Règlement grand-ducal du 10 mars 2014 sur le certificat de qualification des entreprises exploitant des entraîneurs synthétiques de vol pour avions et hélicoptères.

Règlement grand-ducal du 10 mars 2014 sur le certificat de qualification des entreprises exploitant

des entraîneurs synthétiques de vol pour avions et hélicoptères.

Nous Henri, Grand-Duc de Luxembourg, Duc de Nassau,

Vu le règlement (CE) n° 216/2008 modifié du Parlement européen et du Conseil du 20 février 2008 concernant des

règles communes dans le domaine de l’aviation civile et instituant une Agence européenne de la sécurité aérienne, et

abrogeant la directive 91/670/CEE du Conseil, le règlement (CE) n° 1592/2002 et la directive 2004/36/CE;

Vu le règlement (UE) n° 1178/2011 modifié de la Commission du 3 novembre 2011 déterminant les exigences

techniques et les procédures administratives applicables au personnel navigant de l’aviation civile conformément au

règlement (CE) n° 216/2008 du Parlement européen et du Conseil;

Vu la loi modifiée du 31 janvier 1948 relative à la réglementation de la navigation aérienne;

Vu la loi modifiée du 19 mai 1999 ayant pour objet a) de règlementer l’accès au marché de l’assistance en escale à

l’aéroport de Luxembourg; b) de créer un cadre réglementaire dans le domaine de la sûreté de l’aviation civile et, c)

d’instituer une Direction de l’Aviation Civile;

Vu les codes JAR-FSTD (A) – Aeroplane Flight Simulation Training Devices et JAR-FSTD (H) – Helicopter Flight

Simulation Training Devices édictés en date du 1er mai 2008 par les Autorités Conjointes de l’Aviation (JAA: Joint

Aviation Authorities);

Vu les documents administratifs et d’orientation des JAA; Section Six: Entraîneurs synthétiques de vol (FSTD) publiés

en date du 1er février 2008;

Vu l’article 2 (1) de la loi du 12 juillet 1996 portant réforme du Conseil d’Etat et considérant qu’il y a urgence;

Sur le rapport de Notre Ministre du Développement durable et des Infrastructures et après délibération du

Gouvernement en Conseil;

Arrêtons

Champ d’application

Le présent règlement grand-ducal s’applique aux entreprises qui exploitent des entraîneurs synthétiques de vol pour

avions et hélicoptères sur le territoire du Grand-Duché de Luxembourg, dénommées ci-après «les exploitants». Sans

préjudice notamment d’autres conditions complémentaires, techniques, économiques ou sociales qui peuvent exister

par ailleurs, le règlement prescrit les conditions techniques applicables aux exploitants, énoncées dans les codes JAR-

FSTD (A) et JAR-FSTD (H).

Les codes JAR-FSTD (A) et JAR-FSTD (H) figurent à l’annexe I respectivement à l’annexe II du présent règlement

et en font partie intégrante.

Modalités et conditions d’obtention du certificat de qualification des exploitants d’entraîneurs

synthétiques de vol pour avions et hélicoptères

Pour l’exercice de leurs activités de simulation de vol, les exploitants désignés à l’article 1er doivent être titulaires

d’un certificat de qualification les autorisant à pratiquer la simulation de vol, délivré par la Direction de l’Aviation Civile

(DAC) en conformité avec les dispositions afférentes des codes JAR-FSTD (A) et JAR-FSTD (H).

Les codes JAR-FSTD (A) et JAR-FSTD (H) régissent l’octroi et le renouvellement du certificat de qualification ainsi

que l’extension de son champ d’application.

L’octroi du certificat autorisant la pratique de la simulation de vol est soumis en particulier à la condition que

l’exploitant ait nommé un dirigeant responsable ainsi qu’un responsable qualité conformément au paragraphe A.025 du

code JAR-FSTD (A) pour les entraîneurs synthétiques de vol pour avions respectivement au paragraphe H.025 du code

JAR-FSTD (H) pour les entraîneurs synthétiques de vol pour hélicoptères.

Les responsables en question doivent être agréés par la DAC.

Les conditions d’obtention d’un certificat de qualification permettant la pratique de la simulation de vol sont régies

par le paragraphe A.030. du code JAR-FSTD (A) pour les entraîneurs synthétiques de vol pour avions ainsi que par le

paragraphe H.030. du code JAR-FSTD (H) pour les entraîneurs synthétiques de vol pour hélicoptères.

Durée de validité du certificat de qualification

La durée de validité du certificat de qualification initial autorisant à pratiquer les activités de simulation de vol est

d’une année. Le certificat peut être prolongé d’année en année sur demande expresse de l’exploitant. Les modalités

entourant cette durée de validité sont régies par le paragraphe A.020 du code JAR-FSTD (A) pour les entraîneurs

synthétiques de vol pour avions ainsi que par le paragraphe H.020 du code JAR-FSTD (H) pour les entraîneurs

synthétiques de vol pour hélicoptères.

Retrait du certificat de qualification

La DAC peut prononcer le retrait temporaire ou définitif du certificat de qualification autorisant à pratiquer les

activités de simulation de vol ou limiter le domaine d’activité du titulaire du certificat, notamment lorsque

a) les conditions régissant l’octroi du certificat de qualification autorisant à pratiquer les activités de simulation de

vol ne sont plus remplies;

b) des dispositions qui s’avèrent déterminantes pour l’octroi du certificat de qualification ont été violées de manière

grave ou répétée;

c) l’accès à l’entreprise de l’exploitant est interdit à la DAC ainsi qu’aux services compétents désignés à l’article 7

ci-après, ou que l’exploitant refuse de fournir à la DAC les documents requis pour contrôler l’application des

dispositions du présent règlement et des codes JAR-FSTD (A) et JAR-FSTD (H).

Dispositions techniques

Le ministre peut, sur proposition de la Direction de l’aviation civile et dans le but d’assurer un maniement adéquat

des entraîneurs synthétiques de vol pour avions ou hélicoptères, édicter sous forme d’un règlement des instructions

ou des directives qui s’adressent aux exploitants et qui ont pour objet de soumettre à certaines conditions, limiter,

voire interdire certaines opérations.

Ces dispositions techniques énoncent les motifs justifiant leur diffusion et précisent leur champ d’application. Ils

indiquent les mesures que doivent prendre les exploitants pour leur application et complètent les dispositions des

codes JAR-FSTD (A) et JAR-FSTD (H).

Exceptions

Dans des cas dûment motivés, la DAC peut, à titre exceptionnel et provisoire, accorder des dérogations aux

dispositions des codes JAR-FSTD (A) et JAR-FSTD (H) lorsqu’elle estime que le besoin existe, notamment pour

prévenir les cas de rigueur et, sous réserve du respect de toute condition supplémentaire qu’elle considère comme

nécessaire, pour assurer, dans ces cas particuliers, un niveau d’opération jugé équivalent.

Vérifications et surveillance

La DAC peut effectuer les vérifications et la surveillance qu’elle juge nécessaires pour l’application du présent

règlement. Elle peut également, en cas de besoin, avoir recours à cet effet à des organismes spécialisés habilités à cet

effet.

Dispositions transitoires

La DAC peut, en fonction de la complexité technique, fixer à chaque exploitant un délai dans lequel ce dernier doit

adapter son exploitation et son règlement interne aux dispositions du présent règlement. Ce délai ne peut pas dépasser

un an à partir de la date d’entrée en vigueur du présent règlement.

Les règlements internes en usage auprès des exploitants au moment de l’entrée en vigueur du présent règlement

restent en vigueur jusqu’à leur remplacement par de nouveaux règlements internes.

Les autorisations anciennes délivrées uniquement sur base des codes JAR-FSTD (A) et JAR-FSTD (H) sont réputées

avoir été délivrées en conformité avec les dispositions du présent règlement.

Disposition finale

Notre Ministre du Développement durable et des Infrastructures est chargé de l’exécution du présent règlement

qui sera publié au Mémorial.

Le Ministre du Développement durable

Château de Berg, le 10 mars 2014.

et des Infrastructures,

Henri

François Bausch

Annexe I

Code JAR-FSTD (A) – Entraîneurs synthétiques de vol pour avions

Annexe II

Code JAR – FSTD (H) – Entraîneurs synthétiques de vol pour hélicoptères

Joint

Aviation

Requirements

JAR–FSTD A

Aeroplane Flight Simulation

Training Devices

Joint Aviation Authorities

Annexe I

Code JAR-FSTD (A) – Entraîneurs synthétiques de vol pour avions

Printed and distributed by Global Engineering Documents, 15 Inverness Way East, Englewood, Colorado 80112, U S A on behalf of the Joint Aviation Authorities

Committee.

Joint

Aviation

Requirements

JAR–FSTD A

Aeroplane Flight Simulation

Training Devices

Initial issue

1 May 2008

All rights reserved

01.05.08

ii

The members of the Joint Aviation Authorities Committee are representatives of the Civil Aviation

Authorities of the countries that have signed the ‘Arrangements Concerning the Development and the

Acceptance of Joint Aviation Requirements’. A list of these countries is kept by European Civil Aviation

Conference, 3 bis Villa Emile Bergerat, 92522 NEUILLY SUR SEINE Cedex, France.*

Further copies of the Joint Aviation Requirements can be purchased from Information Handling Services

(IHS), whose world-wide offices are listed on the JAA website (www.jaa.nl) and IHS website

(www.global.ihs.com)

For electronic versions of Joint Aviation Authorities Documents please refer to the website of Information

Handling Services (IHS) on www.ihsaviation.com, where you will find information on how to order.

Enquiries regarding the contents should be addressed to the JAA, Saturnusstraat 40-44, PO Box 3000,

2130 KA HOOFDDORP, The Netherlands (publications@jaat.eu).

*These countries are

Albania, Armenia, Austria, [Azerbaijan], Belgium, Bosnia and Herzegovina, Bulgaria, Croatia, Cyprus,

Czech Republic, Denmark, Estonia, European Aviation Safety Agency, Finland, Former Yugoslav Republic

of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg,

Malta, Monaco, Netherlands, Norway, Poland, Portugal, Republic of Moldova, [Republic of Georgia],

Romania, Serbia, Slovak Republic, Slovenia, Spain, Sweden, Switzerland, Turkey, Ukraine, & United

Kingdom

JAR-FSTD A

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CONTENTS (general layout)

JAR–FSTD A

AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

FOREWORD

CHECK LIST OF PAGES

PREAMBLE

SECTION 1 – REQUIREMENTS

SUBPART A

APPLICABILITY

SUBPART B

GENERAL

SUBPART C

AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)

ACJ B

GENERAL

ACJ C

AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

JAR-FSTD A

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CONTENTS (details)

JAR–FSTD A

AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

Paragraph

Page

SECTION 1 – REQUIREMENTS

General and Presentation

1-0-1

SUBPART A – APPLICABILITY

JAR–FSTD A.001

Applicability

1-A-1

SUBPART B – GENERAL

JAR–FSTD A.005

Terminology

1-B-1

SUBPART C – AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

JAR–FSTD A.015

Application for FSTD Qualification

1-C-1

JAR–FSTD A.020

Validity FSTD Qualification

1-C-1

JAR–FSTD A.025

Rules governing FSTD Operators

1-C-1

JAR–FSTD A.030

Requirements for FSTDs qualified on or after

1-C-2

1 August 2008

JAR–FSTD A.031

Requirements for FFSs qualified on or after

1-C-3

1 April 1998 and before 1 August 2008

JAR–FSTD A.032

Requirements for FTDs qualified on or after 1 July 2000

1-C-3

and before 1 August 2008

JAR–FSTD A.033

Requirements for FNPTs qualified on or after 1 July 1999

1-C-3

and before 1 August 2008

JAR–FSTD A.034

Requirements for BITD qualified on or after 1 January 2003

1-C-3

and before 1 August 2008

JAR–FSTD A.035

Requirements for FFSs approved or qualified

1-C-3

before 1 April 1998

JAR–FSTD A.036

Requirements for FTDs approved or qualified

1-C-4

before 1 July 2000

JAR–FSTD A.037

Requirements for FNPTs approved or qualified

1-C-4

before 1 July 1999

JAR–FSTD A.040

Changes to qualified FSTDs

1-C-4

JAR–FSTD A.045

Interim FSTD Qualification

1-C-5

JAR–FSTD A.050

Transferability of FSTD Qualification

1-C-5

Appendix 1 to

FSTD Standards

1-C-7

JAR–FSTD A.030

JAR-FSTD A

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SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)

General and Presentation

2-0-1

ACJ B – GENERAL

ACJ FSTD A.005

Terminology, Abbreviations

2-B-1

ACJ C – AEROPLANE FSTDS

ACJ No. 1 to

FSTD Qualification – Application and Inspection

2-C-1

JAR- FSTD A.015

ACJ No. 2 to

FSTD Evaluations

2-C-6

JAR- FSTD A.015

ACJ FSTD A.020

Validity of an FSTD Qualification

2-C-10

ACJ No. 1 to

Quality System

2-C-10

JAR- FSTD A.025

ACJ No. 2 to

BITD Operators Quality System

2-C-17

JAR-FSTD A.025

ACJ No. 3 to

Installations

2-C-18

JAR-FSTD A.025

ACJ No. 1 to

FSTDs qualified on or after 1 August 2008

2-C-19

JAR-FSTD A.030

Appendix 1 to ACJ No. 1 Validation Test Tolerances

2-C-112

to JAR-FSTD A.030

Appendix 2 to ACJ No. 1 Validation Data Roadmap

2-C-114

to JAR-FSTD A.030

Appendix 3 to ACJ No. 1 Data Requirements for Alternate Engines

2-C-116

to JAR-FSTD A.030

Appendix 4 to ACJ No. 1 Data Requirements for Alternate Avionics

2-C-118

to JAR-FSTD A.030

Appendix 5 to ACJ No. 1 Transport Delay Testing Method

2-C-119

to JAR-FSTD A.030

Appendix 6 to ACJ No. 1 Recurrent Evaluations – Validation Test Data Presentation

2-C-122

to JAR-FSTD A.030

Appendix 7 to ACJ No 1

Applicability

2-C-123

to JAR-FSTD A.030

Appendix 8 to ACJ No 1

General technical Requirements for FSTD Qualification

2-C-125

JAR–FSTD A.030

Levels

ACJ No. 2 to

Guidance on Design and Qualification of Level “A”

2-C-130

JAR-FSTD A.030

Aeroplane FFSs

ACJ No. 3 to

Guidance on Design and Qualification of FNPTs

2-C-132

JAR-FSTD A.030

ACJ No. 4 to

Guidance on Design and Qualification of BITDs

2-C-136

JAR-FSTD A.030

ACJ No.1 to

Engineering Simulator Validation Data

2-C-140

JAR-FSTD A.030(c)(1)

JAR-FSTD A

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Engineering Simulator Validation Data – Approved Guidelines

2-C-141

JAR-FSTD A.030(c)(1)

ACJ to FSTD A.035

FFS Approved or Qualified before 1 April 1998

2-C-143

ACJ to FSTD A.036

FTD Approved or Qualified before 1 July 2000

2-C-145

ACJ to FSTD A.037

FNPT Approved or Qualified before 1 July 1999

2-C-146

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FOREWORD

The Civil Aviation Authorities of certain European countries have agreed common comprehensive

and detailed aviation requirements, referred to as Joint Aviation Requirements (JARs), with a view

to minimising Type Certification problems on joint ventures, to facilitate the export and import of

aviation products, to make it easier for maintenance carried out in one European country to be

accepted by the Civil Aviation Authority in another European country and to regulate commercial

air transport operations.

