a - n° 128 / 21 juillet 2014data.legilux.public.lu/file/eli-etat-leg-memorial-2014... · 1991...

1623

MEMORIALJournal Officiel

du Grand-Duché deLuxembourg

MEMORIALAmtsblatt

des GroßherzogtumsLuxemburg

RECUEIL DE LEGISLATION

A –– N° 110 22 mai 2009

1983

A –– N° 128 21 juillet 2014

S o m m a i r e

Règlement grand-ducal du 10 mars 2014 sur le certificat de qualification des entreprises exploitant des entraîneurs synthétiques de vol pour avions et hélicoptères page 1984

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1984

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:

Art 1er Champ d’applicationLe 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.

Art 2 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.

Art 3 Durée de validité du certificat de qualificationLa 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.

Art 4 Retrait du certificat de qualificationLa 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;

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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).

Art 5 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).

Art 6 ExceptionsDans 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.

Art 7 Vérifications et surveillanceLa 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.

Art 8 Dispositions transitoiresLa 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.

Art 9 Disposition finaleNotre 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

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1986

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

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1987

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

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1988

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 ([email protected]).

*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

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1989

JAR-FSTD A

C-1 01.05.08

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

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INTENTIONALLY LEFT BLANK

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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

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Paragraph Page

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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)

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C-5 01.05.08

ACJ No.2 to 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 ACJ to FSTD A.045 New Aeroplane FFS/FTD Qualification – Additional Information 2-C-147


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FOREWORD

1 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.

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

basis for showing compliance with their national codes. 3 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.

4 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.

5 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.

6 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.

7 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.

8 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. 9 New, amended and corrected text will be enclosed within heavy brackets until a subsequent

‘Amendment’ is issued. 10 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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JOINT AVIATION REQUIREMENTS

CHECK LIST OF PAGES

JAR-FSTD A - AEROPLANE FLIGHT SIMULATION TRAINING DEVICES

Initial issue dated 01 May 2008 The following pages of JAR-FSTD A are now current: Page No Legend Date Title Page Initial issue 01.05.08 ii Initial issue 01.05.08 C-1 Initial Issue 01.05.08 C-2 Initial Issue 01.05.08 C-3 Initial Issue 01.05.08 C-4 Initial Issue 01.05.08 C-5 Initial Issue 01.05.08 C-6 Initial Issue 01.05.08 F-1 Initial Issue 01.05.08 F-2 Initial Issue 01.05.08 CL-1 Initial Issue 01.05.08 CL-2 Initial Issue 01.05.08 CL-3 Initial Issue 01.05.08 CL-4 Initial Issue 01.05.08 P-1 Initial Issue 01.05.08 P-2 Initial Issue 01.05.08 1-0-1 Initial Issue 01.05.08 1-0-2 Initial Issue 01.05.08 1-A-1 Initial Issue 01.05.08 1-A-2 Initial Issue 01.05.08 1-B-1 Initial Issue 01.05.08 1-B-2 Initial Issue 01.05.08 1-C-1 Initial Issue 01.05.08 1-C-2 Initial Issue 01.05.08 1-C-3 Initial Issue 01.05.08 1-C-4 Initial Issue 01.05.08 1-C-5 Initial Issue 01.05.08 1-C-6 Initial Issue 01.05.08 1-C-7 Initial Issue 01.05.08 1-C-8 Initial Issue 01.05.08 1-C-9 Initial Issue 01.05.08 1-C-10 Initial Issue 01.05.08 1-C-11 Initial Issue 01.05.08 1-C-12 Initial Issue 01.05.08 1-C-13 Initial Issue 01.05.08 1-C-14 Initial Issue 01.05.08 1-C-15 Initial Issue 01.05.08 1-C-16 Initial Issue 01.05.08 1-C-17 Initial Issue 01.05.08 1-C-18 Initial Issue 01.05.08

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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.

L U X E M B O U R G

2002

JAR-FSTD A

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L U X E M B O U R G

2003

SECTION 1 JAR-FSTD A

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1 GENERAL

1.1 This Section contains the requirements for aeroplane Flight Simulation Training Devices. 2 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.

L U X E M B O U R G

2004

JAR-FSTD A SECTION 1

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L U X E M B O U R G

2005

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.



L U X E M B O U R G

2006

JAR–FSTD A SECTION 1

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2007


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.


SUBPART B - GENERAL

(JAR-FSTD A.005 continued)

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2009


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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) A 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)

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(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 A 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)

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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)

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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)

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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.


JAR-FSTD A.040 (continued)

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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:

1 Turbo-jet or turbo-prop engines. 2 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. 3 Retractable landing gear. 4 Pressurisation system. 5 De-icing systems 6 Fire detection / suppression system 7 Dual controls 8 Autopilot with automatic approach mode 9 2 VHF transceivers including oxygen masks intercom system 10 2 VHF NAV receivers (VOR, ILS, DME) 11 1 ADF receiver 12 1 Marker receiver 13 1 transponder The following indicators shall be located in the same positions on the instrument panels of both pilots: 1 Airspeed 2 Flight attitude with flight director 3 Altimeter 4 Flight director with ILS (HSI)

5 Vertical speed

6 ADF

7 VOR

8 Marker indication (as appropriate)

9 Stop watch (as appropriate)


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

01.05.08 1-C-8

FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

1.1

G

ener

al

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

a.1

A fully

enclose

d flight dec

k �

�

�

�

a.2

A coc

kpit/

flight dec

k su

fficiently

enclose

d to

exclu

de

distraction,

which

will

replicate that

of the

aeroplane

or

class

of aeroplane

simulated

�

�

�

�

�

a.3

Flight

dec

k, a

full scale replica of

the

aeroplane

simulated

.

Equipment for

operation of

the cockpit win

dows shall

be inclu

ded in

the

FSTD

, but the actual

win

dows

need

not

be operable

.

The

flight

deck

, for FSTD

purposes,

consists of

all

that

space

forwar

d of

a cross

section of

the

fuselage

at

the

most extreme aft setting

of the pilots

' seats

. A

dditional

require

d flight crewmem

ber

duty

stations

an

d those require

d bulkheads aft of

the

pilot seats

are also

consi

dere

d part

of the

flight dec

k an

d shall

replicate the aeroplane.

�

�

�

�

Flight

dec

k observer

seats

are

not

consi

dere

d to

be

additional flight

cre

wmem

ber

duty

stations

and

may

be

omitted

.

Bul

khea

ds containing items such

as switches,

circuit

brea

kers

, supplementary

radio

panels,

etc

. to

which

the

flight cre

w may

require

access

during an

y event

after pre-

flight cockpit preparation is

complete are

considered

essential and

may

not

be omitted

.

Bul

khea

ds containing only

items such

as landing

gear

pin

storage

compartm

ents

, fire

axes

or

extinguishers

, spare light

bul

bs, aircra

ft document

pouches etc.

are

not

consi

dere

d essential and

may

be

omitted

. Such items,

or reasonable

facsimile

, shall still

be availa

ble in

the

FSTD

but

may

be

relocate

d to

a suita

ble location as

near as

practical

to

the

original

position

. Fire

axes an

d an

y similar

purpose instruments

nee

d only

be represente

d in

silhouette

.

a.4

Direction of

movement of

controls

an

d switches

identical

to that

in the aeroplane.

�

�

�

�

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SECTION 1 JAR-FSTD AAppendix 1 to JAR-FSTD A.030 (continued)

FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

1.1

G

ener

al

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

a.5

A full si

ze panel

of replicated

system

(s)

which

will

have

actuation

of controls

an

d switches

that

replicate those of

the aeroplane simulated

.

�

�

The use of

electronically

displa

yed images

with

ph

ysical

overla

y incorporating operable

switches,

knobs,

buttons

replicating aeroplane instruments

panels

may

be acceptable

.

a.6

Coc

kpit/

flight

deck

switches,

instruments

, equipment,

panels

, systems,

primar

y an

d secondar

y flight

controls

su

fficient for

the training events

to be accomplishe

d shall

be locate

d in

a spatially

correct

flight

dec

k area

and

will

operate as

, and

represent

those in

, that aeroplane

or

class of

aeroplane

.

�

�

�

�

For

Multi-

Cre

w

Co-operation

(MC

C) qualification

additional instrumentation an

d in

dicators

may

be

require

d. See

table at

start of

this

appen

dix.

.

For B

ITDs the switches an

d controls

size an

d shape

and

their

location

in the

cockpit shall

be

representative.

a.7

Cre

w mem

bers

seats

shall

be provided

with

su

fficient ad

justment to

allo

w the occupant

to

achieve

the

design

eye

reference

position

appropriate

to the aeroplane or

class

of aeroplane

and

for the

visual s

ystem

to be installe

d to

align

with

that

eye

position

.

