FCTM M2K 006 FLIGHT CREW TECHNIQUES MANUAL A320 A319 2K

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A318/A319/A320/A321

FLIGHT CREW
TECHNIQUES MANUAL
The content of this document is the property of Airbus. It is supplied in confidence and commercial
security on its contents must be maintained. It must not be used for any purpose other than that for
which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must
not be reproduced in whole or in part without permission in writing from the owners of the copyright.
© AIRBUS 2005. All rights reserved.

REFERENCE: GLG A318/A319/A320/A321 FLEET FCTM

ISSUE DATE: 05 SEP 17

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A318/A319/A320/A321
FLIGHT CREW
TECHNIQUES MANUAL

Issue date: 05 SEP 17
This is the FLIGHT CREW TECHNIQUES MANUAL at issue date 05 SEP 17 for the
A318/A319/A320/A321 and replacing last issue dated 19 JUN 17

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TECHNIQUES MANUAL

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TECHNIQUES MANUAL

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SUMMARY OF HIGHLIGHTS
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Design Principles
AOP-10-20-30
Utilization Principles
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SUMMARY OF HIGHLIGHTS
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Descent Preparation
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Descent
PR-NP-SOP-180
Holding
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Configuration Management
PR-NP-SOP-190-GUI
Guidance Management
PR-NP-SOP-260
Go-Around
PR-NP-SP-10-10-1
Cold Weather Operations and Icing Conditions
PR-NP-SP-10-10-3
Windshear
PR-AEP-BRK
BRAKES
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ELEC
PR-AEP-ENG
ENG
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HYD
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MISC
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TABLE OF CONTENTS
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FLIGHT CREW
TECHNIQUES MANUAL

GI General Information
AOP Airbus Operational Philosophy
AS Aircraft Systems
PR Procedures
PIR Preventing Identified Risks

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Subsection Title

Rev. Date

LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
05 SEP 17
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
22 MAR 17
General Information
22 MAR 17
Introduction
22 MAR 17
Objective
22 MAR 17
Design Principles
05 SEP 17
Utilization Principles
05 SEP 17
Design Principles
22 MAR 17
Utilization Principles
22 MAR 17
Procedures Design
22 MAR 17
Tasksharing Rules and Communication
22 MAR 17
General
22 MAR 17
Handling of Cockpit Controls
22 MAR 17
Handling of ECAM/QRH/OEB
22 MAR 17
Handling of Advisory
22 MAR 17
Spurious Caution
22 MAR 17
Use of Summaries
22 MAR 17
Golden Rules for Pilots
19 JUN 17
Bird
22 MAR 17
Auto Flight
22 MAR 17
Autothrust
05 SEP 17
Use of FMS
05 SEP 17
ROW/ROP
19 JUN 17
Rudder
05 SEP 17
TCAS
22 MAR 17
Weather Radar
05 SEP 17
General
05 SEP 17
Preliminary Cockpit Preparation
22 MAR 17
Exterior Walkaround
22 MAR 17
Cockpit Preparation
05 SEP 17
Before Pushback or Start
22 MAR 17
Taxi
05 SEP 17
Before Takeoff
22 MAR 17
Takeoff
22 MAR 17
Climb
19 JUN 17
Cruise
05 SEP 17
Descent Preparation
05 SEP 17
Descent
05 SEP 17
Holding
05 SEP 17
General
22 MAR 17
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PR-NP-SP-10-10-1
PR-NP-SP-10-10-2
PR-NP-SP-10-10-3
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PR-NP-SP-50
PR-AEP-GEN
PR-AEP-AUTOFLT
PR-AEP-BRK
PR-AEP-ELEC
PR-AEP-ENG
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PR-AEP-FUEL
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PIR

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Configuration Management
Guidance Management
Landing
Go-Around
After Landing
Cold Weather Operations and Icing Conditions
Turbulence
Windshear
Green Operating Procedures
Radius to Fix (RF) Legs
Touch and Go
Stop and Go
General
AUTO FLIGHT
BRAKES
ELEC
ENG
F/CTL
FUEL
HYD
L/G
MISC
NAV
SMOKE
Preventing Identified Risks

Rev. Date
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22 MAR 17
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05 SEP 17
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05 SEP 17
22 MAR 17
19 JUN 17

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AIRCRAFT ALLOCATION TABLE
A318/A319/A320/A321
FLIGHT CREW
TECHNIQUES MANUAL

This table gives, for each delivered aircraft, the cross reference between:
-

The Manufacturing Serial Number (MSN).
The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S.
The registration number of the aircraft as known by AIRBUS S.A.S.
The aircraft model.
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MSN

Registration Number

Model

HC-CKN

319-112

2078

HC-CLF

319-112

3408

HC-CRU

320-214

3467

HC-CSB

319-115

3518

HC-CSA

319-115

4100

HC-CSF

320-214

4379

HC-CJM

320-214

4487

HC-CJW

320-214

4547

HC-CJV

320-214

1882

FSN

(1) Evolution code : N=New, R=Revised

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LIST OF MODIFICATIONS
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J0071