JARs are recognised by the Civil Aviation Authorities of participating countries as an acceptable

basis for showing compliance with their national codes.

The content has been prepared using the expertise available in this field as well as the ICAO

Document 9625, the ‘Manual for the Qualification of Flight Simulators’ and added to where

necessary by making use of existing European regulations and the Federal Aviation Requirements

of the United States of America where acceptable.

JAR–FSTD A is issued with no National Variants. It may be felt that the document does not

contain all of the detailed compliance and interpretative information which some Civil Aviation

Authorities and Industry organisations would like to see. However, it is accepted that JAR–FSTD

A should be applied in practice and the lessons learned embodied in future amendments. The

Civil Aviation Authorities of the JAA are therefore committed to early amendment in the light of

experience.

Future development of the requirements of JAR–FSTD A, including the commitment in

Paragraph 4, will be in accordance with the JAA’s Notice of Proposed Amendment (NPA)

procedures. These procedures allow for the amendment of JAR–FSTD A to be proposed by any

organisation or person.

The Civil Aviation Authorities have agreed they should not unilaterally initiate amendment of their

national codes without having made a proposal for amendment of JAR–FSTD A in accordance

with the agreed procedure.

Definitions and abbreviations of terms used in JAR–FSTD A that are considered generally

applicable are contained in JAR–1, Definitions and Abbreviations. However, definitions and

abbreviations of terms used in JAR–FSTD A that are specific to a Subpart of JAR–FSTD A are

normally given in the Subpart concerned or, exceptionally, in the associated compliance or

interpretative material.

Amendments to the text in JAR–FSTD A are issued as Replacement Pages. These show an

effective date and have the same status and applicability as JAR–FSTD A from that date.

New, amended and corrected text will be enclosed within heavy brackets until a subsequent

‘Amendment’ is issued.

Comment/Response documents developed following Notices of Proposed Amendment (NPA)

consultation have been produced by the JAA and are published on the JAA Internet Site

www.jaa.nl. Readers can also apply to JAA for copies of specific Comment/Response Documents

as required.

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JAR-FSTD A - AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

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JAR-FSTD A

Paragraph

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JAR-FSTD A

P-1

01.05.08

PREAMBLE

JAR–FSTD A

Initial Issue

JAR–FSTD A comprises 3 Subparts (A, B and C) in Section 1, and 2 Subparts (B and C) in Section 2.

JAR-FSTD A is a simple amalgamation of JAR STD 1A, 2A, 3A and 4A into one document.

Section 1

Subpart C

Terminology and basic regulatory processes combined

Table of Standards in Appendix 1 to JAR-FSTD A.030 contains the standard for all devices

Section 2

Subpart B

Terminology and Abbreviations rationalised and harmonised with Aircraft STD standards documents.

Subpart C

Regulatory Processes combined.

Table of Objective Tests (ACJ to JAR-FSTD A.030) contains the testing requirements for all devices.

Table of Functions and Subjective Tests (ACJ to JAR-FSTD A.030) contains the testing requirements for all

devices.

JAR-FSTD A

01.05.08

P-2

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD A

1-0-1

01.05.08

SECTION 1 – REQUIREMENTS

GENERAL

1.1

This Section contains the requirements for aeroplane Flight Simulation Training Devices.

PRESENTATION

2.1

The requirements of JAR–FSTD A are presented in two columns on loose pages, each page

being identified by the date of issue and the Amendment number under which it is amended

or reissued.

2.2

Sub-headings are in italic typeface.

2.3

Explanatory Notes not forming part of the requirements appear in smaller typeface.

2.4

New, amended and corrected text will be enclosed within heavy brackets until a subsequent

‘Amendment’ is issued.

2.5

After each paragraph, the various changes and amendments, if any since the initial issue, are

indicated together with their date of issue.

JAR-FSTD A

SECTION 1

01.05.08

1-0-2

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SECTION 1

JAR–FSTD A

1-A-1

01.05.08

SUBPART A – APPLICABILITY

JAR–FSTD A.001 Applicability

JAR–FSTD A as amended applies to those persons,

organisations or enterprises (Flight Simulation Training

Devices (FSTD) operators) or, in the case of BITDs

only, manufacturers seeking initial qualification of

FSTDs.

The version of JAR-FSTD A agreed by the

Authority and used for issue of the initial qualification

shall be applicable for future recurrent qualifications of

the FSTD unless recategorised.

FSTD users shall also gain approval to use the

FSTD as part of their approved training programmes

despite the fact that the FSTD has been previously

qualified.

INTENTIONALLY LEFT BLANK

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JAR–FSTD A

SECTION 1

01.05.08

1-A-2

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SECTION 1

JAR-FSTD A

1-B-1

01.05.08

JAR–FSTD A.005 Terminology

(See ACJ to FSTD A.005)

Because of the technical complexity of FSTD

qualification, it is essential that standard terminology

is used throughout. The following principal terms and

abbreviations shall be used in order to comply with

JAR–FSTD (A). Further terms and abbreviations are

contained in ACJ to FSTD A.005.

(a)

Flight

Simulation

Training

Device

(FSTD). A training device which is a Full Flight

Simulator (FFS), a Flight Training Device (FTD), a

Flight & Navigation Procedures Trainer (FNPT) , or a

Basic Instrument Training Device (BITD).

(b)

Full Flight Simulator (FFS). A full size

replica of a specific type or make, model and series

aeroplane flight deck, including the assemblage of all

equipment and computer programmes necessary to

represent the aeroplane in ground and flight

operations, a visual system providing an out of the

flight deck view, and a force cueing motion system. It

is in compliance with the minimum standards for FFS

Qualification.

(c)

Flight Training Device (FTD). A full size

replica of a specific aeroplane type’s instruments,

equipment, panels and controls in an open flight deck

area or an enclosed aeroplane flight deck, including

the assemblage of equipment and computer software

programmes necessary to represent the aeroplane in

ground and flight conditions to the extent of the

systems installed in the device. It does not require a

force cueing motion or visual system. It is in

compliance with the minimum standards for a specific

FTD Level of Qualification.

(d)

Flight and Navigation Procedures Trainer

(FNPT). A training device which represents the

flight deck or cockpit environment including the

assemblage

of

equipment

and

computer

programmes necessary to represent an aeroplane or

class of aeroplane in flight operations to the extent

that the systems appear to function as in an

aeroplane. It is in compliance with the minimum

standards

for

a

specific

FNPT

Level

of

Qualification.

(e)

Basic Instrument Training Device (BITD). A

ground based training device which represents the

student pilot‘s station of a class of aeroplanes. It may

use screen based instrument panels and springloaded

flight controls, providing a training platform for at

least the procedural aspects of instrument flight.

(f)

Other Training Device (OTD). A training aid

other than FFS, FTD, FNPT or BITD which provides

for training where a complete flight deck environment

is not necessary.

(g)

Flight Simulation Training Device User

Approval (FSTD User Approval). The extent to which

an FSTD of a specified Qualification Level may be

used by persons, organisations or enterprises as

approved by the Authority. It takes account of

aeroplane to FSTD differences and the operating and

training ability of the organisation.

(h)

Flight Simulation Training Device Operator

(FSTD

operator). That

person,

organisation

or

enterprise directly responsible to the Authority for

requesting and maintaining the qualification of a

particular FSTD.

(i)

Flight Simulation Training Device User

(FSTD User). The person, organisation or enterprise

requesting training, checking and testing credits

through the use of an FSTD.

(j)

Flight

Simulation

Training

Device

Qualification (FSTD Qualification). The level of

technical ability of an FSTD as defined in the

compliance document.

(k)

BITD Manufacturer. That organisation or

enterprise being directly responsible to the Authority

for requesting the initial BITD model qualification.

(l)

BITD Model. A defined hardware and

software

combination,

which

has

obtained

a

qualification. Each BITD will equate to a specific

model and be a serial numbered unit.

(m)

Qualification

Test

Guide

(QTG). A

document

designed

to

demonstrate

that

the

performance and handling qualities of an FSTD agree

within prescribed limits with those of the aeroplane

and that all applicable regulatory requirements have

been met. The QTG includes both the aeroplane and

FSTD data used to support the validation.

INTENTIONALLY LEFT BLANK

SUBPART B - GENERAL

(JAR-FSTD A.005 continued)

JAR-FSTD A

SECTION 1

01.05.08

1-B-2

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SECTION 1

JAR-FSTD A

1-C-1

01.05.08

JAR–FSTD A.015 Application

for

FSTD

Qualification

(See ACJ No. 1 to JAR-

FSTD A.015)

(See ACJ No. 2 to JAR-

FSTD A.015)

(a) The FSTD operator requiring evaluation of a

FFS, FTD or FNPT shall apply to the Authority

giving 3 months notice. In exceptional cases this

period may be reduced to one month at the

discretion of the Authority.

(b) An FSTD Qualification Certificate will be

issued following satisfactory completion of an

evaluation of the FFS, FTD or FNPT by the

Authority.

(c) For BITDs the manufacturer of a new BITD

model which requires evaluation shall apply to the

Authority giving 3 months notice. In exceptional

cases this period may be reduced to one month at

the discretion of the Authority.

(d) A BITD Qualification Certificate will be issued

for the BITD model to the manufacturer following

satisfactory completion of an initial evaluation by

the Authority. This qualification certificate is valid

for any devices manufactured to this standard

without the need for the device to be subjected to

further technical evaluation. The BITD model must

clearly be identified by a BITD model number.

(e) The numbering of the BITD model must

clearly

define

the

hardware

and

software

configuration of the qualified BITD model. A

running serial number shall follow the BITD model

identification number.

JAR–FSTD A.020 Validity

of

FSTD

Qualification

(See ACJ to JAR-FSTD

A.020)

(a) An FSTD qualification is valid for 12 months

unless otherwise specified by the Authority.

(b) An FSTD qualification revalidation can take

place at any time within the 60 days prior to the

expiry of the validity of the qualification document.

The new period of validity shall continue from the

expiry date of the previous qualification document.

(c) The Authority shall refuse, revoke, suspend or

vary an FSTD qualification, if the provisions of

JAR–FSTD A are not satisfied.

(d) The qualification of each BITD model serial

number is valid for 36 months from the

commencement of operation, unless reduced by the

Authority. It is the operator‘s responsibility to

apply for the revalidation of the qualification.

JAR–FSTD A.025 Rules

Governing

FSTD

Operators

(See ACJ No. 1 to JAR-

FSTD A.025)

(See ACJ No. 2 to JAR-

FSTD A.025)

(See ACJ No. 3 to JAR-

FSTD A.025)

The FSTD operator shall demonstrate his capability

to maintain the performance, functions and other

characteristics specified for the FSTD Qualification

Level as follows

(a) Quality System

(1)

Quality

System

shall

be

established and a Quality Manager designated to

monitor compliance with, and the adequacy of,

procedures required to ensure the maintenance

of

the

Qualification

Level

of

FSTDs.

Compliance monitoring shall include a feedback

system to the Accountable Manager to ensure

corrective action as necessary.

(2)

The Quality System shall include a

Quality Assurance Programme that contains

procedures designed to verify that the specified

performance, functions and characteristics are

being

conducted

in

accordance

with

all

applicable

requirements,

standards

and

procedures.

(3)

The Quality System and the Quality

Manager shall be acceptable to the Authority.

(4)

The

Quality

System

shall

be

described in relevant documentation.

(b) Updating. A link shall be maintained between

the operator’s organization, the Authority and the

relevant manufacturers to incorporate important

modifications, especially

(1)

Aeroplane modifications that are

essential for training and checking shall be

introduced into all affected FSTDs whether or

not enforced by an airworthiness directive.

(2)

Modification of FSTDs, including

motion and visual systems (where applicable)

SUBPART C – AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

JAR-FSTD A.020(d) (continued)

JAR-FSTD A

SECTION 1

01.05.08

1-C-2

(i)

When essential for training

and checking, FSTD operators shall

update their FSTDs (for example in the

light of data revisions). Modifications of

the FSTD hardware and software that

affect handling, performance and systems

operation or any major modifications of

the motion or visual system shall be

evaluated to determine the impact on the

original

qualification

criteria.

FSTD

operators shall prepare amendments for

any affected validation tests. The FSTD

operator shall test the FSTD to the new

criteria.

(ii)

The Authority shall be advised

in advance of any major changes to

determine if the tests carried out by the

FSTD operator are satisfactory. A special

evaluation of the FSTD may be necessary

prior to returning it to training following

the modification.

(3)

BITD operators shall maintain a link

between their own organisation, the Authority

and the BITD manufacturer to incorporate

important modifications.

(c) Installations. Ensure that the FSTD is housed

in a suitable environment that supports safe and

reliable operation.

(1)

The FSTD operator shall ensure that

the FSTD and its installation comply with the

local regulations for health and safety. However,

as a minimum all FSTD occupants and

maintenance personnel shall be briefed on FSTD

safety to ensure that they are aware of all safety

equipment and procedures in the FSTD in case

of emergency.

(2)

The FSTD safety features such as

emergency stops and emergency lighting shall

be checked at least annually and recorded by the

FSTD operator.

(d) Additional

Equipment.

Where

additional

equipment has been added to the FSTD, even

though not required for qualification, it will be

assessed to ensure that it does not adversely affect

the quality of training. Therefore any subsequent

modification, removal or unserviceability could

affect the qualification of the device.

JAR–FSTD A.030 Requirements for FSTD

qualified on or after 1

August 2008

(See Appendix 1 to JAR–

FSTD A.030)

(See ACJ No. 1 to JAR-

FSTD A.030)

(See ACJ No. 2 to JAR-

FSTD A.030)

(See ACJ No. 3 to JAR-

FSTD A.030)

(See ACJ No. 4 to JAR-

FSTD A.030)

(See ACJ No. 1 to JAR-

FSTD A.030(c)(1))

(See ACJ No. 2 to JAR-

FSTD A.030(c)(1))

(a) Any FSTD submitted for initial evaluation on

or after 1 August 2008 will be evaluated against

applicable

JAR–FSTD

criteria

for

the

Qualification

Levels

applied

for.