�

�

�

b.1

Circuit breakers that

affect

proce

dures an

d/or

result

in o

bserva

ble cockpit in

dications

properly

located

an

d functionally

accurate.

�

�

�

�

�

�

�

�

L U X E M B O U R G

2018


01.05.08 1-C-10

FFS

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LEVE

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1.1

G

ener

al

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

c.1

Flight

dynamics model

that accounts

for

various

com

binations

of

drag

an

d thrust

normally

encountere

d in

flight

correspon

ding

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

con

figuration.

�

�

�

�

�

�

�

�

�

�

For FTD

Levels

1 an

d 2 aero

dynamic

modelling

sufficient to

permit accurate

systems operation an

d in

dication is

accepta

ble.

For FN

PTs

and

BITDs class specific modelling is

acceptable

.

d.1

All relevant

instrument in

dications

involve

d in

the

simulation

of the

applicable

aeroplane

shall

automatically

respond

to control movement

by a

flight crewmem

ber or

induced

disturbance

to the

simulated

aeroplane

; e.g

., turbulence

or win

d shear.

�

�

�

�

�

�

�

�

�

�

For FN

PTs

instrument in

dications

suf

ficient

for

the

training events

to be accomplishe

d. Reference

ACJ

No.

3 to

JAR

-FSTD

A.0

30.

For

BITDs instrument in

dications

su

fficient

for the

training events

to be accomplishe

d. Reference

ACJ

No.

4 to

JAR

-FSTD

A.0

30.

d.2

Lighting environment

for panels

an

d instruments

shall be su

fficient for

the operation

being conducte

d.

�

�

�

�

�

�

For FTD

Level

2 lighting environment shall

be as per

aeroplane.

e.1

Communications

, navigation,

an

d caution

and

warning

equipment correspon

ding

to that

installe

d 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 correspon

ding

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)

.

�

�

�

�

L U X E M B O U R G

2019

1-C-11 01.05.08


FFS

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STA

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G

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A

B C

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2 I

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CC

CO

MP

LIA

NC

E

e.3

Navigational

data

with

the

correspon

ding

approach

facilities.

Navigation ai

ds shoul

d be

usa

ble

within

range

without restriction.

�

�

�

�

�

�

�

�

�

�

For FTD

1 applies

where

navigation equipment is

replicated

.

For all FFSs an

d FTDs

2 where

use

d for area

or

airfiel

d competence training or

checking,

navigation

data

shoul

d be

updated

within

28

days

.

For F

NPT

s and

BIT

Ds c

ompl

ete

navi

gatio

nal d

ata

for

at le

ast 5

diff

eren

t Eur

opea

n ai

rpor

ts w

ith

corr

espo

ndin

g pr

ecis

ion

and

non-

prec

isio

n ap

proa

ch

proc

edur

es in

clud

ing

curr

ent u

pdat

ing

with

in a

per

iod

of 3

mon

ths.

f.1

In a

ddition

to the

flight crewmem

ber

duty

stations

, three suita

ble seats

for the instructor

, delegate

d examiner

and

Authorit

y inspector. The Authorit

y will

consider

options

to this

standar

d base

d on

unique

cockpit configurations

. These seats shall provide

adequate

vision to

the

pilot’s

panel

and

for

war

d win

dows.

Observer seats need

not

represent

those

foun

d in

the

aeroplane

but

in the case

of FSTDs

fitte

d with

a motion system

, the seats shall

be

adequately

secured

to the

floor

of the FSTD

, fitte

d with

positive

restraint

devices an

d be

of su

fficient

integrity

to sa

fely

restrain

the

occupant

during an

y known or

pre

dicted

motion system

excursion

.

�

�

�

�

�

�

�

�

�

�

For

FTDs

and

FNPT’s

suita

ble

seating

arrangements

for

the

Instructor

and

Examiner

or

Authorit

y’s

Inspector shoul

d be

provi

ded.

For

BITDs suita

ble viewing arrangements

for

the

Instructor

shoul

d be

provi

ded.

L U X E M B O U R G

2020


01.05.08 1-C-12

FFS

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MP

LIA

NC

E

g.1

FSTD

systems shall simulate applicable

aeroplane

system

operation,

both on

the

groun

d an

d in

flight

. S

ystems shall

be operative to

the

extent that

all

normal

, abnormal

, an

d emergenc

y operating

procedures

can

be accomplishe

d.

�

�

�

�

�

�

�

�

For FTD

Level

1, applies

where

system

is simulated

. For F

NPTs

systems shall be operative to

the extent

that

it shall be possible

to per

form

all normal

, abnormal

and

emergenc

y operations

as may

be appropriate

to the

aeroplane or

class

of aeroplanes

being

simulated

and

as

require

d for the

training

.

h.1

Instructor

controls

shall enable

the operator

to

control all require

d system

varia

bles

an

d insert

abnormal

or

emergenc

y conditions

into

the

aeroplane systems.

�

�

�

�

�

�

�

�

�

�

Where

applicable

and

as require

d for training the

follo

wing shall be availa

ble

:

- Position an

d flight

free

ze.

- A

facilit

y to

ena

ble the

dynamic

plotting

of the

flight path on

approaches,

commencing

at the

final

approach

fix, inclu

ding

the vertical pro

file

- Har

d copy

of map

and

approach plot

L U X E M B O U R G

2021

1-C-13 01.05.08


FFS

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1.1

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ener

al

A

B C

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1

2 I

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CC

CO

MP

LIA

NC

E

i.1

Control forces an

d control travel shall correspond

to

that

of the

replicated

aeroplane

. Control forces shall

react in the same manner as

in the aeroplane un

der

the same

flight con

ditions

.

�

�

�

�

�

�

�

�

�

For FTD

Level

2 Control

forces

and

control travel

should

correspond

to

that

of

the

replicated

aeroplane

with

CT&

M.

It is

not

inten

ded that

the

device

shoul

d be

flown manually

other

than

for short

perio

ds

when

the

autopilot

is temporaril

y disengaged

.

For FN

PT

Level

I an

d BITDs control

forces

and

control travel shall

broa

dly correspond

to that

of the

replicated

aeroplane

or class of

aeroplane

. Control

force changes

due to

an

increase

/decrease in

aircra

ft spee

d are not necessary

.

In a

ddition

for F

NPT

Level I

I and

MC

C control forces

and control travels

shall respon

d in

the same

manner un

der the same

flight conditions as

in the

aeroplane or

class

of aeroplane

being

simulated

.

L U X E M B O U R G

2022


01.05.08 1-C-14

FFS

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al

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

j.1

Groun

d handling an

d aero

dynamic

programming

shall inclu

de:

(1)

Groun

d E

ffect

. For example:

round

-out

, flare

, an

d touchdown.

This

requires

data

on lift,

drag

, pitching

moment, trim

, and

power

groun

d ef

fect

.

(2)

Groun

d reaction – reaction of

the

aeroplane

upon

contact

with

the runway

during landing to

include strut

deflections

, tyre

friction,

si

de

forces

, an

d other appropriate

data,

such as

weight an

d spee

d, necessary

to identif

y the

flight con

dition an

d configuration.

(3)

Groun

d handling characteristics – steering

inputs

to

include crosswin

d, bra

king

, thrust

reversing,

deceleration an

d turning ra

dius

.

�

�

�

�

�

�

Statement o

f Compliance require

d. Tests

require

d.

For

Level

‘A’ FFS

, generic

groun

d handling to

the

extent

that allo

ws turns

within

the

con

fines

of the

runway

, adequate

control on

flare

, touchdown an

d roll-out (including

from

a cross

-win

d landing)

onl

y is

acceptable

.

For FN

PTs

a generic

groun

d handling model

nee

d only

be provided

to enable

representative

flare

and

touch

down ef

fects.

L U X E M B O U R G

2023

1-C-15 01.05.08


FFS

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CO

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NC

E

k.1

Win

dshear

models shall provide training in

the

specific skills require

d for recognition

of

win

d shear

phenomena an

d execution of

recover

y manoeuvres.

Such models shall be representative of

measure

d or

acci

dent

derived

win

ds,

but

may

include

simplifications

which

ensure repeatable

encounters.

For example,

models may

consist

of in

dependent

varia

ble

win

ds in

multiple

simultaneous components.

Win

d models shall

be availa

ble

for the

follo

wing

critical phases of

flight

:

(1)

Prior to ta

ke-o

ff rotation

(2)

At lift

-off

(3)

During initial

clim

b

(4)

Short

final

approach

�

�

Tests require

d.

