ABD0036_F.pdf

ABD0036

AIRBUS INDUSTRIE Airbus Directives (ABD) and Procedures

Numbering/Naming

The content of this document is the property of Airbus Industrie. 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 Industrie 2000 - All rights reserved

Airbus Industrie Airbus Documentation Office 31707 Blagnac CEDEX France Tel. : 33 (0)5 61 93 49 93 Fax : 33 (0)5 61 93 27 44

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming Table of Contents 0

Foreword

1

Introduction 1-1 1-2 1-3 1-4

2

Numbering/Naming - General 2-1 2-2 2-3 2-4 2-5

3

General Identification of Functions and Techniques Definitions Language and Abbreviations Relationships

Definition and Specification of Aircraft 3-1 3-2 3-3 3-4 3-5 3-6 3-7 3-8 3-9

4

General Reference Documents Applicability Organization of ABD0036

Aircraft Project Identification Aircraft Definition Documentation - Refer to ABD0069 - Aircraft Definition Glide Specification of Systems Specification of Airbus Designed Assemblies/Sub-assemblies/Items Specification of Non Standard Items (Equipment) Specification of Standard Items Specification of Materials Specification of Processes Specification of Tools and Test Equipment

Aircraft Functions 4-1 4-2 4-3 4-4 4-5

4-6

4-7

4-8

4-9

General ATA Specification 100 - Background The ATA Specification 100 and Airbus Airbus ATA Breakdown Establishment Sequence (Refer to Section 6-3) Responsibilities 4-5-1 Allocation of ATA Refs and Titles 4-5-2 Data Centralization Rules for Allocating ATA Refs 4-6-1 XX-00-00 and XX-X0-00 4-6-2 XX-XX-00 Level 4-6-3 XX-XX-XX level Rules for Allocating Titles 4-7-1 Systems/Sub-systems (XX-00-00/XX-X0-00) 4-7-2 Sub-sub-systems (XX-XX-00) 4-7-3 Significant Items (XX-XX-XX) 4-7-5 Use of the Dash (-) Data Storage and Outputs 4-8-1 General 4-8-2 Contents of the DB ATA REF 4-8-3 Outputs Amendment Procedure 4-9-1 General 4-9-2 Request for Amendment 4-9-3 Revision Service

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Date: 3 May 2000

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Numbering/Naming Table of Contents (Continued) 5

Drawn Parts 5-1 5-2 5-3 5-4

6

Non-Standard Items (Equipment/Components/Items) 6-1 6-2

6-3 6-4

6-5

6-6

6-7

7

General Identification 6-2-1 General 6-2-2 FIN and Functional Designation 6-2-3 Equipment/Component/Item Specification Number and Associated Standardized TechnoLogical Description 6-2-4 PN and Supplier's Technological Description (on equipment nameplates, associated documentation such as Component Maintenance Manual (CMM), etc.) 6-2-5 Multicomponent Assemblies Allocation Sequence and Relationships Between Terms Rules for Naming - Functional Designations 6-4-1 General 6-4-2 Responsibility 6-4-3 Form and Content of the Functional Designation Rules for Naming - Standardized Technological Description 6-5-1 General 6-5-2 Responsibility 6-5-3 Form and Content of the Description Naming - Application 6-6-1 Functional Designation Application 6-6-2 Standardized Technological Description 6-6-3 Supplier's Technological Description Messages on Display Units: Applicable Rules 6-7-1 General 6-7-2 Information 6-7-3 Operational Instructions 6-7-4 Status Reports

Standard Items 7-1 7-2 7-3

8

General Identification Rules for Numbering Rules for Naming 5-4-1 General Rules 5-4-2 Sources for Naming 5-4-3 Detail Parts - Content and Form 5-4-4 Sub-assemblies/Assemblies - Content and Form 5-4-5 Installations - Content and Form 5-4-6 Notes on Drawings 5-4-7 Applications

General Terminology Identification of Standard Items 7-3-1 Standard Part Number 7-3-2 Standard Item Description

Materials 8-1 8-2

New materials Existing Materials Page: TOC - 2

Issue: F

Date: 3 May 2000

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Numbering/Naming Table of Contents (Continued) 9

Processes 9-1 9-2 9-3 9-4

General New Processes Existing Processes 9-3-1 Processes Existing in English For Further Details

10 Tools and Test Equipment (T/E) 10-1 10-2 10-3 10-4

General Identification Rules for Numbering Rules for Naming 10-4-1 General Information 10-4-2 As Regards Tools in Particular

11 Engineering Documentation 12 Modification Proposals and Modifications 12-1 General 12-2 Numbering 12-3 Naming 12-3-1 General 12-3-2 Content and Form 12-3-3 Titles of Change Identification Number (CIN) 12-3-4 Recommended Verbs

13 Service Bulletins 13-1 General 13-2 Numbering 13-3 Titles

14 Conversion Instructions 14-1 General 14-2 Numbering 14-3 Titles

15 Service Information Letters 15-1 General 15-2 Numbering 15-3 Titles

16 Requests for Work 16-1 General 16-2 Numbering 16-3 Titles

17 Data Centralization


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Numbering/Naming Table of Contents (Continued) Appendices: Aircraft Constituents - Catalogs of Standard Terms Foreword A - Functions B - Drawn Parts C - Notes for Use on Drawings D - Constituent Assemblies E - Standard Items F - Non Standard Items - Standard Main Words for Functional Designations G - (Intentionally left blank) H - Tools and Test Equipment - Standard Main Words - Signature Sheets, Record Of Revisions (ROR) and List of Effective Pages (LEP)


Date: 3 May 2000

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Numbering/Naming 0

Foreword Aircraft Purchase Agreements stipulate that Technical Publications shall comply with ATA (Air Transport Association of America) Specifications. The standards described in the Airbus Reference Language document set shall be observed. Where appropriate the principles of Simplified English (AECMA) shall be used. The Airbus Reference Language document set comprises the following ABDs: - ABD0036 - Numbering/Naming Covers general numbering and naming rules for aircraft functions and products. Includes a separate appendix of reference catalogs of standard terms. - ABD0037 - Airbus Approved Abbreviations Handbook (AAAH) Lists the abbreviations approved for use within the Airbus environment. - ABD0046 - Units of Measurement Provides guidelines for the selection and use of units, symbols and procedures for conversion and rounding. - ABD0056 - Glossary of Airbus Terms and Expressions (GATE) Lists all the terms which are used in Airbus matters together with their meaning (in the Airbus environment) to ensure a common understanding between AIB disciplines and offer a reference for relations with Airworthiness Authorities, Customers, Members/Associated Partners and Suppliers/Sub-Contractors. Note: ABD0037 and ABD0056 will be superseded by AP2080 during the year 2000

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Date: 3 May 2000

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Numbering/Naming 1

Introduction

1-1

General This ABD provides rules for coherent definition and application of Numbering and Naming requirements for aircraft functions and constituents. The objective is to obtain maximum consistency: - From the Design stage to the Product Support stage. - Between documents and what is actually on the aircraft (labels/placards/markings and messages shown on display units). - Between Aircraft Projects (starting from A340/A330) to facilitate Cross Qualification for Crew and Maintenance Personnel. This consistency is essential not only for our Customers but also for Airbus Industrie and the Members (due to the wide use of Electronic Data Processing - EDP). Where directives already exist to cover the above requirements this ABD simply refers to the relevant directives. Otherwise the rules are laid down in this ABD.

1-2

Reference Documents - ATA 100 Specification. - ARINC Characteristics/Specifications. - ABD0037 - Airbus Approved Abbreviations Handbook (AAAH). - ABD0046 - Units of Measurement. - ABD0056 - Glossary of Airbus Terms and Expressions (GATE).

1-3

Applicability Applicable to all current and future production Airbus aircraft, including development of existing aircraft and aircraft definition evolution, eg: modification.

1-4

Organization of ABD0036 ABD0036 is organized in general accordance with the order of events in which aircraft/aircraft items are numbered and named. The following chart shows this sequence, and refers to the relevant sections of this ABD, or to any other document, for the corresponding rules. Catalogs of Standard Terms are provided in the appendix to this ABD.


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming

Naming Subject

- General • Units of Measurement • Abbreviations • Terms and Expressions - Aircraft

Numbering Rules

ABD0046

Rules

Catalogs

ABD0046

ABD0046

ABD0037 ABD0056

ABD0037 ABD0056

ACMR

ACMR

Glossary Identification Configuration

Aircraft Certification Register Aircraft Configuration Management Rules (ACMR)

- Functions

- Systems - Equipment - Components - Standard Items

ABD0036 ABD0036/ABD0004 ABD0036/ABD0004 ABD0036/ABD0004

ABD0036 ABD0036 ABD0036 ABD0036

ATB Catalog F-G Catalog F-G Catalog E

- Drawings

Titles of: - Assemblies - Sub-assemblies - Parts

ABD0004

ABD0036

Catalog B-C

- Specifications (Technical)

- Aircraft - Systems

ABD0051/ABD0060 ABD0200

ABD0036 ABD0200

BAABI

- Materials - Standard Items - Equipment - Processes

ABD0033 ABD0032 ABD0007, 0010, 0017, 0100, 0200 ABD0034

ABD0036 ABD0036 ABD0036 ABD0036

- Technical Design Directive

ABD0035

ABD0035

- Tools and Test Equipment

ABD0024 ABD0012

ABD0036

- System Description

ABD0020 ABD0050 *

- Airframe

ABD0040

ABD0040

- A/C Certification Documents

ABD0004, ABD0061, ABD0040, ABD0200

ABD0036

- Modification

- Mod Proposals - Modifications

Aircraft Configuration Management Rules (ACMR)

- Service Bulletins - Service Information Letters SB Guide SB Guide - Conversion Instructions ABD0038

ABD0024

ABD0020 ABD0050 *

ABD0036 ABD0036 ABD0036 ABD0036 ABD0036

* From A340.


Date: 3 May 2000

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Numbering/Naming 2

Numbering/Naming - General

2-1

General An aircraft, for the purpose of this ABD, is composed of: - data and documentation for definition, description and justification, - the aircraft itself which comprises functions and the techniques, (i.e.: the aircraft constituent items), used to fulfil these functions.

2-2

Identification of Functions and Techniques Functions are identified by a title and a reference number in accordance with ATA Specification 100 (refer to Section 4). Techniques have basically two types of identification: - a Functional Designation together with a Functional Identification Number (FIN). These are used when an item is considered only from a functional aspect. They usually relate to items of equipment or to Standard Items with a significant function, - a Technological Description together with a Part Number. These are used when an item is considered from a technological aspect. They are used for all types of items. Note: Technological Descriptions and Part Numbers can be allocated by Airbus Members and Associated Partners. In this case the descriptions are referred to as Standardized Technological Descriptions. They can also be allocated by suppliers, in which case they are referred to as Suppliers' Technological Descriptions.

2-3

Definitions Functional Designation (refer to Chapter 6) Title describing the function of equipment/components or significant items of an aircraft system/circuit/installation. Standardized Technological Description (refer to Chapter 6) The Standardized Technological Description is a term used to describe the basic technical function of an item. It must be consistent with the basic part of the Functional Designation. Specification Reference and Title For items defined by means of a Technical Specification (refer to ABD0010/0200), the title of the Technical Specification shall be the Standardized Technological Description, written in the normal order of words in English, eg: Retractable Landing Light, not Light-Retractable, Landing. Suppliers' Technological Description If, in response to a specification, a supplier can offer an item which is in his current range and can be supplied as an "off the shelf" item it may retain its identification. In such cases the following descriptions can apply: - a Functional Designation, - a Standardized Technological Description, - a Supplier's Technological Description.


Date: 3 May 2000

AIRBUS INDUSTRIE

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Numbering/Naming 2-4

Language and Abbreviations All text shall be in the English language using aeronautical terminology in common use e.g. as used by the ATA The reference documents to be used are Webster's Third New international Dictionary of the English Language or Webster's Collegiate Dictionary and the Catalogs of Standard Terms to be found in the appendix to this ABD. The use of abbreviations is permitted. The rules governing their use and catalogs of abbreviations approved for use are included in ABD0037 - Airbus Approved Abbreviations Handbook.

2-5

Relationships The relationships between terms is shown in chart form in paragraph 6-3.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 3

Definition and Specification of Aircraft

3-1

Aircraft Project Identification At the beginning of a new Aircraft Project, Airbus Industrie identifies the new aircraft by means of a reference, comprising the Type, Series, Model, Variant and Configuration: - Refer to Aircraft Configuration Management Rules (ACMR) and ABD0056 Chapter 4. The allocated reference is recorded in the Aircraft Certification Register for Aircraft Types and Models.

3-2

Aircraft Definition Documentation - Refer to ABD0069 - Aircraft Definition Glide

3-3

Specification of Systems - Refer to: * ABD0100 and ABD0200 - System Definition and Specifications

3-4

Specification of Airbus Designed Assemblies/Sub-assemblies/Items - Refer to: * ABD0004 - Definition Dossier

3-5

Specification of Non Standard Items (Equipment) - Refer to: * ABD0100 and 0200 - Equipment - General Technical Requirements (Supersedes ABD0010 Equipment - Specifications) * ABD0017 - Equipment - Off-the-Shelf * ABD0007 - Equipment - General Technical Requirements

3-6

Specification of Standard Items - Refer to: * ABD0032 - Standard Items * ABD0055 - European Standards

3-7

Specification of Materials - Refer to: * ABD0033 - Materials * ABD0043 - Materials Consumable

3-8

Specification of Processes - Refer to: * ABD0034 - Processes

3-9

Specification of Tools and Test Equipment - Refer to: * ABD0024 - Aircraft – Tool Mfr and Test Equipment * ABD0012 -Equipment - Tool and Test Equipment


Date: 3 May 2000

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ABD0036

Numbering/Naming 4

Aircraft Functions

4-1

General An aircraft consists of: - functions which are necessary for the aircraft to meet its specification, - techniques by which the functions are achieved. Functions are numbered and named in general accordance with ATA Spec. No. 100 - SPECIFICATION FOR MANUFACTURERS TECHNICAL DATA, generally known as "ATA 100".

4-2

ATA Specification 100 - Background First issued in 1956, the objective of ATA Specification 100 is to standardize the presentation of data provided by manufacturers to airlines, so that the same information can be found in generally the same place and form whatever the aircraft and/or the manufacturer. As regards functions, the objective is achieved by a standard system of breaking the aircraft down into its functions, and of numbering and naming them. This system is known as the ATA breakdown system. The numbers are known as ATA References, and provide a unique addressing system. ATA Specification 100 breaks an aircraft down into its functions as follows: - Systems (known as Chapters in related publications). - Sub-Systems (or Sections). - Sub-Sub-Systems (or Sub-Sections). - Units (or Subjects). Each function group has a standard 6-digit number (the ATA Ref.) and a name (known as a title). These are specified in ATA Specification 100 as far as the sub-system level, common to any aircraft. From the sub-sub-system level, each individual manufacturer continues the allocation to suit the aircraft involved. The breakdown system is based on an alphabetical sequence using titles allocated to Systems, eg: Air Conditioning Chapter 21-00-00 Auto Flight Chapter 22-00-00 Communications Chapter 23-00-00 Within each System are Sub-Systems. For example, ATA Chapter 21 deals with the Air Conditioning System and provides for a range of sub-systems, eg: Compression ATA Ref. 21-10-00 Distribution ATA Ref. 21-20-00 Each Sub-System (eg: Distribution ATA Ref. 21-20-00) is further divided into Sub-Sub-Systems. "Distribution" (21-20-00) provides a number of Sub-Sub-Systems including: Cabin Air Distribution ATA Ref. 21-21-00 and Recirculation Cockpit Air Ventilation ATA Ref. 21-22-00 Each Sub-Sub-System (referred to as circuits or installations), comprises Units (components). "Cabin Air Distribution and Recirculation" (21-21-00) includes for example: Filter-Recirculation ATA Ref. 21-21-41 Check Valve-Recirculation ATA Ref. 21-21-42


Date: 3 May 2000

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ABD0036


The ATA Specification 100 and Airbus The ATA Specification 100 itself states that the standards it establishes are "recommendatory in nature" but that they "become mandatory to the extent they may be incorporated into the purchase agreements executed between the individual suppliers and the individual operators". Airbus General Purchase Agreements stipulate general compliance with ATA Specification 100 for contractual Technical Publications, therefore Airbus is committed to following ATA Specification 100. For this reason and in order to achieve maximum consistency between Airbus data, (both that supplied to customers and that used as a basis for the data supplied to customers), and between this data and the aircraft itself, a specific Airbus ATA Breakdown is established at XX-XX-00 level at the outset of each new Program/Project, and is later completed at XX-XX-XX level. Each Sub-Sub-System is allocated: - A circuit identification consisting of two letters. - Its own ATA Ref. (XX-XX-00). - A title (Refer to section 4-7). Each unit within a Sub-Sub-System is allocated: - A Functional Item Number (FIN) - Ref. ABD0004. - An associated ATA Ref. (XX-XX-XX). - A title (Refer to Section 4-7). The resulting Breakdown is used as a basis for the numbering of drawings and documents. Examples include: - Aircraft Standard Specification. - Detail Specifications. - Technical Design Directives (TDD). - Mechanical drawings. - Electrical drawings. - Electrical wires. - Equipment specifications. - System Description Notes (SDN). - Airframe Certification Documentation (ACD). - Certification documentation. - Documents/data for relations with customers (eg: Technical Publications). The remainder of this chapter gives the details of when, how and by whom ATA numbers and names are to be allocated.