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K3154

Incorp. Date

WING STRUCTURE-INTRODUCTION OF A WING TIP
INCORPORATING A TIP FENCE FOR 72T MTOW A/C

22 MAR 17

FUSELAGE - REAR FUSELAGE - ADAPT STRUCTURE
OF SECTION 17 TO 19 TO A319 DEFINITION

Applicable to: HC-CKN, HC-CLF, HC-CSA, HC-CSB
P10383
31-1334 04
22 MAR 17
31-1414 03
Applicable to: ALL
P10694

22-1296 06

Title

22 MAR 17

22 MAR 17

Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CSB
P11856
22-1315 05
22 MAR 17

INDICATING/RECORDING SYSTEMS FLIGHT
WARNING COMPUTER (FWC) INSTALL FWC
STANDARD H2-F5
AUTO-FLIGHT - FMGC ACTIVATE "MOD NAV IN GO
AROUND" ON FMGC
AUTO - FLIGHT FMGC: ACTIVATE NO AP
DISCONNECTION BELOW MDA/MDH UNTIL MISSED
APPROACH POINT

Applicable to: ALL
P3379

22 MAR 17

Applicable to: ALL
P3560

INDICATING/RECORDING SYSTEMS - GENERAL DEFINE PIN PROGRAMMING FOR STD VERSIONS

22 MAR 17

Applicable to: ALL
P4319

AUTO FLIGHT - FMGC - PROVIDE TIME CONSTRAINT
AND TEN CHARACTERS RTE IDENT FUNCTIONS

22 MAR 17

Applicable to: ALL
P4320

AUTO FLIGHT/FCU DEFINE FD ENGAGEMENT IN
CROSSED BARS AT GO AROUND

22 MAR 17

Applicable to: ALL
P4576

AUTO FLIGHT - ACTIVATE GLOBAL SPEED
PROTECTION AND FD DISENGAGEMENT UPON
SPEED CONDITIONS

22 MAR 17

LANDING GEAR-GENERAL WHEELS AND BRAKES
EQUIPMENT COST REDUCTION ELECTRICAL
ALTERNATE BRAKING
Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CRU, HC-CSA, HC-CSB, HC-CSF
P4808
22 MAR 17 LANDING GEAR - GENERAL - WHEELS AND BRAKES
- EQUIPMENT COST REDUCTION BSCU REDESIGN
Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CRU, HC-CSA, HC-CSB, HC-CSF
P5518
22 MAR 17 LANDING GEAR - GENERAL - NORMAL BRAKING INTRODUCE STD 8 BSCU TWIN VERSION
Applicable to: ALL
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MODIFICATION
P5768

Linked SB

Incorp. Date
22 MAR 17

Title

ELECTRICAL POWER - AC EMERGENCY
GENERATION - ACTIVATE ON A320 SAME
ELECTRICAL EMERG. CONFIGURATION THAN A321
Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CRU, HC-CSF
P6375
22 MAR 17 LANDING GEAR-PARKING/ULTIMATE EMERGENCY
BRAKING -INSTALL A PRESSURE SWITCH (PARKING
BRAKE SYSTEM IMPROVEMENT
Applicable to: ALL
P7218
22 MAR 17 AUTOFLIGHT - FLIGHT MANAGEMENT AND
GUIDANCE COMPUTER (FMGC) DEVELOP FMS 2ND
GENERATION HONEYWELL STEP1
Applicable to: ALL
P7519
22 MAR 17 AUTOFLIGHT - FMGC - INSTALL FMGC CFM
C13042AA01 (EQUIPPED WITH FMS2 HONEYWELL)
Applicable to: ALL
P7721
32-1247 02
22 MAR 17 LANDING GEAR - WHEELS AND BRAKES REMOVE
THE TEMPORARY REVISIONS 5.02.00/23 AND
5.03.00/23 ON FLIGHT MANAL
Applicable to: ALL
P7790
22 MAR 17 AUTO FLIGHT FLIGHT MANAGEMENT AND
GUIDANCE SYSTEM ACTIVATE FMA ENHANCEMENT
FUNCTION
Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CLF, HC-CRU, HC-CSA, HC-CSB, HC-CSF
P8440
32-1291 01
22 MAR 17 LANDING GEAR - WHEELS AND BRAKES
INTRODUCE GOODRICH DURACARB CARBON
BRAKES WITH ANTI - OXYDAN "M1"
Applicable to: ALL
P9171
22 MAR 17 NAVIGATION - ADIRS INTRODUCE AIR DATA
MONITORING FUNCTION
Applicable to: HC-CJV, HC-CJW
22-1359 05
22 MAR 17 AUTO-FLIGHT-FLIGHT MANAGEMENT AND
GUIDANCE COMPUTER (FMGC)-INSTALL FMGC
HONEYWELL H2C13 ON CFM A/C
Applicable to: HC-CJM, HC-CJV, HC-CJW, HC-CKN, HC-CLF, HC-CSB
22-1480 03
12 APR 17 AUTO FLIGHT-FLIGHT AUGMENTATION (FAC)
DEFINE STOP RUDDER INPUT WARNING FUNCTION
ON AIRCRAFT
Applicable to: HC-CLF, HC-CSA, HC-CSB, HC-CSF
22-1559 02
19 JUN 17 AUTO FLIGHT - GENERAL - ACTIVATE ROPS
FUNCTION
Applicable to: HC-CSB