See

ACJ

No

1 to

JAR

-FSTD

A.0

30, Para

2.3,

g.

l.1

Instructor

controls

for

environmental

effects

including

win

d spee

d an

d direction

shall

be

provided

.

�

�

�

�

�

�

�

�

�

�

For FTDs environment m

odelling su

fficient to permit

accurate

systems operation an

d in

dication.

L U X E M B O U R G

2024


01.05.08 1-C-16

FFS

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al

A

B C

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CO

MP

LIA

NC

E

m.1

Stopping an

d directional control

forces

shall

be

representative

for at

least the

follo

wing runway

conditions

base

d on

aeroplane

relate

d data

:

(1)

Dry

(2)

Wet

(3)

Icy

(4)

Patch

y wet

(5)

Patch

y ic

y

(6)

Wet

on ru

bber

resi

due in

touchdown

zone

.

�

�

Statement o


d.

Objective Tests require

d for

(1),

(2),

(3), Sub

jective

chec

k for (

4), (

5), (

6).

n.1

Bra

ke and

tyre

failure

dynamics

(including antis

kid)

an

d decrease

d brake

efficienc

y due

to

brake

temperatures shall be representative an

d base

d on

aeroplane relate

d data

.

�

�

Statement o


d.

Sub

jective test

is require

d for

decrease

d braking

efficienc

y due to

bra

ke temperature

, if applicable

.

o.1

A means

for quic

kly an

d ef

fectivel

y conducting

daily

testing of

FSTD

programming an

d hard

ware shall be

availa

ble.

�

�

Statement o


d.

p.1

Computer

capacity

, accuracy

, resolution,

an

d dynamic

response shall be su

fficient to

fully

support

the overall

fidelity

, including its

evaluation an

d testing.

�

�

�

�

�

�

Statement o


d.

L U X E M B O U R G

2025

1-C-17 01.05.08


FFS

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E

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

an

d upgrade evaluations

will

inclu

de control

free response

(pitch,

roll and

yaw

controller)

measurements

recor

ded at

the controls

. The measure

d responses shall correspon

d to

those of

the

aeroplane

in ta

ke-o

ff, cruise,

and

lan

ding

configurations

.

(1)

For aeroplanes

with

irreversi

ble control systems,

measurements

may

be obtained

on the ground

if

proper

pitot static

inputs are provide d

to represent

conditions typical of

those

encountered

in

flight.

Engineering validation or

aeroplane

manufacturer

rationale

will

be su

bmitted

as

justification to

groun

d test

or omit a configuration.

(2)

For FSTDs requiring

static

and

dynamic

tests

at

the controls

, special

test

fixtures

will

not

be

require

d during initial

evaluation if the FSTD

operator

’s

MQTG

shows

both

te

xt

fixture

results

and

alternate test

metho

d results

such

as computer

data

plots

, which

were obtained

concurrently

. Repetition

of

the

alternate

metho

d during initial

evaluation may

then

satis

fy this

requirement.

�

�

Tests require

d.

L U X E M B O U R G

2026


01.05.08 1-C-18

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1.1

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al

A

B C

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1

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CC

CO

MP

LIA

NC

E

r.1

One

of the

follo

wing two metho

ds is

accepta

ble as

a

means

to prove

compliance:

�

�

�

�

�

�

�

�

�

�

Tests require

d.

For Level

‘A’ &

‘B’ FFSs,

and

applicable

systems

for

FTDs,

FN

PTs

and

BITDs the maximum

permissi

ble

dela

y is

300

millisecon

ds.

(1

) Transport Delay

: A

transport

dela

y test

may

be

used

to

demonstrate

that the FSTD

system

response

does

not

excee

d 15

0 milliseconds.

This test

shall

measure

all the

dela

y encountere

d by

a step signal

migrating

from

the

pilot’s

control through the control

loading electronics

an

d interfacing

through all the

simulation so

ftware modules

in the correct order

, using

a handshaking protocol

, finally

through

the

normal

output

inter

faces to

the

motion system

, to

the

visual

system

and

instrument displays.

(see

next page)

L U X E M B O U R G

2027

1-C-19 01.05.08


FFS

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A

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1

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LIA

NC

E

(continue

d)

(2)

Latenc

y: The

visual

system

, flight

deck

instruments

and

initial motion system

response

shall respond

to a

brupt pitch,

roll an

d ya

w inputs

from

the

pilot's

position

within

150

milliseconds

of the

time,

but

not

before the time,

when the

aeroplane

would

respon

d un

der the

same

conditions.

L U X E M B O U R G

2028


01.05.08 1-C-20

FL

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TRA

ININ

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EV

ICE

STA

NDARDS

FFS

LE

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FTD

LE

VEL

FNPT

LEVE

L B

ITD

CO

MP

LIA

NC

E

1.1

G

ener

al

A

B C

D

1

2 I

II M

CC

s.1

Aerod

ynamic

modelling shall be provided

. This

shall

include,

for aeroplanes

issued

an

original

type

certi

ficate after June

198

0, low

altitu

de level

flight

ground

effect

, Mach ef

fect

at high

altitu

de, normal

an

d reverse

dynamic

thrust

ef

fect

on

control

surfaces,

aeroelastic

representations

, an

d representations

of

non-linearities

due to

si

deslip

base

d on

aeroplane

flight

test

data

provi

ded

by the

manufacturer.

�

�

Statement of

Compliance require

d. Mach ef

fect

, aeroelastic

representations

, an

d non-linearities

due to

sideslip

are

normally

included

in the

FSTD

aero

dynamic

model

. The

Statement o

f Compliance

shall a

ddress

each of

these

items.

Separate tests

for thrust

effects an

d a Statement of

Compliance

are require

d.

t.1

Modelling that

inclu

des the ef

fects of

airframe an

d engine

icing.

�

�

�

�

Statement o


d.

SO

C shall

describe the ef

fects that

provide

training

in

the

specific

skills

require

d for

recognition

of icing phenomena an

d execution of

recovery

.

u.1

Aerod

ynamic

and

groun

d reaction modelling

for the

effects of

reverse

thrust on

directional control shall

be provi

ded.

�

�

�

Statement o


d.

(page

2–C–4

4).

v.1

Realistic

aeroplane

mass properties,

including mass,

centre

of

gravity

an

d moments

of

inertia

as

a

function of

pa

yloa

d an

d fuel

loading shall

be

implemente

d.

�

�

�

�

Statement of

Compliance

require

d at

initial

evaluation.

SO

C shall include a range of

tabulate

d target

values to

ena

ble a

demonstration of

the

mass properties model

to

be con

ducted

from

the

instructor

’s station.

w.1

Sel

f-testing

for FSTD

har

dware an

d programming to

determine compliance

with

the

FSTD

per

formance

tests shall

be provi

ded.

Evi

dence of

testing shall

include

FSTD

num

ber,

date

, time,

conditions,

tolerances

, an

d the appropriate

depen

dent

varia

bles

portra

yed

in comparison

with

the

aeroplane

stan

dard

.

�

�

Statement o


d. Tests

require

d.

L U X E M B O U R G

2029

1-C-21 01.05.08


FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

CO

MP

LIA

NC

E

1.1

G

ener

al

A

B C

D

1

2 I

II M

CC

x.1

Timel

y an

d permanent up

date

of

hard

ware an

d programming su

bsequent

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

require

d.

�

�

�

�

�

�

�

�

�

�

L U X E M B O U R G

2030


01.05.08 1-C-22

FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

2.

M

otio

n sy

stem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

a.1

Motion cues

as perceive

d by

the

pilot

shall be representative of

the

aeroplane

, e.g.

touch

down cues

shall

be a

function

of the simulated

rate

of descent

.

�

�

�

�

For FSTDs

where

motion systems are

not specifically

require

d, but

have

been

ad

ded,

the

y will

be assessed

to ensure

that

they

do

not adversel

y af

fect

the

qualification of

the FSTD

.

b.1

A motion system

shall:

(1)

Provi

de su

fficient cueing

, which

may

be

of

a generic

nature

to

accomplish the require

d tasks.

�

Statement o


d.

Tests require

d.

(2

) Have a minimum

of

3 degrees of

freedom

(pitch,

roll

& heave)

.

�

(3

) Pro

duce

cues at

least

equivalent to

those of

a six

-degrees

-of-freedom

synergistic

platform

motion system

.

�

�

c.1

A means

of

recording

the

motion

response

time as

require

d.

�

�

�

�

L U X E M B O U R G

2031

1-C-23 01.05.08


FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

2.

M

otio

n sy

stem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

d.1

Motion ef

fects programming shall inclu

de:

(1)

Effects of

runway

rum

ble,

oleo

de

flections

, groundspee

d, uneven

runway

, centreline

lights

and

taxi

way

characteristics.