4-4

Airbus ATA Breakdown Establishment Sequence (Refer to Section 6-3) The sequence of activities leading to the establishment of the ATA Breakdown is as follows: A - Identification of all functions at XX-X0-00 and XX-XX-00 level, at the outset of each Airbus project, or as and when new functions are introduced. B - Identification of all items required to fulfill the functions. Allocation of FINs and associated Functional Designations (Refer to ABD0004 - Definition Dossier, for numbering rules, and ABD0036 for functional designations). C - Allocation of functional ATA References (XX-XX-11 to XX-XX-99) and related titles for those detail functions (items) considered to be significant for maintenance.

Example: For A330/A340 Page: 4 - 2 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming ATA REF.

CIRCUIT LETTER

21-12-00

HG

FIN

TITLE Cabin Air Distr & Recirculation

21-21-42

5214HG Check Valve-Recirculation

21-21-48

212HG 213HG

Valve-Recirculation Valve-Recirculation

4-5

Responsibilities

4-5-1

Allocation of ATA Refs and Titles

4-5-1-1

General The responsibility for ATA Specification 100 Breakdown establishment is split into two major levels. - XX-X0-00 and XX-XX-00 (Sub-System and Sub-Sub-System: Circuit/Installation). - XX-XX-XX (Significant Item). The Design Offices have overall technical responsibility. Maximum agreement shall be reached between the Members involved. Outstanding decisions shall be taken during the System Interface activities.

4-5-1-2

XX-X0-00 and XX-XX-00 - Overall control: For mechanical items - Non-Specific Design Work (NSDW) level 1. For electrical/electromechanical items - NSDW level 2. - Allocation: NSDW Airbus Member Design Office (see worksharing document, Report 6, applicable to the relevant aircraft project). - General coordination for harmonization: Aerospatiale Matra. In case of problems, the final decision lies with AIB and will be taken by TF7-WG1.

4-5-1-3

XX-XX-01 to XX-XX-99 - Overall control: Member responsible for specific manual or responsible for specific ATA Chapter as defined in Report 6. - Allocation: Technical Publications with the agreement of NSDW Design Office. - General coordination for harmonization: Aerospatiale Matra. In case of problems, the final decision lies with AIB (Customer Services Directorate).

4-5-1-4

Coordinators Each Airbus Member has one coordinator, with assistant coordinators if required, to handle proposals and decisions. - Refer to AM2002 StB, QDB and ACmAB Directory for further details

4-5-2

Data Centralization As decisions are taken they are entered in a dedicated central data base, known as the DB ATA REF (Refer to Paragraph 4-8). General responsibility for the data base, and for inputs, follow-up and archives lies with Aerospatiale Matra.


Date: 3 May 2000

ABD0036


4-6

Rules for Allocating ATA Refs

4-6-1

XX-00-00 and XX-X0-00 At the beginning of an Aircraft Project, numbering at 3-digit level shall be in conformity with the ATA Specification 100 at the revision status defined by the relevant project management. If the aircraft technology is not catered for by this Revision of the ATA Specification 100 a request for amendment to the specification shall be submitted to the ATA/AIA Committee as follows: 1. At the earliest stage possible (i.e. when the general design concepts have been established with reasonable certainty), the Design Organization must submit requests for additions or modifications, with justification, to the AIB Customer Services - Technical Publications Organization Breakdown Coordinator, with a copy to the other coordinators. The request should preferably include a proposal of the text to be included in the Specification 100. 2 . AIB then submit the proposal to the AIA/ATA committee at the earliest opportunity. 3 . The proposal can be considered to be usable after acceptance by AIB. EMBED ATB Coordinator

ATA 100 Representative

See applicable BAABI

MAAP Proposal Design Office or Tech Pubs

In ATA 100?

No

No Feed back

Yes

AIB ATA 100 Group (TPMM) Yes

Proposal presented to TF7WG1 and discussed with relevant member.

AIB ATA 100 Representative

No

TF7-WG1 Yes

Yes No

DB ATA Ref

AIA/ATA Committee (TICC)

ATA Working Group

ATA Working Group

ATA Working Group

ATA Working Group


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming 4-6-2

XX-XX-00 Level To ensure consistency the ATA Breakdown of the preceding Program/Project shall be taken as reference. Changes may be made only if required by the aircraft technology.

4-6-3

XX-XX-XX level

4-6-3-1

A 6 digit ATA Ref. is allocated to those items which require specific airframe documentation i.e. A - Those governed by the Maintenance Review Board (MRB) for scheduled actions. B - Those governed by the Maintenance Planning Document (MPD) which is an implementation of the MRB. C - Those subject to GO/NO-GO/GO-IF classification in the Master Minimum Equipment List (MMEL) and the Configuration Deviation List (CDL). D - Those governed by the various onboard monitoring systems. In this case, any change to the ATA Reference or Functional Designation of the Line Replaceable Unit (LRU) may only be made after Design Office agreement to modify the software of the corresponding computers (involves raising an aircraft Modification). All LRUs monitored by the central warning and maintenance systems shall be identified by the code letter "M" (monitored) in the DB ATA REF. E - Additional Line Replaceable Units/Items (LRU/LRI). F - Those requiring a special/specific maintenance action. Note: The Breakdown does not allocate ATA References to Component Maintenance Manuals th th (Vendor, Manufacturer). These ATA References, from 4 to 6 digit, are the responsibility of the Supplier.

4-6-3-2

Reference Documents - Electric/electronic systems/circuits: Use the Principle Diagram (PD). - Mechanical sub-systems: Use the relevant Functional Diagram (FD).

4-6-3-3

Rules for Numbering th th These rules explain how to number 5 and 6 digit ATA References. - Gaps shall be provided between the allocated ATA References (-11/-99) in order to allow for incorporation of: • additional significant items, • aircraft modifications. - Existing ATA References shall never be renumbered to insert new FINs. - Several FINs may be covered by the same 6 digit ATA Reference if they do not require a specific reference for the purposes of onboard monitoring systems, or if typical maintenance procedures are applicable. - Because of onboard monitoring systems, ATA References at XX-XX-XX level shall not be changed unless required by an aircraft Modification.

A - ATA chapters Chap 05

Chap 06

th

th

- For 05-10 to 05-19: no 5 and 6 digits. th th - For 05-21 to 05-29: Following A320 rules the 4 and 5 digits include the th major zone, and the 6 digit is always 0. eg: Inspection in zone 121 = ATA ref. 05-21-20. th th - For 05-51 to 05-59: 5 and 6 digits allocated sequentially. th th - The 5 and 6 digits consist of the relevant ATA chapter. eg: Fuselage stations = ATA ref. 06-31-53. Page: 4 - 5

Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming st

nd

rd

th

Chaps 07 to 10

- Follow ATA Specification 100 rules for the 1 , 2 and 3 digits. The 4 digit th th is a sequential number and the 5 and 6 digits are always 0.

Chaps 11 and 12

- The 5 and 6 digits consist of the relevant ATA chapter and the title is that of the ATA chapter. eg: exterior placards and markings for the Fuel System = ATA ref. 11-21-28 Fuel.

Chaps 20 to 45

- The 5 and 6 digits are allocated in accordance with the general rules contained in paragraph B.

Chap 49

- The 5 and 6 digits are allocated in accordance with the APU manufacturer's breakdown, except for items which are under the aircraft manufacturer's responsibility and are therefore numbered in accordance with the general rules contained in paragraph B. Note: in the event that the APU manufacturer's breakdown numbering does not conform to the AIB system, renumbering to obtain conformance is permissible.

Chap 51

- The 5 and 6 digits are numbered sequentially, so giving the compiler freedom to allocate numbers in an unbroken sequence or to leave some numbers free for allocation at a later date.

Chap 52

- The 5 and 6 digits are allocated in accordance with the general rules contained in paragraph B.

Chaps 53 to 57

- The 5 digit is allocated in accordance with the general rules contained in th paragraph B. As far as possible the 6 digit should be allocated so that the same item appearing in adjacent sections throughout the aircraft has the th th same 5 and 6 digits in the different sub-chapters. Agreement between the members during ATA ref allocation is required to achieve this consistency.

Chaps 71 to 80

- The 5 and 6 digits are allocated in accordance with the engine manufacturer's breakdown, except for items which are under the aircraft manufacturer's responsibility which are numbered in accordance with the general rules contained in paragraph B.

th

th

th

th

th

th

th

th

th

th

th

th

th

Note: Special allocation Rules for chapters 91 to 99. Chap 91

- (Main Wire Routing, Panels, and Wiring List - WDM only). - 91-01-00 thru 91-09-00 (main wire routing by zone): the last three digits reflect, in general, the major zone. - 91-10-00 thru 91-19-00: the last three digits correspond in general to the VU panel identification allocated by the Design Office. - 91-20-00 thru 91-99-00: reserved for Aircraft Wiring List (AWL). Split by the AWL computer program according to the circuits.

Chap 92

- Engine data Same breakdown system as for Chap 91.

Chap 93 - 99

- Reserved for military versions of aircraft.


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming th

th

B - General rules for the allocation of 5 and 6 digits th a) First stage - establishment of 5 digit by reference to following table. th

th

5 /6 DIGIT 1x 2x 3x 4x 5x 6x 7x 8x 9x

ELECTRICAL/MECHANICAL Electrical (inputs) Electrical (indicators) Electrical (Computers) Mechanical (Mechanical items in electrical systems) Electrical (Electromechanical) Mechanical Mechanical Mechanical Reserved for airline requests

Note 1: Where 1x, 2x, 3x or 5x is full, then further 5-digit electrical items should be included in 4x or 6x. Similarly, where 4x, 6x, 7x or 8x is full, then further mechanical items should be included in 3x or 5x. th

th

Note 2: In exceptional cases, where, for example, the 5 /6 digits 4x and 6x thru 8x and 3x and th th 5x have been used up in a purely mechanical chapter, and further 5 and 6 digits are required, then extension into 1x and 2x is allowed. th Similarly, in purely (or mainly) electrical chapters, extension is allowed into 5 digits 7 and 8. th

b) Second stage - Establishment of 6 Digit (XX-XX-XX) th th The 6 digit is numbered sequentially within the 5 digit range selected in the first stage. The compiler has the freedom to allocate the numbers in an unbroken sequence or to leave some numbers free for use at a later date. (eg: - 11, - 13, - 15…).

4-7

Rules for Allocating Titles

4-7-1

Systems/Sub-systems (XX-00-00/XX-X0-00) Titles shall be in general conformity with ATA Specification 100 at the applicable Revision status. Minor deviations are however, acceptable, if justified. eg: 27-10-00 is AILERON AND TAB in ATA Specification 100. In the Airbus ATA 100 Breakdown, it is simply AILERON, as there are no tabs on the ailerons. Titles for additions or modifications to the ATA Specification 100 shall be included in the proposals to the AIA/ATA Committee (Refer to Paragraph 4-6). They shall be precise, concise and fit in with the ATA style.

4-7-2

4-7-3

Sub-sub-systems (XX-XX-00) Correspond to the installations and circuits of a specific Aircraft Project. To be based on the Breakdown of the previous Airbus Program/Project in so far as the technical definition of the new project is identical. Titles shall be concise but sufficiently general to satisfy further end usage and shall not be influenced by different sub-sub-system configuration or sources of major equipment supply. Significant Items (XX-XX-XX)


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming 4-7-3-1

General For items which have a significant function (such as Equipment/Component/Item, Standard Items, Assy/Sub Assy) within a system, sub-system/sub-sub-system, a title is allocated as specified below.

4-7-3-2

Items Identified by a FIN The title of the ATA Reference shall be consistent with the functional designation given to the item involved (refer to chapter 6 for the rules governing functional designations). This means that: - The main word shall be indicated first, followed by a dash and then the function on the aircraft, plus the complementary modifier where really necessary. But - Abbreviations shall not be used unless the item is commonly referred to by its abbreviation (see rules for abbreviations in paragraph 4-7-4) or unless they are extremely common, eg: MLG (Main Landing Gear). - A given ATA Reference may cover more than one FIN, in which case the title shall be limited to the parts of the functional designation which are common to all the FINs. Example: Functional Designation

ATA Ref. Title

1206 GM ACTG CYL-MLG DOOR, L 1207 GM ACTG CYL-MLG DOOR, R

32-33-11 ACTUATING CYLINDER - MLG DOOR 1206 GM 1207 GM

1CE1 ELAC-1 1CE2 ELAC-2 1CE3 ELAC-3

27-91-13 ELAC (Elevator Aileron Computer) 1CE1 1CE2 1CE3

4-7-3-3

Items Not Identified by a FIN For maintenance significant assemblies/subassemblies the titles shall be of a form similar to Functional Designations, and the same rules shall be followed.

4-7-4

Use of Abbreviations - Refer to ABD0037 - Airbus Approved Abbreviations Handbook (AAAH) for approved abbreviations. Abbreviations shall be used under the following conditions: XX-X0-00 and XX-XX-00 Designation in full of the function, in each ATA Reference where it is quoted, followed by: - The abbreviations of the function if one exists, in single parentheses ( ), eg: 31-60-00 Electronic Instrument System (EIS) 31-61-00 Electronic Instrument System (EIS) Control However, in the case of internationally known abbreviations for common functions eg: ILS, ATC. It is not necessary to complete with the full name. - Complementary information, including abbreviations other than that of the function, in double parentheses eg: 24-23-00 AC Auxiliary Generation ((APU Generator, GCU))


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming Abbreviations between (( )) are not indicated in full at XX-X0-00, XX-XX-00 level since they are generally related to equipment (XX-XX-XX).

XX-XX-XX For items commonly known by an abbreviation the main word shall consist of the abbreviation (as in the functional designation for the item), and shall be followed by the name in full between parentheses eg: XX-XX-XX FQIC (Fuel Quantity Indication Computer).

4-7-5

Use of the Dash (-) The dash is used at XX-00-00 and XX-XX-XX level only. At XX-00-00 level, it separates the indication "GENERAL" from the system title eg: XX-00-00 Air Conditioning - General. At XX-XX-XX level, it separates the main word of the functional designation of a significant item from the principal modifier (function). eg: XX-XX-XX Check Valve - Green Reservoir Return - Refer to Chapter 6-4 for rules concerning functional designations.

4-8

Data Storage and Outputs

4-8-1

General All ATA Ref. data, when approved, is entered and stored in a central data base, the DB ATA REF. This data base is accessible on line through the Airbus network.

4-8-2

Contents of the DB ATA REF The Data Base contains at least the following parameters: - Aircraft Project Identity. - ATA references XX-00-00 to XX-XX-00 allocated to Systems/Sub-systems. • Their associated circuit letters (where applicable). • The corresponding Title. • NSDW Level 1 and/or Level 2 Airbus Member responsible. - Functional Item Number (FIN) allocated to Significant Items. * • Its associated Functional Designation. • Corresponding XX-XX-XX ATA Reference. • Indication of whether the FIN is related to a significant item monitored by an onboard monitoring system. * A significant Item is any item which requires specific airframe documentation. - ATA Reference history status. • Applicable for. • Provision for. • Deactivated by an aircraft modification. Note 1: As soon as an ATA Reference has been allocated and used for identification it cannot be deleted but only deactivated for new design. Note 2: Never reuse a deactivated ATA Reference where Design Office drawings data/ documents could be in circulation under this reference. Page: 4 - 9

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming - Aircraft Modification Proposal Number with its status indication: • Before. • After. - Aircraft Series for which it is valid (A340-200, A340-300, A330-200…). - Date of data input or amendment. Refer to each individual Breakdown document for further details.

4-8-3

Outputs The following documents are extracted from, or repeat at least some of the contents of the DB ATA REF.: The Basic Approved ATA 100 Breakdown Index (BAABI) is an index limited to 4-digit ATA Refs. It is agreed to and signed by all the Breakdown coordinators, and thus represents the official reference for the development and updating of drawings 00X007 10000. The BAABI is under the general responsibility of Aerospatiale Matra Design Office. It contains: - ATA refs, limited to XX-00-00 XX-X0-00 XX-XX-00 - The title in English and French. - The FIN, limited to the circuit identification (two letters or four figures and two letters). eg: HH - 5000 HH - For each ATA REF fields are provided for movement codes, remarks, provisional code, standard, effectivity and levels of responsibility. The BAABI is a computer output, extracted from the DB ATA REF. Drawing 00X007 10000 "Drawing/Data Numbering is the official drawing form of the BAABI allowing its use for Design data. Envelope ATA 100 Breakdown (The envelope ATA 100 Breakdown (6 digit) is extracted per Aircraft Project or Family). - Is a computer listing which contains all the same information contained in the DB ATA REF down to th th 5 and 6 digit level. Note: For TECHNICAL PUBLICATIONS responsibility refer to the TPWD (Technical Publications Worksharing Document), also extracted from the DB ATA REF. The ATA 100 Index is extracted per aircraft Type or Series (A300, A300-600, A310-200, A310-300, A320 etc.). - It is limited to: • ATA Reference, limited to XX-00-00 XX-X0-00 XX-XX-00 • Functional Designation. • Circuit letters. It is issued as a pocket booklet which is distributed to AIB Field Service Representatives and to some Airlines for use as an addressing system providing easy access to contractual Technical Publications.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


Amendment Procedure

4-9-1

General Once an ATA Reference/title has been introduced a revision/amendment is allowed only if justified by an aircraft modification (cost repercussions very high).

4-9-2

Request for Amendment

4-9-2-1

Amendment of FIRST FOUR Digits (XX-XX-00) Any amendment or new issue has to be first approved by the relevant coordinator of the Member and will be considered only as official if accepted by all relevant Member's Design Office coordinators. Note: Amendments to 3 digit ATA References are only official after acceptance by AIB.