(1) Evolution code : N=New, R=Revised, E=Effectivity

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TABLE OF CONTENTS

FCTM Purpose.........................................................................................................................................................A
FCTM Content......................................................................................................................................................... B
Introduction to the Preventing Identified Risks....................................................................................................... C
Questions and Suggestions.................................................................................................................................... D
Abbreviations............................................................................................................................................................E

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TECHNIQUES MANUAL

TABLE OF CONTENTS

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GENERAL INFORMATION
A318/A319/A320/A321
FLIGHT CREW
TECHNIQUES MANUAL

FCTM PURPOSE
Ident.: GI-00016234.0001001 / 20 MAR 17
Applicable to: ALL

The Flight Crew Techniques Manual (FCTM ) provides complementary information to the Flight Crew
Operating Manual (FCOM).
The FCTM provides the flight crew with:
‐ The general Airbus operational philosophy (e.g. design and utilization principles, golden rules for
pilots)
‐ Additional information to the FCOM procedures (the “why" to do and the “how" to do)
‐ Best practices, operating techniques on maneuvers, and handling
‐ Information on situation awareness.
If the FCTM data differs from the FCOM data, the FCOM remains the reference.
FCTM CONTENT
Ident.: GI-00018007.0001001 / 20 MAR 17
Applicable to: ALL

The FCTM has 5 sections:
GENERAL INFORMATION
This section provides information on:
‐ The FCTM purpose
‐ The FCTM content
‐ The introduction to the Preventing Identified Risks
‐ The abbreviations.
AIRBUS OPERATIONAL PHILOSOPHY
This section is divided into four sub-sections:
1. Design Philosophy:
This sub-section describes the Airbus design and utilization principles of:
‐ The cockpit
‐ The fly-by-wire
‐ The procedures.
2. Tasksharing rules and communication:
This sub-section describes the general tasksharing and communication rules in normal and
abnormal operations.
3. Management of Abnormal Operations:

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GENERAL INFORMATION
A318/A319/A320/A321
FLIGHT CREW
TECHNIQUES MANUAL

This sub-section describes how the flight crew should manage abnormal operations (e.g.
Handling of ECAM alerts, QRH, ADVISORY)
4. Golden Rules for Pilots:
This sub-section describes the Airbus "GOLDEN RULES FOR PILOTS".
AIRCRAFT SYSTEMS
This section provides supplementary information and operating techniques on the use of specific
systems (e.g. BIRD, TCAS)
PROCEDURES
This section provides in normal and abnormal operations:
‐ Best practices (why to, how to, what if not done)
‐ Maneuvers and handling techniques
This section is divided into two sub-sections:
1. Normal Procedures (including Supplementary Procedures)
2. Abnormal and Emergency Procedures.
PREVENTING IDENTIFIED RISKS
This section provides the glossary of the identified risks and potential consequences that the flight
crew may encounter.
INTRODUCTION TO THE PREVENTING IDENTIFIED RISKS
Ident.: GI-00016235.0001001 / 20 MAR 17
Applicable to: ALL

The aim of this chapter is to highlight some of the risks and potential consequences that the flight
crew may encounter, in order to improve:
‐ The awareness of the flight crew with regards to these risks
‐ The risk management.
Refer to PIR Introduction.
QUESTIONS AND SUGGESTIONS
Ident.: GI-00018644.0001001 / 20 MAR 17
Applicable to: ALL

For any questions or comments related to this manual, the Operator’s Flight Operations Management
may contact the Airbus Flight Operations Support & Training Standards department.

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TECHNIQUES MANUAL

ABBREVIATIONS
Ident.: GI-00018009.0001001 / 20 MAR 17
Applicable to: ALL

A
Abbreviation
A>B
A≥B
A
Source Exif Data: 
File Type                       : PDF
File Type Extension             : pdf
MIME Type                       : application/pdf
Linearized                      : No
Page Count                      : 454
Language                        : en
Title                           : FCTM
Creator                         : Airbus (AIB)&AEROGAL (GLG)
Date                            : 2017:10:02 14:30:57-05:00
Create Date                     : 2017:10:02 14:30:57-05:00
Creator Tool                    : OPS Composer (OPSC) 2.14A build 7143
PDF Version                     : 1.4
Producer                        : FO to PDF Converter (FPC) 1.5
Page Layout                     : SinglePage
Page Mode                       : UseOutlines
Author                          : Airbus (AIB)&AEROGAL (GLG)
Keywords                        : Production Identifier 5344, Cockpit delivery No, Exchange version 10.0, Customer logo Yes, Effectivity type ACN, Revision date Tue Sep 05 14:28:43 COT 2017

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