(2)

Buf

fets

on

the

ground

due

to

spoiler/speed

brake extension an

d thrust

reversal

.

(3)

Bumps

associate

d with

the

landing

gear

.

(4)

Buf

fet

during

extension

and

retraction of

landing gear

.

(5)

Buf

fet in

the

air

due to

flap an

d spoiler/speed

brake extension.

(6)

Approach to

stall

buffet.

(7)

Touchdown cues

for m

ain an

d nose

gear

.

(8)

Nose

wheel

scu

ffing

.

(9)

Thrust

effect

with

bra

kes set.

(See

next page)

�

�

�

�

For

Level

‘A’FFS

: Ef

fects may

be of

a

generic

nature su

fficient to

accomplish

the require

d tasks.

L U X E M B O U R G

2032


01.05.08 1-C-24

FFS

LE

VEL

FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

2.

M

otio

n sy

stem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

d.1

(continue

d)

(10)

Mach an

d manoeuvre

buf

fet.

(11)

Tyre

failure

dynamics.

(12)

Engine

mal

function

and

engine

damage.

(13)

Tail an

d po

d strike.

�

�

�

�

e.1

Motion vi

brations

: Tests

with

recorded

results

that

allo

w the comparison

of

relative amplitu

des versus

frequency

are

require

d.

Characteristic

motion

vibrations

that

result

from

operation of

the

aeroplane

in

so far

as vi

bration mar

ks an event or

aeroplane state that

can

be sensed

at the

flight

deck

shall

be present

. The FSTD

shall be programmed

and

instrumente

d in

such

a manner that

the characteristic

vi

bration modes

can

be measure

d an

d compare

d with

aeroplane

data.

�

Statement o


d.

Tests require

d.

L U X E M B O U R G

2033

1-C-25 01.05.08


FS L

EVE

L FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

3 V

isua

l Sys

tem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

a.1

The visual

system

shall meet all the

stan

dards enumerated

as applicable

to

the level o

f qualification requeste

d by

the

applicant.

�

�

�

�

�

�

For FTDs,

FN

PT

1s and

BITDs,

when visual

systems have

been

ad

ded

by the FSTD

operator

even though

not

attracting specific

credits

, the

y will

be assessed

to ensure that

they

do not a

dversely

affect

the qualification

of the FSTD

.

For FTDs if the visual

system

is to

be use

d for the training of

manoeuvring

by visual

reference

(such

as route

and

airfiel

d competence)

then the visual

system

shoul

d at

least compl

y with

that

require

d for level A

FFS

.

b.1

Continuous

minimum

collimated

visual

field

-of-vie

w o

f 45

degrees horizontal and

30

degrees

vertical

field

of

view

simultaneousl

y for each pilot.

�

�

S

OC

is accepta

ble in

place

of this test

.

b.2

Continuous

, cross-cockpit,

minimum

collimated

visual

field

of view

provi

ding

each

pilot

with

180

degrees

horizontal

and

40

degrees vertical

field

of

view

. Application of

tolerances require

the

field

of

vie

w to

be not

less

than a total o

f 17

6 measure

d degrees horizontal field

of vie

w

(including not less

than

±88 measure

d degrees either

side of

the

centre

of the

design

eye

point

) and

not

less

than

a total

of 3

6 measure

d degrees vertical

field

of

view

from

the

pilot’s

and

co-pilot’s

eye

points

.

�

�

Consi

deration shall

be given

to optimising

the vertical

field

of view

for

the

respective

aeroplane cut-o

ff angle.

SO

C is

accepta

ble in

place

of this test

.

L U X E M B O U R G

2034


01.05.08 1-C-26

FS L

EVE

L FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

3 V

isua

l Sys

tem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

b.3

A visual

system

(night/dus

k or

day

) capa

ble

of provi

ding

a fiel

d-of

-vie

w o

f a minimum

of

45

degrees horizontally

an

d 30

degrees

vertically

, unless

restricted

by the type

of

aeroplane,

simultaneousl

y for each

pilot,

including ad

justable

cloud

base an

d visi

bilit

y.

�

�

The visual

system

nee

d not

be collimated

but

shall be capa

ble of

meeting the stan

dards laid

do

wn in

Part 3

and

4 (Validation,

Functions

and

Su

bjective Tests

- See

ACJ

No.

1 to

JAR

-FSTD

A.

030)

.

SO

C is

accepta

ble in

place

of this test

.

c.

1 A

means

of recor

ding

the visual

response

time

for visual s

ystems.

�

�

�

�

�

�

d.1

System

Geometry

. The

system

fitte

d shall

be free

from

optical

discontinuities an

d arte

facts that

create non-realistic

cues.

�

�

�

�

�

�

Test

require

d. A

Statement o

f Compliance is

acceptable

in place

of this test

.

e.1

Visual te

xtural

cues to

assess sink

rate

and

depth perception

during ta

ke-o

ff an

d 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

attitu

de shall correlate to

the

simulated

attitu

de in

dicator.

�

�

�

�

Statement o


d.

g.1

Occulting

- A

minimum

of ten levels

shall

be availa

ble.

�

�

�

�

Occulting shall be

demonstrate

d.

Statement o


d.

h.1

Sur

face

(Vernier)

resolution shall occupy

a visual

angle

of not greater than

2 arc

minutes

in the visual

display

use

d on

a

scene

from

the pilot’s

eyepoint.

�

�

Test

and

Statement of

Compliance require

d containing

calculations

confirming

resolution.

L U X E M B O U R G

2035

1-C-27 01.05.08


FS L

EVE

L FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

3 V

isua

l Sys

tem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

i.1

Sur

face

contrast

ratio

shall

be

demonstrate

d by

a raster

drawn test

pattern

sho

wing a contrast

ratio

of not

less

than

5:1

�

�

Test

and

Statement o


d.

j.1

Highlight

brightness

shall

be

demonstrate

d using a raster

dra

wn test

pattern

. The

highlight

brightness

shall not

be less

than

20 cd

/m2

(6ft-lam

berts

).

�

�

Test

and

Statement o


d.

Use

of calligraphic lights to

enhance

raster

brightness

is accepta

ble.

k.1

Light point si

ze –

not

greater

than

5 arc

minutes

.

�

�

Test

and

Statement o


d.

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 o

f compliance require

d.

l.2

Light point contrast

ratio

– not

less than

25

:1.

�

�

Test

and

Statement o

f compliance require

d.

m.1

Daylight

, twilight

and

night

visual

capa

bilit

y as

applicable

for level of

qualification sought

.

�

�

�

�

Statement of

Compliance

require

d for

system

capability

.

System

objective an

d scene content tests

are require

d.

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

�

�

�

�

L U X E M B O U R G

2036


01.05.08 1-C-28

FS L

EVE

L FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

3 V

isua

l Sys

tem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

m.3

Total scene content shall

be compara

ble

in detail to that

pro

duce

d by

100

00 visible

te

xtured

surfaces an

d (in

da

y)

6000

visi

ble lights or

(in

twilight or night)

1500

0 visi

ble

lights,

an

d su

fficient system

capacity

to

displa

y 16

simultaneousl

y moving ob

jects.

�

�

m.4

The system

, when used

in training,

shall

provide

in

daylight

, full

colour

presentations

and

suf

ficient

sur

faces

with

appropriate

te

xtural

cues

to

conduct a

visual

approach

, landing

and

airport

movement

(taxi

). Sur

face

sha

ding

effects

shall be consistent

with

simulated

(static

) sun position.

�

�

L U X E M B O U R G

2037

1-C-29 01.05.08


FS L

EVE

L FTD

LE

VEL

FNPT

LEVE

L B

ITD

FL

IGHT S

IMU

LATOR

TRA

ININ

G D

EV

ICE

STA

NDARDS

3 V

isua

l Sys

tem

A

B C

D

1

2 I

II M

CC

CO

MP

LIA

NC

E

m.5

The system

, when used

in training,

shall

provide at

twilight, as

a minimum

, full

colour

presentations

of re

duce

d am

bient

intensity

, su

fficient

surfaces

with

appropriate

textural

cues that

include self-

illuminated

ob

jects

such

as

road

networ

ks, ramp

lighting

and

airport

signage,

to conduct a visual

approach,

landing

and

airport movement

(taxi

). Scenes shall include a

definable

horizon

an

d typical terrain

characteristics such

as

fields,

roads an

d bo

dies

of

water

an

d surfaces illuminated

by

representative

ownship lighting

(e.g

. landing lights)

. If

provided

, directional horizon

lighting shall

have

correct

orientation an

d be

consistent

with

sur

face

sha

ding

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

re

duce

d am

bient

intensity

that removes

groun

d cues

that

are not self-illuminating or

illuminated

by

ownship lights

(e.g

. lan

ding

lights

).