Recurrent

evaluations of a FSTD will be based on the same

version of JAR-FSTD A that was applicable for its

initial evaluation. An upgrade will be based on the

currently applicable version of JAR-FSTD A.

(b) A FSTD shall be assessed in those areas that

are essential to completing the flight crewmember

training and checking process as applicable.

(c) The FSTD shall be subjected to

(1)

Validation tests and

(2)

Functions & subjective tests

(d) Data shall be of a standard that satisfies the

Authority before the FSTD can gain a Qualification

Level.

(e) The FSTD operator shall submit a QTG in a

form and manner that is acceptable to the

Authority.

(f) The QTG will only be approved after

completion of an initial or upgrade evaluation, and

when all the discrepancies in the QTG have been

addressed to the satisfaction of the Authority. After

inclusion of the results of the tests witnessed by the

Authority, the approved QTG becomes the Master

QTG (MQTG), which is the basis for the FSTD

qualification and subsequent recurrent FSTD

evaluations. A copy of the MQTG shall be

delivered by the BITD manufacteurer together with

any BITD model delivered to an Operator.

(g) The FSTD operator shall

(1)

Run the complete set of tests

contained within the MQTG progressively

between

each

annual

evaluation

by

the

Authority. Results shall be dated and retained in

JAR-FSTD A.025(b) (continued)

SECTION 1

JAR-FSTD A

1-C-3

01.05.08

order to satisfy both the FSTD operator and the

Authority that FSTD standards are being

maintained; and

(2)

Establish a Configuration Control

System to ensure the continued integrity of the

hardware and software of the qualified FSTD.

JAR-FSTD A.031 Requirements

for

FFS

qualified on or after 1

April 1998 and before 1

August 2008

Any FFS submitted for initial evaluation on or after

1 April 1998 and before 1 August 2008, shall

automatically

be

granted

an

equivalent

qualification under JAR-FSTD A with effect from

the re-evaluation conducted at the end of the

current validity period. This re-evaluation, and all

future

re-evaluations,

will

be

conducted

in

accordance with the requirements of the same

version of JAR-STD 1A, which was applicable for

its last evaluation prior to implementation of JAR-

FSTD A. Any upgrade will be based on the

currently applicable version of JAR-FSTD A.

JAR-FSTD A.032 Requirements for Flight

Training

Devices

(FTD)

qualified on or after 1

July 2000 and before 1

August 2008

Any FTD submitted for initial evaluation on or

after 1 January 2000 and before 1 August 2008,

shall automatically be granted an equivalent

qualification under JAR-FSTD A with effect from

the re-evaluation conducted at the end of the

current validity period. This re-evaluation, and all

future

re-evaluations,

will

be

conducted

in

accordance with of the same version of JAR-STD

2A, which was applicable for its last evaluation

prior to implementation of JAR-FSTD A. Any

upgrade will be based on the currently applicable

version of JAR-FSTD A.

JAR-FSTD A.033 Requirements for Flight

& Navigation Procedures

Trainers (FNPT) qualified

on or after 1 July 1999

and before 1August 2008

Any FNPT submitted for initial evaluation on or

after 1 July 1999 and before 1 August 2008, shall

automatically

be

granted

an

equivalent

qualification under JAR-FSTD A with effect from

the re-evaluation conducted at the end of the

current validity period. This re-evaluation, and all

future

re-evaluations,

will

be

conducted

in

accordance with the requirements of the same

version of JAR-STD 3A, which was applicable for

its last evaluation prior to implementation of JAR-

FSTD A. Any upgrade will be based on the

currently applicable version of JAR-FSTD A.

JAR-FSTD A.034 Requirements for Basic

Instrument

Training

Devices (BITD) qualified

on or after 1 January 2003

and before 1 August 2008

Any BITD submitted for initial evaluation on or

after 1 January 2003 and before 1 August 2008,

shall automatically be granted an equivalent

qualification under JAR-FSTD A with effect from

the re-evaluation conducted at the end of the

current validity period. This re-evaluation, and all

future

re-evaluations,

will

be

conducted

in

accordance with the requirements of the same

version of JAR-STD 4A, which was applicable for

its last evaluation prior to implementation of JAR-

FSTD A. Any upgrade will be based on the

currently applicable version of JAR-FSTD A.

JAR–FSTD A.035 Requirements

for

Full

Flight

Simulators

approved

or

qualified

before 1 April 1998

(See ACJ to JAR-FSTD

A.035)

(a) FFS approved or qualified in accordance with

national regulations of JAA Member States before

1 April 1998 will either be recategorised or will

continue to maintain their approval under the

Grandfather Rights provision, in accordance with

sub-paragraphs (c) and (d) below. For FFS that are

not re-categorized, maximum credit shall under no

circumstances exceed originally issued National

credits.

(b) FFS’s, neither previously recategorised nor

with an approval maintained under the Grandfather

Rights provision, will be qualified in accordance

with JAR–FSTD A.030.

(c) FFS that are not recategorised but that have a

primary reference document used for their testing,

may be qualified by the Authority to an equivalent

JAR–FSTD A Qualification Level, either AG, BG,

CG

or

DG.

An

upgrade

requires

the

recategorisation of the FFS.

(1)

To gain and maintain an equivalent

Qualification Level, these FFS shall be assessed

JAR-FSTD A.030(g) (continued)

JAR-FSTD A.033 (continued)

JAR-FSTD A

SECTION 1

01.05.08

1-C-4

in those areas that are essential to completing

the flight crewmember training and checking

process, as applicable.

(2)

The FFS shall be subjected to

(i)

Validation tests; and

(ii)

Functions and subjective tests.

(d) FFS that are not recategorised and that do not

have a primary reference document used for their

testing shall be qualified by special arrangement.

Such FFS will be issued with a Special Category

and shall be subjected to functions and subjective

tests corresponding to those detailed in this

document. In addition any previously recognised

validation test shall be used.

JAR–FSTD A.036 Requirements for Flight

Training

Devices

approved

or

qualified

before 1 July 2000

(See ACJ to JAR-FSTD

A.036)

(a) FTDs approved or qualified in accordance with

national regulations of JAA Members States before

1 July 2000 either will be recategorised or will

continue to maintain their approval under the

Grandfather Rights provision, in accordance with

JAR–FSTD A.036(c) and JAR–FSTD A.036 (d).

(b) FTDs, neither previously recategorised nor

with an approval maintained under the Grandfather

Rights provision, will be qualified in accordance

with JAR–FSTD A.030.

(c) FTDs that are not recategorised but that have a

primary reference document used for their testing

may be qualified by the Authority to an equivalent

JAR–FSTD Qualification Level, either 1G or 2G.

These Qualification Levels refer to similar credits

achieved by JAR–FSTD A Level 1 and 2.

(1)

To gain and maintain an equivalent

Qualification Level, these FTDs shall be

assessed in those areas which are essential to

completing the flight crew member training and

checking process, including

(i)

Longitudinal,

lateral

and

directional

handling

qualities

(where

applicable);

(ii)

Performance on the ground

and in the air;

(iii) Specific

operations

where

applicable;

(iv) Flight deck configuration;

(v)

Functioning during normal,

abnormal,

emergency

and,

where

applicable non normal operation;

(vi) Instructor station function and

FTD control, and

(vii) Certain

additional

requirements

depending

on

the

Qualification Level and the installed

equipment.

(2)

The FTD shall be subjected to

(i)

Validation Tests, and

(ii)

Functions

and

Subjective

Tests.

(d) FTDs that are not recategorised and that do not

have a primary reference document used for their

testing shall be qualified by special arrangement.

(1)

Such FTDs will be issued with

Special Categories.

(2)

These FTDs shall be subjected to the

same Functions and Subjective Tests referred to

in JAR–FSTD A.036(c) (2) (ii).

(3)

In

addition

any

previously

recognised Validation Test shall be used.

JAR–FSTD A.037 Requirements for Flight

Navigation

and

Procedures

Trainers

approved

or

qualified

before 1 July 1999

(See ACJ to JAR-FSTD

A.037)

(No Longer Applicable)

JAR–FSTD A.040 Changes

to

qualified

FSTD

(a) Requirement to notify major changes to a

FSTD. The operator of a qualified FSTD shall

inform the Authority of proposed major changes

such as

(1)

Aeroplane

modifications,

which

could affect FSTD qualification.

(2)

FSTD hardware and or software

modifications that could affect the handling

qualities,

performances

or

system

representations.

(3)

Relocation of the FSTD; and

(4)

Any deactivation of the FSTD.

JAR-FSTD A.035(c) (continued)

JAR-FSTD A.036 (continued)

SECTION 1

JAR-FSTD A

1-C-5

01.05.08

The Authority may complete a special evaluation

following major changes or when a FSTD appears

not to be performing at its initial Qualification

Level.

(b) Upgrade of a FSTD. A FSTD may be upgraded

to a higher Qualification Level. Special evaluation

is required before the award of a higher Level of

Qualification.

(1)

If an upgrade is proposed the FSTD

operator shall seek the advice of the Authority

and give full details of the modifications. If the

upgrade evaluation does not fall upon the

anniversary of the original qualification date, a

special evaluation is required to permit the

FSTD to continue to qualify even at the

previous Qualification Level.

(2)

In the case of a FSTD upgrade, an

FSTD operator shall run all validation tests for

the requested Qualification Level. Results from

previous evaluations shall not be used to

validate FSTD performance for the current

upgrade.

(c) Relocation of a FSTD

(1)

In instances where a FSTD is moved

to a new location, the Authority shall be advised

before the planned activity along with a

schedule of related events.

(2)

Prior to returning the FSTD to

service at the new location, the FSTD operator

shall perform at least one third of the validation

tests and, functions and subjective tests to

ensure that the FSTD performance meets its

original qualification standard. A copy of the

test documentation shall be retained together

with the FSTD records for review by the

Authority.

(3)

An evaluation of the FSTD in

accordance with its original JAA qualification

criteria shall be at the discretion of the

Authority.

(d) Deactivation of a currently qualified FSTD

(1)

If a FSTD operator plans to remove

a FSTD from active status for prolonged

periods, the Authority shall be notified and

suitable controls established for the period

during which the FSTD is inactive.

(2)

The FSTD operator shall agree a

procedure with the Authority to ensure that the

FSTD can be restored to active status at its

original Qualification Level.

JAR–FSTD A.045 Interim

FSTD

Qualification

(See ACJ to FSTD A.045)

(a) In case of new aeroplane programmes, special

arrangements shall be made to enable an interim

Qualification Level to be achieved.

(b) For

Full

Flight

Simulators,

an

Interim

Qualification Level will only be granted at levels

A, B or C.

(c) Requirements, details relating to the issue, and

the period of validity of an interim Qualification

Level will be decided by the Authority.

JAR–FSTD A.050 Transferability of FSTD

Qualification

When there is a change of FSTD operator

(a) The new FSTD operator shall advise the

Authority in advance in order to agree upon a plan

of transfer of the FSTD.

(b) At the discretion of the Authority, the FSTD

shall be subject to an evaluation in accordance with

its original JAA qualification criteria.

(c) Provided that the FSTD performs to its original

standard, its original Qualification Level shall be

restored. Revised user approval(s) may also be

required.

INTENTIONALLY LEFT BLANK

JAR-FSTD A.040 (continued)

JAR-FSTD A

SECTION 1

01.05.08

1-C-6

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD A

1-C-7

01.05.08

Appendix 1 to JAR-FSTD A.030

Flight Simulation Training Device Standards

This appendix describes the minimum Full Flight Simulator (FFS), Flight Training Device (FTD), Flight and

Navigation Procedures Trainer (FNPT) and Basic Instrument Training Devices (BITD) requirements for

qualifying devices to the required Qualification Levels. Certain requirements included in this section shall be

supported with a statement of compliance (SOC) and, in some designated cases, an objective test. The SOC will

describe how the requirement was met. The test results shall show that the requirement has been attained. In

the following tabular listing of FSTD standards, statements of compliance are indicated in the compliance

column.

For FNPT use in Multi-Crew Co-operation (MCC) training the general technical requirement are expressed in

the MCC column with additional systems, instrumentation and indicators as required for MCC training and

operation.

For MCC (Multi Crew Co-operation) minimum technical requirements are as for Level II, with the following

additions or amendments

Turbo-jet or turbo-prop engines.

Performance reserves, in case of an engine failure, to be in accordance with JAR-25. These may

be simulated by a reduction in the aeroplane gross mass.

Retractable landing gear.

Pressurisation system.

De-icing systems

Fire detection / suppression system

Dual controls

Autopilot with automatic approach mode

2 VHF transceivers including oxygen masks intercom system

2 VHF NAV receivers (VOR, ILS, DME)

1 ADF receiver

1 Marker receiver

1 transponder

The following indicators shall be located in the same positions on the instrument panels of both pilots

Airspeed

Flight attitude with flight director

Altimeter

Flight director with ILS (HSI)

Vertical speed

ADF

VOR

Marker indication (as appropriate)

Stop watch (as appropriate)

INTENTIONALLY LEFT BLANK

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-8

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

a.1

A fully enclosed flight deck

a.2

A cockpit/flight deck sufficiently enclosed to exclude

distraction, which will replicate that of the aeroplane

or class of aeroplane simulated

a.3

Flight deck, a full scale replica of the aeroplane

simulated.

Equipment for operation of the cockpit windows shall

be included in the FSTD, but the actual windows

need not be operable.

The flight deck, for FSTD purposes, consists of all

that space forward of a cross section of the fuselage

at the most extreme aft setting of the pilots' seats.

Additional required flight crewmember duty stations

and those required bulkheads aft of the pilot seats

are also considered part of the flight deck and shall

replicate the aeroplane.

Flight deck observer seats are not considered to be

additional flight crewmember duty stations and may

be omitted.

Bulkheads containing items such as switches, circuit

breakers, supplementary radio panels, etc. to which

the flight crew may require access during any event

after pre-flight cockpit preparation is complete are

considered essential and may not be omitted.

Bulkheads containing only items such as landing

gear pin storage compartments, fire axes or

extinguishers, spare light bulbs, aircraft document

pouches etc. are not considered essential and may

be omitted. Such items, or reasonable facsimile,

shall still be available in the FSTD but may be

relocated to a suitable location as near as practical

to the original position. Fire axes and any similar

purpose instruments need only be represented in

silhouette.

a.4

Direction of movement of controls and switches

identical to that in the aeroplane.

1-C-9

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

a.5

A full size panel of replicated system(s) which will

have actuation of controls and switches that

replicate those of the aeroplane simulated.

The use of electronically displayed images with

physical overlay incorporating operable switches,

knobs, buttons replicating aeroplane instruments

panels may be acceptable.

a.6

Cockpit/flight deck switches, instruments, equipment,

panels, systems, primary and secondary flight controls

sufficient for the training events to be accomplished shall

be located in a spatially correct flight deck area and will

operate as, and represent those in, that aeroplane or

class of aeroplane.

