZ 28009KT 4000 RA FEW008 OVC025 7/5 Q1015 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=134.VR=136.V2=140.CONF=3 FLEX= 47

if STD Crew : CM1

-

if NON STD

Crew : CM1

or CM2 (1)

-

if RH qual

Crew: CM1 (2)


During Climb INIT FL 350. ATA 21: EMERG DESC - structural damage

Radar vectors for ILS approach RWY 33R During approach: ATA32: L/G NOT LOCKED DOWN LEFT Insert Left BLG not locked down. Keep the failure inserted. The gravity extension requested by ECAM will allow the affected gear to downlock On intercept hdg: Fail AP -if required. Set FD’s OFF. Raw data approach

02.50 Landing

00.05

02.55

Init T/O RWY 24, SID ROA 1S to join ROA. Same weather MTOW - ZFW = 58T ZFWCG = 29 FUEL = 15.5T V1=153.VR=162.V2=162. CONF=1+F.FLEX=54

If STD Crew: CM2

- if NON STD

Crew: CM1

or CM2 (1) -

if RH qual

Crew: CM2 (2)


Overweight landing procedure (or reduce weight on IOS)





00.20

03.45

Init T/O - LFZZ - RW33R Insert route PAT 33R Weather: Set RVR 0125 and ceiling OVC001 ZFW = 58T ZFWCG = 29 FUEL = 7T V1=134.VR=136.V2=140. CONF=3. FLEX= 47 CAT II/III training. 1 take-off / 1 go-around - due Auto Land warning / 1 landing

CM1

00.05 03.50 Rejected take off + Evacuation due to inextinguishable engine fire

(1) (2) See notes on previous page. RECURRENT PROGRAM COMPLETED - SEE DETAILS ON BACK PAGE (OR ATTACHMENT) DATE: ●●●●●●●●● SATISFACTORY NOT SATISFACTORY INSTRUCTOR’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●● TRAINEE’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●●

A320



CHECKING SESSION E

E FC4 04.02 Page 1

Issue 10 SEP 2012

CHECKING-E_EFC4

BRIEFING ROOM Review technical: Rejected Landing/Early Go-around Review CRM: Communication SIMULATOR SETUP - FLT NBR: AIRBUS 102 POS INIT: LFML RWY 13L - Gate 9A V1=151 VR=151 V2=152 CONF=1+F FLEX=51 WX INIT: LOW VISIBILITY OPERATION ACFT INIT LFML 17007KT 0150 OVC001 8/7 Q1002 ZFW: 58T

:


: Nil



00.25



//

if NON STD

Crew : CM1

or CM2 (2)

1.1/1.3/1.4


During climb: ATA 31 EIS2.2/3.9.1 3.4.11 DMC 2 FAULT

During Climb: ATA 24 ELEC AC BUS 1 FAULT 3.4.4 During cruise: TCAS 3.6.9 Radar vectors for ILS CAT II / III approach RWY36L 6.2 Go around 6.3 01.35 Landing CAT II / III RWY 36L 6.4

00.05

01.40



2.5.2


3.4.8/ 3.9.3.4





A320



CHECKING SESSION E

E FC4 04.02 Page 2

Issue 10 SEP 2012

CHECKING-E_EFC4


00.15 02.15 Break

00.15

02.30



-

if NON STD

Crew: CM1

or CM2 (2)


2.3 3.6.5 *

During climb ATA 21 Air pack 1 + 2 fault 3.4.1 *


3.9.3.1 3.4.8 *


00.05

03.15



2.3 2.5.2


3.4.8 3.9.3.4




00.05

03.55

Init T/O - LFLL - RWY 36L LFLL 34007KT 0125 OVC001 8/7 Q1002 ZFW 58T ZFWCG = 29 FUEL + 7T V1=159 VR=159 V2=160 CONF=1+F FLEX = 52

*

00.05 04.00


(1) (2) See notes on previous page. JAR-FCL references to fill JAR FCL FORM 1.240 1.1/1.3/1.4/1.5/1.6/2.2/2.3/2.5.2/2.6/3.4.1/3.4.4/3.4.8/3.4.11/3.6.1/3.6.2/3.6.5/3.6.9/3.9.1/3.9.3.1/3.9.3.4/3.9.4/4.3/5.3/5.5/6.1/6.2/6.3/6.4. RECURRENT PROGRAM COMPLETED - SEE DETAILS ON BACK PAGE (OR ATTACHMENT) DATE: ●●●●●●●●● SATISFACTORY NOT SATISFACTORY INSTRUCTOR’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●● TRAINEE’s NAME: ●●●●●●●●● SIGNATURE: ●●●●●●●●●

E FC4 RECURRENT TRAINING AND CHECKING A320...

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