�

�

�

�

L U X E M B O U R G

2038


01.05.08 1-C-30

FFS

LEVE

L FTD

LE

VEL

FNPT

LEV

EL

BITD

CO

MPL

IAN

CE

FLIG

HT SI

MU

LATOR

TRA

ININ

G D

EVIC

E STA

NDARDS

4 S

ound

Sys

tem

A

B

C

D

1 2

I II

MC

C

a.1

Signi

ficant flight

dec

k soun

ds which

result

from

pilot actions

correspon

ding

to those

of the aeroplane or

class

of aeroplane

.

�

�

�

�

�

�

�

�

�

For FN

PT Level

I and

BITD

engine soun

ds

only

nee

d be

availa

ble

b.1

Sound

of

precipitation,

rain

removal

equipment and

other

signi

ficant aeroplane

noises

perceptible

to

the pilot

during

normal

and

abnormal

operations

and

the

soun

d of

a crash

when the FSTD

is

landed

in e

xcess of

limitations

.

�

�

Statement o


d.

c.1

Compara

ble amplitu

de and

frequency

of

flight

deck

noises,

inclu

ding

engine an

d airframe soun

ds. The

sounds shall be co

-or

dinate

d with

the require

d weather

.

�

Tests require

d.

d.1

The

volume

control shall have

an

in

dication of

sound

level

setting

which

meets

all qualification requirements

.

�

�

�

�

L U X E M B O U R G

2039

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

L U X E M B O U R G

2040

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 ([email protected]).

*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

L U X E M B O U R G

2041

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


SUBPART A — APPLICABILITY

SUBPART B — GENERAL

SUBPART C — HELICOPTER FLIGHT SIMULATION TRAINING DEVICES


ACJ B — GENERAL

ACJ C — HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

L U X E M B O U R G

2042

JAR-FSTD H

01.05.08 C-2


L U X E M B O U R G

2043

JAR-FSTD H

C-3 01.05.08

CONTENTS (details)

JAR–FSTD H

HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

Paragraph Page SECTION 1 – REQUIREMENTS


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

L U X E M B O U R G

2044

JAR-FSTD H

Paragraph Page

01.05.08 C-4



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

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JAR-FSTD H

Paragraph Page

C-5 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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JAR-FSTD H

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JAR-FSTD H

F-1 01.05.08

FOREWORD

1 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.

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

basis for showing compliance with their national codes. 3 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.

4 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.

5 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.

6 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.

7 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.

8 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. 9 New, amended and corrected text will be enclosed within heavy brackets until a subsequent

Amendment’ is issued. 10 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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JAR-FSTD H

CL-1 01.05.08

JOINT AVIATION REQUIREMENTS

CHECK LIST OF PAGES

JAR-FSTD H - HELICOPTER FLIGHT SIMULATION TRAINING DEVICES

Initial issue dated 01 May 2008 The following pages of JAR-FSTD H are now current: Page No Legend Date Title Page Initial issue 01.05.08 ii Initial issue 01.05.08 C-1 Initial Issue 01.05.08 C-2 Initial Issue 01.05.08 C-3 Initial Issue 01.05.08 C-4 Initial Issue 01.05.08 C-5 Initial Issue 01.05.08 C-6 Initial Issue 01.05.08 F-1 Initial Issue 01.05.08 F-2 Initial Issue 01.05.08 CL-1 Initial Issue 01.05.08 CL-2 Initial Issue 01.05.08 CL-3 Initial Issue 01.05.08 CL-4 Initial Issue 01.05.08 P-1 Initial Issue 01.05.08 P-2 Initial Issue 01.05.08 1-0-1 Initial Issue 01.05.08 1-0-2 Initial Issue 01.05.08 1-A-1 Initial Issue 01.05.08 1-A-2 Initial Issue 01.05.08 1-B-1 Initial Issue 01.05.08 1-B-2 Initial Issue 01.05.08 1-C-1 Initial Issue 01.05.08 1-C-2 Initial Issue 01.05.08 1-C-3 Initial Issue 01.05.08 1-C-4 Initial Issue 01.05.08 1-C-5 Initial Issue 01.05.08 1-C-6 Initial Issue 01.05.08 1-C-7 Initial Issue 01.05.08 1-C-8 Initial Issue 01.05.08 1-C-9 Initial Issue 01.05.08 1-C-10 Initial Issue 01.05.08 1-C-11 Initial Issue 01.05.08 1-C-12 Initial Issue 01.05.08 1-C-13 Initial Issue 01.05.08 1-C-14 Initial Issue 01.05.08 1-C-15 Initial Issue 01.05.08 1-C-16 Initial Issue 01.05.08 1-C-17 Initial Issue 01.05.08 1-C-18 Initial Issue 01.05.08

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01.05.08 CL-2

1-C-19 Initial Issue 01.05.08 1-C-20 Initial Issue 01.05.08 1-C-21 Initial Issue 01.05.08 1-C-22 Initial Issue 01.05.08 1-C-23 Initial Issue 01.05.08 1-C-24 Initial Issue 01.05.08 1-C-25 Initial Issue 01.05.08 1-C-26 Initial Issue 01.05.08 1-C-27 Initial Issue 01.05.08 1-C-28 Initial Issue 01.05.08 2-0-1 Initial Issue 01.05.08 2-0-2 Initial Issue 01.05.08 2-B-1 Initial Issue 01.05.08 2-B-2 Initial Issue 01.05.08 2-B-3 Initial Issue 01.05.08 2-B-4 Initial Issue 01.05.08 2-B-5 Initial Issue 01.05.08 2-B-6 Initial Issue 01.05.08 2-B-7 Initial Issue 01.05.08 2-B-8 Initial Issue 01.05.08 2-C-1 Initial Issue 01.05.08 2-C-2 Initial Issue 01.05.08 2-C-3 Initial Issue 01.05.08 2-C-4 Initial Issue 01.05.08 2-C-5 Initial Issue 01.05.08 2-C-6 Initial Issue 01.05.08 2-C-7 Initial Issue 01.05.08 2-C-8 Initial Issue 01.05.08 2-C-9 Initial Issue 01.05.08 2-C-10 Initial Issue 01.05.08 2-C-11 Initial Issue 01.05.08 2-C-12 Initial Issue 01.05.08 2-C-13 Initial Issue 01.05.08 2-C-14 Initial Issue 01.05.08 2-C-15 Initial Issue 01.05.08 2-C-16 Initial Issue 01.05.08 2-C-17 Initial Issue 01.05.08 2-C-18 Initial Issue 01.05.08 2-C-19 Initial Issue 01.05.08 2-C-20 Initial Issue 01.05.08 2-C-21 Initial Issue 01.05.08 2-C-22 Initial Issue 01.05.08 2-C-23 Initial Issue 01.05.08 2-C-24 Initial Issue 01.05.08 2-C-25 Initial Issue 01.05.08 2-C-26 Initial Issue 01.05.08 2-C-27 Initial Issue 01.05.08 2-C-28 Initial Issue 01.05.08 2-C-29 Initial Issue 01.05.08 2-C-30 Initial Issue 01.05.08 2-C-31 Initial Issue 01.05.08 2-C-32 Initial Issue 01.05.08 2-C-33 Initial Issue 01.05.08 2-C-34 Initial Issue 01.05.08 2-C-35 Initial Issue 01.05.08 2-C-36 Initial Issue 01.05.08 2-C-37 Initial Issue 01.05.08 2-C-38 Initial Issue 01.05.08 2-C-39 Initial Issue 01.05.08 2-C-40 Initial Issue 01.05.08