For Multi-Crew Co-operation (MCC) qualification

additional instrumentation and indicators may be

required. See table at start of this appendix..

For BITDs the switches and controls size and shape

and

their

location

in

the

cockpit

shall

be

representative.

a.7

Crew members seats shall be provided with

sufficient adjustment to allow the occupant to

achieve

the

design

eye

reference

position

appropriate to the aeroplane or class of aeroplane

and for the visual system to be installed to align with

that eye position.

b.1

Circuit breakers that affect procedures and/or result

in observable cockpit indications properly located

and functionally accurate.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-10

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

c.1

Flight dynamics model that accounts for various

combinations

of

drag

and

thrust

normally

encountered in flight corresponding to actual flight

conditions, including the effect of change in

aeroplane attitude, sideslip, thrust, drag, altitude,

temperature, gross weight, moments of inertia,

centre of gravity location, and configuration.

For FTD Levels 1 and 2 aerodynamic modelling

sufficient to permit accurate systems operation and

indication is acceptable.

For FNPTs and BITDs class specific modelling is

acceptable.

d.1

All relevant instrument indications involved in the

simulation

of

the

applicable

aeroplane

shall

automatically respond to control movement by a

flight crewmember or induced disturbance to the

simulated aeroplane; e.g., turbulence or wind shear.

For FNPTs instrument indications sufficient for the

training events to be accomplished. Reference ACJ No.

3 to JAR-FSTD A.030.

For BITDs instrument indications sufficient for the

training events to be accomplished. Reference ACJ No.

4 to JAR-FSTD A.030.

d.2

Lighting environment for panels and instruments

shall be sufficient for the operation being conducted.

For FTD Level 2 lighting environment shall be as per

aeroplane.

e.1

Communications,

navigation,

and

caution

and

warning equipment corresponding to that installed in

the applicant’s aeroplane with operation within the

tolerances prescribed for the applicable airborne

equipment.

For FTD 1 applies where the appropriate systems

are replicated.

e.2

Navigation equipment corresponding to that of the

replicated aeroplane or class of aeroplanes, with

operation within the tolerances prescribed for the actual

airborne equipment. This shall include communication

equipment (interphone and air/ground communications

systems).

1-C-11

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

e.3

Navigational data with the corresponding approach

facilities. Navigation aids should be usable within

range without restriction.

For FTD 1 applies where navigation equipment is

replicated.

For all FFSs and FTDs 2 where used for area or

airfield competence training or checking, navigation

data should be updated within 28 days.

For FNPTs and BITDs complete navigational data for

at least 5 different European airports with

corresponding precision and non-precision approach

procedures including current updating within a period

of 3 months.

f.1

In addition to the flight crewmember duty stations,

three suitable seats for the instructor, delegated

examiner and Authority inspector. The Authority will

consider options to this standard based on unique

cockpit configurations. These seats shall provide

adequate vision to the pilot’s panel and forward

windows. Observer seats need not represent those

found in the aeroplane but in the case of FSTDs

fitted with a motion system, the seats shall be

adequately secured to the floor of the FSTD, fitted

with positive restraint devices and be of sufficient

integrity to safely restrain the occupant during any

known or predicted motion system excursion.

For

FTDs

and

FNPT’s

suitable

seating

arrangements for the Instructor and Examiner or

Authority’s Inspector should be provided.

For BITDs suitable viewing arrangements for the

Instructor should be provided.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-12

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

g.1

FSTD systems shall simulate applicable aeroplane

system operation, both on the ground and in flight.

Systems shall be operative to the extent that all

normal,

abnormal,

and

emergency

operating

procedures can be accomplished.

For FTD Level 1, applies where system is simulated.

For FNPTs systems shall be operative to the extent that

it shall be possible to perform all normal, abnormal and

emergency operations as may be appropriate to the

aeroplane or class of aeroplanes being simulated and

as required for the training.

h.1

Instructor controls shall enable the operator to

control all required system variables and insert

abnormal

or

emergency

conditions

into

the

aeroplane systems.

Where applicable and as required for training the

following shall be available

Position and flight freeze.

A facility to enable the dynamic plotting of the

flight path on approaches, commencing at the

final approach fix, including the vertical profile

Hard copy of map and approach plot

1-C-13

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

i.1

Control forces and control travel shall correspond to

that of the replicated aeroplane. Control forces shall

react in the same manner as in the aeroplane under

the same flight conditions.

For FTD Level 2 Control forces and control travel

should

correspond

to

that

of

the

replicated

aeroplane with CT&M. It is not intended that the

device should be flown manually other than for short

periods

when

the

autopilot

is

temporarily

disengaged.

For FNPT Level I and BITDs control forces and

control travel shall broadly correspond to that of the

replicated aeroplane or class of aeroplane. Control

force changes due to an increase/decrease in

aircraft speed are not necessary.

In addition for FNPT Level II and MCC control forces

and control travels shall respond in the same

manner under the same flight conditions as in the

aeroplane or class of aeroplane being simulated.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-14

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

j.1

Ground handling and aerodynamic programming

shall include

(1)

Ground Effect. For example: round-out, flare,

and touchdown. This requires data on lift,

drag, pitching moment, trim, and power ground

effect.

(2)

Ground reaction – reaction of the aeroplane

upon contact with the runway during landing to

include strut deflections, tyre friction, side

forces, and other appropriate data, such as

weight and speed, necessary to identify the

flight condition and configuration.

(3)

Ground handling characteristics – steering

inputs to include crosswind, braking, thrust

reversing, deceleration and turning radius.

Statement of Compliance required. Tests required.

For Level ‘A’ FFS, generic ground handling to the

extent that allows turns within the confines of the

runway, adequate control on flare, touchdown and

roll-out (including from a cross -wind landing) only is

acceptable.

For FNPTs a generic ground handling model need

only be provided to enable representative flare and

touch down effects.

1-C-15

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

k.1

Windshear models shall provide training in the

specific skills required for recognition of wind shear

phenomena and execution of recovery manoeuvres.

Such models shall be representative of measured or

accident

derived

winds,

but

may

include

simplifications which ensure repeatable encounters.

For example, models may consist of independent

variable winds in multiple simultaneous components.

Wind models shall be available for the following

critical phases of flight

(1)

Prior to take-off rotation

(2)

At lift-off

(3)

During initial climb

(4)

Short final approach

Tests required.

See ACJ No 1 to JAR-FSTD A.030, Para 2.3, g.

l.1

Instructor

controls

for

environmental

effects

including wind speed and direction shall be

provided.

For FTDs environment modelling sufficient to permit

accurate systems operation and indication.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-16

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

m.1

Stopping and directional control forces shall be

representative for at least the following runway

conditions based on aeroplane related data

(1)

Dry

(2)

Wet

(3)

Icy

(4)

Patchy wet

(5)

Patchy icy

(6)

Wet on rubber residue in touchdown zone.

Statement of Compliance required.

Objective Tests required for (1), (2), (3), Subjective

check for (4), (5), (6).

n.1

Brake and tyre failure dynamics (including antiskid)

and decreased brake efficiency due to brake

temperatures shall be representative and based on

aeroplane related data.

Statement of Compliance required.

Subjective test is required for decreased braking

efficiency due to brake temperature, if applicable.

o.1

A means for quickly and effectively conducting daily

testing of FSTD programming and hardware shall be

available.

Statement of Compliance required.

p.1

Computer

capacity,

accuracy,

resolution,

and

dynamic response shall be sufficient to fully support

the overall fidelity, including its evaluation and

testing.

Statement of Compliance required.

1-C-17

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

q.1

Control feel dynamics shall replicate the aeroplane

simulated.

Free response of the controls shall match that of the

aeroplane within the tolerances specified. Initial and

upgrade evaluations will include control free response

(pitch, roll and yaw controller) measurements recorded at

the controls. The measured responses shall correspond to

those of the aeroplane in take-off, cruise, and landing

configurations.

(1)

For aeroplanes with irreversible control systems,

measurements may be obtained on the ground if

proper pitot static inputs are provided to represent

conditions typical of those encountered in flight.

Engineering validation or aeroplane manufacturer

rationale will be submitted as justification to ground

test or omit a configuration.

(2)

For FSTDs requiring static and dynamic tests

at the controls, special test fixtures will not be

required during initial evaluation if the FSTD

operator’s MQTG shows both text fixture

results and alternate test method results such

as computer data plots, which were obtained

concurrently.

Repetition

of

the

alternate

method during initial evaluation may then

satisfy this requirement.

Tests required.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-18

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

r.1

One of the following two methods is acceptable as a

means to prove compliance

Tests required.

For Level ‘A’ & ‘B’ FFSs, and applicable systems for

FTDs, FNPTs and BITDs the maximum permissible

delay is 300 milliseconds.

(1) Transport Delay: A transport delay test may be

used to demonstrate that the FSTD system response

does not exceed 150 milliseconds. This test shall

measure all the delay encountered by a step signal

migrating from the pilot’s control through the control

loading electronics and interfacing through all the

simulation software modules in the correct order, using

a handshaking protocol, finally through the normal

output interfaces to the motion system, to the visual

system and instrument displays.

(see next page)

1-C-19

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE STANDARDS

1.1 General

B

C

D

I

II

MCC

COMPLIANCE

(continued)

(2)

Latency

The

visual

system,

flight

deck

instruments and initial motion system response

shall respond to abrupt pitch, roll and yaw inputs

from the pilot's position within 150 milliseconds

of the time, but not before the time, when the

aeroplane would respond under the same

conditions.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-20

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

COMPLIANCE

1.1 General

B

C

D

I

II

MCC

s.1

Aerodynamic modelling shall be provided. This shall

include, for aeroplanes issued an original type

certificate after June 1980, low altitude level flight

ground effect, Mach effect at high altitude, normal

and reverse dynamic thrust effect on control

surfaces,

aeroelastic

representations,

and

representations of non-linearities due to sideslip

based on aeroplane flight test data provided by the

manufacturer.

Statement of Compliance required. Mach effect,

aeroelastic representations, and non-linearities

due to sideslip are normally included in the FSTD

aerodynamic model. The Statement of Compliance

shall address each of these items. Separate tests

for thrust effects and a Statement of Compliance

are required.

t.1

Modelling that includes the effects of airframe and

engine icing.

Statement of Compliance required.

SOC shall describe the effects that provide

training

in

the

specific

skills

required

for

recognition of icing phenomena and execution of

recovery.

u.1

Aerodynamic and ground reaction modelling for the

effects of reverse thrust on directional control shall

be provided.

Statement of Compliance required.

(page 2–C–44).

v.1

Realistic aeroplane mass properties, including mass,

centre of gravity and moments of inertia as a

function of payload and fuel loading shall be

implemented.

Statement of Compliance required at initial

evaluation. SOC shall include a range of tabulated

target values to enable a demonstration of the

mass properties model to be conducted from the

instructor’s station.

w.1

Self-testing for FSTD hardware and programming to

determine compliance with the FSTD performance

tests shall be provided. Evidence of testing shall

include FSTD number, date, time, conditions,

tolerances, and the appropriate dependent variables

portrayed

in

comparison

with

the

aeroplane

standard.

Statement of Compliance required. Tests required.

1-C-21

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

COMPLIANCE

1.1 General

B

C

D

I

II

MCC

x.1

Timely and permanent update of hardware and

programming subsequent to aeroplane modification

sufficient for the Qualification Level sought.

y.1

Daily pre-flight documentation either in the daily log

or in a location easily accessible for review is

required.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-22

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

2. Motion system

B

C

D

I

II

MCC

COMPLIANCE

a.1

Motion cues as perceived by the pilot

shall be representative of the aeroplane,

e.g. touchdown cues shall be a function

of the simulated rate of descent.

For FSTDs where motion systems are

not specifically required, but have been

added, they will be assessed to ensure

that they do not adversely affect the

qualification of the FSTD.

b.1

A motion system shall

(1)

Provide sufficient cueing, which

may be of a generic nature to

accomplish the required tasks.

Statement of Compliance required.

Tests required.

(2)

Have a minimum of 3 degrees of

freedom (pitch, roll & heave).

(3) Produce cues at least equivalent to

those of a six-degrees-of-freedom

synergistic platform motion system.

c.1

means

of

recording

the

motion

response time as required.

1-C-23

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

2. Motion system

B

C

D

I

II

MCC

COMPLIANCE

d.1

Motion effects programming shall include

(1)

Effects of runway rumble, oleo

deflections, groundspeed, uneven

runway,

centreline

lights

and

taxiway characteristics.

(2)

Buffets on the ground due to

spoiler/speedbrake extension and

thrust reversal.

(3)

Bumps associated with the landing

gear.

(4)

Buffet

during

extension

and

retraction of landing gear.

(5)

Buffet in the air due to flap and

spoiler/speedbrake extension.

(6)

Approach to stall buffet.

(7)

Touchdown cues for main and nose

gear.

(8)

Nose wheel scuffing.

(9)

Thrust effect with brakes set.

(See next page)

For Level ‘A’FFS: Effects may be of a

generic nature sufficient to accomplish

the required tasks.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-24

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

2. Motion system

B

C

D

I

II

MCC

COMPLIANCE

d.1

(continued)

(10) Mach and manoeuvre buffet.

(11) Tyre failure dynamics.

(12) Engine malfunction and engine

damage.

(13) Tail and pod strike.

e.1

Motion vibrations: Tests with recorded

results that allow the comparison of

relative amplitudes versus frequency are

required.

Characteristic

motion

vibrations

that

result from operation of the aeroplane in

so far as vibration marks an event or

aeroplane state that can be sensed at the

flight deck shall be present. The FSTD

shall be programmed and instrumented in

such a manner that the characteristic

vibration modes can be measured and

compared with aeroplane data.

Statement of Compliance required.

Tests required.

1-C-25

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

3 Visual System

B

C

D

I

II

MCC

COMPLIANCE

a.1

The visual system shall meet all the

standards enumerated as applicable to

the level of qualification requested by the

applicant.

For FTDs, FNPT 1s and BITDs, when visual

systems have been added by the FSTD

operator even though not attracting specific

credits, they will be assessed to ensure that

they do not adversely affect the qualification

of the FSTD.

For FTDs if the visual system is to be used

for the training of manoeuvring by visual

reference

(such

as

route

and

airfield

competence) then the visual system should

at least comply with that required for level A

FFS.

b.1

Continuous minimum collimated visual

field-of-view of 45 degrees horizontal and

degrees

vertical

field

of

view

simultaneously for each pilot.

SOC is acceptable in place of this test.

b.2

Continuous,

cross-cockpit,

minimum

collimated visual field of view providing

each pilot with 180 degrees horizontal

and 40 degrees vertical field of view.