4-9-2-2

Amendment of 5 /6 Digit (XX-XX-XX) Any amendment has to be first approved by the relevant coordinator of the Members.

th

th

It will be considered as officially approved only when accepted by all Member Coordinators.

4-9-2-3

Procedure After internal approval the request shall be sent to the coordinators by FAX or electronic mail. The message shall contain (at least): - Aircraft Project. - Nature of the request. • We intend to create the following ATA Ref.: • We intend to amend the following: • We intend to deactivate the following ATA Ref. REMINDER: an existing ATA reference cannot be deleted (historical follow-up). - Title. - Circuit (if any) - FIN involved (if any). - A/C Modification - Proposal Number. - Level 1 and Level 2 Members. - Reason for deviation. - An indication of whether the ATA Ref. is new with respect to ATA Specification 100. Note: Where a new ATA Reference is not in accordance with the ATA Specification 100, the message shall mention it. Due to the importance of the consequences, a reply shall be given as follows: - within 20 working days for 4 digit ATA References. - within 10 working days for 5/6 digit ATA References, (attention should be paid to holidays/ vacation periods). The originator may consider the request for amendment as accepted only when acknowledged by the Aerospatiale Matra organization responsible for the DB ATA REF. Each coordinator has to arrange internal coordination and to record by using the pre-printed Request for Amendment form.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 4-9-3

Revision Service The DB ATA REF is updated on a daily basis.

Consequently, the availability of the data is as follows: - On line: continuous. - BAABI and drawing 00X007 10000 • No regular revision service is scheduled. • The distribution list is handled by AM-B Design Office. - Envelope ATBX: Quarterly basis. • On magnetic tape (where no on line capability, or on special request). • On paper (limited distribution). - ATA 100 Index (Booklet) • No regular revision service is scheduled. The distribution list of the above two outputs is handled by AIB, Customer Services - Technical Publications Organization.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 5

Drawn Parts

5-1

General These are items designed by AIB Members/Associated Partners or Subcontractors, and are consequently defined by means of the drawing set.

5-2

Identification These items are identified by a Part Number (PN) and by a Name selected from the "Standard Terms for Drawn Parts" listed in catalog B in the Appendix to this ABD.

5-3

Rules for Numbering Refer to ABD0004 - Definition Dossier.

5-4

Rules for Naming

5-4-1

General Rules The golden rule is CONSISTENCY. This applies at two levels: (1) The same name shall be allocated to the same type of part, and this: - whatever the aircraft project, - whatever the aircraft section, - whatever the AIB Member/Associated Partner/Subcontractor. (2) The same name shall be used for the same PN in all applications: - drawings and/or associated documents (whatever the type: detail, assembly, and whatever the sheets: picture, schedule), - technical publications (CMMM, IPC, SRM, etc.).

5-4-2

Sources for Naming To achieve the required level of consistency, a catalog of standard names is provided in the separate Appendix to this ABD: - Appendix B - Drawn Parts. If it is necessary to quote names of systems/sub-systems/sub-sub-systems, refer to drawing 00X00710000 (X representing the letter specific to the aircraft involved) or to the equivalent Basic Approved ATA 100 Breakdown Index (BAABI). Names of Non Standard Items in schedules of installation drawings shall be coherent with the ECDB Functional Designation field, (Ref. 6-4-3). The titles of the Installation Drawings of a Non Standard Item shall reflect at least the main word of the Functional Designation allocated to this item.

5-4-3

Detail Parts - Content and Form Detail parts shall be identified in accordance with paragraph 5-2. The description for a given part shall always be the same whatever the sub-assembly or assembly on which the item is installed. Page: 5 - 1

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming In the case of castings and forgings, it is the name describing the part which shall be used, (not the word "CASTING", "FORGING", (eg: STRUT - MLG DRAG)). Part names are limited to 21 characters. They must therefore: - be brief, - be sufficiently general to allow further end usage without needing to be changed but contain sufficient information to categorize the part. The main identifying noun or noun phrase shall be placed first, to facilitate the automated selection of parts. eg: SUPPORT It shall be followed, if required, by a dash and then the most significant modifier or modifying phrase, which will further describe the part so as to distinguish it from other parts of a similar name. eg: SUPPORT - TUBULAR Articles, prepositions and conjunctions such as "AN", "THE", "OF", "FOR" shall not appear in the part name. For drawings representing single detail parts, the name of the part and the title of the drawing shall be identical. eg: Dwg No XX F535 X0001 SUPPORT-TUBULAR PN F535 X0001 SUPPORT-TUBULAR

5-4-4

Sub-assemblies/Assemblies - Content and Form The rules are basically the same as for detail parts with the following difference: - Titles for Sub-assembly/Assembly drawings shall contain the word ASSY with the main identifying noun or noun phrase. eg: SUPPORT ASSY

5-4-5

Installations - Content and Form The rules are basically the same as for detail parts with the following difference: - Title of installation drawings shall contain the word INSTL with the main identifying noun or noun phrase. eg: SUPPORT INSTL

5-4-6

Notes on Drawings - Refer to Appendix C - Notes for Use on Drawings.

5-4-7

Applications The names are allocated by means of Design Office drawings. These are then used as a source for various other documents. eg: - System Description Notes. - Airframe Certification Document. - Certification documents. - Contractual technical publications. • Drawing Aperture Cards (DAC). • Structural Repair Manual (SRM). • Component Maintenance Manual Manufacturer (CMMM). • Illustrated Parts Catalog (IPC). • Service Bulletins (SB).


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 6

Non-Standard Items (Equipment/Components/Items)

6-1

General These are items made by outside Suppliers. For the technical definition of the terms, Ref.: * ABD0000: Aircraft Constituents. Non-Standard Items can be categorized in two ways: - Off the Shelf selected: already existing for other Aircraft Programs/Projects. Ref.: * ABD0017/ABD0200 - Equipment - Off the Shelf. - Newly designed: subject to an individual specification. Ref.: * ABD0010/ABD0200 - Equipment - Specification.

6-2

Identification

6-2-1

General Non Standard Items are identified by: - A Functional Item Number (FIN) and its associated Functional Designation. - An Equipment/Component/Item Specification Number and the associated Standardized Technological Description (refer to 6-5). - A Part Number (PN) and its associated Supplier's Technological Description as allocated by the supplier (Refer to paragraph 6-6).

6-2-2

FIN and Functional Designation These are both allocated by the Airbus Industrie Members and are specific within a given project. Ref.: * ABD0004 - Definition Dossier

6-2-3

Equipment/Component/Item Specification Number and Associated Standardized TechnoLogical Description These are also both allocated by the Airbus Industrie Members. The Standardized Technological Description shall be independent of the source of supply, and the aircraft project and system/circuit/installation in which the item will be integrated.

6-2-4

PN and Supplier's Technological Description (on equipment nameplates, associated documentation such as Component Maintenance Manual (CMM), etc.) - Newly designed items shall be allocated the Standardized Technological Description as defined by the corresponding Equipment/Component/Item specification. - Off the shelf selected equipment which is modified to suit a specific Airbus definition shall be allocated the Standardized Technological Description as defined by the corresponding Equipment/ Component/Item specification. If the equipment is used without modification: • Airbus Industrie Members shall use the Standardized Technological Description as defined in the corresponding Equipment/Component/Item validation Specification.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


Multicomponent Assemblies Equipment can consist of various modules. In such cases, the above identification methods are valid for items, including the bare equipment, combined to form an assembly and for the assembly itself.

6-3

Allocation Sequence and Relationships Between Terms The chart on page 6-3 illustrates the sequence of events involved in the numbering and naming of Equipment, Components and Items for a new aircraft project or a new installation/circuit definition. The following chart indicates the relationship between the various terms and emphasizes the need for consistency. AIRCRAFT FUNCTION (LIGHTING)

FUNCTIONAL DESIGNATION

FUNCTIONAL DESIGNATION (LIGHT-NAVIGATION, LEFT WING)

FUNCTIONAL DESIGNATION

STANDARDIZED TECHNOLOGICAL DESCRIPTION (LIGHT-NAVIGATION)

FIN & FUNCTIONAL DESIGNATION (7LA LIGHT-NAVIGATION, LEFT WING)

TITLE OF TECHNICAL SPECIFICATION (NAVIGATION LIGTHS-WING)

DRAWINGS (PRINCIPLE AND FUNCTIONAL DIAGRAMS)

DATA BANKS DOCUMENTATION

ECDB

SUPPLIER'S TECHNOLOGICAL DESCRIPTION (LIGHT UNIT)


Date: 3 May 2000

ABD0036


Functional Analysis Allocation of: - 4 digit ATA Reference + - Title - Circuit letters (where required) - Record of Responsibilities

- Identification of all aircraft functions - Segregation in elementary Circuit/Installation

System Definition and Interfacing Specification

Allocation of: - FIN - Functional Designation

Identification of all items (eg: Equipment for each function/system)

Establishment of preliminary Equipment/Component/Item Technical Specifications

Allocation of: - Specification Reference - Standardized Technological Description

Identification of Maintenance Significant Items (MSI)

Allocation of: - 6 digit ATA Reference

Confirmation or correction of: - Specification Reference - Standardized Technological Description (Note:may also have repercussions on Functional Designation)

Establishment of final, contractual Technical Specifications

- Selection of Supplier - Establishment of customized specification(s) ALLOCATION SEQUENCE

Allocation of: - PN - Part Number - Supplier's Technological Description


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


Rules for Naming - Functional Designations

6-4-1

General The following rules apply to all items with a FIN, eg: - Equipment (whether Off-the-Shelf or new Airbus specific). - Components or Sub-components of equipment considered as being themselves Line Replaceable Units (LRU). - Functionally Significant Standard Items. A Functional Designation shall indicate what the item involved is, and what it does on the aircraft and in the system/circuit involved. It shall also include, where relevant, any related system, unit or location data. As a general rule, each FIN has a single Functional Designation which does not change, whatever the source of supply (PN) of the item involved. In general, Functional Designations are allocated at the same time as the FINs, on the Functional Diagrams (FD) and Principle Diagrams (PD) and are then loaded in the Equipment Central Data Bank (ECDB). They are structured in agreement with the basic rules set out in paragraph 6-4-3. Later, they are used in other applications such as: - labels, - markings, - display unit messages, - ATA 100 Breakdown (Refer to Chap. 4), - Contractual Technical Publications. Depending on the application, they can be used: - as defined in paragraph 6-4-3, - in whole or in part (eg: labels), - with or without abbreviations, - with or without the Main Word first (eg: Display Unit Messages). eg: The ATA 100 Breakdown uses Functional Designations at 6 digit level: - with the Main Word first, - but often in part only (several FINs for one ATA Reference), - and very limited abbreviations. Display Unit Messages also use Functional Designations: - with abbreviations, - but often only the Main Word, - and always in the normal order of words (not "Main Word first" layout). (Ref. paragraph 6-6). But, whatever the form used in the above applications: - the basic Functional Designations allocated on Functional Diagrams and Principle Diagrams and loaded in ECDB shall always follow ABD0004 and ABD0036 (Paragraph 6-4-3) (i.e. Main Word first, etc.), - the wording shall be identical.


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming Directives for Item category

ABD0004/0005/0036 DWG/ECDB…

Not monitored

Main Word First

Monitored (Screen messages)

Main Word First

ABD0018/0048/0100/ 0200 SCREEN

Normal Word Order

This means that the fact that some information on a drawing may result in a screen message does not change the need for the drawing to follow ABD0004 and ABD0036.

6-4-2

Responsibility - Ref. Applicable Worksharing Document (known as Report 6) • For pure Mechanical Items, the NSDW Level 1 Member shall allocate the FINs and associated Functional Designation on the relevant Mechanical Functional Diagram. • For Electrical and Electromechanical Items (items which have at least one electrical connection), the NSDW/SDW Level 2 Member shall allocate the FINs and associated Functional Designations on the relevant Electrical Principle Diagram. • Where an equipment is classified "Electromechanical" it can appear simultaneously on the Mechanical Functional and Electrical Principle Diagrams. In this case the electrical FIN shall prevail in any common Data Base, and harmonization shall be cleared in the framework of the system Interface activities for any other documents.

6-4-3

Form and Content of the Functional Designation Functional Designations consist of: - a Main Word or Words (20 characters max.), - a Principal Modifier, - a Complementary Modifier, where applicable, the total not to exceed 54 characters. st

The Main Word shall be separated from any Modifier by a dash (21 digit max, no spaces either side of the dash). Modifiers shall be separated from each other by a comma. eg: RELAY-LOW LEVEL DET, Y HYD RSVR - The Main Word(s) shall be a basic description of the item (ie: the minimum information needed to categorize the item, eg: Relay, Pump…). Ideally, the Standardized Technological Description (Refer to 6-7-1) should be used. It shall form at least part of the Standardized Technological Description (indicated on the Equipment/Component Specification) which is stored in a specific field in the ECDB, (Refer to 6-5). eg: Standardized Technological Main word of Functional Description Designation • RELAY • RELAY • PUMP-HYDRAULIC • PUMP • ACTUATOR-LINEAR • ACTUATOR • VALVE-CHECK, 1/2 IN • CHECK VALVE • TRANSDUCER-PRESSURE • PRESS XDCR In the case of equipment commonly referred to by their abbreviation the whole abbreviation shall be considered as the Main Word. Page: 6 - 5 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming eg: Standardized Technological Description FQIC ECB IDG

Main word of Functional Designation FQIC ECB IDG

If a suffix is required it shall be considered as a complementary modifier. Correct use of the Main Word(s) ensures consistency between eg: Functional/Principle Diagrams, Messages on Display Units, Placards, Labels, Markings and Technical Publications. For this reason, it is essential that the form and content shall remain constant in all applications. In addition, the Main Words of Functional Designations for items common to more than one Airbus Program/Project shall not change from one Program/Project to another, because of the repercussions on the Standardized Technological Descriptions and therefore on the documents that use them. To facilitate selection of Main Words, and to ensure consistency of content and form throughout all applications where Main Words are used, a catalog of the Standard Main Words to be used is included in the separate Appendix to this ABD: - Refer to Appendix F - Non Standard Items - Standard Main Words for Functional Designations. If any additions/amendments to the catalog should prove necessary, the catalog shall be completed using the procedure indicated in the Foreword to the Appendix on page FW-1.

- The Principal Modifier shall reflect the function carried out by the item of equipment, in the particular aircraft, and System/Circuit involved. In some instances, it may include identifying information. eg: RELAY-LOW LEVEL IND, Y HYD RSVR PRESS SW-FUEL PUMP 1, L WING TANK Numerical suffixes must, if space permits, be separated from the term by a space. In the case of Panel-mounted items, eg: Pushbutton Switches, Annunciators, Circuit Breakers etc., there shall be consistency both as regards content and form between the Principal Modifier and the Labels on the Panels. These shall be presented in a cascade form, starting with the title of the Panel, each level being separated by a slash (/). eg: P/BSW - FLT CTL/FAC 1 P/BSW - FUEL/L TK PUMPS/1

- The Complementary Modifier shall give any related system, unit or location data. eg: RELAY - LOW LEVEL IND, Y HYD RSVR Abbreviations may be used in Principal and Complementary Modifiers. They shall be taken from ABD0037 - Airbus Approved Abbreviations Handbook (AAAH). However, the following abbreviations shall be used systematically: L for Left R Right ENG 1 Engine 1 ENG 2 Engine 2 CAPT Captain F/O First Officer Page: 6 - 6 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming G B Y SYS

Green (Hydraulic System) Blue (Hydraulic System) Yellow (Hydraulic system) System

Numerical suffixes must, if space permits, be separated from the term by a space. Further examples of Functional Designations: FIN 30GA 31GA 10LA

MAIN WORD PROX SENSOR PROX SENSOR LT

PRINCIPAL MODIFIER - NLG DOORS CLOSED - NLG DOORS CLOSED - NAVIGATION

COMPLEMENTARY MODIFIER SYS 1 SYS 2 R WING TIP

6-5

Rules for Naming - Standardized Technological Description

6-5-1

General The Standardized Technological Description identifies the nature and category of an item in general terms, eg: Proximity Sensor. Being independent of a specific function it allows the item to be used in several applications across several projects or programs. It shall be consistent with the title of the Technical Specification for the item and with the basic part of the Functional Designation.

6-5-2

Responsibility The reference document for Technical Specification title definition is the Functional Diagram/Principle Diagram. The responsibility for detail functional design is allocated to the NSDW Level 2. Any conflicts shall be settled with the Level 1 organization. The necessary coordination shall be ensured via the System Interface activities.

6-5-3

Form and Content of the Description - General The Standardized Technological Description shall reflect, as regards content but not necessarily form (the order of words may be different), the Main Word of the Functional Designation. This may be completed with any other technological information considered absolutely essential. However, the name shall be sufficiently general to allow for any future use in applications not originally envisaged. This means that in general, Standardized Technological Descriptions shall not be related to any specific type of aircraft or system. eg: Filter-Air Filter-Fuel Pump-Fuel Pump-Hydraulic Pump-Water


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming However, in some cases (eg: for computers), where the design of the equipment is so specific to a given function as to preclude any possibility of it being used for another function, mention of the system/function is accepted eg: • Fuel Quantity Indication Computer (FQIC). • Air Data Inertial Reference Unit (ADIRU).