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CL-3 01.05.08

2-C-41 Initial Issue 01.05.08 2-C-42 Initial Issue 01.05.08 2-C-43 Initial Issue 01.05.08 2-C-44 Initial Issue 01.05.08 2-C-45 Initial Issue 01.05.08 2-C-46 Initial Issue 01.05.08 2-C-47 Initial Issue 01.05.08 2-C-48 Initial Issue 01.05.08 2-C-49 Initial Issue 01.05.08 2-C-50 Initial Issue 01.05.08 2-C-51 Initial Issue 01.05.08 2-C-52 Initial Issue 01.05.08 2-C-53 Initial Issue 01.05.08 2-C-54 Initial Issue 01.05.08 2-C-55 Initial Issue 01.05.08 2-C-56 Initial Issue 01.05.08 2-C-57 Initial Issue 01.05.08 2-C-58 Initial Issue 01.05.08 2-C-59 Initial Issue 01.05.08 2-C-60 Initial Issue 01.05.08 2-C-61 Initial Issue 01.05.08 2-C-62 Initial Issue 01.05.08 2-C-63 Initial Issue 01.05.08 2-C-64 Initial Issue 01.05.08 2-C-65 Initial Issue 01.05.08 2-C-66 Initial Issue 01.05.08 2-C-67 Initial Issue 01.05.08 2-C-68 Initial Issue 01.05.08 2-C-69 Initial Issue 01.05.08 2-C-70 Initial Issue 01.05.08 2-C-71 Initial Issue 01.05.08 2-C-72 Initial Issue 01.05.08 2-C-73 Initial Issue 01.05.08 2-C-74 Initial Issue 01.05.08 2-C-75 Initial Issue 01.05.08 2-C-76 Initial Issue 01.05.08 2-C-77 Initial Issue 01.05.08 2-C-78 Initial Issue 01.05.08 2-C-79 Initial Issue 01.05.08 2-C-80 Initial Issue 01.05.08 2-C-81 Initial Issue 01.05.08 2-C-82 Initial Issue 01.05.08 2-C-83 Initial Issue 01.05.08 2-C-84 Initial Issue 01.05.08 2-C-85 Initial Issue 01.05.08 2-C-86 Initial Issue 01.05.08 2-C-87 Initial Issue 01.05.08 2-C-88 Initial Issue 01.05.08 2-C-89 Initial Issue 01.05.08 2-C-90 Initial Issue 01.05.08 2-C-91 Initial Issue 01.05.08 2-C-92 Initial Issue 01.05.08 2-C-93 Initial Issue 01.05.08 2-C-94 Initial Issue 01.05.08 2-C-95 Initial Issue 01.05.08 2-C-96 Initial Issue 01.05.08 2-C-97 Initial Issue 01.05.08 2-C-98 Initial Issue 01.05.08 2-C-99 Initial Issue 01.05.08 2-C-100 Initial Issue 01.05.08 2-C-101 Initial Issue 01.05.08 2-C-102 Initial Issue 01.05.08 2-C-103 Initial Issue 01.05.08

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01.05.08 CL-4

2-C-104 Initial Issue 01.05.08 2-C-105 Initial Issue 01.05.08 2-C-106 Initial Issue 01.05.08 2-C-107 Initial Issue 01.05.08 2-C-108 Initial Issue 01.05.08 2-C-109 Initial Issue 01.05.08 2-C-110 Initial Issue 01.05.08 2-C-111 Initial Issue 01.05.08 2-C-112 Initial Issue 01.05.08 2-C-113 Initial Issue 01.05.08 2-C-114 Initial Issue 01.05.08 2-C-115 Initial Issue 01.05.08 2-C-116 Initial Issue 01.05.08 2-C-117 Initial Issue 01.05.08 2-C-118 Initial Issue 01.05.08 2-C-119 Initial Issue 01.05.08 2-C-120 Initial Issue 01.05.08 2-C-121 Initial Issue 01.05.08 2-C-122 Initial Issue 01.05.08 2-C-123 Initial Issue 01.05.08 2-C-124 Initial Issue 01.05.08 2-C-125 Initial Issue 01.05.08 2-C-126 Initial Issue 01.05.08 2-C-127 Initial Issue 01.05.08 2-C-128 Initial Issue 01.05.08 2-C-129 Initial Issue 01.05.08 2-C-130 Initial Issue 01.05.08 2-C-131 Initial Issue 01.05.08 2-C-132 Initial Issue 01.05.08 2-C-133 Initial Issue 01.05.08 2-C-134 Initial Issue 01.05.08 2-C-135 Initial Issue 01.05.08 2-C-136 Initial Issue 01.05.08 2-C-137 Initial Issue 01.05.08 2-C-138 Initial Issue 01.05.08 2-C-139 Initial Issue 01.05.08 2-C-140 Initial Issue 01.05.08 2-C-141 Initial Issue 01.05.08 2-C-142 Initial Issue 01.05.08 2-C-143 Initial Issue 01.05.08 2-C-144 Initial Issue 01.05.08 2-C-145 Initial Issue 01.05.08 2-C-146 Initial Issue 01.05.08 2-C-147 Initial Issue 01.05.08 2-C-148 Initial Issue 01.05.08

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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

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SECTION 1 JAR-FSTD H

1-0-1 01.05.08


1 GENERAL 1.1 This Section contains the requirements for helicopter Flight Simulation Training Devices. 2 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.


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JAR-FSTD H SECTION 1

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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

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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.


SUBPART B – GENERAL

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

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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) A 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)

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(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)

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JAR-FSTD H.032 Requirements for Flight Training Devices (FTD) qualified on or after 1 January 2004 and before 1 August 2008

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


(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.



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JAR–FSTD H.037 Requirements for Flight Navigation Procedures Trainers approved or qualified before 1 January 2003 (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


(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


L U X E M B O U R G

2065


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.



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

L U X E M B O U R G

2066


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:

1 Multi engine and multi pilot helicopter

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

3 Anti icing or de-icing systems

4 Fire detection / suppression system

5 Dual controls

6 Autopilot with upper modes

7 2 VHF transceivers

8 2 VHF NAV receivers (VOR, ILS, DME)

9 1 ADF receiver

10 1 Marker receiver

11 1 transponder

12 Weather radar

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

1 Airspeed

2 Flight attitude

3 Altimeter and radio altimeter

4 HSI

5 Vertical speed

6 ADF

7 VOR, ILS, DME

8 Marker indication

9 Stop watch

L U X E M B O U R G

2067

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

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

a.1

A f

light

dec

k th

at i

s a

full-

scal

e repl

ica

of t

he

helic

opte

r si

mul

ated

. A

dditi

onal

requ

ired

crew

mem

ber

duty

sta

tions

and

tho

se r

equi

red

bulk

head

s af

t of

th

e pi

lot

seat

s ar

e al

so

cons

ider

ed pa

rt

of

the

cockpi

t an

d sh

all

repl

icat

e th

e he

licop

ter.

�

�

�

�

�

�

A

flig

ht d

eck

that

rep

licat

es th

e he

licop

ter.

�

�

�

�

�

a.2

The

fligh

t dec

k, in

clud

ing

the

inst

ruct

or’s

sta

tion

is fu

lly e

nclo

sed.

�

�

�

�

A

flig

ht d

eck,

inc

ludi

ng t

he i

nstr

ucto

r’s s

tatio

n th

at

is

suffi

cien

tly

clos

ed

off

to

excl

ude

dist

ract

ions

.

�

�

�

�

�

�

�

b.1

Full

size

pa

nels

w

ith

func

tiona

l co

ntro

ls,

switc

hes,

in

stru

men

ts

and

prim

ary

and

seco

ndar

y fli

ght

cont

rols

, w

hich

sh

all

be

oper

atin

g in

the

cor

rect

dire

ctio

n an

d w

ith t

he

corr

ect r

ange

of m

ovem

ent.

�

�

�

�

�

�

�

For FTD

Lev

el 1

as

appr

opria

te fo

r the

repl

icat

ed

syst

em

The

use

of e

lect

roni

cally

displ

ayed

im

ages

with

ph

ysic

al o

verla

y in

corp

orat

ing

oper

able

sw

itche

s,

knob

s an

d bu

ttons

may

be

accept

able

. Thi

s op

tion

is n

ot a

ccep

tabl

e fo

r ana

logu

e in

stru

men

ts in

FFS

.

Fu

nctio

nal

cont

rols

, sw

itche

s, i

nstr

umen

ts a

nd

prim

ary

and

seco

ndar

y fli

ght

cont

rols

suf

ficie

nt

for

the

trai

ning

ev

ents

to

be

ac

compl

ishe

d,

shal

l be

loc

ated

in

a sp

atia

lly c

orre

ct a

rea

of

the

fligh

t dec

k.

�

�

�

�

Th

e us

e of

ele

ctro

nica

lly d

ispl

ayed

im

ages

with

ph

ysic

al o

verla

y in

corp

orat

ing

oper

able

sw

itche

s,

knob

s an

d bu

ttons

is a

ccep

tabl

e.

L U X E M B O U R G

2068

01.05.08 1-C-8


JAR- FSTD H SECTION 1

FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

c.1

Ligh

ting

for pa

nels

and

inst

rum

ents

sha

ll be

as

per t

he h

elic

opte

r. �

�

�

�

�

�

Li

ghtin

g fo

r pa

nels

and

ins

trum

ents

sha

ll be

su

ffici

ent f

or th

e tr

aini

ng e

vent

s

�

�

�

�

�

c.2

Flig

ht d

eck

ambi

ent l

ight

ing

envi

ronm

ent s

hall

be

dyna

mic

ally

con

sist

ent w

ith th

e vi

sual

displ

ay a

nd

suffi

cien

t for

the

train

ing

even

t.