Application of tolerances require the field

of view to be not less than a total of 176

measured degrees horizontal field of view

(including not less than ±88 measured

degrees either side of the centre of the

design eye point) and not less than a total

of 36 measured degrees vertical field of

view from the pilot’s and co-pilot’s eye

points.

Consideration shall be given to optimising

the vertical field of view for the respective

aeroplane cut-off angle.

SOC is acceptable in place of this test.

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-26

FS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

3 Visual System

B

C

D

I

II

MCC

COMPLIANCE

b.3

A visual system (night/dusk or day) capable

of providing a field-of-view of a minimum of

45 degrees horizontally and 30 degrees

vertically, unless restricted by the type of

aeroplane, simultaneously for each pilot,

including adjustable cloud base and visibility.

The visual system need not be collimated but

shall be capable of meeting the standards laid

down in Part 3 and 4 (Validation, Functions and

Subjective Tests - See ACJ No.1 to JAR-FSTD

A.030).

SOC is acceptable in place of this test.

c.1

A means of recording the visual response

time for visual systems.

d.1

System Geometry. The system fitted shall

be free from optical discontinuities and

artefacts that create non-realistic cues.

Test required. A Statement of Compliance is

acceptable in place of this test.

e.1

Visual textural cues to assess sink rate

and depth perception during take-off and

landing shall be provided.

For Level ‘A’ FFS visual cueing shall be

sufficient to support changes in approach

path by using runway perspective.

f.1

Horizon, and attitude shall correlate to the

simulated attitude indicator.

Statement of Compliance required.

g.1

Occulting - A minimum of ten levels shall

be available.

Occulting shall be demonstrated.

Statement of Compliance required.

h.1

Surface (Vernier) resolution shall occupy

a visual angle of not greater than 2 arc

minutes in the visual display used on a

scene from the pilot’s eyepoint.

Test and Statement of Compliance required

containing

calculations

confirming

resolution.

1-C-27

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

3 Visual System

B

C

D

I

II

MCC

COMPLIANCE

i.1

Surface

contrast

ratio

shall

be

demonstrated by a raster drawn test

pattern showing a contrast ratio of not

less than 5:1

Test and Statement of Compliance required.

j.1

Highlight

brightness

shall

be

demonstrated using a raster drawn test

pattern. The highlight brightness shall not

be less than 20 cd/m2 (6ft-lamberts).

Test and Statement of Compliance required.

Use of calligraphic lights to enhance raster

brightness is acceptable.

k.1

Light point size – not greater than 5 arc

minutes.

Test and Statement of Compliance required.

This is equivalent to a light point resolution

of 2.5 arc minutes.

l.1

Light point contrast ratio – not less than

10:1

Test and Statement of compliance required.

l.2

Light point contrast ratio – not less than

25:1.

Test and Statement of compliance required.

m.1

Daylight,

twilight

and

night

visual

capability as applicable for level of

qualification sought.

Statement

of

Compliance

required

for

system capability.

System objective and scene content tests

are required.

m.2

The visual system shall be capable of

meeting, as a minimum, the system

brightness and contrast ratio criteria as

applicable for level of qualification sought

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-28

FS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

3 Visual System

B

C

D

I

II

MCC

COMPLIANCE

m.3

Total scene content shall be comparable

in detail to that produced by 10000 visible

textured surfaces and (in day) 6000

visible lights or (in twilight or night) 15000

visible

lights,

and

sufficient

system

capacity to display 16 simultaneously

moving objects.

m.4

The system, when used in training, shall

provide

in

daylight,

full

colour

presentations and sufficient surfaces with

appropriate textural cues to conduct a

visual approach, landing and airport

movement (taxi). Surface shading effects

shall be consistent with simulated (static)

sun position.

1-C-29

01.05.08

SECTION 1

JAR-FSTD A

Appendix 1 to JAR-FSTD A.030 (continued)

FS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

3 Visual System

B

C

D

I

II

MCC

COMPLIANCE

m.5

The system, when used in training, shall

provide at twilight, as a minimum, full

colour presentations of reduced ambient

intensity,

sufficient

surfaces

with

appropriate textural cues that include self-

illuminated

objects

such

as

road

networks,

ramp

lighting

and

airport

signage, to conduct a visual approach,

landing and airport movement (taxi).

Scenes shall include a definable horizon

and typical terrain characteristics such as

fields, roads and bodies of water and

surfaces illuminated by representative

ownship lighting (e.g. landing lights). If

provided, directional horizon lighting shall

have correct orientation and be consistent

with surface shading effects.

m.6

The system, when used in training, shall

provide at night, as a minimum, all

features applicable to the twilight scene,

as defined above, with the exception of

the need to portray reduced ambient

intensity that removes ground cues that

are not self-illuminating or illuminated by

ownship lights (e.g. landing lights).

JAR-FSTD A

SECTION 1

Appendix 1 to JAR-FSTD A.030 (continued)

01.05.08

1-C-30

FFS LEVEL

FTD

LEVEL

FNPT LEVEL

BITD

COMPLIANCE

FLIGHT SIMULATOR TRAINING DEVICE

STANDARDS

4 Sound System

B

C

D

I

II

MCC

a.1

Significant flight deck sounds which result

from pilot actions corresponding to those

of the aeroplane or class of aeroplane.

For FNPT Level I and BITD engine sounds

only need be available

b.1

Sound of precipitation, rain removal

equipment and other significant aeroplane

noises perceptible to the pilot during

normal and abnormal operations and the

sound of a crash when the FSTD is

landed in excess of limitations.

Statement of Compliance required.

c.1

Comparable amplitude and frequency of

flight deck noises, including engine and

airframe sounds. The sounds shall be co-

ordinated with the required weather.

Tests required.

d.1

The

volume

control

shall

have

an

indication of sound level setting which

meets all qualification requirements.

Printed and distributed by Global Engineering Documents, 15 Inverness Way East, Englewood, Colorado 80112, U S A on behalf of the Joint Aviation Authorities

Committee.

Joint

Aviation

Requirements

JAR–FSTD H

Helicopter

Flight Simulation Training Devices

Initial issue

01 May 2008

All rights reserved

Annexe II

Code JAR-FSTD (H) – Entraîneurs synthétiques de vol pour hélicoptèrers

01.05.08

ii

The members of the Joint Aviation Authorities Committee are representatives of the Civil Aviation

Authorities of the countries that have signed the ‘Arrangements Concerning the Development and the

Acceptance of Joint Aviation Requirements’. A list of these countries is kept by European Civil Aviation

Conference, 3 bis Villa Emile Bergerat, 92522 NEUILLY SUR SEINE Cedex, France.*

Further copies of the Joint Aviation Requirements can be purchased from IHS, Inc. , whose world-wide

offices are listed on the JAA website (www.jaa.nl) and IHS website (www.global.ihs.com).

For electronic versions of Joint Aviation Authorities Documents please refer to the website of IHS, Inc. on

www.ihs.com, where you will find information on how to order.

Enquiries regarding the contents should be addressed to the JAA, Saturnusstraat 40-44, PO Box 3000,

2130 KA HOOFDDORP, The Netherlands (publications@jaat.eu).

*These countries are

Albania, Armenia, Austria, [Azerbaijan], Belgium, Bosnia and Herzegovina, Bulgaria, Croatia, Cyprus,

Czech Republic, Denmark, Estonia, European Aviation Safety Agency, Finland, Former Yugoslav Republic

of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg,

Malta, Monaco, Netherlands, Norway, Poland, Portugal, Republic of Moldova, [Republic of Georgia],

Romania, Serbia, Slovak Republic, Slovenia, Spain, Sweden, Switzerland, Turkey, Ukraine, & United

Kingdom

JAR-FSTD H

C-1

01.05.08

CONTENTS (general layout)

JAR–FSTD H

HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

FOREWORD

CHECK LIST OF PAGES

PREAMBLE

SECTION 1 – REQUIREMENTS

SUBPART A

APPLICABILITY

SUBPART B

GENERAL

SUBPART C

HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)

ACJ B

GENERAL

ACJ C

HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

JAR-FSTD H

01.05.08

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CONTENTS (details)

JAR–FSTD H

HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

Paragraph

Page

SECTION 1 – REQUIREMENTS

General and Presentation

1-0-1

SUBPART A – APPLICABILITY

JAR–FSTD H.001

Applicability

1-A-1

SUBPART B – GENERAL

JAR–FSTD H.005

Terminology

1-B-1

SUBPART C – HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

JAR–FSTD H.015

Application for FSTD Qualification

1-C-1

JAR–FSTD H.020

Validity FSTD Qualification

1-C-1

JAR–FSTD H.025

Rules governing FSTD Operators

1-C-1

JAR–FSTD H.030

Requirements for FSTDs qualified on or after

1-C-2

1 August 2008

JAR–FSTD H.031

Requirements for FFS qualified on or after

1-C-2

1 April 2001 and before 1 August 2008

JAR–FSTD H.032

Requirements for FTDs qualified on or after 1 January 2004

1-C-3

and before 1 August 2008

JAR–FSTD H.033

Requirements for FNPTs qualified on or after 1 January 2003

1-C-3

and before 1 August 2008

JAR–FSTD H.035

Requirements for FFSs approved or qualified

1-C-3

before 1 April 2001

JAR–FSTD H.036

Requirements for FTDs approved or qualified

1-C-3

before 1 January 2004

JAR–FSTD H.037

Requirements for FNPTs approved or qualified

1-C-4

before 1 January 2003

JAR–FSTD H.040

Changes to qualified FSTDs

1-C-4

JAR–FSTD H.045

Interim FSTD Qualification

1-C-5

JAR–FSTD H.050

Transferability of FSTD Qualification

1-C-5

Appendix 1 to

FSTD Standards

1-C-6

JAR–FSTD H.030

JAR-FSTD H

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Page

01.05.08

C-4

SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)

General and Presentation

2-0-1

ACJ B – GENERAL

ACJ FSTD H.005

Terminology, Abbreviations

2-B-1

ACJ C – HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

ACJ No. 1 to

FSTD Qualification – Application and Inspection

2-C-1

JAR-FSTD H.015

ACJ No. 2 to

FSTD Evaluations

2-C-7

JAR-FSTD H.015

ACJ to

Validity of FSTD Qualification

2-C-10

JAR-FSTD H.020

ACJ No. 1 to

Quality System

2-C-10

JAR-FSTD H.025

ACJ No. 2 to

Installations

2-C-16

JAR-FSTD H.025

ACJ No. 1 to

FSTDs qualified on or after 1 August 2008

2-C-17

JAR-FSTD H.030

Appendix 1 to ACJ No. 1

Validation Test Tolerances

2-C-106

to JAR-FSTD H.030

Appendix 2 to ACJ No. 1

Validation Data Roadmap

2-C-108

to JAR-FSTD H.030

Appendix 3 to ACJ No. 1 Rotor Aerodynamic Modeling Techniques

2-C-110

to JAR-FSTD H.030

Appendix 4 to ACJ No. 1 Vibration Platforms for Helicopter FSTDs

2-C-112

to JAR-FSTD H.030

Appendix 5 to ACJ No. 1 Transport Delay Testing Method

2-C-114

to JAR-FSTD H.030

Appendix 6 to ACJ No. 1 Recurrent Evaluations – Validation Test Data Presentation

2-C-117

to JAR-FSTD H.030

Appendix 7 to ACJ No 1

Applicability

2-C-118

to JAR-FSTD H.030

Appendix 8 to ACJ No 1

Visual Display Systems

2-C-119

JAR–FSTD H.030

Appendix 9 to ACJ No 1

General technical Requirements for FSTD Qualification

2-C-122

JAR–FSTD H.030

Levels

ACJ No. 2 to

Guidance on Design & Qualification of Level ‘A’ Helicopter FFS

2-C-127

JAR-FSTD H.030

ACJ No. 3 to

Guidance on Design & Qualification of Helicopter FTDs

2-C-129

JAR-FSTD H.030

ACJ No. 4 to

Use of Data for Helicopter FTDs

2-C-132

JAR-FSTD H.030

ACJ No. 5 to

Guidance on Design & Qualification of Helicopter FNPTs

2-C-133

JAR-FSTD H.030

JAR-FSTD H

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01.05.08

ACJ No. 1 to

Engineering Simulator Validation Data

2-C-141

JAR-FSTD H.030(c)(1)

ACJ No. 2 to

Engineering Simulator Validation Data – Approved Guidelines

2-C-142

JAR-FSTD H.030(c)(1)

ACJ to FSTD H.035

FFS Approved or Qualified before 1 April 2001

2-C-144

ACJ to FSTD H.037

FNPTs Approved or Qualified before 1 January 2003

2-C-145

ACJ to FSTD H.045

New Helicopter FFS/FTD Qualification

2-C-146

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FOREWORD

The Civil Aviation Authorities of certain European countries have agreed common comprehensive

and detailed aviation requirements, referred to as Joint Aviation Requirements (JARs), with a view

to minimising Type Certification problems on joint ventures, to facilitate the export and import of

aviation products, to make it easier for maintenance carried out in one European country to be

accepted by the Civil Aviation Authority in another European country and to regulate commercial

air transport operations.

JARs are recognised by the Civil Aviation Authorities of participating countries as an acceptable

basis for showing compliance with their national codes.

The content has been prepared using the expertise available in this field and added to where

necessary by making use of existing European regulations and the Federal Aviation Requirements

of the United States of America where acceptable.

JAR–FSTD H is issued with no National Variants. It may be felt that the document does not

contain all of the detailed compliance and interpretative information which some Civil Aviation

Authorities and Industry organisations would like to see. However, it is accepted that JAR–FSTD

H should be applied in practice and the lessons learned embodied in future amendments. The

Civil Aviation Authorities of the JAA are therefore committed to early amendment in the light of

experience.

Future development of the requirements of JAR–FSTD H, including the commitment in

Paragraph 4, will be in accordance with the JAA’s Notice of Proposed Amendment (NPA)

procedures. These procedures allow for the amendment of JAR–FSTD H to be proposed by any

organisation or person.

The Civil Aviation Authorities have agreed they should not unilaterally initiate amendment of their

national codes without having made a proposal for amendment of JAR–FSTD H in accordance

with the agreed procedure.

Definitions and abbreviations of terms used in JAR–FSTD H that are considered generally

applicable are contained in JAR–1, Definitions and Abbreviations. However, definitions and

abbreviations of terms used in JAR–FSTD H that are specific to a Subpart of JAR–FSTD H are

normally given in the Subpart concerned or, exceptionally, in the associated compliance or

interpretative material.

Amendments to the text in JAR–FSTD H are issued as Replacement Pages. These show an

effective date and have the same status and applicability as JAR–FSTD H from that date.

New, amended and corrected text will be enclosed within heavy brackets until a subsequent

Amendment’ is issued.