- Form of the Description The Standardized Technological Description consists of: • a main identifying noun, • complementary information relative to the operating mode/application of the item, • if necessary, application information. The total not to exceed 21 characters including spaces and/or special characters such as dash/ comma. The main identifying noun shall be separated from the complementary information by a dash (-). Any additional information shall be separated from the rest by a comma (,). eg: • Pump • Pump-Hydraulic • Valve-Fuel • Valve-Fuel, Remote Ctl • Valve-Pressure Holding In some instances some common items may be adopted for specific functions. In such a case this specific functional aspect may be included in the description. eg: • Valve-Air, Skin • Bearing-Steady, Kink As in the case of Functional Designations for Non Standard Items (eg: computers) usually identified by their abbreviations, the abbreviation shall be considered as the full description (i.e.: identifying noun plus complementary information). eg: • Fuel Quantity Indication Computer (FQIC) Note: Every effort shall be made by systems specialists to restrict use of this type of abbreviation to major/complex equipment. Use of too many abbreviations of this kind does not enhance comprehension by airline mechanics and CMM users.

- Description Consistency Every effort must be made to ensure consistency in the Standardized Technological Descriptions use in Airbus documents: • both within the same project, whatever the supplier and whoever the Member, • and from one Airbus project to another.

6-6

Naming - Application

6-6-1

Functional Designation Application The Functional Designation shall be used in all applications (Data Banks/Documents) where the FIN is the major means of identification. eg: - Functional Diagram * - Principle Diagram * - Related theoretical equipment definition list * - ATB ATA 100 Breakdown at 6 digit level (of the Aircraft Project concerned) - ECDB: Functional Designation field - Labels in cockpit Page: 6 - 8

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming - Labels on structure near equipment/components - Installation drawings - Exterior markings - Messages on display units - Contractual Technical Publications * Note: At this stage of the Design phase, only the function to be fulfilled by an equipment is identified (not the selected technique: Supplier, Part Number and installation requirements).

6-6-2

Standardized Technological Description - The Standardized Technological Description shall be used in all applications (data banks/ documents) where the Item Technical Specification reference is the major means of identification in relation to a FIN(s): • Non-Standard Item (Technical) Specification Title * ABD0007 - Equipment - General Technical Requirements * ABD0010 - Equipment - Specification * ABD0017/0100/0200 - Equipment - Off the shelf • ECDB Equipment Central Data Bank • Purchase activities at call for tender stage

6-6-3

Supplier's Technological Description - The Supplier's Technological Description shall be used in all applications (data banks/ documents) where the Item Part Number (PN) is the major means of identification in relation to a FIN(s): • Non-Standard Item identification plate • Bar codes • ECDB: Supplier's description (in English) field • Non-Standard Item supply related data/documents • Aircraft Inspection Report (AIR) • Purchase activities at contract signature stage.

6-7

Messages on Display Units: Applicable Rules From A340/A330, AIB is committed, by the Airlines to ensure a Cross Qualification of Air Crew and Maintenance Personnel (with reference to A320).

6-7-1

General Since the messages on Display Units are of prime importance for Aircraft Operation and Safety, special attention shall be paid to their establishment. Flight Test and Training organizations shall be involved.

6-7-2

6-7-3

Messages on Display Units may be classified according to the following: - Information - Operational instructions - Status reports Information This category covers two kinds of displays: - symbols related to instrumentation, - texts which generally use Functional Designations. Operational Instructions The applicable rules are those related to Check List (on board the aircraft).


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


Status Reports The messages which are shown on display units are split into three blocks. - ATA Reference or: • function concerned (Circuit/Installation), • or the item involved. - FIN of the item(s) involved. - TEXT: • either the Functional Designation of the function concerned, • or a statement in the normal order of words incorporating the Main Word(s) of the Functional Designation of the equipment involved. This does not affect the rules for compiling Functional Designations.

If the statement in the normal order of words is used, it shall be compiled by the NSDW Level 2 for the display unit software in conjunction with the System Specialist concerned. The statement shall be so written that the Flight Crews will be able to easily understand the message. This is of obvious importance in cases of emergency.

Refer to ABD0048 and ABD0018 - Equipment - Electronics Maintainability and ABD0100/ABD0200 for new projects.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 7

Standard Items

7-1

General The term "Standard Item" relates generally to items that are widely used throughout an aircraft or across Aircraft Projects with no specific function allocation (eg: fasteners, electrical connectors).

7-2

Terminology Due to the complexity of the work organization/splitting, reference shall be made to ABD0032 for definition of Standardization Terminology and detailed information on procedures and practices related to standards activities within Airbus Industrie.

7-3

Identification of Standard Items Standard Part Numbers and associated Technological Descriptions are used.

7-3-1

Standard Part Number Ref: * ABD0032 - Standard Items Where Standard Items are used to ensure a specific function they are identified additionally in the engineering documents by means of Functional Item Numbers (FIN) and the associated Functional Designations in accordance with ABD0004 - Drawing System and ABD0036 - chapter 6-4. Note: Suppliers identify Standard Items either by the official Standard Part Numbers or by internally defined additional Part Numbers (proprietary PNs).

7-3-2

Standard Item Description The description consists of an introductory part (Main Word) identifying the general subject and of additional technological Information, where applicable. Ref: * ABD0032 - Standard Items - The complete description is used as a title on the Standard itself (reproduced in the Airbus Standards Manual). - Parts of the description are used, for example, in Design Office lists/handbooks/files/drawing schedules. In this case the name used shall: • reflect that indicated on the relevant standard, • be limited to the minimum amount of information required to categorize the item (the "Main Word" plus other information considered necessary). "Main Words" are to be selected from the "Catalog of Standard Names", Catalog E of the Appendix to this ABD. If a "Main Word" not yet listed in Appendix E is needed, the update procedure indicated on page FWD-01 shall be followed. Note that the Technical Publications IPC shall use the same Technological Description as that laid down by the Standardization Specialists/Design Office.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 8

Materials

8-1

New Materials Apply AECMA CN/DIR 1 directives for the preparation of standards, and associated ENs (European Standards) which may be specific to each category of product (EN 2500). eg: Plate - Al Alloy

8-2

Existing Materials Use the existing name.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 9

Processes

9-1

General Some manufacturing processes are: - Surface treatment/protection. - Finishing, coating, sealing. - Heat treatment, machining, forming. - Bonding, welding, riveting. - Assembly and installation. - Marking.

9-2

New Processes In the case of newly defined processes, existing specifications may be taken as reference, provided that the title is self-explanatory (to ensure coherence between old and new documents).

9-3

Existing Processes

9-3-1

Processes Existing in English Title to be retained.

9-3-2

Processes to be translated into English: apply the same rules as for a new process. Where the title in the national language does not reflect the intended purpose of the process, it is acceptable that the title in English does not reflect exactly the original title.

9-4

For Further Details Ref: * ABD0034 - Processes - Policy and Management


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 10

Tools and Test Equipment (T/E)

10-1

General Tools and Test Equipment are items designed either by AIB Members/Associated Partners or Subcontractors, or by equipment manufacturers acting as Suppliers. The following rules apply in all cases.

10-2

Identification These items are identified by a Part Number (PN) and by a name (functional designation).

10-3

Rules for Numbering Ref: * ABD0012 - Suppliers - Tools and Test Equipment * ABD0024 - Aircraft MFR – Tool and Test Equipment

10-4

Rules for Naming Names shall be of a form similar to Functional Designations.

10-4-1

General Information Functional Designations consist of: - a main word or words, - a principal modifier, - a complementary modifier, if necessary. The main word shall be separated from the principal modifiers by a dash (-). Modifiers shall be separated from each other by a comma (,).

10-4-2

As Regards Tools in Particular

10-4-2-1

The number of characters permitted is: - 21: For the drawing title (Tool and Test Equipment (T/E) Data Base (TEDB) field DRAWING DESCRIPTION, T/E drawing titles, T/E Index (TEI)) which may include abbreviations if necessary. - 54: For the title in full (TEDB field "EDESC", Illustrated Tool Equipment (TEM), Aircraft Maintenance Manual…). IMPORTANT: The title in full and the abbreviated title shall be identical as regards content. Only the form of the words used may be different. This means that titles shall be concise.

10-4-2-2

The main word(s) shall consist of the basic technological description of the item (i.e. the minimum information needed to categorize the item). eg: MOORING KIT - NLG ACCESS STEPS - CABIN CHOCKS - RUN UP, MLG Words such as SET, TOOL, EQUIPMENT shall not be used alone wherever possible.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 10-4-2-3

The principal modifier shall reflect the function carried out by the tool (i.e. what the tool is used for). eg: MOORING KIT - NLG ACCESS STEPS - CABIN CHOCKS - RUN UP, MLG

10-4-2-4

The complementary modifier, if applicable, shall give any related systems, unit or location data, etc. eg: CHOCKS - RUN UP, MLG

10-4-2-5

Names of any aircraft systems or equipment quoted in the tool title must be consistent with at least the basic part of the Functional Designation. Refer to the applicable Airbus ATA 100 Breakdown and to the applicable list of Functional Designations. Item Tool eg: FINXXXX PROBE-ICE DET PNXX…COVER-ICE DETECTOR PROBE FINYYXX IDG PNYY…HOLDING FIXTURE-IDG, CFM ATA REF 25XXXX COCKPIT CARPET-COCKPIT PROTECTION ATA REF 25XXXX FMS LOADER-FMS…

10-4-2-6

Abbreviations shall be taken from ABD0037 - Airbus Approved Abbreviations Handbook (AAAH). If further abbreviation is needed for drawing titles due to limitation of space, proceed by deleting vowels, starting from the right.

10-4-2-7

Tools common to two or more Airbus projects (same PN) shall keep the same name for all projects.

10-4-2-8

Supplier-furnished tools shall keep the name given to them by the supplier.

10-4-2-9

For further details, ref: * ABD0012 - Suppliers - Tools and Test Equipment * ABD0024 - Aircraft Manufacture - Tools and Test Equipment


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 11

Engineering Documentation Specifications of Documentation produced for Airbus and used for Design Engineering are contained in AM2000 (Procedural Documentation, Means & Methods Mapping). The specifications also indicate the associated reference directives.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 12

Modification Proposals and Modifications

12-1

General The definition of the design of an aircraft and any changes to the design are managed by a system of Modification Proposals (MP) which, when accepted for implementation, become Modifications (MOD). An MP is associated with a MOD by a Change Identification Number (CIN). To ensure that modification data can be stored in EDP systems, so facilitating its easy retrieval in order to define an aircraft configuration, it is essential that MPs and MODs shall be correctly numbered and titled.

12-2

Numbering The method of numbering of MPs and MODs is defined at the start of an Aircraft Project/Program by the appropriate General Modification Committee (GMC). Refer to Aircraft Configuration Management Rules (ACMR) which is an updated version of the earlier Airbus Industrie Modifications Handbook (AIMH).

12-3

Naming

12-3-1

General In naming, the term "Subject" applies only to MPs. The term "Title" is applied only to MODs/CINs/ Service Bulletins. It is important that names are correct and consistent as they are used for data extraction and enquiry purposes. Both MPs and MOD's require names and the rules for establishing names are common to both. As soon as a modification is certificated its title and the subjects of the associated MPs names should not be revised/amended. Consequently, they have to be correctly formulated at an early stage of definition. Titles for CINs depend on application (see 12-3-3-2) but generally follow the subject of the MP. The length of titles shall not exceed 3 lines of 39 characters (117 characters including spaces). Abbreviations shall be kept to a minimum and without exception shall comply with ABD0037 - Airbus Approved Abbreviations Handbook.

12-3-2

Content and Form

12-3-2-1

General MP subjects and MOD titles shall be written in accordance with the ATA Specification 100 rules for Service Bulletin titles. This avoids having to change subjects/titles for Service Bulletins. According to ATA Specification 100, the MP title shall generally consist of three categories of information: - Designation of the major affected ATA Specification 100 Chapter. - Designation of the major item affected. - Description of the modification objective. Detail considerations are explained in the following text.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 12-3-2-2

Major ATA Specification 100 Chapter Affected Great care shall be taken to select the correct ATA Specification 100 Chapter (2 digit level) as it determines the numbering of the affected Service Bulletins. The designation of the affected ATA Specifiication 100 Chapter shall be taken from the ATA 100 Breakdown applicable to the Aircraft Project/Program involved, eg: - Fuselage - Communications - Flight Controls Exceptionally, and only if necessary for comprehension, the ATA section or Sub-section designation, taken from the applicable ATA 100 Breakdown, may be added. eg: Water/Waste - Water Storage

12-3-2-3

Major Items Affected Generally it is necessary to state, after the ATA Specification 100 chapter: - the Designation of the Major Item involved eg: Flight Controls - Flap Actuators - or the location of the area affected, eg: Fuselage - Aft Intermediate Section Note: A/C Sections shall be identified by their name but never by their number (only known by Design and Production but never by customers).

12-3-2-4

Modification Objective Shall be a brief description of the objective to be attained on the aircraft. This shall be expressed in the imperative form. eg: Communications - Install Boomset Flight Controls - Flap Actuators - Modify Hub Flange This description shall not describe the reason for the MOD/MP, i.e. the origin of the problem or the work content (this is covered by the Technical Repercussion Sheet - TRS).

12-3-3

Titles of Change Identification Number (CIN)

12-3-3-1

General A CIN comprises a Modification Number and the associated MP number and these are inseparable. The Modification Number may precede the MP number or vice versa. Each CIN shall be allocated a significant title which reflects the purpose of the MP(s)/MOD(s). CIN titles are used in Technical Publications (for highlights in Manuals, Service Bulletin titles, etc.), so it is extremely important that both MP and MOD titles are significant and correct. Several cases of association between MP and MOD may occur.

12-3-3-2

One MP = One MOD The title of the MOD and the Subject of the MP shall be identical.

12-3-3-3

Two or More MP's = One MOD The modification itself may carry a general title allocated by the General Modification Committee (GMC) and each MP may have a different Subject. Page: 12 - 2

Issue: F

Date: 3 May 2000

ABD0036


The Title allocated to each CIN shall be the same as the MP Subject (if accurate and acceptable). Examples: - 40YYYY/SYYYY1 - 40YYYY/DYYYY2 - 40YYYY/DYYYY3

Equipment/Furnishings Lights - Lighted Signs Equipment/Furnishings

- Define Cabin Layout for AFR - Install Bilingual Lighted Signs - Cabin - Install Textile covered DADO Panels

12-3-3-4

Collective MODS Two or more MP's = one MOD. Identical rules as 12-3-3-3.

12-3-3-5

One MP Included In More Than One MOD Identical rules as 12-3-3-3.

12-3-4

Recommended Verbs

12-3-4-1

The following verbs are recommended for use in subjects and titles: - Definition : - define ............. to provide ............. to introduce ............. - Installation : - install ............. for provision of ............. - Validation: - validate ............. for ............. Customer/Standard - Definition Evolution: - modify ............. to adapt to improve to increase/decrease to re-design to replace to delete


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 13

Service Bulletins

13-1

General Service Bulletins (SB) are technical instruction documents issued to customers. There are several types of AIB Service Bulletins: eg: - Alert SBs. - SBs raised to cover modifications to be retrofitted by customers. - Inspection Service Bulletins (not further to a Mod). - Evaluation Service Bulletins (nor further to a Mod). - Service Bulletins raised by AIB to cover Vendor Service Bulletins. - Simplified Service Bulletins. - Advance Service Bulletins.

13-2

Numbering Refer to Airbus Industrie Service Bulletin Guide.

13-3

Titles All Service Bulletins raised to cover a single Mod/MP (CIN) shall be given the same title as the CIN involved. eg: Flight Controls - Flap actuactor Modify hub flange Where a Service Bulletin covers more than one CIN, or only part of a CIN, the SB title must be adapted from the CIN title but shall still follow the basic principles set out in Chapter 12 of this ABD. Titles of Inspection and Evaluation Service Bulletins for which there is no CIN number shall also follow the basic rules set out in Chapter 12 of this ABD.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 14

Conversion Instructions

14-1

General The purpose of Conversion Instructions is, in general, to cover retrofit of modifications at Airbus Industrie facilities under Airbus Industrie responsibility. Ref: * ABD0038 - Aircraft - Conversion Instruction (CI).

14-2

Numbering Refer to Airbus Industrie Service Bulletin Guide.

14-3

Titles For titles, the rules stipulated in chapter 13 of this ABD are applicable.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 15

Technical Instructions This chapter is no longer applicable and has been deleted

16

Service Information Letters

16-1

General Service Information Letters (SIL) are issued to give general information to operators.

16-2

Numbering SILs shall be numbered in a sequence defined by the Airbus Industrie Customer Services Directorate.

16-3

Titles Titles of SILs follow the same rules as Service Bulletins (refer to Chapter 13 of the ABD). For further information, refer to Airbus Industrie Service Bulletin Guide.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 17

Requests for Work

17-1

General The Request For Work (RFW) is a document of a general nature used to request a study or work to be accomplished.

17-2

Numbering RFWs shall be numbered in a sequence defined by Airbus Industrie.

17-3

Titles The title shall reflect the technical nature of the work requested, and shall be in conformity with Chapter 12 of this ABD.