�

�

Th

e am

bien

t lig

htin

g sh

ould

pro

vide

an

even

leve

l of i

llum

inat

ion

whi

ch is

not

di

stra

ctin

g to

the pi

lot.

�

�

�

�

�

�

�

d.1

Rel

evan

t flig

ht d

eck

circ

uit b

reak

ers

shal

l be

loca

ted

as p

er t

he h

elic

opte

r an

d sh

all f

unct

ion

accu

rate

ly

whe

n in

volv

ed

in

oper

atin

g pr

oced

ures

or

m

alfu

nctio

ns

requ

iring

or

in

volv

ing

fligh

t cr

ew

resp

onse

.

�

�

�

�

�

�

�

�

�

�

e.1

Effe

ct

of

aero

dyna

mic

ch

ange

s fo

r va

rious

co

mbi

natio

ns o

f ai

rspe

ed a

nd p

ower

nor

mal

ly

enco

unte

red

in

fligh

t, in

clud

ing

the

effe

ct

of

chan

ge i

n he

licop

ter

attit

ude,

aer

odyn

amic

and

pr

opul

sive

fo

rces

an

d m

omen

ts,

altit

ude,

te

mpe

ratu

re,

mas

s, c

entre

of

grav

ity l

ocat

ion

and

conf

igur

atio

n.

�

�

�

�

�

�

�

�

�

�

Ef

fects

of C

g, m

ass

and

conf

igur

atio

n ch

ange

s are

not

requ

ired

for F

NPT

Lev

el I.

A

erod

ynam

ic a

nd e

nviro

nmen

t m

odel

ling

shal

l be

su

ffici

ent

to pe

rmit

accu

rate

sy

stem

s op

erat

ion

and

indi

catio

n.

�

L U X E M B O U R G

2069

1-C-9 01.05.08



FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

COMPLIANCE

e.2

Aer

odyn

amic

mod

ellin

g w

hich

inc

lude

s gr

ound

ef

fect

, ef

fect

s of

ai

rfram

e an

d ro

tor

icin

g (if

appl

icab

le),

aero

dyna

mic

in

terfe

renc

e ef

fect

s be

twee

n th

e ro

tor

wak

e an

d fu

sela

ge,

influ

ence

of

the

roto

r on

con

trol a

nd s

tabi

lizat

ion

syst

ems,

an

d repr

esen

tatio

ns

of

nonl

inea

ritie

s du

e to

si

desl

ip, v

orte

x rin

g an

d re

treat

ing

blad

e st

all.

�

�

�

�

�

�

�

f.1

Val

idat

ion

fligh

t te

st d

ata

shal

l be

use

d as

the

ba

sis

for

fligh

t an

d pe

rform

ance

and

sys

tem

s ch

arac

teris

tics.

�

�

�

�

R

epre

sent

ativ

e/ge

neric

ae

rody

nam

ic

data

ta

ilore

d to

the

helic

opte

r w

ith fi

delit

y su

ffici

ent t

o m

eet

the

obje

ctiv

e te

sts

and

suffi

cien

t to

per

mit

accu

rate

sys

tem

ope

ratio

n an

d in

dica

tion.

�

�

�

�

�

�

�

Aer

odyn

amic

da

ta

need

no

t be

ne

cess

arily

ba

sed

on fl

ight

test

dat

a.

g.1

All

rele

vant

flig

ht d

eck

inst

rum

ent

indi

catio

ns

auto

mat

ical

ly r

espo

nd to

con

trol

mov

emen

t by

a cr

ewm

embe

r, he

licop

ter

perfo

rman

ce,

or

exte

rnal

sim

ulat

ed e

nviro

nmen

tal

effe

cts

upon

th

e he

licop

ter

�

�

�

�

�

�

�

�

�

�

�

L U X E M B O U R G

2070

01.05.08 1-C-10



FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

COMPLIANCE

h.1

All

rele

vant

co

mm

unic

atio

ns,

navi

gatio

n,

caut

ion

and

war

ning

eq

uipm

ent

shal

l co

rrespo

nd t

o th

at in

stal

led

in t

he h

elic

opte

r. A

ll si

mul

ated

na

viga

tion

aids

w

ithin

ra

nge

shal

l be

us

able

w

ithou

t re

stric

tion.

N

avig

atio

nal

data

sha

ll be

cap

able

of

bein

g up

date

d.

�

�

�

�

�

�

�

For FT

D 1

app

lies

whe

re t

he app

ropr

iate

sys

tem

s ar

e repl

icat

ed.

h.2

Nav

igat

ion

equipm

ent

corr

espo

ndin

g to

tha

t of

a

helic

opte

r, w

ith

oper

atio

n w

ithin

th

e to

lera

nces

typ

ical

ly app

lied

to t

he a

irbor

ne

equipm

ent. Th

is s

hall

incl

ude

com

mun

icat

ion

equipm

ent

(inte

rpho

ne

and

air/

grou

nd

com

mun

icat

ions

sys

tem

s).

�

�

�

�

h.3

Nav

igat

iona

l da

ta

with

th

e co

rrespo

ndin

g appr

oach

faci

litie

s. N

avig

atio

n ai

ds s

houl

d be

us

able

with

in ra

nge

with

out r

estri

ctio

n

�

�

�

�

�

�

�

�

�

�

�

For FF

Ss

and FT

Ds

the

navi

gatio

n da

taba

se

shou

ld b

e up

date

d w

ithin

28

days

.

For FN

PTs

compl

ete

navi

gatio

nal

data

for

at

leas

t 5

diffe

rent

E

urop

ean

airp

orts

w

ith

corr

espo

ndin

g pr

ecis

ion

and

non-pr

ecis

ion

appr

oach

pr

oced

ures

in

clud

ing

curr

ent

upda

ting

with

in a

per

iod

of 3

mon

ths.

i.1

In a

dditio

n to

the

fligh

t cre

wm

embe

r sta

tions

, at l

east

tw

o su

itabl

e se

ats

for t

he in

stru

ctor

and

an

addi

tiona

l ob

serv

er

shal

l be

pr

ovid

ed pe

rmitt

ing

adeq

uate

vi

sion

to

th

e cr

ewm

embe

rs' pa

nel

and

forw

ard

win

dow

s. O

bser

ver

seat

s ne

ed

not

repr

esen

t th

ose

foun

d in

th

e he

licop

ter

but

shal

l be

ad

equa

tely

se

cure

d to

th

e flo

or

of

the

flight

si

mul

ator

, fitt

ed w

ith p

ositi

ve re

stra

int d

evic

es a

nd b

e

�

�

�

�

Th

e Au

thor

ity w

ill co

nsid

er opt

ions

to th

is s

tand

ard

base

d on

uniqu

e co

ckpi

t con

figur

atio

ns.

Any

addi

tiona

l sea

ts in

stal

led

shal

l be

equipp

ed w

ith

sim

ilar s

afet

y pr

ovis

ions

.

L U X E M B O U R G

2071

1-C-11 01.05.08



FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

COMPLIANCE

of s

uffic

ient

inte

grity

to s

afel

y re

stra

in th

e oc

cupa

nt

durin

g an

y kn

own

or pr

edic

ted

mot

ion

syst

em

excu

rsio

n.

i.2

Cre

wm

embe

r sea

ts s

hall

affo

rd th

e capa

bilit

y fo

r the

oc

cupa

nts

to b

e ab

le t

o ac

hiev

e th

e de

sign

eye

re

fere

nce po

sitio

n.

In

ad

ditio

n to

th

e fli

ght

crew

mem

ber s

tatio

ns, a

t lea

st tw

o su

itabl

e se

ats

for

the

inst

ruct

or a

nd a

n ad

ditio

nal

obse

rver

sha

ll be

pr

ovid

ed pe

rmitt

ing

adeq

uate

vi

sion

to

th

e cr

ewm

embe

rs' p

anel

and

forw

ard

win

dow

s.

�

�

�

�

�

�

�

The

inst

ruct

or's

and

obse

rver

’s s

eats

nee

d no

t repr

esen

t tho

se fo

und

in th

e he

licop

ter.

L U X E M B O U R G

2072

01.05.08 1-C-12



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

j.1 FF

S

syst

ems

shal

l si

mul

ate

the

appl

icab

le

helic

opte

r sy

stem

ope

ratio

n, b

oth

on t

he g

roun

d an

d in

flig

ht.