Comment/Response documents developed following Notices of Proposed Amendment (NPA)

consultation have been produced by the JAA and are published on the JAA Internet Site

www.jaa.nl. Readers can also apply to Central JAA for copies of specific Comment/Response

Documents as required.

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JOINT AVIATION REQUIREMENTS

CHECK LIST OF PAGES

JAR-FSTD H - HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

Initial issue dated 01 May 2008

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JAR-FSTD H

Paragraph

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JAR- FSTD H

P-1

01.05.08

PREAMBLE

JAR–FSTD H

Initial Issue

JAR–FSTD H comprises 3 Subparts (A, B and C) in Section 1, and 2 Subparts (B and C) in Section 2.

JAR-FSTD H is a simple amalgamation of JAR STD 1H, 2H and 3H into one document.

Section 1

Subpart A

Applicability to all Helicopter FSTD

Subpart B

Terminology for all Helicopter FSTD and implementation

Subpart C

Basic regulatory processes

Table of Standards in Appendix 1 to JAR-FSTD H.030 contains the standard for all devices

Section 2

Subpart B

Terminology and Abbreviations rationalised and harmonised with Helicopter STD standards documents.

Subpart C

Regulatory Processes combined.

Table of Objective Tests (ACJ No. 1 to JAR-FSTD H.030) contains the testing requirements for all devices.

Table of Functions and Subjective Tests (ACJ No. 1 to JAR-FSTD H.030) contains the testing requirements for

all devices

JAR-FSTD H

01.05.08

P-2

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD H

1-0-1

01.05.08

SECTION 1 – REQUIREMENTS

GENERAL

1.1

This Section contains the requirements for helicopter Flight Simulation Training Devices.

PRESENTATION

2.1

The requirements of JAR–FSTD H are presented in two columns on loose pages, each page

being identified by the date of issue and the Amendment number under which it is amended

or reissued.

2.2

Sub-headings are in italic typeface.

2.3

Explanatory Notes not forming part of the requirements appear in smaller typeface.

2.4

New, amended and corrected text will be enclosed within heavy brackets until a subsequent

‘Amendment’ is issued.

2.5

After each paragraph, the various changes and amendments, if any since the initial issue, are

indicated together with their date of issue.

INTENTIONALLY LEFT BLANK

JAR-FSTD H

SECTION 1

01.05.08

1-0-2

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD H

1-A-1

01.05.08

JAR–FSTD H.001 Applicability

JAR–FSTD H as amended applies to those

persons, organisations or enterprises (Flight

Simulation Training Devices (FSTD) operators)

seeking initial qualification of FSTDs.

The version of JAR-FSTD H agreed by the

Authority and used for issue of the initial

qualification shall be applicable for future

recurrent qualifications of the FSTD unless

recategorised.

FSTD users shall also gain approval to use

the FSTD as part of their approved training

programmes despite the fact that the FSTD

has been previously qualified.

INTENTIONALLY LEFT BLANK

INTENTIONALLY LEFT BLANK

SUBPART A - APPLICABILITY

SUBPART A - APPLICABILITY

JAR-FSTD H

SECTION 1

01.05.08

1-A-2

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD H

1-B-1

01.05.08

JAR–FSTD H.005 Terminology

(See ACJ to FSTD H.005)

Because of the technical complexity of FSTD

qualification,

it

is

essential

that

standard

terminology is used throughout. The following

principal terms and abbreviations shall be used in

order to comply with JAR–FSTD (H). Further

terms and abbreviations are contained in ACJ to

FSTD H.005.

(a)

Flight

Simulation

Training

Device

(FSTD). A training device which is a Full Flight

Simulator (FFS), a Flight Training Device (FTD), a

Flight & Navigation Procedures Trainer (FNPT).

(b)

Full Flight Simulator (FFS). A full size

replica of a specific type or make, model and series

helicopter flight deck, including the assemblage of

all equipment and computer programmes necessary

to represent the helicopter in ground and flight

operations, a visual system providing an out of the

flight deck view, and a force cueing motion system.

It is in compliance with the minimum standards for

FFS Qualification.

(c)

Flight Training Device (FTD). A full size

replica of a specific helicopter type’s instruments,

equipment, panels and controls in an open flight

deck area or an enclosed helicopter flight deck,

including the assemblage of equipment and

computer software programmes necessary to

represent the helicopter in ground and flight

conditions to the extent of the systems installed in

the device. It does not require a force cueing

motion or visual system. It is in compliance with

the minimum standards for a specific FTD Level of

Qualification.

(d)

Flight and Navigation Procedures Trainer

(FNPT). A training device which represents the

flight deck or cockpit environment including the

assemblage

of

equipment

and

computer

programmes necessary to represent a helicopter in

flight operations to the extent that the systems

appear to function as in a helicopter. It is in

compliance with the minimum standards for a

specific FNPT Level of Qualification.

(e)

Other Training Device (OTD). A training

aid other than FFS, FTD or FNPT which provides

for training where a complete flight deck

environment is not necessary.

(f)

Flight Simulation Training Device User

Approval (FSTD User Approval). The extent to

which an FSTD of a specified Qualification Level

may be used by persons, organisations or

enterprises as approved by the Authority. It takes

account of helicopter to FSTD differences and the

operating and training ability of the organization.

(g)

Flight

Simulation

Training

Device

Operator

(FSTD

operator). That

person,

organisation or enterprise directly responsible to

the Authority for requesting and maintaining the

qualification of a particular FSTD.

(h)

Flight Simulation Training Device User

(FSTD

User). The

person,

organization

or

enterprise requesting training, checking and testing

credits through the use of an FSTD.

(i)

Flight

Simulation

Training

Device

Qualification (FSTD Qualification). The level of

technical ability of an FSTD as defined in the

compliance document.

(j)

Qualification

Test

Guide

(QTG). A

document designed to demonstrate that the

performance and handling qualities of an FSTD

agree within prescribed limits with those of the

helicopter and that all applicable regulatory

requirements have been met. The QTG includes

both the helicopter and FSTD data used to support

the validation.

INTENTIONALLY LEFT BLANK

SUBPART B – GENERAL

JAR-FSTD H.005(f) (continued)

JAR-FSTD H

SECTION 1

01.05.08

1-B-2

INTENTIONALLY LEFT BLANK

SECTION 1

JAR-FSTD H

1-C-1

01.05.08

JAR–FSTD H.015 Application

for

FSTD

Qualification

(See ACJ No. 1 to JAR-

FSTD H.015)

(See ACJ No. 2 to JAR-

FSTD H.015)

(a)

The FSTD operator requiring evaluation

of a FFS, FTD, or FNPT shall apply to the

Authority giving 3 months notice. In exceptional

cases this period may be reduced to one month

at the discretion of the Authority.

(b)

An FSTD Qualification Certificate will be

issued following satisfactory completion of an

evaluation of the FFS, FTD or FNPT by the

Authority.

JAR–FSTD H.020

Validity

of

FSTD

Qualification

(See

ACJ

to

JAR-FSTD

H.020)

(a)

A FSTD qualification is valid for 12

months

unless

otherwise

specified

by

the

Authority.

(b)

A FSTD qualification revalidation can

take place at any time within the 60 days prior to

the expiry of the validity of the qualification

document. The new period of validity shall

continue from the expiry date of the previous

qualification document.

(c) The Authority shall refuse, revoke, suspend

or vary a FSTD qualification, if the provisions of

JAR–FSTD H are not satisfied.

JAR–FSTD H.025 Rules

Governing

FSTD

Operators

(See ACJ No. 1 to JAR-

FSTD H.025)

(See ACJ No. 2 to JAR-

FSTD H.025)

The FSTD operator shall demonstrate his

capability to maintain the performance, functions

and other characteristics specified for the FSTD

Qualification Level as follows

(a)

Quality System

(1)

Quality

System

shall

be

established and a Quality Manager designated

to monitor compliance with, and the adequacy

of,

procedures

required

to

ensure

the

maintenance of the Qualification Level of

FSTDs. Compliance monitoring shall include a

feedback system to the Accountable Manager

to ensure corrective action as necessary.

(2)

The Quality System shall include a

Quality Assurance Programme that contains

procedures

designed

to

verify

that

the

specified

performance,

functions

and

characteristics

are

being

conducted

in

accordance with all applicable requirements,

standards and procedures.

(3)

The

Quality

System

and

the

Quality Manager shall be acceptable to the

Authority.

(4)

The

Quality

System

shall

be

described in relevant documentation.

(b)

Updating. A link shall be maintained

between

the

operator’s

organization,

the

Authority and the relevant manufacturers to

incorporate important modifications, especially

(1)

Helicopter modifications which are

essential for training and checking shall be

introduced into all affected FSTDs whether or

not enforced by an airworthiness directive.

(2)

Modification of FSTDs, including

motion and visual systems (where applicable)

(i)

When essential for training

and checking, FSTD operators shall

update their FSTDs (for example in the

light of data revisions). Modifications of

the FSTD hardware and software which

affect

handling,

performance

and

systems

operation

or

any

major

modifications of the motion or visual

system shall be evaluated to determine

the impact on the original qualification

criteria. FSTD operators shall prepare

amendments for any affected validation

tests. The FSTD operator shall test the

FSTD to the new criteria.

(ii)

The

Authority

shall

be

advised

in

advance

of

any

major

changes to determine if the tests carried

out

by

the

FSTD

operator

are

satisfactory. A special evaluation of the

FSTD

may

be

necessary

prior

to

returning it to training following the

modification.

(c)

Installations. Ensure that the FSTD is

housed in a suitable environment which supports

safe and reliable operation.

SUBPART C – HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

JAR-FSTD H.025(a) (continued)

JAR-FSTD H

SECTION 1

01.05.08

1-C-2

(1)

The FSTD operator shall ensure

that the FSTD and its installation comply with

the local regulations for health and safety.

However, as a minimum all FSTD occupants

and maintenance personnel shall be briefed

on FSTD safety to ensure that they are

aware

of

all

safety

equipment

and

procedures in

the

FSTD

in

case

of

emergency.

(2)

The FSTD safety features such

as emergency stops and emergency lighting

shall be checked at least annually and

recorded by the FSTD operator.

(d)

Additional

Equipment.

Where

additional equipment has been added to the

FSTD

even

though

not

required

for

qualification, it will be assessed to ensure that

it does not adversely affect the quality of

training.

Therefore

any

subsequent

modification, removal or unserviceability of

such equipment could affect the qualification of

the device.

JAR–FSTD H.030 Requirements for FSTD

qualified on or after 1

August 2008

(See Appendix 1 to JAR–

FSTD H.030)

(See ACJ No. 1 to JAR-

FSTD H.030)

(See ACJ No. 2 to JAR-

FSTD H.030)

(See ACJ No. 3 to JAR-

FSTD H.030)

(See ACJ No. 4 to JAR-

FSTD H.030)

(See ACJ No. 5 to JAR-

FSTD H.030)

(a) Any FSTD submitted for initial evaluation

on or after 1 August 2008 will be evaluated

against applicable JAR-FSTD H criteria for the

Qualifications levels for which qualification has

been applied. Recurrent evaluations of a FSTD

will be based on the same version of JAR-

FSTD H that was applicable for its initial

evaluation. An upgrade will be based upon the

currently applicable version of JAR-FSTD H.

(b)

A FSTD shall be assessed in those

areas which are essential to completing the

flight crew member training, testing and

checking process as applicable.

(c)

The FSTD shall be subjected to

(1)

Validation tests and

(2)

Functions & subjective tests

(d)

Data shall be of a standard that

satisfies the Authority before the FSTD can

gain a Qualification Level.

(e)

The FSTD operator shall submit a

QTG in a form and manner which is acceptable

to the Authority.

(f)

The QTG will only be approved after

completion of an initial or upgrade evaluation,

and when all the discrepancies in the QTG

have been addressed to the satisfaction of the

Authority. After inclusion of the results of the

tests witnessed by the Authority, the approved

QTG becomes the Master QTG (MQTG), which

is the basis for the FSTD qualification and

subsequent recurrent FSTD evaluations

(g)

The FSTD operator shall

(1)

Run the complete set of tests

contained within the MQTG progressively

between each annual evaluation by the

Authority. Results shall be dated and

retained in order to satisfy both the FSTD

operator and the Authority that FSTD

standards are being maintained; and

(2)

Establish a Configuration Control

System to ensure the continued integrity of

the hardware and software of the qualified

FSTD.

JAR-FSTD H.031 Requirements

for

FFS

qualified on or after 1

April 2001 and before 1

August 2008

Any FFS submitted for initial evaluation on or

after 1 April 2001 and before 1 August 2008,

shall automatically be granted an equivalent

qualification under JAR-FSTD H with effect

from the re-evaluation conducted at the end of

the current validity period. This re-evaluation,

and all future re-evaluations, will be conducted

in accordance with the requirements of the

same version of JAR-STD 1H, which was

applicable for its last evaluation prior to

implementation of JAR-FSTD H. Any upgrade

will be based on the currently applicable

version of JAR-FSTD H.

JAR-FSTD H.025(c) (continued)

JAR-FSTD H.030(c) (continued)

SECTION 1

JAR-FSTD H

1-C-3

01.05.08

JAR-FSTD H.032

Requirements

for

Flight Training Devices (FTD) qualified on

or after 1 January 2004 and before 1 August

Any FTD submitted for initial evaluation on or

after 1 January 2004 and before 1 August

2008, shall automatically be granted an

equivalent qualification under JAR-FSTD H

with effect from the re-evaluation conducted at

the end of the current validity period. This re-

evaluation, and all future re-evaluations, will be

conducted

in

accordance

with

the

requirements of the same version of JAR-STD

2H, which was applicable for its last evaluation

prior to implementation of JAR-FSTD H. Any

upgrade will be based on the currently

applicable version of JAR-FSTD H.

JAR-FSTD H.033 Requirements for Flight &

Navigation

Procedures

Trainers (FNPT) qualified

on or after 1 January 2003

and before 1 August 2008

Any FNPT submitted for initial evaluation on or

after 1 January 2003 and before 1 August

2008, shall automatically be granted an

equivalent qualification under JAR-FSTD H

with effect from the re-evaluation conducted at

the end of the current validity period. This re-

evaluation, and all future re-evaluations, will be

conducted

in

accordance

with

the

requirements of the same version of JAR-STD

3H, which was applicable for its last evaluation

prior to implementation of JAR-FSTD H. Any

upgrade will be based on the currently

applicable version of JAR-FSTD H.

JAR–FSTD H.035 Requirements

for

Full

Flight

Simulators

approved

or

qualified

before 1 April 2001

(See ACJ to JAR-FSTD

H.035)

(a)

FFS

approved

or

qualified

in

accordance with national regulations of JAA

Member States before 1 April 2001 will either

be recategorised or will continue to maintain

their approval under the Grandfather Rights

provision, in accordance with sub-paragraphs

(c) and (d) below. For FFS which are not re-

categorized, maximum credit shall under no

circumstances

exceed

originally

issued

National credits.