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming 18

Data Centralization Numbering and Naming Data are progressively centralized to be accessible (consultation and input where mutually agreed) by the Airbus Industrie Members and Associated Partners, via the Airbus Network. - Ref: * ABD0008 - EDP - Data Computerization * ABD0057 - EDP - Applications Interfaces * ABD0058 - EDP - Applications Descriptions


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Airbus Directives (ABD) and Procedures

Numbering/Naming Appendices

Aircraft Constituents Catalog of Standard Terms The content of this document is the property of Airbus Industrie. 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 Industrie 2000 - All rights reserved

Airbus Industrie Programmes and Processes Directorate

31707 Blagnac CEDEX France Tel. : 33 (0)5 61 93 49 93 Fax : 33 (0)5 61 93 27 44

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming Aircraft Constituents - Catalog of Standard Terms FOREWORD

In order to ensure full coherence between Members and in application of ABD0036, Standard Terms are presented in catalog form according to the following classification: A - FUNCTIONS B - DRAWN PARTS C - NOTES FOR USE ON DRAWINGS D - CONSTITUENT ASSEMBLIES E - STANDARD ITEMS F - NON STANDARD ITEMS - STANDARD MAIN WORDS FOR FUNCTIONAL DESIGNATIONS G - (INTENTIONALLY LEFT BLANK) H - TOOL AND TEST EQUIPMENT STANDARD MAIN WORDS The above Catalogs are under the responsibility of TF7, Airbus Reference Language Working Group, acting on behalf of the Standardisation Board (StB). Note: Coherence of Messages displayed on screens (across Aircraft Projects/Between Members) is ensured by Aerospatiale Matra Airbus Design Office as Level 1 - Overall responsibility. Some typical usages are indicated in each Catalog.

Updating Procedure Requests for introduction of new terms shall be sent to your local TF1M-WG1 - representative (Reference AM 2002 – StB, QDB and ACmAB Directory).

Page: FW - 1 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming Aircraft Constituents - Catalog of Standard Terms

Aircraft

Functions - Rules: Chapter 4 - Catalog: A

Structure - Rules: Chapter 4 - Catalog: D

Systems - Rules: Chapter 4 - Catalog: A

Techniques

Drawn Parts - Rules: Chapter 5 - Catalog: B

Suppliers originated - Rules: Chapters 6-7 - Catalog: E-F-G - Materials • Metallic • Non metallic • Composites • Consumable - Standard Items (eg: Bolts, Connectors, etc.) - Non Standard Items (eg: Equipment)

- Detail Parts - Sub-Assembly - Assembly

Processes - Rules: Chapter 9 - Catalog: None

Tool and Test Equipment - Rules: Chapter 10 - Catalog: H

General Interrelation Flow Chart

Page: FW - 2 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036

Numbering/Naming Aircraft Constituents - Catalog of Standard Terms

A - FUNCTIONS

1 . Aircraft Functions Aircraft Functions are identified by ATA 100 References: - Ref: * ABD0036, Chapter 4, for Numbering and Naming rules. ATA 100 References. are given at these levels: XX-00-00 (System) XX-X0-00 (Sub-system) XX-XX-00 (Sub-sub-system: Installation/Circuit) These levels are recorded for each Aircraft/Program/Project in the applicable Basic Approved ATA Breakdown Index (BAABI) and can be consulted on line on the Airbus network, in the DB ATA REF (entry by ATA Ref.). Contact for further information: Aerospatiale Matra Airbus (Reference AM 2002, TF7, for names of contacts).

2 . Units Units are allocated a 6 digit Reference: XX-XX-11 and (Units) XX-XX-99 This Reference corresponds to Maintenance Significant Items, (MSI). Their titles for ATA Reference purposes can be consulted on line in the DB ATA REF, or on hard copy in the applicable Envelope ATA 100 Breakdown. The Functional Designations can be consulted on line by FIN in: - ECDB - Equipment Central Data Bank - BDME - Banque de Désignations Multilangues Eléments (Data bank of aircraft component terms)

3 . New Aircraft Program/Project As functions are specific to each Aircraft Program/Project, there is no catalog of standard Titles/ Functional Designations. To achieve consistency, for a new Aircraft Program/Project, consult the BAABI and/or Functional Designations of the preceding Aircraft Program/Project.

4 . Usage eg: - Functional Diagrams (FD). - Principle Diagrams (PD). - Wiring Diagrams (WD). - Instrument Panels. - Labels/Placards. - Messages on Screens. - Contractual Technical Publications.

Page: A - 1 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


B - DRAWN PARTS This catalog provides standard terms for drawn parts listed in their Schedules (application of ABD0004Drawing System): • Ref: * ABD0036, Chapter 5, for Numbering and Naming rules. They can also be consulted on line on the Airbus network in: - BDME (Banque de Désignation Multilangues Eléments). (Data bank of aircraft component terms) - MMDB (Mechanical Main Data Bank). Consultation by Part Number (PN).

Usage - Component Maintenance Manual Manufacturer (CMMM). - Aircraft Illustrated Parts Catalog (IPC). - Structure Repair Manual (SRM). - Service Bulletins (SB).

Page: B - 1 Issue: F

Date: 3 May 2000

ABD0036


B - DRAWN PARTS AILERON ANGLE ANGLE - FORMED ANGLE - JOGGLED ANGLE - JOINT ANGLE - PICKUP ANGLE - REINFORCING ANGLE - SEALING ANGLE FITTING - LOWER ANGLE FLOOR ARM ARM - SUPPORT ARMREST ATTACHMENT - PYLON AXLE

BAFFLE BALL BEARING BALL JOINT BAR BAR - TORSION BASEPLATE BEAM BEAM - CROSS BEAM - DOOR BEAM - KEEL BEAM - LONGITUDINAL BEAM - SUPPORT BEARING BELLCRANK BELLCRANK ASSY BELLOWS BELT BELT - SEAT BEVEL GEAR BIN - WASTE BLANK BLANKET - INSULATION BLANKET - OVERFRAME BLIND - ROLLER BLOCK TERMINAL BOBBIN BODY - ROD BOGIE BOLT BOX BOX - CENTER WING BOX - JUNCTION BRACKET BRAKE

BRUSH BUFFER BULKHEAD BULKHEAD - PRESSURE BUMPER - TAIL BUNDLE BUSBAR BUSHING BUSHING - ECCENTRIC BUSHING - KNURLED BUSHING - PLAIN BUSHING - SHOULDERED BUSHING - SPLIT BUSHING - THREADED

CABLE CABLE - CONTROL CABLE END CAM CAN CAP CARPET CASE CASING CASTING CHAIN CHANNEL CHASSIS - FLIGHT CONTROLS CLAMP CLAMP BLOCK CLEAT CLIP COCKPIT COLLAR COLUMN - CONTROL CONDUIT CONNECTION CONNECTION - BULKHEAD CONNECTION - GROUND CONNECTOR CONNECTOR - DUMMY CONSOLE CONTROL - AILERON CONTROL - ELEVATOR CONTROL - RUDDER CONTROL UNIT COUPLING COUPLING - STRAIGHT COUPLING - WELDED COVER Page: B - 2

Issue: F

Date: 3 May 2000

ABD0036


B - DRAWN PARTS COWL CRADLE CRANK CRUCIFORM CUP CYLINDER - OXYGEN

DADO PANEL DAMPER DEFLECTOR DIFFUSER DISC D-NOSE DOOR DOOR - ACCESS DOOR - LANDING GEAR DOUBLER DRAIN DUCT DUCT - EXHAUST

ECCENTRIC ELBOW ELBOW - WELDED ELECTRICAL BOX EXTRUSION EYE END

FACE - FRONT FAIRING FAIRING - BELLY FAIRLEAD FASTENER FEEDTHROUGH FERRULE FILLET FIREWALL FISHPLATE FITTING FITTING - CORNER FITTING - CROWN FITTING - FIXED FITTING - FRAME BASE FITTING - GUIDE FITTING - HINGE FITTING - INNER FITTING - JOINT FITTING - LOWER

FITTING - OUTER FITTING - PICKUP FITTING - PIVOT FITTING - SEALING FITTING - UPPER FLANGE FLAP FLIGHT KIT FLOOR FOOTREST FORGING FORGING - DIE FORK FORK - TELESCOPIC FRAME FRAME SECTION FRAMEWORK FRONTIER DRAWING FUSE FUSELAGE

GASKET GEAR GEAR BOX GEOMETRY DRAWING GLARESHIELD GRILLE GUARD - CABLE GUARD - SWITCH GUSSET GUTTER

HANDLE HANDRAIL HARNESS HARNESS - SAFETY HAT SECTION HATCH HEAD HEADREST HEATSHIELD HINGE HOLDER - CUP HOOK HOSE HOUSING HOUSING - HANDLE MECH HUB


Date: 3 May 2000

ABD0036


B - DRAWN PARTS ICY DRAWING INDICATOR - VISUAL INLET INSERT INTERFACE DRAWING ISOLATOR

JOINT JOINT - EXPANSION JOINT SWIVEL JUMPER

KEY KNOB

L SECTION LADDER LANDING LANDING GEAR - MAIN LANDING GEAR - NOSE LATCH LEADING EDGE LEAFSPRING LENS LEVER LINK LINK - ROTATING LINKAGE LOCKNUT LOCKPLATE LOCKWASHER LOWER SURFACE - WING LUG

MANIFOLD MAST MAST - DRAIN MEMBER - ARCH MEMBER - CROSS MEMBRANE MEMBRANE - VAPOR SEAL MODULE MOUNT MOUNT-ENGINE

NACELLE NOSE SECTION NOZZLE NUT NUT - ANCHOR NUT - CASTELLATED NUT - SLOTTED NUT PLATE

O-RING OUTLET OUTLET - BLOWING OUTLET - EXTRACTION OUTLING DRAWING

PACKING - PROFILE PACKING - SEALING PAD PAN - DRIP PANEL PANEL - ACCESS PANEL - INSTRUMENT PANEL - LIGHTING PANEL - LINING PANEL - OVERHEAD PANEL - PRESSURE PARTITION PAWL PEDALS - RUDDER PIN PIN - FAILSAFE PIN - HINGE PIN - LOCATING PIN - LOCKING PIN - RIGGING PIN - SHOULDERED PIPE PIPE RUN PISTON PLACARD PLATE PLATE - BACKING PLATE - BASE PLATE - BENT PLATE - BLANKING PLATE - CLOSING PLATE - COVER PLATE - LOWER Page: B - 4

Issue: F

Date: 3 May 2000

ABD0036


B - DRAWN PARTS PLATE - MOUNTING PLATE - REINFORCING PLATE - SEALING PLATE - SIDE PLUG PLUG - BREAK PLUMBING INSTL POST POST - CARGO COMPARTMENT POTENTIOMETER POWER SUPPLY UNIT PULLEY PYLON - ENGINE PYRAMID

QUADRANT

RACEWAY RACK RAIL RECEPTACLE RELAY RELAY BOX RESTRICTOR RETAINER - SEAL RIB RIB - FALSE RING RING - BACKUP RING - RETAINER RING - RETAINING RING - STOP RIVET RIVET - BLIND RIVET - COUNTERSUNK ROD ROLLER

SCOOP SCREEN SCREWSEAL SEAL - BLADE SEAL - LIP SEAL - PRESSURE SECTION SECTION - BENT SECTION - SEALING SENSOR

SHAFT SHAFT - DRIVE SHAFT - SPLINED SHANK SHELF SHELL SHELL - HALF SHIM SHIM - LOCATING SHIM - PEEL SHOCK ABSORBER SHOE SHROUD - FLAP SIDE STICK SIDESTAY SKIN SLAT SLEEVE SLIDE SLIDER SPACER SPAR SPAR - FALSE SPAR - FRONT SPAR - REAR SPAR - SMALL SPLICE SPOOL SPRING STABILIZER - VERTICAL STIFFENER STOP STOPPER - CRACK STOWAGE STOWAGE - FLASHLIGHT STOWAGE - MASK STRAP STRAP - JOINT STRINGER STRIP STRIP - COVER STRIP - FOAM STRIP - MATING STRIP - REINFORCING STRIP - RUBBING STRIP - SEALING STRIP - TRAILING EDGE STRIP - VELCRO STRUT STUD SUPPORT


Date: 3 May 2000

ABD0036


B - DRAWN PARTS SUPPORT - TUBULAR SUPPORT PLATE - CONNECTOR SURFACE - CONTROL SWITCH SWITCH - LIMIT SWITCH - PUSHBUTTON SWITCH - ROTARY SWITCH - SELECTOR SWITCH - TOGGLE

YOKE

Z SECTION

T SECTION TAB TAB - BONDING TAIL CONE TANK TAPE - ADHESIVE TAPPING TEE - VERTICAL TRACK - FLAP TRACK - SEAT TRAILING EDGE TRANSDUCER TRIFORM TRIPOD TRUNNION TUBE TUBE-TORSION

UNION UPPER SURFACE - WING

VENTURI VISOR - SUN

WASHER WEB WEB - FRONT WEB - REAR WEB - WELDED WEDGE WHEEL WINDOW WING WIRE WIRE ROUTING WIRING


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


C - NOTES FOR USE ON DRAWINGS This catalog provides a list of standard Notes to be used by all AIB Members/Associated Partners on their drawings. May be completed, as necessary, by the equivalent notes in their national language: • Ref: * ABD0004 - Drawing System, Part 1, for further details.

Usage - Component Maintenance Manual Manufacturer (CMMM). - Aircraft Maintenance Manual (AMM). - Structural Repair Manual (SRM). - Aircraft Wiring Manual (AWM) chapter related - Standard Practices. - Service Bulletins (SB).

Page: C - 1 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


C - NOTES FOR USE ON DRAWINGS Apply Protective Treatment To…

- OBERFLAECHENSCHUTZ AUFGETRAGEN NACH… - PROTECTION DES… - APLICAR TRATAMIENTO DE PROTECCION PARA…

Apply… Grease to all bolts

- ALLE BOLZEN MIT FETT… EINGEFETTET - ENDUIRE TOUS LES BOULONS AVEC DE GRAISSE - APLICAR GRASA… A TODOS LOS BULONES

LA

Break Sharp Edges

- KANTEN GEBROCHEN - ABATTRE LES ANGLES VIFS - MATAR ARISTAS

Coat Holes, Thread Reliefs and Threads With Dry Lubricant

- TROCKEN-SCHMIERMITTEL AUF BOHRUNGEN, GEWINDE-AUSLAUF UND GEWINDE AUFTRAGEN - APPLICATION DE LUBRIFIANT SEC DANS ALESAGE, GORGE ET FILETAGE - APLICAR LUBRICANTE SECO ENTALADRO, RANURA Y ROSCA

Chamfer

- ANGEFAST - CHANFREIN - CHAFLAN

Cement Placard Per…

- BAUTEILSCHILD GEKLEBT NACH… - COLLAGE DE L'ETIQUETTE SUIVANT… - PEGAR ETIQUETA SEGUN…

Counterdrill To Match Existing Holes

- SENKUNGEN AN BESTEHENDE BOHRUNGEN ANGEPASST - FIXATIONS EXISTANTES A REPRENDRE - CONTRATALADRAR CON LOS TALADROS EXISTENTES

Counterbore… Dia

- VERSENKT Ø - LAMAGE Ø… - LAMADO… Ø

Csink… 0x… Dia

- GESENKT - FRAISAGE 0… A…0 - AVELLANAR… 0 X… Ø

Coat… With…

- … AUFGETRAGEN - ENDUIRE… AVEC… - CUBRIR… CON…

Cement Parts Items… Using…

- POSITIONEN… MIT KLEBER…. EINGEKLEBT - COLLAGE DES PIECES… AVEC… - PEGAR LAS PIEZAS… CON…

Crimp One Side Only

- NUR AUF EINER SEITE AUFGEQUETSCHT - SERTISSAGE UN COTE SEULEMENT - GRAPAR EN UNA SOLA CARA

Drill Per…

- GEBOHRT NACH… - ALESAGES SUIVANT… - TALADRAR SEGUN…

Drill To Match Existing Holes In Part No. …

- BESTEHENDE BOHRUNGEN IN PART No. … ABGESTIMMT MIT - PERCAGE EN ACCORD AVEC PIECE No. … - TALADRAR DE ACUERDO CON TALADROS DE PIEZA No. …


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


C - NOTES FOR USE ON DRAWINGS Effective Aircraft Subsequent

(Or

A/C)

No. …

And

- GUELTIG AB FLUGZEUG… (UND FOLGENDE) - APPLICABLE AVION No. … ET SUIVANTS - APLICABLE AL AVION No.… Y SIGUIENTES

Identify Per

- GEKENNZEICHNET NACH… - MARQUAGE SUIVANT… - IDENTIFICAR SEGUN…

Install Per

- EINGEBAUT NACH… - IMPLANTATION SUIVANT… - INSTALAR SEGUN…

Insert Bolts With Anti Corrosion Paste

- BOLZEN MIT KORROSIONSSCHUTZPASTE EINGESETZT - BOULONS MIS EN PLACE AVEC PATE ANTICORROSION - INTRODUCIR BULONES CON PASTA ANTICORROSIVA

Machine With Mill Cutter… Dia

- MIT Ø… FRAESER BEARBEITET - USINAGE FRAISE R… - MECANIZAR CON FRESA… Ø

Mark With A Paint Dot

- MIT FARBTUPFER MARKIERT - TRAIT DE PEINTURE - IDENTIFICAR CON PINTURA

Mark Direction Of Flow

- FLIESSRICHTUNG GEKENNZEICHNET - MARQUAGE SENS D'ECOULEMENT - MARCAR EL SENTIDO DEL FLUJO

Make From

- ABGEWANDELT AUS… - PRIS DANS… - FABRICADO DE…

No Paint Reliefs

Over

Threads

And

Into

Thread

- GEWINDE UND GEWINDEAUSLAUF OHNE FARBE - PAS DE PEINTURE SUR LES FILETAGES ET LES GORGES - NO PINTAR SOBRE ROSCAS NI SALIDAS DE ROSCAS

Protect Per

- OBERFLAECHENSCHUTZ NACH… - PROTECTION DE L'ENSEMBLE - PROTECCION SEGUN

Paint Visible Surfaces Per…

- FARBANSTRICH ALLER SICHTBAREN FLAECHEN NACH… - PEINTURE SURFACES APPARENTES SUIVANT… SURFACE VISIBLE PEINTURE SUIVANT… - PINTAR LAS SUPERFICIES VISIBLES SEGUN…

Ref. To Dwgs

- SIEHE ZEICHNUNGEN - PLANS A CONSULTER - PLANO DE REFERENCIA


Date: 3 May 2000

AIRBUS INDUSTRIE

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D - CONSTITUENT ASSEMBLIES According to ABD0056 - GATE a Constituent Assembly is a Major structural aircraft section which is supplied to the production line for final assembly of the aircraft (eg: fuselage, wings, doors, flaps, slats). This catalog lists the major Aircraft Constituent Assemblies. To ensure full coherence between Aircraft Programs/Projects, it has to be taken as reference for any new ATA 100 Breakdown preparation.

Usage - Technical Specifications (for subcontract). - Drawing Set. - Aircraft Inspection Report (AIR). - Contractual Technical Publication.

Page: D - 1 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

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D - CONSTITUENT ASSEMBLIES CABIN: Whole of the main deck area behind the cockpit. Note: In combi configuration this comprises a passenger compartment plus main deck cargo compartment.

COCKPIT COMPARTMENTS - CARGO • LOWER DECK (FWD, AFT, BULK) • MAIN DECK - EQUIPMENT • AIR CONDITIONING • AVIONICS • HYDRAULICS

DOOR - PASSENGER/CREW (FWD, MID, AFT) - EMERGENCY EXIT - CARGO COMPARTMENT (FWD, AFT, BULK, MAIN DECK) - LANDING GEAR - SERVICING

EMPENNAGE - HORIZONTAL • TRIMMABLE HORIZONTAL STABILIZER (THS) • ELEVATORS - VERTICAL • VERTICAL STABILIZER • RUDDER

FUSELAGE - NOSE FORWARD FUSELAGE - FORWARD FUSELAGE - CENTER FUSELAGE - REAR FUSELAGE - TAIL CONE

LANDING GEAR - CENTERLINE - MAIN (MLG) - NOSE (NLG) - LANDING GEAR WELL - WINGS LEFT, RIGHT (L, R)


Date: 3 May 2000

AIRBUS INDUSTRIE

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D - CONSTITUENT ASSEMBLIES MOVING SURFACES ON THE WING - AILERONS - FLAPS • INBOARD • OUTBOARD - SLATS (1, 2, 3 etc.) - SPOILERS

FUEL TANKS - INNER - OUTER - CENTER - TRIM


Date: 3 May 2000

AIRBUS INDUSTRIE

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E - STANDARD ITEMS This Catalog lists Standard Main Words to be used to allocate Title to New Standards: Ref: * ABD0032 - Standard Items * ABD0036 - Numbering/Naming, Chapter 7

Usage - New Standards. - Standards Manual (SM). - Component Maintenance Manual Manufacturer (CMMM). - Illustrated Parts Catalog (IPC). - Aircraft Wiring Equipment Lists (AWL). - Structural Repair Manual (SRM). - Service Bulletins (SB).

Page: E - 1 Issue: F

Date: 3 May 2000

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E - STANDARD ITEMS ACTUATOR ADAPTOR ANGLE ANNUNCIATOR ASHTRAY BACKSHELL BAG BALL BALL END-WIRE ROPE BAND - IDENTIFICATION BAR BAR-FLAT BAR-HEX BAR-ROUND BARREL BASE BASE-MOUNTING BEARING BEARING-BALL BEARING-ELASTIC BEARING-ROLLER BEARING-SELF-ALIGNING BEARING-SPHERICALBELLOWS BELT BLOCK-ISOLATOR BLOCK-TERMINAL BOBBIN BODY BOLT BOLT-TAPER-LOCK BOOT BOOT-PROTECTIVE BOX BRAID BREATHER BRUSH BUFFER-DOOR BUMPER BUS BUSHING BUSHING-ELASTOMER BUTTON C/B-DUMMY CABLE-COAXIAL CAP CAPACITOR CAPSULE-LAMP CARPET CHAIN

CHAIN-BEAD CHANNEL-GANG CIRCUIT BREAKER CLAMP CLAMP BLOCK CLAMP-END CLEAT CLIP CLOTH-WIRE COLLAR CONDUIT CONNECTION-BULKHEAD CONNECTOR CONNECTOR-PLUG CONNECTOR-RACK CONNECTOR-RECEPTACLE CONTACT CONTACT-DUMMYCONTACT-PIN CONTACT-SOCKET CORD CORD-BUNGEE CORD-COAXIAL COUPLING COVER COVER-ENGINE CROSS CUP CURTAIN CUSHION DETECTOR DETECTOR-CURRENT DIAPHRAGM DIFFUSER DIODE DISCHARGER-STATIC DRAIN DUCT ELBOW ELBOW-XX DEG EXTRACTOR EYE END-TRNBLK

FABRIC FAIRLEAD FASTENER FASTENER-BUTTERFLY Page: E - 2

Issue: F

Date: 3 May 2000

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E - STANDARD ITEMS FASTENER-CAMLOC FASTENER-HOOK/LOOP FASTENER-MAGNETIC FASTENER-ZIP FERRULE FILM FILTER FITTING-LUBRICATION FLANGE FORK FUSE FUSE-DC, LIMITER TYPE GAGE-STRAIN GASKET GLASSCLOTH GRID-EXPANDED METAL GRIP GROMMET GUARD-SWITCH HANGER-COAT HINGE HOLDER HOLDER-ASHTRAY HOLDER-CUP HOLDER-FUSE HOLDER-PENCIL HOOK HORN HOSE INDICATOR-MAGNETIC INDUCTOR INSERT INSULATOR ISOLATOR JACK JOINT-EXPANSION

KNOB-CONTROL KNOB-PULL LAMP LATCH

LEAD-BONDING LENS LEVER LIGHT-CEILING LIGHT-INDICATOR LIGHT-READING LIGHT-UTILITY LINK LOCK LOCK-BALL LOCKBOLT LOCKWIRE LUG MAGNET MARKER-CABLE MICROSWITCH MODULE MODULE-DUMMY MOUNT MOUNT-ISOLATOR NEEDLE NET NUTNUT-ANCHOR NUT-BLIND NUT-CLIP NUT-JAM NUT-LOCKING NUT-SELF-ALIGNING NUT-SELF-LOCKING "O RING" OLIVE PAD PAD-TEFLON PANEL-MIRROR PILLAR PIN PIN-BALL PIN-COTTER PIN-GROOVED PIN-HI-LOK PIN-QUICK RELEASE PIN-SHEAR PIN-SPRING PIN-TAPER PINS-LOCATING Page: E - 3

Issue: F

Date: 3 May 2000

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E - STANDARD ITEMS PLATE PLATE-BONDING PLATE-MOUNTING PLUG PLUG-BLANKING PLUG-SEALING POTENTIOMETER PULLEY PUSHBUTTON RACK RAIL RECEPTACLE RECEPTACLE-DUMMY RECEPTACLE-GND POWER RECTIFIER REDUCER RELAY RESISTOR RETAINER RHEOSTAT RIBBON RING RING-BACKUP RING-RETAINING RIVET RIVET-SPLIT ROD ROD END ROLLER SCREW SEAL SEAL-UP SEAL-PRESSURE SETSCREW SHEATH SHIELD SHIM-PEEL SHUNT SKIRT SLEEVE SLEEVE-HEAT SHRINK SLEEVE-RETENTION SLEEVE-SOLDER SLIDE SOCKET SPACER SPLICE SPYGLASSSTOP STOP-CABLE

STRAP STREAMER-WARNING STRIKE STRIP STRIP-IDENTIFICATION STRIP-RUB STUD STUD-BONDING STUD-PUSH-ON SWITCH SWITCH-LIMIT SWITCH-PROXIMITY SWITCH-PUSHBUTTON SWITCH-ROTARY SWITCH-TOGGLE TAB TAG TAPE TAPE-ADHESIVE TAPE-HOOK TAPE-LACING TAPE-LOOPTARGET TEE TEE-HEAT SHRINK TERMINAL TERMINAL-CHAIN THREAD TIE-CABLE TIMER-STATIC TRANSFORMER TRIGGER TRIPOD TRUNNION TUBE TUBE-FLUORESCENT TUBING END TUBING-HEAT SHRINK UNION VALVE

Page: E - 4 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

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F - NON STANDARD ITEMS - STANDARD MAIN WORDS FOR FUNCTIONAL DESIGNATIONS This list provides: 1 - A basic list of Main Words for use in Component Functional Designations. 2 - A standard presentation of these Main Words, for use in all AIRBUS Projects, whatever the industrial worksharing and/or transfers of responsibility, to obtain maximum consistency in wording content and layout between: - all labels: • in the cockpit • stuck on the structure next to the equipment - interior markings - exterior markings - messages on display units - any lists of components using the FIN and functional designation eg: • Nomenclature of Principle Diagrams and Functional Diagrams • Aircraft Wiring List • Aircraft Maintenance Manual component location information

Consideration of above has led to widespread use of abbreviations, selected on the following basis and order of priority: 1 - Abbreviations used in the cockpit. 2 - Abbreviations commonly used (eg: in System Description Notes - SDN, Technical Publications). 3 - Abbreviations which are considered to be useful and understandable, and therefore suitable for use on placards, display units, etc. 4 - Abbreviations necessary to limit the main word to 20 characters. Any Main Words not in the above three categories are left in full. The abbreviations used are all approved in ABD0037 Airbus Approved Abbreviations Handbook (AAAH). This list also includes Main Words used in the Airbus ATA 100 Breakdowns at 6 digit level for Assemblies or Structural Items. These do not have FINs but their designations are constructed in the same manner as those for items with FINs. If necessary, the main words listed can be used with the word "Assy" (assembly). They can also be used in the plural. Consequently, main words including the word "assy" are not included in the list, unless they cannot be used without "assy". The list does not include names of major assemblies, such as "aileron", "slat" or "spoiler", as these are listed in Appendix D - Constituent Assemblies. .

Page: F - 1 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

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F - NON STANDARD ITEMS - STANDARD MAIN WORDS FOR FUNCTIONAL DESIGNATIONS Specific Recommendations 1: Items included in this list, but not requiring Functional Designations - BUNDLES (WIRE) - CONNECTORS (PLUGS/RECEPTACLES) - DIODES - RELAY BASES - RELAY BOXES - TERMINAL BLOCKS 2: Words not to be used on their own as main words - ASSEMBLY - BOX - DEVICE - EQUIPMENT - FITTING - PANEL - UNIT 3: Preferred terms - ACTUATOR or - ACTUATING CYLINDER - CHECK VALVE - VALVE - UNIT

not JACK not NON RETURN VALVE not COCK not BOX, for items which are units (eg: control units). BOX to be restricted to items such as RELAY BOXES, JUNCTION BOXES, etc.


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference)

Form to be Used (Funct. Designations, Placards, etc.) ACCLRM ACCESS COVER ACCESS DOOR ACCESS FAIRING ACCESS PNL ACCU ACOUSTIC FILTER ACTG CYL ACTG MECH ACTUATOR ADAPTOR ADAPTOR PLATE ACT ADJUSTER ASSY AIR CHILLER UNIT ADIRU

ACCELEROMETER ACCESS COVER ACCESS DOOR ACCESS FAIRING ACCESS PANEL ACCUMULATOR ACOUSTIC FILTER ACTUATING CYLINDER ACTUATING MECHANISM ACTUATOR ADAPTOR ADAPTOR PLATE ADDITIONAL CENTER TANK ADJUSTER ASSY AIR CHILLER UNIT AIR DATA/INERTIAL REFERENCE UNIT AIR DATA COMPUTER AIR DATA MODULE AIR FILTER AIR INLET AIR INTAKE AIR OUTLET AIR RADIO UNIT AIRSPEED INDICATOR ALTERNATOR ALTIMETER AMMETER AMPLIFIER AMPLIFIER UNIT ANALYSER ANNUNCIATOR

ADC ADM AIR FILTER AIR INLET AIR INTAKE AIR OUTLET AIR RADIO UNIT ASI ALTERNATOR ALTM AMMETER AMPLIFIER AMPLIFIER UNIT ANALYSER ANN

ANNUNCIATOR LIGHT

ANN LT

ANTENNA APRON AREA DISTRIBUTION BOX ARM ARTIFICIAL FEEL MECHANISM ARTIFICIAL FEEL UNIT ASH TRAY

ANTENNA APRON ADB ARM ARTIFICIAL FEEL MECHANISM ARTF FEEL UNIT ASH TRAY

REMARKS

Square type lights used on VU panels Term encompassing all types of indicators, warning/caution lights, annunciators etc. Tech Pubs only

Tech Pubs only


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) ASYMMETRY POSITION PICKOFF UNIT ATOMIZER ATTACH FITTING ATTACHMENT ATTACHMENT BRACKET ATTENDANT PANEL ATTENUATOR ATTITUDE MONITOR ATTITUDE SENSOR AUDIO CONTROL PANEL AUDIO MANAGEMENT UNIT AURAL WARNING BOX AUTOMATIC CALL-OUT BOX AUTOMATIC SELECTOR AUTOMATIC SELECTOR VALVE AUTOTRANSFORMER AUXILIARY POWER UNIT AVIONICS EQUIPMENT VENTILATION COMPUTER AXE AXLE SLEEVE

Form to be Used (Funct. Designations, Placards, etc.) APPU ATOMIZER ATTACH FITTING ATTACHMENT ATTACHMENT BRACKET ATTENDANT PANEL ATTENUATOR ATT MON ATT SENSOR ACP AMU AURAL WARN BOX ACOB AUTO SEL AUTO SEL VALVE A/XFMR APU AEVC

REMARKS

Tech Pubs only Tech Pubs only Tech Pubs only

Pitch trim rotation

AXE AXLE SLEEVE


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) BACK-UP YAW DAMPER UNIT BAFFLE BAG BALL JOINT BALL UNIT BALLAST BALLAST UNIT BAR BASE BASSINET BATTERY BATTERY CHARGE LIMITER BEAM BEAM STEERING UNIT BEARING BELLOWS BEVEL GEARBOX BLADE BLEED MONITORING COMPUTER BLINKER BLOWER BOARD BOGIE BEAM BOOMSET BOTTLE BRACKET BRAKE BRAKING/STEERINGCONTROL UNIT BREAKOUT PANEL BULB BULKHEAD BUNDLE BUS TIE CONTACTOR BUZZER BYPASS VALVE

Form to be Used (Funct. Designations, Placards, etc.) BYDU BAFFLE BAG BALL JOINT BALL UNIT BALLAST BALLAST UNIT BAR BASE BASSINET BAT BCL BEAM BSU BEARING BELLOWS BEVEL GEARBOX BLADE BMC

REMARKS

eg: relay base

SATCOM

BLINKER BLOWER BOARD BOGIE BEAM BOOMSET BOTTLE BRACKET BRK BSCU BREAKOUT PNL BULB BULKHEAD BUNDLE BTC BUZZER BYPASS VALVE

Tech Pubs only eg: wire bundle


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) CABIN DISTRIBUTION UNIT CABIN PASSENGER MANAGEMENT UNIT CABIN TELECOMMUNICATIONS UNIT CABIN TELEPHONE UNIT CABIN UNIT CABINET CABLE CABLE ASSEMBLY CADENSICON CALIBRATION MEMORY MODULE CALL PANEL CAN CAN ASSEMBLY CANISTER CAP CAPACITOR CARPET CARRIAGE CARRIER CARTRIDGE CAUTION LIGHT CEILING PANEL CENTERBODY CENTERING MECHANISM CENTERING SPRING ROD CENTERING ROD CENTRAL MAINTENANCE COMPUTER CENTRALIZED FAULT DISPLAY INTERFACE UNIT CHANGEOVER VALVE CHARGE VALVE CHARTHOLDER CHECK VALVE CHIP DETECTOR CIRCUIT BREAKER CIRCUIT BREAKER BOX CIRCUIT BREAKER MONITORING UNIT CIRCUIT BREAKER PANEL CLACK VALVE

Form to be Used (Funct. Designations, Placards, etc.) CABIN DISTRIBUTION UNIT CPMU

REMARKS

CABIN TELECOM UNIT CABIN TELEPHONE UNIT CABIN UNIT CABINET CABLE CABLE ASSY CADENSICON CMM CALL PNL CAN CAN ASSY CANISTER CAP CAPACITOR CARPET CARRIAGE CARRIER CARTRIDGE CAUT LT CEILING PNL CENTERBODY CENTERING MECHANISM CENTERING SPRING ROD CENTERING ROD CMC

Rectangular amber lights

Tech Pubs only

CFDIU CHANGEOVER VALVE CHARGE VALVE CHARTHOLDER CHECK VALVE CHIP DET C/B C/B BOX CBMU C/B PNL CLACK VALVE Page: F - 6

Issue: F

Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference)

Form to be Used (Funct. Designations, Placards, etc.) CLAMP CLINOMETER CLOSET CLOCK CVR COFFEE MAKER COLLAPSIBLE STRETCHER COMBINER CSU CNA COMPARISON UNIT COMPARTMENT COMPASS COMPENSATOR COMPRESSOR CMPTR CONDITIONER CONDUIT CNCTN BOX CONNECTOR CSM/G