(b)

FFS’s neither recategorised nor with

an approval maintained under the Grandfather

Rights

provision,

will

be

qualified

in

accordance with JAR–FSTD H.030.

(c)

FFS that are not recategorised but that

have a primary reference document used for

their testing may be qualified by the Authority

to an equivalent JAR–FSTD H Qualification

Level, either AG, BG, CG or DG. An upgrade

requires the recategorisation of the FFS.

(1)

To

gain

and

maintain

an

equivalent Qualification Level, these FFS

shall be assessed in those areas which are

essential to completing the flight crew

member training and checking process, as

applicable.

(2)

The FFS shall be subjected to

(i)

Validation tests; and

(ii)

Functions and subjective

tests.

(d)

FFS that are not recategorised and

that do not have a primary reference document

used for their testing, shall be qualified by

special arrangement. Such FFS will be issued

with a Special Category and shall be subjected

to functions and subjective tests corresponding

to those detailed within this document. In

addition any previously recognised validation

test shall be used.

JAR–FSTD H.036 Requirements for Flight

Training

Devices

approved

or

qualified

before 1 January 2004

No longer applicable.

INTENTIONALLY LEFT BLANK

JAR-FSTD H.035(a) (continued)

JAR-FSTD H

SECTION 1

01.05.08

1-C-4

JAR–FSTD H.037 Requirements for Flight

Navigation

Procedures

Trainers

approved

or

qualified before 1 January

(See ACJ to JAR-FSTD

H.037)

(a)

FNPTs

or

devices

approved

or

qualified

in

accordance

with

national

regulations of JAA Members States before 1

January 2003 will either be recategorised or

will continue to maintain their approval under

the

Grandfather

Rights

provision,

in

accordance with sub-paragraphs (c) and (d)

below. Grandfather Rights shall cease to exist

on the 1st January 2009. For FNPT which are

not recategorised maximum credits shall under

no circumstances exceed originally issued

National credits.

(b)

Recategorised FNPTs will be qualified

in accordance with JAR-FSTD H.030.

(c)

FNPTs that are not recategorised, but

that have a primary reference document used

for their testing, may continue under previous

authorisation, provided that they continue to

comply with the primary reference document.

(1)

To

gain

and

maintain

their

equivalent qualification level, these FNPTs

shall be assessed in those areas which are

essential to completing the flight crew

member training process, as applicable.

(2)

The devices shall be subjected

to

(i)

Validation tests and

(ii)

Functions and subjective

tests.

(d)

FNPTs that are not recategorised and

that do not have a primary reference document

used for their testing shall be qualified by

special arrangement. Such FNPTs will be

issued with a Special Category and shall be

subjected to Functions and Subjective Tests

corresponding to those detailed within this

document.

In

addition

any

previously

recognized Validation tests shall be used.

JAR–FSTD H.040 Changes

to

qualified

FSTD

(a)

Requirement to notify major changes

to a FSTD. The operator of a qualified FSTD

shall inform the Authority of proposed major

changes such as

(1)

Helicopter modifications which

could affect FSTD qualification.

(2)

FSTD hardware and or software

modifications

which

could

affect

the

handling qualities, performance or system

representations.

(3)

Relocation of the FSTD; and

(4)

Any deactivation of the FSTD.

The Authority may complete a special

evaluation following major changes or when a

FSTD appears not to be performing at its initial

Qualification Level.

(b)

Upgrade of a FSTD. A FSTD may be

upgraded to a higher Qualification Level.

Special evaluation is required before the award

of a higher Level of Qualification.

(1)

If an upgrade is proposed the

FSTD operator shall seek the advice of the

Authority and give full details of the

modifications. If the upgrade evaluation

does not fall upon the anniversary of the

original

qualification

date,

a

special

evaluation is required to permit the FSTD to

continue to qualify even at the previous

Qualification Level.

(2)

In the case of a FSTD upgrade,

an FSTD operator shall run all validation

tests for the requested Qualification Level.

Results from previous evaluations shall not

be used to validate FSTD performance for

the current upgrade.

(c)

Relocation of a FSTD

(1)

In instances where a FSTD is

moved to a new location, the Authority shall

be advised before the planned activity along

with a schedule of related events.

(2)

Prior to returning the FSTD to

service at the new location the FSTD

operator shall perform at least one third of

the validation tests and all functions and

subjective tests to ensure that the FSTD

performance meets its original qualification

standard. A copy of the test documentation

shall be retained together with the FSTD

records for review by the Authority.

(3)

An evaluation of the FSTD in

accordance

with

its

original

JAA

qualification

criteria

shall

be

at

the

discretion of the Authority.

(d)

Deactivation of a currently qualified

FSTD

JAR-FSTD H.040(a) (continued)

SECTION 1

JAR-FSTD H

1-C-5

01.05.08

(1)

If a FSTD operator plans to

remove a FSTD from active status for

prolonged periods, the Authority shall be

notified and suitable controls established for

the period during which the FSTD is

inactive.

(2)

The FSTD operator shall agree a

procedure with the Authority to ensure that

the FSTD can be restored to active status at

its original Qualification Level.

JAR–FSTD H.045 Interim

FSTD

Qualification

(See ACJ to JAR-FSTD

H.045)

(a)

In

the

case

of

new

helicopter

programmes, special arrangements shall be

made to enable an interim Qualification Level

to be achieved.

(b) For Full Flight Simulators, an interim

Qualification Level will only be granted at

levels A, B or C

(c)

Requirements, details relating to the

issue, and the period of validity of an interim

Qualification Level will be decided by the

Authority.

JAR–FSTD H.050 Transferability of FSTD

Qualification

When there is a change of FSTD operator

(a)

The new FSTD operator shall advise

the Authority in advance in order to agree upon

a plan of transfer of the FSTD.

(b)

At the discretion of the Authority, the

FSTD shall be subject to an evaluation in

accordance with its original JAA qualification

criteria.

(c)

Provided that the FSTD performs to its

original standard, its original Qualification

Level

shall

be

restored.

Revised

user

approval(s) may also be required.

INTENTIONALLY LEFT BLANK

INTENTIONALLY LEFT BLANK

JAR-FSTD H.040(d) (continued)

JAR-FSTD H

SECTION 1

01.05.08

1-C-6

Appendix 1 to JAR-FSTD H.030

Flight Simulation Training Device Standards General

This appendix describes the minimum Full Flight Simulator (FFS), Flight Training Device (FTD) and

Flight Navigation Procedures Trainer (FNPT) requirements for qualifying devices to the required

Qualification Levels. Certain requirements included in this section shall be supported with a statement

of compliance (SOC) and, in some designated cases, an objective test. The SOC will describe how the

requirement was met. The test results shall show that the requirement has been attained. In the

following tabular listing of FSTD standards, statements of compliance are indicated in the compliance

column.

For FNPT use in Multi-Crew Co-operation (MCC) training the general technical requirement are

expressed in the MCC column with additional systems, instrumentation and indicators as required for

MCC training and operation.

For MCC (Multi Crew Co-operation) minimum technical requirements are as for Level II or III, with the

following additions or amendments

Multi engine and multi pilot helicopter

Performance reserves, in case of an engine failure, to be in accordance with CAT. A criteria.

Anti icing or de-icing systems

Fire detection / suppression system

Dual controls

Autopilot with upper modes

2 VHF transceivers

2 VHF NAV receivers (VOR, ILS, DME)

1 ADF receiver

1 Marker receiver

1 transponder

Weather radar

The following indicators shall be located in the same positions on the instrument panels of both pilots

Airspeed

Flight attitude

Altimeter and radio altimeter

HSI

Vertical speed

ADF

VOR, ILS, DME

Marker indication

Stop watch

1-C-7

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

a.1

A flight deck that is a full-scale replica of the

helicopter

simulated.

Additional

required

crewmember duty stations and those required

bulkheads aft of the pilot seats are also

considered part of the cockpit and shall

replicate the helicopter.

A flight deck that replicates the helicopter.

a.2

The flight deck, including the instructor’s station

is fully enclosed.

A flight deck, including the instructor’s station

that is sufficiently closed off to exclude

distractions.

b.1

Full size panels with functional controls,

switches,

instruments

and

primary

and

secondary flight controls, which shall be

operating in the correct direction and with the

correct range of movement.

For FTD Level 1 as appropriate for the replicated

system

The use of electronically displayed images with

physical overlay incorporating operable switches,

knobs and buttons may be acceptable. This option

is not acceptable for analogue instruments in FFS.

Functional controls, switches, instruments and

primary and secondary flight controls sufficient

for the training events to be accomplished,

shall be located in a spatially correct area of

the flight deck.

The use of electronically displayed images with

physical overlay incorporating operable switches,

knobs and buttons is acceptable.

01.05.08

1-C-8

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTIO

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

c.1 Lighting for panels and instruments shall be as

per the helicopter.

Lighting for panels and instruments shall be

sufficient for the training events

c.2 Flight deck ambient lighting environment shall be

dynamically consistent with the visual display and

sufficient for the training event.

The ambient lighting should provide an

even level of illumination which is not

distracting to the pilot.

d.1

Relevant flight deck circuit breakers shall be located

as per the helicopter and shall function accurately

when

involved

in

operating

procedures

or

malfunctions requiring or involving flight crew

response.

e.1

Effect of aerodynamic changes for various

combinations of airspeed and power normally

encountered in flight, including the effect of

change in helicopter attitude, aerodynamic and

propulsive

forces

and

moments,

altitude,

temperature, mass, centre of gravity location

and configuration.

Effects of Cg, mass and configuration changes are not

required for FNPT Level I.

Aerodynamic and environment modelling shall

be

sufficient

to

permit

accurate

systems

operation and indication.

1-C-9

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

COMPLIANCE

e.2

Aerodynamic modelling which includes ground

effect, effects of airframe and rotor icing (if

applicable), aerodynamic interference effects

between the rotor wake and fuselage, influence

of the rotor on control and stabilization systems,

and representations of nonlinearities due to

sideslip, vortex ring and retreating blade stall.

f.1

Validation flight test data shall be used as the

basis for flight and performance and systems

characteristics.

Representative/generic

aerodynamic

data

tailored to the helicopter with fidelity sufficient to

meet the objective tests and sufficient to permit

accurate system operation and indication.

Aerodynamic data need not be necessarily

based on flight test data.

g.1

All relevant flight deck instrument indications

automatically respond to control movement by a

crewmember,

helicopter

performance,

or

external simulated environmental effects upon

the helicopter

01.05.08

1-C-10

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

COMPLIANCE

h.1

All

relevant

communications,

navigation,

caution

and

warning

equipment

shall

correspond to that installed in the helicopter.

All simulated navigation aids within range

shall

be

usable

without

restriction.

Navigational data shall be capable of being

updated.

For FTD 1 applies where the appropriate systems

are replicated.

h.2

Navigation equipment corresponding to that

of a helicopter, with operation within the

tolerances typically applied to the airborne

equipment. This shall include communication

equipment

(interphone

and

air/ground

communications systems).

h.3

Navigational data with the corresponding

approach facilities. Navigation aids should be

usable within range without restriction

For FFSs and FTDs the navigation database

should be updated within 28 days.

For FNPTs complete navigational data for at

least

different

European

airports

with

corresponding

precision

and

non-precision

approach

procedures

including

current

updating within a period of 3 months.

i.1

In addition to the flight crewmember stations, at least

two suitable seats for the instructor and an additional

observer shall be provided permitting adequate

vision to the crewmembers' panel and forward

windows. Observer seats need not represent

those found in the helicopter but shall be

adequately secured to the floor of the flight

simulator, fitted with positive restraint devices and be

The Authority will consider options to this standard

based on unique cockpit configurations.

Any additional seats installed shall be equipped with

similar safety provisions.

1-C-11

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

COMPLIANCE

of sufficient integrity to safely restrain the occupant

during any known or predicted motion system

excursion.

i.2

Crewmember seats shall afford the capability for the

occupants to be able to achieve the design eye

reference position. In addition to the flight

crewmember stations, at least two suitable seats for

the instructor and an additional observer shall be

provided

permitting

adequate

vision

to

the

crewmembers' panel and forward windows.

The instructor's and observer’s seats need not

represent those found in the helicopter.

01.05.08

1-C-12

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

j.1

FFS systems shall simulate the applicable

helicopter system operation, both on the ground

and in flight.

Systems shall be operative to the extent that

normal, abnormal, and emergency operating

procedures

appropriate

to

the

simulator

application can be accomplished. Once activated,

proper system operation shall result from system

management by the flight crew and not require

input from instructor controls.

j.2

FTD systems represented shall be fully operative

to

the

extent

that

normal,

abnormal

and

emergency

operating

procedures

can

be

accomplished. Once activated, proper system

operation shall result from system management by

the flight crew and not require input from instructor

controls.

j.3

The systems should be operative to the extent that

it should be possible to perform normal, abnormal,

and emergency operations appropriate to a

helicopter as required for training. Once activated,

proper systems operations should result from the

system management by the crewmember and not

require any further input from the instructor’s

controls.

k.1

The instructor shall be able to control system

variables and insert abnormal or emergency

conditions into the helicopter systems.

Independent freeze and reset facilities shall be

provided.

FNPT I: applicable only to enable the instructor to

carry

out

selective

failure

of

basic

flight

instruments and navigation equipment.

For FNPT Level I: Ability to set the FNPT to

minimum IMC speed or above

1-C-13

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

l.1

Control forces and control travel which correspond

to that of the replicated helicopter. Control forces

shall react in the same manner as in the helicopter

under the same flight conditions.

For Level A only static control force

characteristics need to be tested.

Control forces and control travel shall be

representative of the replicated helicopter under the

same flight conditions as in the helicopter..

For FTD level 1 as appropriate for the system

training required

Control forces and control travel shall broadly

correspond to that of a helicopter.

Only static control force characteristics need to be tested.

Control forces and control travels shall respond in

the same manner under the same flight conditions

as in a helicopter.

Only static control force characteristics need to be tested.

l.2

Cockpit control dynamics, which replicate the

helicopter simulated. Free response of the controls

shall match that of the helicopter within the given

tolerance. Initial and upgrade evaluation will include

control free response (cyclic, collective, and pedal)

measurements recorded at the controls. The

measured responses shall correspond to those of

the helicopter in ground operations, hover, climb,

cruise, and auto-rotation.

For helicopters with irreversible control systems,

measurements may be obtained on the ground.

Engineering validation or helicopter manufacturer

rationale will be submitted as justification for

ground test or to omit a configuration.

For FFS requiring static and dynamic tests at the

controls, special test fixtures will not be required

during the initial evaluations if the FSTD operator’s

QTG shows both test fixture results and alternate

test method results, such as computer data plots,

which were obtained concurrently. Use of the

alternate method during initial evaluation may then

satisfy this test requirement.