CLAMP CLINOMETER CLOSET CLOCK COCKPIT VOICE RECORDER COFFEE MAKER COLLAPSIBLE STRETCHER COMBINER COMMAND SENSOR UNIT COMMON NOZZLE ASSEMBLY COMPARISON UNIT COMPARTMENT COMPASS COMPENSATOR COMPRESSOR COMPUTER CONDITIONER CONDUIT CONNECTION BOX CONNECTOR CONSTANT SPEED MOTOR/GENERATOR CONTACTOR CONTAINER CONTROL & DISPLAY UNIT CONTROL & INDICATING UNIT CONTROL & MONITORING UNIT CONTROL BOX CONTROL LEVER CONTROL MECHANISM CONTROL MODULE

CNTOR CONTAINER CDU CTL & IND UNIT CTL & MONG UNIT CTL BOX CTL LEVER CONTROL MECHANISM CTL MODULE

CONTROL LEVER CONTROL PANEL CONTROL SWITCH CONTROL UNIT CONTROL VALVE CONTROLLER CONVERTER COOLER COOLING UNIT COUPLER COUPLING COUPLING BOX

CTL LEVER CTL PNL CTL SW CTL UNIT CTL VALVE CONT CONV COOLER COOL UNIT COUPLER CPLG CPLG BOX

REMARKS

Engines (RR) Tech Pubs only

Tech Pubs only eg: for cockpit fire control module


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) COUPLING HALF COUPLING UNIT COVER COVERING COWL COWL DOOR CRADLE CREDIT CARD READER CRYPTO VOICE UNIT CURRENT COMPARATOR CURRENT TRANSFORMER CURTAIN CUTOUT VALVE CYLINDER

Form to be Used (Funct. Designations, Placards, etc.) CPLG HALF CPLG UNIT COVER COVERING COWL COWL DOOR CRADLE CREDIT CARD READER CRYPTO VOICE UNIT CURRENT COMPARATOR CT CURTAIN CUTOUT VALVE CYL

REMARKS

Tech Pubs only Tech Pubs only Engines


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) DADO PANEL DAMPENER DAMPER DATA MANAGEMENT UNIT DECODER DECODER/ENCODER UNIT DELAY VALVE DEMISTER DENSITOMETER DESCENT DEVICE DETECTION UNIT DETECTOR DETECTOR UNIT DIAPHRAGM DIFFUSER DIGITAL ACMS RECORDER DIGITAL AIDS RECORDER DIGITAL DISTANCE RADIO MAGNETIC INDICATOR DIGITAL FLIGHT DATA ACQUISITION UNIT DIGITAL FLIGHT DATA RECORDER DIGITAL INTERFACE UNIT DIMMER DIODE DIPLEXER DIPLEXER/LOW NOISE AMPLIFIER DIRECTOR DISCHARGER DISPENSER DISPLAY DISPLAY MANAGEMENT COMPUTER DISPLAY PANEL DISPLAY UNIT DISCHARGE HEAD DISK DIVIDER DOGHOUSE DOOR DOWN DRIVE DOWN LOADER

Form to be Used (Funct. Designations, Placards, etc.) DADO PNL DAMPENER DAMPER DMU DECODER DEU DELAY VALVE DEMISTER DENSITOMETER DESCENT DEVICE DET UNIT DET DET UNIT DIAPHRAGM DIFFUSER DAR DAR DDRMI

REMARKS

A340 A320

DFDAU DFDR DIU DIMMER DIODE DIPLEXER D/LNA DIR DISCHARGER DISPENSER DISPLAY DMC DISPLAY PNL DU DISCHARGE HEAD DISK DIVIDER DOGHOUSE DOOR DOWN DRIVE DOWN LOADER

Interior furnishings


Date: 3 May 2000

AIRBUS INDUSTRIE

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) DRAG STAY DRAIN DRAIN MAST DRIVE ASSEMBLY DRIVE SHAFT DRIVE UNIT DUAL DRIVE DUAL SHUTTLE VALVE DUAL VALVE DUCT

Form to be Used (Funct. Designations, Placards, etc.) DRAG STAY DRAIN DRAIN MAST DRIVE ASSY DRIVE SHAFT DRIVE UNIT DUAL DRIVE DUAL SHUTTLE VALVE DUAL VALVE DUCT

REMARKS


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) ELECTRICAL BOX ELECTRICAL CONNECTION BOX ELECTRICAL FLIGHT CONTROL UNIT ELECTRICAL GENERATION INTERFACE UNIT ELECTRICAL CONTACTOR MANAGEMENT UNIT ELECTRICAL HARNESS ELECTRIC PUMP ELECTRONIC BOX ELECTRONIC CONTROL BOX ELECTRONIC CONTROL UNIT ELECTRONIC ENGINE CONTROL ELECTRONIC LIBRARY COMPUTER ELECTRONIC MODULE ELEMENT ELEVATOR ELEVATOR AILERON COMPUTER EMERGENCY EXIT ENCODER END CAP ENGAGE UNIT ENGINE ENGINE BUILD-UP UNIT ENGINE ELECTRONIC CONTROLLER ENGINE INTERFACE UNIT ENGINE INTERFACE AND VIBRATION MONITORING UNIT ENGINE RELAY UNIT ENGINE VIBRATION MONITORING UNIT ENTRANCE GUIDE ESCAPE SLIDE/RAFT EXCHANGER EXCITER EXPANSION UNIT EXTERNAL POWER CONTACTOR EXTINGUISHER EXTRACTOR

Form to be Used (Funct. Designations, Placards, etc.) ELEC BOX ELEC CONNECTION BOX EFCU

REMARKS

EGIU ECMU ELECTRICAL HARNESS ELEC PUMP ELECTRONIC BOX ECB ECU EEC ELC

APU Engines (CFM) Engines (PW)

ELEK MODULE ELEMENT ELEVATOR ELAC EMERGENCY EXIT ENCODER END CAP ENGAGE UNIT ENGINE EBU EEC

Tech Pubs only

Engines (RR)

EIU EIVMU

Engines

ERU EVMU

Engines (PW)

ENTRANCE GUIDE ESCAPE SLIDE/RAFT EXCHANGER EXCITER EXPANSION UNIT EPC EXTINGUISHER EXTRACTOR Page: F - 11

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) EXTRACTOR PLUG

Form to be Used (Funct. Designations, Placards, etc.) EXTRACTOR PLUG

REMARKS


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) FAIRING FAN FAN HEATER FAUCET FAX MACHINE FEEDBACK POSITION PICK-OFF UNIT FEEDER FEEL & LIMITATION COMPUTER FENCE FILLET FILLING PORT FILTER FIRE DETECTION UNIT FIRST AID KIT FITTING FIXED FAIRING FIXED PARTITION FLAP FLASH LIGHT FLASHER FLASHER UNIT FLEXIBLE DRIVE SHAFT FLEXIBLE HOSE FLEXIBLE PUSH PULL CONTROL FLEXIBLE SHAFT FLIGHT AUGMENTATION COMPUTER FLIGHT CONTROL COMPUTER FLIGHT CONTROL DATA CONCENTRATOR FLIGHT CONTROL PRIMARY COMPUTER FLIGHT CONTROL SECONDARY COMPUTER FLIGHT CONTROL UNIT FLIGHT DATA ENTRY PANEL FLIGHT DATA INTERFACE UNIT FLIGHT KIT FLIGHT MANAGEMENT & GUIDANCE COMPUTER FLIGHT MANAGEMENT, GUIDANCE & ENVELOPE COMPUTER

Form to be Used (Funct. Designations, Placards, etc.) FAIRING FAN FAN HEATER FAUCET FAX MACHINE FPPU FEEDER FLC FENCE FILLET FILLING PORT FILTER FDU FIRST AID KIT FITTING FIXED FAIRING FIXED PARTITION FLAP FLASH LT FLASHER FLASHER UNIT FLEX DRIVE SHAFT FLEX HOSE FLEX PUSH PULL CTL FLEX SHAFT FAC

REMARKS

Tech Pubs only Tech Pubs only

FCC FCDC FCPC FCSC FCU FDEP FDIU FLIGHT KIT FMGC FMGEC


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) FLIGHT MANAGEMENT COMPUTER FLIGHT WARNING COMPUTER FLOAT VALVE FLOODLIGHT FLOOR DISCONNECT BOX FLOOR PANEL FLOOR STRUCTURE FLOPPY DISK DRIVE FLOW DIVIDER FLUORESCENT TUBE FLUSH LINE FOOT REST FOOT WARMER FRAME FRAMEWORK FREQUENCY METER FUEL CONTROL & MONITORING COMPUTER FUEL LEVEL SENSING CONTROL UNIT FUEL LINE FUEL METERING UNIT FUEL QUANTITY INDICATION COMPUTER FUSE FUSIBLE PLUG

Form to be Used (Funct. Designations, Placards, etc.) FMC FWC FLOAT VALVE FLOOD LT FDB FLOOR PNL FLOOR STRUCTURE FLOPPY DISK DRIVE FLOW DIVIDER FLUOR TUBE FLUSH LINE FOOT REST FOOT WARMER FRAME FRAMEWORK FREQ METER FCMC

REMARKS


FLSCU FUEL LINE FMU FQIC

Engines

FUSE FUSIBLE PLUG


Date: 3 May 2000

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) GAGE GAGE ASSEMBLY GALLEY GEARBOX GENERATOR GENERATOR CONTROL UNIT GENERATOR LINE CONTACTOR GLOBAL POSITIONING SYSTEM SENSOR UNIT GLOVES GOGGLES GROUND CONNECTOR GROUND POWER CONTROL UNIT GROUND PROXIMITY WARNING COMPUTER GROUND REFRIGERATION UNIT GUIDE GYROSCOPIC UNIT

Form to be Used (Funct. Designations, Placards, etc.) GAGE GAGE ASSY GALLEY GEARBOX GEN GCU GLC GPSSU

REMARKS

Tech Pubs only

GLOVES GOGGLES GND CNCTR GPCU GPWC GRU GUIDE GYRO UNIT


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) HAND GRIP HAND MICROPHONE HAND PUMP HANDCUFFS HANDLE HANDSET HARNESS HEAD HEAD-UP DISPLAY COMPUTER HEADSET HEATER HEATER ELEMENT HEAT EXCHANGER HEATING PANEL HEATING PLATE HIGH POWER AMPLIFIER HINGE ARM HOIST POINT HOLDER HORN HOSE HOURMETER HOUSING HUB CAP HYDRAULIC BLOCK HYDRAULIC CONTROL UNIT HYDRAULIC SYSTEM MONITORING UNIT HYDROMECHANICAL UNIT

Form to be Used (Funct. Designations, Placards, etc.) HAND GRIP HAND MIC HAND PUMP HANDCUFFS HANDLE HANDSET HARNESS HEAD HUDC HEADSET HEATER HEATER ELEMENT HEAT EXCHANGER HTG PNL HTG PLATE HPA HINGE ARM HOIST POINT HOLDER HORN HOSE HOURMETER HOUSING HUB CAP HYDRAULIC BLOCK HCU HSMU

REMARKS

SATCOM Tech Pubs only Tech Pubs only

HMU


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) IGNITION UNIT INCUBATOR INDICATION PANEL INDICATOR INDICATOR BOX INDICATOR LIGHT INDICATOR PLATE INDIVIDUAL AIR OUTLET INERTIAL REFERENCE UNIT INERTIAL SYSTEM DISPLAY UNIT INFORMATION PANEL INJECTOR INSTRUMENTATION POSITION PICKOFF UNIT INSULATION INTAKE INTEGRATED DRIVE GENERATOR INTERCOM UNIT INTERCONNECTING BOX INTERFACE BOX INTERFACE UNIT INTERPHONE BOX INTERROGATOR ISOLATION VALVE BLOCK ISOLATOR

Form to be Used (Funct. Designations, Placards, etc.) IGNITION UNIT INCUBATOR IND PNL IND IND BOX IND LT

REMARKS Engines (RR)

Rectangular lights, any color except red or amber

IND PLATE INDIVIDUAL AIR OUTLET IRU ISDU INFO PNL INJECTOR IPPU INSULATION INTAKE IDG

Tech Pubs only

INTERCOM UNIT INTERCONNECTING BOX INTERFACE BOX INTFC UNIT INTPH BOX INTRG ISOL VALVE BLOCK ISOLATOR


Date: 3 May 2000

AIRBUS INDUSTRIE

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F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) JACK JACK PANEL JET LIGHT JET PUMP JOYSTICK JUNCTION JUNCTION BOX

Form to be Used (Funct. Designations, Placards, etc.) JACK JACK PNL JET LIGHT JET PUMP JOYSTICK JUNCTION JUNCTION BOX

REMARKS


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) KEEL BEAM KEYBOARD

Form to be Used (Funct. Designations, Placards, etc.) KEEL BEAM KEYBOARD

REMARKS Tech Pubs only


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) LAMP LANDING GEAR CONTROL AND INTERFACE UNIT LATCH LAVATORY LEAD LEADING EDGE LEG LEVER LEVER ASSY LIFE VEST LIFT AND REST BLOCK LIGHT LIGHT BARRIER LIGHTBOARD LIGHT PANEL LIGHT UNIT LIMIT SWITCH LIMITATION UNIT LIMITER LINEAR ACCELEROMETER LINEAR VARIABLE DIFFERENTIAL TRANSDUCER LINE GEARBOX LINING LINK LINKAGE LIQUID CRYSTAL DISPLAY LOADER LOADMETER LOCAL AREA NETWORK HUB LOCK LOCK SPRING LOCK STAY LOGIC UNIT LOOP LOUD SPEAKER

Form to be Used (Funct. Designations, Placards, etc.) LAMP LGCIU LATCH LAVATORY LEAD LEADING EDGE LEG LEVER LEVER ASSY LIFE VEST LIF AND REST BLOCK LT LT BARRIER LTBOARD LT PNL LT UNIT LIM SW LIMITATION UNIT LIMITER LA LVDT

REMARKS


LINE GEARBOX LINING LINK LINKAGE LCD LOADER LOADMETER LAN HUB LOCK LOCK SPRING LOCK STAY LOGIC UNIT LOOP LOUD SPEAKER


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) MACHINE MAGNETIC LEVEL INDICATOR MAINTENANCE & RECORDING INTERFACE UNIT MAINTENANCE TEST PANEL MANAGEMENT PANEL MANAGEMENT UNIT MANIFOLD MANIFOLD ASSEMBLY MANUAL SELECTOR MANUAL SELECTOR VALVE MASK MASTER CYLINDER MASTER SWITCH MASTER VALVE MEGAPHONE MEMORIZED FAULT ANNUNCIATOR MEMORY MODULE MICROPHONE MICROSWITCH MICROSWITCH UNIT MIRROR MIXER MIXER UNIT MODEM PROCESSOR UNIT MODE SELECTOR UNIT MODULATION UNIT MODULE MONITOR MONITORING UNIT MOTOR MOTOR ASSEMBLY MOTOR CONVERTER MOUNT MOUNTING ADAPTER MOUNTING TRAY MOUNTING TRAY ENGINE MUFFLER MULTIPURPOSE CONTROL & DISPLAY UNIT MULTIPLEXER MULTIPURPOSE DISK DRIVE UNIT

Form to be Used (Funct. Designations, Placards, etc.) MACHINE MLI MRIU

REMARKS

MTP MGT PNL MU MANIFOLD MANIFOLD ASSEMBLY MAN SEL MAN SEL VALVE MASK MASTER CYL MASTER SW MASTER VALVE MEGAPHONE MFA MEMORY MODULE MIC MSW MSW UNIT MIRROR MIXER MIXER UNIT MODEM PROCESSOR UNIT MSU MODULATION UNIT MODULE MONITOR MONITORING UNIT MOTOR MOTOR ASSY MOTOR CONV MOUNT MTG ADPTR MTG TRAY MTG TRAY ENG (MTE) MUFFLER MCDU

Tech Pubs only

MUX MDDU


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) NAVIGATION DISPLAY NET NIPPLE NOZZLE

Form to be Used (Funct. Designations, Placards, etc.) ND NET NIPPLE NOZZLE

REMARKS


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) ON BOARD REPLACEABLE MODULE OPTICAL DISPLAY UNIT OPTICAL HEAD UNIT OUTLET OVEN OVERPRESSURE DOOR OVERSPEED PROTECTION UNIT

Form to be Used (Funct. Designations, Placards, etc.) OBRM

REMARKS

ODU OHU OUTLET OVEN OVERPRESSURE DOOR OPU


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) PACK PALLET STOP PARAVISUAL DISPLAY PARAVISUAL INDICATOR PARTITION PASSENGER CONTROL UNIT PASSENGER SERVICE/INFORMATION UNIT PASSENGER SERVICE UNIT PELMET PERMANENT MAGNET ALTERNATOR PHOTOLUMINESCENT STRIP PHOTORESISTOR PICKUP PILOT VALVE PINION ASSEMBLY PINTLE PIN PITCH ATTITUDE SENSOR PITCH TRIMMER PLACARD PLATE PLENUM CHAMBER PLUG PLUNGING JOINT PORT POSITION PICKOFF UNIT POSITION SWITCH POSITION TRANSDUCER POTENTIOMETER POWER CONTROL UNIT POWER PACK POWER SUPPLY DECOUPLING UNIT POWER SUPPLY UNIT POWER TRANSFER UNIT POWER UNIT PRECOOLER PRESELECTOR PRESSURE GAGE PRESSURE REDUCER PRESSURE SEAL PRESSURE SWITCH PRESSURE TRANSDUCER

Form to be Used (Funct. Designations, Placards, etc.) PACK PALLET STOP PVD PVI PARTITION PAX CTL UNIT PSIU