FTD Level 2 data can be representative/generic

and need not necessarily be based on flight test

data.

01.05.08

1-C-14

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

m.1 Ground handling and aerodynamic programming to

include the following

Ground effect - hover and transition IGE.

(Ground reaction - reaction of the helicopter upon

contact with the landing surface during landing to

include strut deflections, tire or skid friction, side

forces, and other appropriate data, such as weight

and speed, necessary to identify the flight condition

and configuration.

Ground handling characteristics -- control inputs to

include braking, deceleration turning radius and the

effects of crosswind.

Level A can utilise generic simulation of ground

effect and ground handling.

Ground handling and aerodynamic ground effects

models should be provided to enable lift-off, hover,

and touch down effects to be simulated and

harmonized with the sound and visual system.

Generic ground handling and aerodynamic

ground effects models should be provided to

enable lift-off, hover, and touch down effects

to be simulated and harmonized with the

sound and visual system.

1-C-15

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

n.1

Instructor controls for

(i) Wind speed and direction

(ii) Turbulence

(iii) Other atmospheric models to support the

required training.

Examples: Generic atmospheric models of local wind

patterns around mountains and structures..

(iv) Adjustment of cloud base and visibility.

(v) Temperature and barometric pressure.

o.1

Representative stopping and directional control

forces for at least the following landing surface

conditions based on helicopter related data, for a

running landing.

(i)

Dry

(ii)

Wet (soft surface and hard surface)

(iii)

Icy

(iv)

Patchy Wet

(v)

Patchy Icy

p.1

Representative brake and tire failure dynamics.

q.1

Cockpit control dynamics, which replicate the

helicopter simulated. Free response of the

controls shall match that of the helicopter within

the

given

tolerance.

Initial

and

upgrade

evaluation will include control free response

(cyclic, collective, and pedal) measurements

recorded

at

the

controls.

The

measured

responses shall correspond to those of the

helicopter in ground operations, hover, climb,

For helicopters with irreversible control systems,

measurements may be obtained on the ground.

Engineering validation or helicopter manufacturer

rationale will be submitted as justification for

ground test or to omit a configuration.

For FFS requiring static and dynamic tests at the

controls, special test fixtures will not be required

during the initial evaluations if the FSTD perator’s

QTG shows both test fixture results and alternate

01.05.08

1-C-16

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

cruise, and auto-rotation.

test method results, such as computer data plots,

which were obtained concurrently. Use of the

alternate method during initial evaluation may

then satisfy this test requirement. FTD Level 2

aerodynamic data can be representative/generic

and need not necessarily be based on flight test

data.

r.1

(1)

Transport delay. Transport delay is the

time between control input and the individual

hardware (systems) responses.

As an alternative, a Latency test may be used

to demonstrate that the flight simulator

system does not exceed the permissible

delay.

For FTD Level 1, only instrument response is

required within a maximum permissible delay of

200 milliseconds

For Level 'A' & 'B' FFS and Level 2 FTD the

maximum permissible delay is 150 milliseconds

For Level 'C' & ‘D’ FFS and Level 3 FTD the

maximum permissible delay is 100 milliseconds

(2)

Latency. Relative response of the visual

system, cockpit instruments and initial motion

system response shall be coupled closely to

provide integrated sensory cues. These systems

shall respond to abrupt pitch, roll, and yaw

inputs at the pilot's position within the

permissible delay, but not before the time, when

the helicopter would respond under the same

conditions. Visual scene changes from steady

state disturbance shall occur within the system

dynamic response limit but not before the

resultant motion onset.

For FTD Level 1 and FNPT Level I, only instrument

response is required within a maximum permissible

delay of 200 milliseconds

For Level 'A' & 'B' FFS, Level 2 FTD and FNPT

Level II and III the maximum permissible delay is

150 milliseconds

For Level 'C' & 'D' FFS and Level 3 FTD the

maximum permissible delay is 100 milliseconds

1-C-17

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.1 General

B

C

D

I

II

III

MCC

s.1

A means for quickly and effectively testing

FSTD programming and hardware. This may

include an automated system, which could

be used for conducting at least a portion of

the tests in the QTG.

Recommended for FTD Level 1,FNPT Level I and II

Automatic flagging of "out-of-tolerance" tests results

is encouraged.

Self-testing for FSTD hardware and programming

to

determine

compliance

with

the

FSTD

performance tests. Evidence of testing shall

include FSTD number, date, time, conditions,

tolerances, and the appropriate dependent

variables portrayed in comparison with the

helicopter standard

t.1

A system allowing for timely continuous updating of

FSTD hardware and programming consistent with

helicopter modifications.

u.1

The FSTD operator shall submit a Qualification

Test Guide in a form and manner acceptable to the

Authority. A recording system shall be provided that

will enable the FSTD performance to be compared

with QTG criteria.

v.1

FSTD computer capacity, accuracy, resolution and

dynamic response sufficient for the Qualification

Level sought.

w.1

Daily preflight documentation either in the daily

log or in a location easily accessible for review.

01.05.08

1-C-18

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD STANDARDS

1.2 Motion System

B

C

D

I

II

III

MCC

COMPLIANCE

a.1

Motion cues as perceived by the pilot shall be

representative of the helicopter, e.g. touchdown

cues should be a function of the simulated rate of

descent.

Motion tests to demonstrate that each axes onset

cues are properly phased with pilot input and

helicopter response.

b.1

A motion system

Having a minimum of 3 degrees of freedom

(pitch, roll, heave) to accomplish the required

task.

6 degrees of freedom synergistic platform

motion system

The instructor's and observer’s seats need not

represent those found in the helicopter.

For level B, a reduced motion performance

envelope is acceptable.

c.1 A means of recording the motion response time

as required

See para 1.1 (r.1) above.

1-C-19

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.2 Motion System

B

C

D

I

II

III

MCC

d.1

Special effects programming to include the

following

(1) Runway rumble, oleo deflections, effects

of groundspeed and uneven surface

characteristics.

(2) Buffet due to translational lift.

(3) Buffet during extension and retraction of

landing gear.

(4) Buffet due to high speed and retreating

blade stall.

(5) Buffet due to vortex ring.

(6) Representative cues resulting from;

(i) touchdown

(ii) translational lift.

(7) Antitorque device ineffectiveness.

(8) Buffet due to turbulence.

For level A it may be of a generic nature

sufficient to accomplish the required tasks.

See Appendix 4 to ACJ No. 1 to JAR-FSTD

H.030 para 2.2 on Vibration Platforms for

Helicopter FSTDs.

01.05.08

1-C-20

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.2 Motion System

B

C

D

I

II

III

MCC

e.1 Characteristic vibrations/buffets that result

from operation of the helicopter and which

can be sensed in the cockpit. Simulated

cockpit vibrations to include seat(s), flight

controls and instrument panel(s), although

these need not be tested independently.

Statement of Compliance required.

Tests required with recorded results which

allow the comparison of relative amplitudes

versus frequency in the longitudinal, lateral

and vertical axes with helicopter data.. Steady

state tests are acceptable.

See Appendix 4 to ACJ No. 1 to JAR-FSTD

H.030 para 2.2 on Vibration Platforms for

Helicopter FSTDs.

1-C-21

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.3 Visual System

B

C

D

I

II

III

MCC

a.1

Visual system capable of meeting all the standards

of this paragraph and the respective paragraphs of

validation tests as well as functions and subjective

tests as applicable to the Level of Qualification

requested by the FSTD operator.

The choice of the display system and of the field of

view requirements should fully consider the intended

use of the FSTD. The balance between training and

testing/checking may influence the choice and

geometry of the display system. In addition the

diverse

operational

requirements

should

be

addressed.

b.1

Visual system capable of providing at least a 45

degree horizontal and 30 degree vertical field of

view simultaneously for each pilot.

Visual system capable of providing at least a 75

degrees horizontal and 40 degrees vertical field of

view simultaneously for each pilot.

“Continuous”, cross-cockpit, minimum visual field of

view providing each pilot with 150 degrees

horizontal and 40 degrees vertical

A minimum of 75 degrees horizontal field of view on

either side of the zero degree azimuth line relative to

the helicopter fuselage is required.

b.2

“Continuous,” cross-cockpit, minimum visual field of

view providing each pilot with 150 degrees

horizontal and 60 degrees vertical

A minimum of 75 degrees horizontal field of view on

either side of the zero degree azimuth line relative to

the helicopter fuselage is required. This will allow an

offset per side of the horizontal field of view if

required for the training.

Where training tasks require extended fields of view

beyond the 150 degrees x 60 degrees, then such

extended fields of view should be provided.

b.3

.“Continuous” cross cockpit, minimum visual field of

view providing each pilot with180 degrees horizontal

and 60 degrees vertical

A minimum of 75 degrees of horizontal field of view

on either side of zero degrees azimuth line relative

to the helicopter fuselage is required. This will allow

an offset per side of the horizontal field of view if

required for the training.

Where training tasks require extended fields of view

beyond the 180 degrees x 60 degrees, then such

extended fields of view shall be provided.

01.05.08

1-C-22

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.3 Visual System

B

C

D

I

II

III

MCC

c.1

A means of recording the visual response time for

the visual system shall be provided.

d.1

Visual cues to assess rate of change of height,

translational displacements and rates, during takeoff

and landing.

For Level 'A', Visual cueing sufficient to support

changes in approach path by using FATO

perspective

Visual cues to assess rate of change of height,

height AGL, translational displacements and rates,

during

takeoff,

low

altitude/low

airspeed

manoeuvring, hover, and landing.

e.1

Test procedures to quickly confirm visual system

colour, RVR, focus, intensity, level horizon, and

attitude as compared with the specified parameters.

Statement of compliance required. Test required

f.1

A minimum of 10 levels of occulting. This capability

should be demonstrated by a visual model through

each channel.

Statement of compliance required. Test required

g.1

Surface (Vernier) resolution shall be demonstrated

by a test pattern of objects shown to occupy a visual

angle of not greater than 3 arc minutes in the visual

display used on a scene from the pilot's eye point..

Statement of compliance required. Test required

h.1

Lightpoint size shall not be greater than 6 arc

minutes

This is equivalent to a light point resolution of 3 arc

minutes.

Lightpoint size shall not be greater than 8 arc

minutes

This is equivalent to a light point resolution of 4 arc

minutes.

1-C-23

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.3 Visual System

B

C

D

I

II

III

MCC

i.1

Daylight, dusk, and night visual scenes with

sufficient scene content to recognise aerodromes,

heliports, terrain, and major landmarks around the

Final Approach and Take-off (FATO) area and to

successfully accomplish low airspeed/low altitude

manoeuvres to include lift-off, hover, translational

lift, landing and touchdown.

j.1

A visual database sufficient to support the requirements,

including

(i)

Specific areas within the database

needing higher resolution to support

landings, take-offs and ground cushion

exercises and training away from a

heliport. Including elevated helipad,

helidecks and confined areas

(ii)

For cross-country flights sufficient scene

details to allow for ground to map

navigation over a sector length equal to

30 minutes at an average cruise speed.

(iii)

For offshore airborne radar approaches

(ARA), harmonized visual/radar

representations of installations.

(iv)

(For training in the use of Night Vision

Goggles (NVG) a visual display with the

ability to represent various scenes with

the required levels of ambient

light/colour.

Generic database is acceptable only for FTDs and

FNPTs.

Where applicable

Where applicable

Where applicable

01.05.08

1-C-24

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.3 Visual System

B

C

D

I

II

III

MCC

k.1

Daylight, twilight (dusk/dawn) and night visual

capability for system brightness and contrast ratio

criteria as applicable for level of qualification

sought.

Night and Dusk scene

The ambient lighting should provide an even level of

illumination, which is not distracting to the pilot.

k.2

The visual system should be capable of producing

Full colour presentations.

Full colour texture shall be used to enhance visual cue

perception for illuminated landing surfaces.

k.3

The visual system should be capable of

producing, as a minimum

(1) A scene content comparable in detail with that

produced by 6,000 polygons for daylight and 1000

visible light points for night and dusk scenes for the

entire visual system.

(2) A scene content comparable in detail with that

produced by 4,000 polygons for daylight and 5000

visible light points for night and dusk scenes for the

entire visual system

(3) A scene content comparable in detail with

that produced by 6,000 polygons for daylight

and 7000 visible light points for night and

dusk scenes for the entire visual system.

Statement of Compliance required.

Test required.

Freedom of apparent quantization and other

distracting visual effects are also applicable for

Levels A and B.

l.1

Surface contrast ratio

Demonstration model

Not less than 5:1.

Not less than 8:1

1-C-25

01.05.08

Appendix 1 to JAR-FSTD H.030 (continued)

SECTION 1

JAR–FSTD H

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.3 Visual Systems

B

C

D

I

II

III

MCC

l.2

Lightpoint contrast ratio.

Not less than 25:1.

m.1

Highlight Brightness. The minimum light measured at

the pilot's eye position should be

14 cd/m² (4 ft-Lamberts)

17 cd/m² (5ft-Lamberts)

20 cd/m² (6 ft-Lamberts)

01.05.08

1-C-26

Appendix 1 to JAR-FSTD H.030 (continued)

JAR- FSTD H

SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD STANDARDS

1.4

Sound Systems

B

C

D

I

II

III

MCC

a.1

Significant flight deck sounds, and those, which

result from pilot actions corresponding to those

of the helicopter shall be provided.

For FTD level 1 as appropriate for the system

training required.

Statement of Compliance required for FFS.

a.2

Sounds due to engines, transmission and rotors

should be available

b.1

Sound of precipitation, windshield wipers, the

sound resulting from a blade strike and a crash

condition when operating the helicopter in

excess of limitations.

Crash sounds may be generic

Statement of Compliance or Demonstration of

representative sounds required.

c.1

Realistic amplitude and frequency of cockpit

acoustic environment.

Objective steady-state tests required

d.1

The volume control shall have an indication of

sound level setting which meets all qualification

requirements.

SECTION 1

JAR-FSTD H

1-C-27

01.05.08

These standards always refer to the type of helicopter being simulated, except for FNPT, which may be generic.

For FNPT, the term “the/a helicopter” is used to represent the aircraft being modelled which can be a specific

helicopter type, a family of similar helicopter types or a totally generic helicopter.

Wherever the term runway is used, it includes runways and FATO/TLOF.

INTENTIONALLY LEFT BLANK

Appendix 1 to JAR-FSTD H.030 (continued)

JAR-FSTD H

SECTION 1

01.05.08

1-C-28

INTENTIONALLY LEFT BLANK

Editeur

Service Central de Législation, 43, boulevard F.-D. Roosevelt, L-2450 Luxembourg

Imprimeur: Association momentanée Imprimerie Centrale / Victor Buck