REMARKS

Tech Pubs only

Tech Pubs only

PSU PELMET PMA PHOTOLUMINESCENT STRIP PHOTORESISTOR PICKUP PILOT VALVE PINION ASSY PINTLE PIN PAS PITCH TRIMMER PLACARD PLATE PLENUM CHAMBER PLUG PLUNGING JOINT PORT PPU POS SW POS XDCR POT PCU POWER PACK PSDU POWER SUPPLY UNIT PTU POWER UNIT PRECOOL PRESEL PRESS GAGE PRESS REDUCER PRESS SEAL PRESS SW PRESS XDCR Page: F - 24

Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) PRESSURIZATION UNIT PRIMARY FLIGHT DISPLAY PRINTED CIRCUIT BOARD PRINTER PRIORITY VALVE PROBE PROBE HEAT COMPUTER PROJECTOR PROTECTION UNIT PROPULSION MULTIPLEXER PROTECTOR PROXIMITY DETECTOR PROXIMITY SENSOR PROXIMITY SWITCH PUMP PUSHBUTTON SWITCH

Form to be Used (Funct. Designations, Placards, etc.) PRESS UNIT PFD PCB PRINTER PRIORITY VALVE PROBE PHC PROJECTOR PROTECTION UNIT PMUX PROTECTOR PROX DET PROX SENSOR PROX SW PUMP P/BSW

REMARKS


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) QUADRANT QUICK ACCESS RECORDER

Form to be Used (Funct. Designations, Placards, etc.) QUADRANT QAR

REMARKS ATB only


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) RACK RADIO FREQUENCY UNIT RADIO MAGNETIC INDICATOR RADIO MANAGEMENT PANEL RADOME RAM AIR TURBINE RANDOM ACCESS DIGITAL VIDEO REPRODUCER RATE GYRO RATE GYRO UNIT RATE OF TURN UNIT READER RECEIVER RECEIVER PROCESSOR UNIT RECEPTACLE RECORDER RECTIFIER REDUCER REFRIGERATION UNIT REFRIGERATOR REGULATOR REHEATER RELAY RELAY BOX RELIEF VALVE REMINDER UNIT REMOTE CHARGE CONVERTER REMOTE CONTROL CIRCUIT BREAKER REPRODUCER RESERVOIR RESISTOR REST BLOCK RESTRICTOR RESTRICTOR VALVE RETAINER RETAINING RING RETRACTION MECHANISM RHEOSTAT RIB ROD ROLLER ROLLER ASSEMBLY ROLLER BLIND

Form to be Used (Funct. Designations, Placards, etc.) RACK RFU RMI RMP RADOME RAT RADVR

REMARKS

RATE GYRO RATE GYRO UNIT RATE OF TURN UNIT READER RECEIVER RPU RCPT RCDR RECTIFIER REDUCER REFRIGERATION UNIT REFRIGERATOR REGULATOR REHEATER RELAY RELAY BOX RELIEF VALVE REMINDER UNIT RCC RCCB REPRODUCER RSVR RESISTOR REST BLOCK RESTRICTOR RESTRICTOR VALVE RETAINER RETAINING RING RETRACTION MECHANISM RHEOSTAT RIB ROD ROLLER ROLLER ASSY ROLLER BLIND

Tech Pubs only


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) ROLLER TRACK ROTARY VARIABLE DIFFERENTIAL TRANSDUCER ROTOR RUDDER

Form to be Used (Funct. Designations, Placards, etc.) ROLLER TRACK RVDT

REMARKS Tech Pubs only

ROTOR RUDDER


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) SAFETY VALVE SATELLITE DATA UNIT SCREEN SCREWJACK SCUFF PLATE SEAL SEAT SEAT TRACKS SEAT ELECTRONIC BOX SELCAL CODE PANEL SELECTION PANEL SELECTION UNIT SELECTOR SELECTOR SWITCH SELECTOR VALVE SELF SEALING COUPLING SENSING ELEMENT SENSOR SEPARATOR SEQUENCE VALVE SEQUENCER SERVER SERVICE PANEL SERVICE UNIT SERVO ACTUATOR SERVO CONTROL SERVO MECHANISM SERVOVALVE SHAFT SHIELD SHOCK ABSORBER SHOCKMOUNT SHROUD SHUNT SHUTOFF VALVE SHUTTLE VALVE SIDE STAY SIDE STICK ASSEMBLY SIDE STICK TRANSDUCER UNIT SIDEWALL PANEL SIGHT GLASS SIGHT GLASS SIGN SIGNAL CONDITIONER SKIN

Form to be Used (Funct. Designations, Placards, etc.) SAFETY VALVE SDU SCREEN SCREWJACK SCUFF PLATE SEAL SEAT SEAT TRACKS SEB SELCAL CODE PANEL SEL PNL SEL UNIT SEL SEL SW SEL VALVE SELF SEALING CPLG SNSG ELEM SENSOR SEPARATOR SEQUENCE VALVE SEQUENCER SERVER SERVICE PANEL SERVICE UNIT SERVO ACTR SERVO CTL SERVO MECHANISM SERVOVALVE SHAFT SHIELD SHOCK ABSORBER SHOCKMOUNT SHROUD SHUNT SOV SHUTTLE VALVE SIDE STAY SIDE STICK ASSY STTU SIDEWALL PNL SIGN SIGNAL CONDTR SKIN

REMARKS

Tech Pubs only

ATB only



Tech Pubs only Page: F - 29

Issue: F

Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) SKIN PANEL SKIN PLATES SLAT/FLAP CONTROL COMPUTER SLIDE SLIDING UNION SMOKE DETECTION CONTROL UNIT SOCKET SOFTWARE SOLENOID SOLENOID VALVE SPAR SPAR BOX SPARK IGNITER SPHERICAL BEARING SPOILER SPOILER ELEVATOR COMPUTER SPRING ROD STAIRCASE HOUSING STARTER STATIC INVERTER STEADY BEARING STEADY BEARING ASSEMBLY STICK SHAKER STIFFENERS STOWAGE STOWAGE BOX STRAINER STRAP STRIKE STRINGER STRINGERS & SKIN STRIP STRUT SUNVISOR SUPPORT SUPPORT FITTING SUPPORT STRUTS SUSPENSION SWITCH SWITCH PANEL SWITCH UNIT

Form to be Used (Funct. Designations, Placards, etc.) SKIN PANEL SKIN PLATES SFCC

REMARKS Tech Pubs only Tech Pubs only

SLIDE SLIDING UNION SDCU SOCKET SOFTWARE SOLENOID SOL VALVE SPAR SPAR BOX SPARK IGNITER SPHERICAL BEARING SPOILER SEC SPRING ROD STAIRCASE HOUSING STARTER STAT INV STEADY BRG STEADY BRG ASSY STICK SHAKER STIFFENERS STOWAGE STOWAGE BOX STRAINER STRAP STRIKE STRINGER STRINGERS & SKIN STRIP STRUT SUNVISOR SUPPORT SUPPORT FITTING SUPPORT STRUTS SUSPENSION SW SW PNL SW UNIT

ATB only ATB only

ATB only

Tech Pubs only ATB only Tech Pubs only

Tech Pubs only ATB only Tech Pubs only


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) SWITCHING UNIT SYMBOL GENERATOR UNIT SYSTEM DATA ACQUISITION CONCENTRATOR SYSTEM DATA ANALOG CONVERTER SYSTEM ISOLATION CONTACTOR

REMARKS

Form to be Used (Funct. Designations, Placards, etc.) SWITCHING UNIT SGU SDAC

A320

SDAC

A310

SIC


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) TABLE TACHOMETER TAIL CONE TANK TAPE REPRODUCER TAPPING REPEATER UNIT TAPPING UNIT TELEPHONE TELEPHONY BOX TELESCOPIC DUCT TENSION REGULATOR TERMINAL TERMINAL BLOCK TEST PANEL TEST PORT TEST UNIT THERMAL FUSE THERMAL SWITCH THERMOCOUPLE THERMOCOUPLE RAKE THERMOSTAT THROTTLE VALVE THRUST CONTROL COMPUTER THRUST RATING PANEL TIMER TIP TIRE TIRE PRESSURE INDICATING COMPUTER TOILET TOOL KIT TORQUE LIMITER TORQUE LINK TORQUE MOTOR TORQUE SHAFT TORQUE SHAFT ASSEMBLY TRACK TRAILING EDGE TRANSCEIVER TRANSDUCER TRANSDUCER UNIT TRANSFORMER TRANSFORMER RECTIFIER TRANSMITTER

Form to be Used (Funct. Designations, Placards, etc.) TABLE TACHOMETER TAIL CONE TK TAPE RPDR TAPPING REPEATER UNIT TAPPING UNIT TELEPHONE TELEPHONY BOX TELESCOPIC DUCT TENSION REG TERMINAL TERMINAL BLOCK TEST PANEL TEST PORT TEST UNIT THERMAL FUSE THRM SW THERMOCOUPLE THERMOCOUPLE RAKE THERMOSTAT THROTTLE VALVE TCC TRP TIMER TIP TIRE TPIC TOILET TOOL KIT TORQUE LIMITER TORQUE LINK TORQUE MOTOR TORQUE SHAFT TORQUE SHAFT ASSY TRACK TRAILING EDGE XCVR XDCR XDCR UNIT XFMR TR XMTR

REMARKS

Tech Pubs only

Tech Pubs only

Tech Pubs only

Landing gear

Tech Pubs only


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) TRANSMITTER UNIT TRANSPONDER TRIMMER TRUNCHEON TUBE TUBING TUNER TURBINE TURBOFAN TURNBUCKLE LINK

Form to be Used (Funct. Designations, Placards, etc.) XMTR UNIT XPDR TRIMMER TRUNCHEON TUBE TUBING TUNER TURBINE TURBOFAN TURNBUCKLE LINK

REMARKS

Tech Pubs only


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) UPLOCK ASSEMBLY UPLOCK MECHANISM

Form to be Used (Funct. Designations, Placards, etc.) UPLOCK ASSY UPLOCK MECHANISM

REMARKS


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) V BAND CLAMP VALVE VALVE BLOCK VAPOR SEAL VENT VENT PROTECTOR VENT TUBE VENT VALVE VENTILATION UNIT VERTICAL SPEED INDICATOR VIBRATION ISOLATOR VIDEO CONTROL CENTER VOLTMETER

Form to be Used (Funct. Designations, Placards, etc.) V BAND CLAMP VALVE VALVE BLOCK VAPOR SEAL VENT VENT PROTECTOR VENT TUBE VENT VALVE VENTILATION UNIT VSI VIBRATION ISOLATOR VIDEO CONTROL CENTER VOLTMETER

REMARKS


Date: 3 May 2000

ABD0036


F - NON STANDARD ITEMS (Functional Designations) MAIN WORD In full (for reference) WATER ICE PROTECTION DATA UNIT WARNING LIGHT WARNING LIGHT DISPLAY PANEL WASTE BOX WAVE GUIDE WAVE GUIDE ASSEMBLY WEIGHT AND BALANCE COMPUTER WHEEL WINDOW HEAT COMPUTER WINDOW WINDSHIELD GUIDANCE DISPLAY COMPUTER WINDSHIELD WING TIP BRAKE

Form to be Used (Funct. Designations, Placards, etc.) WIPDU WARN LT WLDP

REMARKS

Rectangular red lights

WASTE BOX WAVE GUIDE WAVE GUIDE ASSY WBC WHEEL WHC WINDOW WGDC WINDSHIELD WTB


Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


G - (INTENTIONALLY LEFT BLANK)

Page: G - 1 Issue: F

Date: 3 May 2000

AIRBUS INDUSTRIE

ABD0036


H - TOOLS AND TEST EQUIPMENT STANDARD MAIN WORDS Ref: * ABD0024 – Aircraft MFR - Tool and Test Equipment

Page: H - 1 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming Issue/Revision Approval Sheet - Engineering Standardization Board - Members: Name and Signature

ISSUE

A

B

C

D

E

F

DATE

Nov 25/87

Jan 26/88

Nov 30/88

Jan 15/92

Sep 28/95

May 00

Aerospatiale

M. JAMMY Signed

-

M. JAMMY Signed

F. PICARD Signed

JM. THOMAS Signed

J. ALCOUFFE Signed

BELAIRBUS-SONACA

-

-

-

V. MUNGRE Signed

P. GERBOVITS Signed

P. GERBOVITS Signed

British Aerospace

SJ. SWADLING Signed

-

SJ. SWADLING Signed

JA. JUPP Signed

TG. CHAMBERS Signed

E. SMITH Signed

CASA

F. CASTRO Signed

-

K. SCHLEICHER Signed




H. HORSTKEMPER

H. HORSTKEMPER

Signed

Signed

H. STEINBECK Signed

H. STEINBECK Signed

K. THOMAS Signed

DA FOKKER Airbus Industrie

D. KNOSPE Signed

-

D. KNOSPE Signed

W. DIDSZUHN Signed

W. DIDSZUHN Signed

G.THOMAS Signed

Standardization Board Chairman

D. KNOSPE Signed

-

D. KNOSPE Signed

JP. SAINT-GIRONS

W. SCHNEIDER Signed

Y. LEGALL Signed

Signed

In signing this document, the Members and Associated Partners of Airbus Industrie commit themselves to follow in their work on Airbus Industrie aircraft the Rules which are set out in this ABD. Changes to this procedure and/or improvements have to be authorized by Airbus Industrie in agreement with the Partners and issued by Airbus Industrie in agreement with the Members and issued by Airbus Industrie, except for those changes in the areas provided for domestic requirements.


Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming Issue/Revision Approval Sheet - Task Force 7- Members: Name and Signature

ISSUE

A

B

C

D

E

F

DATE

Nov 25/87

Jan 26/88

Nov 30/88

Jan 15/92

Sep 28/95

May 3/00

Aerospatiale

D. NOWACZYK Signed

-

D. NOWACZYK Signed

JM. BUZZETTI Signed

JM. BUZZETTI Signed

M. BAYONNE Signed

British Aerospace

JP. BOTTEREL Signed

-

JP. BOTTEREL Signed

J. TONGE Signed

J. TONGE Signed

G. LONSDALE Signed

CASA

J. LLORENTE Signed

-

J. LLORENTE Signed

J. LLORENTE -

F. LOPEZ BENITO

P. CONESA-LOPEZ

Signed

Signed

DA

JP. BURGARD Signed

-

JP. BURGARD Signed

JP. BURGARD Signed

J. Mc CARTNEY Signed

J. Mc CARTNEY Signed

BELAIRBUS-SONACA

-

-

-

-

-

Airbus Industrie

A. QUESNEY Signed

-

A. QUESNEY Signed

A. QUESNEY Signed

R. ASCOUGH Signed

T. HOLLINGWORTH

Task Coordinator

K. BARTHE Signed

-

K. BARTHE Signed

K. BARTHE Signed

K. BARTHE Signed

K. BARTHE Signed

WG1 Chairman

P. BRUNET Signed

-

P. BRUNET Signed

P. BRUNET Signed

P. BRUNET Signed

TF7 CHAIRMAN Signed

TF1M Chairman

K.L. SHAW Signed

-

K.L. SHAW Signed

E. SMITH Signed

E. SMITH Signed

Standardization Board Executive Secretary

A. QUESNEY Signed

-

A. QUESNEY Signed

A. QUESNEY Signed

K. HANCOCK Signed

FOKKER

Signed

S SILVERTHORN Signed

Note: When replacing earlier Signature Pages, indicate the Name and Signed at the level of the relevant Issue Index/Date. Page: 0 - 2 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming Record Of Revisions EFFECT ON ISSUE

DATE

REASON FOR REVISION PAGE

PARAGRAPH

A

Nov 25/87

Basic issue.

B

Jan 26/88

Editorial Revision.

C

Nov 30/88

Completion of chapters 8, thru 17. Update of Appendix D.

D

Jan15/92

- Foreword: added. - Wording improvements. - Cancellation of duplicated instruction. - Appendices: replaced by catalogs • Sequence: rearranged • Introduction: added

E

Sep 28/95

All

F

May 3/00

All

Full updating and revision. Full updating and revision.

Page: ROR - 1 Issue: F

Date: 3 May 2000

ABD0036

AIRBUS INDUSTRIE Numbering/Naming List of Effective Pages Page

Issue

Page

Issue

Page

Issue

TOC-1 TOC-2 TOC-3 TOC-4

F F F F

12-1 12-2 12-3

F F F

13-1

F

0-1

F 14-1

F

1-1 1-2

F F

15-1

F

2-1 2-2

F F

16-1

F

17-1

F

3-1

F F F F F F F F F F F F

F F

F F F F F F F F F F F F F F F

4-1 4-2 4-3 4-4 4-6 4-7 4-8 4-9 4-10 4-11 4-12

FW-1 FW-2

F-22 F-23 F-24 F-25 F-26 F-27 F-28 F-29 F-30 F-31 F-32 F-33 F-34 F-35 F-36 G-1

F

A-1

F H-1

F

B-1 B-2 B-3 B-4 B-5 B-6

F F F F F F

0-1 0-2

F F

ROR-1

F

LEP-1

F

C-1 C-2 C-3

F F F

5-1 5-2

F F

6-1 6-2 6-3 6-4 6-5 6-8 6-9 6-10

F F F F F F F F

D-1 D-2 D-3

F F F

E-1 E-2 E-3 E-4

F F F F

7-1

F

8-1

F

9-1

F

10-1 10-2

F F

11-1

F

F-1 F-3 F-4 F-6 F-7 F-8 F-9 F-10 F-11 F-12 F-13 F-14 F-21

F F F F F F F F F F F F F

Page

Issue

Page

Issue

Page: LEP - 1 Issue: F

Date: 3 May 2000

ABD0036_F.pdf

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