Sys

tem

s sh

all

be ope

rativ

e to

th

e ex

tent

th

at

norm

al,

abno

rmal

, an

d em

erge

ncy

oper

atin

g pr

oced

ures

appr

opria

te

to

the

sim

ulat

or

appl

icat

ion

can

be a

ccompl

ishe

d. O

nce

activ

ated

, pr

oper

sys

tem

ope

ratio

n sh

all r

esul

t fro

m s

yste

m

man

agem

ent

by t

he f

light

cre

w a

nd n

ot r

equi

re

inpu

t fro

m in

stru

ctor

con

trols

.

�

�

�

�

j.2 FT

D s

yste

ms

repr

esen

ted

shal

l be

fully

ope

rativ

e to

th

e ex

tent

th

at

norm

al,

abno

rmal

an

d em

erge

ncy

oper

atin

g pr

oced

ures

ca

n be

ac

compl

ishe

d.

Onc

e ac

tivat

ed, pr

oper

sy

stem

op

erat

ion

shal

l res

ult f

rom

sys

tem

man

agem

ent b

y th

e fli

ght c

rew

and

not

requ

ire inpu

t fro

m in

stru

ctor

co

ntro

ls.

�

�

�

j.3 Th

e sy

stem

s sh

ould

be

oper

ativ

e to

the

exte

nt th

at

it sh

ould

be po

ssib

le to

per

form

nor

mal

, abn

orm

al,

and

emer

genc

y op

erat

ions

appr

opria

te

to

a he

licop

ter a

s requ

ired

for t

rain

ing.

Onc

e ac

tivat

ed,

prop

er s

yste

ms

oper

atio

ns s

houl

d re

sult

from

the

sy

stem

man

agem

ent b

y th

e cr

ewm

embe

r an

d no

t requ

ire

any

furth

er

inpu

t fro

m

the

inst

ruct

or’s

co

ntro

ls.

�

�

�

�

k.1

The

inst

ruct

or s

hall

be a

ble

to c

ontro

l sys

tem

va

riabl

es a

nd in

sert

abno

rmal

or e

mer

genc

y co

nditi

ons

into

the

helic

opte

r sys

tem

s.

Indepe

nden

t fre

eze

and

rese

t fa

cilit

ies

shal

l be

pr

ovid

ed.

�

�

�

�

�

�

�

�

�

�

�

FNPT

I:

appli

cabl

e on

ly to

ena

ble

the

inst

ruct

or t

o ca

rry

out

sele

ctiv

e fa

ilure

of

ba

sic

fligh

t in

stru

men

ts a

nd n

avig

atio

n eq

uipm

ent.

For FN

PT

Leve

l I:

Abilit

y to

se

t th

e FN

PT

to

min

imum

IMC

spe

ed o

r abo

ve

L U X E M B O U R G

2073

1-C-13 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

l.1

Con

trol f

orce

s an

d co

ntro

l tra

vel w

hich

cor

resp

ond

to t

hat

of t

he r

eplic

ated

hel

icop

ter.

Con

trol

forc

es

shal

l rea

ct in

the

sam

e m

anne

r as

in th

e he

licop

ter

unde

r the

sam

e fli

ght c

ondi

tions

.

�

�

�

�

For L

evel

A o

nly

stat

ic c

ontro

l for

ce

char

acte

ristic

s ne

ed to

be

test

ed.

C

ontro

l fo

rces

an

d co

ntro

l tra

vel

sh

all

be

repr

esen

tativ

e of

the

repl

icat

ed h

elic

opte

r und

er th

e sa

me

fligh

t con

ditio

ns a

s in

the

helic

opte

r..

�

�

�

For FTD

leve

l 1 a

s appr

opria

te fo

r the

sys

tem

tra

inin

g requ

ired

C

ontro

l fo

rces

an

d co

ntro

l tra

vel

shal

l br

oadl

y co

rresp

ond

to th

at o

f a h

elic

opte

r.

�

Onl

y sta

tic c

ontro

l forc

e ch

arac

teris

tics

need

to b

e te

sted.

C

ontro

l for

ces

and

cont

rol t

rave

ls s

hall

resp

ond

in

the

sam

e m

anne

r un

der

the

sam

e fli

ght c

ondi

tions

as

in a

hel

icop

ter.

�

�

�

Onl

y st

atic

cont

rol fo

rce

char

acte

ristic

s nee

d to

be

test

ed.

l.2

Coc

kpit

cont

rol d

ynam

ics,

whi

ch repl

icat

e th

e he

licop

ter s

imul

ated

. Fre

e re

spon

se o

f the

con

trols

sh

all m

atch

that

of t

he h

elic

opte

r with

in th

e gi

ven

tole

ranc

e. In

itial a

nd upg

rade

eva

luat

ion

will

incl

ude

cont

rol f

ree

resp

onse

(cyc

lic, c

olle

ctiv

e, a

nd p

edal

) m

easu

rem

ents

reco

rded

at t

he c

ontro

ls. T

he

mea

sure

d re

spon

ses

shal

l cor

resp

ond

to th

ose

of

the

helic

opte

r in

grou

nd ope

ratio

ns, h

over

, clim

b,

crui

se, a

nd a

uto-

rota

tion.

�

�

�

�

�

For

helic

opte

rs w

ith i

rreve

rsib

le c

ontro

l sy

stem

s,

mea

sure

men

ts m

ay b

e ob

tain

ed o

n th

e gr

ound

. En

gine

erin

g va

lidat

ion

or h

elic

opte

r m

anuf

actu

rer

ratio

nale

w

ill be

su

bmitt

ed

as

just

ifica

tion

for

grou

nd te

st o

r to

omit

a co

nfig

urat

ion.

For FF

S requ

iring

sta

tic a

nd d

ynam

ic t

ests

at

the

cont

rols

, sp

ecia

l te

st f

ixtu

res

will

not

be r

equi

red

durin

g th

e in

itial

eva

luat

ions

if th

e FSTD

ope

rato

r’s

QTG

sho

ws

both

tes

t fix

ture

res

ults

and

alte

rnat

e te

st m

etho

d re

sults

, suc

h as

compu

ter

data

plo

ts,

whi

ch

wer

e ob

tain

ed

conc

urre

ntly

. U

se

of

the

alte

rnat

e m

etho

d du

ring

initi

al e

valu

atio

n m

ay th

en

satis

fy th

is te

st requ

irem

ent.

FTD

Lev

el 2

dat

a ca

n be

rep

rese

ntat

ive/

gene

ric

and

need

not

nec

essa

rily

be b

ased

on

fligh

t te

st

data

.

L U X E M B O U R G

2074

01.05.08 1-C-14


JAR- FSTD H SECTION 1 m

.1

Gro

und

hand

ling

and

aero

dyna

mic

pro

gram

min

g to

in

clud

e th

e fo

llow

ing:

Gro

und

effe

ct -

hove

r and

tran

sitio

n IG

E.

(Gro

und

reac

tion

- rea

ctio

n of

the

helic

opte

r upo

n co

ntac

t with

the

land

ing

surfa

ce d

urin

g la

ndin

g to

in

clud

e st

rut d

efle

ctio

ns, t

ire o

r ski

d fri

ctio

n, s

ide

forc

es, a

nd o

ther

app

ropr

iate

dat

a, s

uch

as w

eigh

t an

d sp

eed,

nec

essa

ry to

iden

tify

the

flight

con

ditio

n an

d co

nfig

urat

ion.

Gro

und

hand

ling

char

acte

ristic

s --

con

trol i

nput

s to

in

clud

e br

akin

g, d

ecel

erat

ion

turn

ing

radi

us a

nd th

e ef

fect

s of

cro

ssw

ind.

�

�

�

�

Le

vel

A ca

n ut

ilise

gene

ric s

imul

atio

n of

gro

und

effe

ct a

nd g

roun

d ha

ndlin

g.

G

roun

d ha

ndlin

g an

d ae

rody

nam

ic g

roun

d ef

fect

s m

odel

s sh

ould

be pr

ovid

ed to

ena

ble

lift-o

ff, h

over

, an

d to

uch

dow

n ef

fect

s to

be

si

mul

ated

an

d ha

rmon

ized

with

the

soun

d an

d vi

sual

sys

tem

.

�

�

G

ener

ic g

roun

d ha

ndlin

g an

d ae

rody

nam

ic

grou

nd e

ffect

s m

odel

s sh

ould

be pr

ovid

ed to

en

able

lift-

off,

hove

r, an

d to

uch

dow

n ef

fect

s to

be

sim

ulat

ed a

nd h

arm

oniz

ed w

ith th

e so

und

and

visu

al s

yste

m.

�

�

�

L U X E M B O U R G

2075

1-C-15 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

n.1

Inst

ruct

or c

ontro

ls fo

r

(i) W

ind

spee

d an

d di

rect

ion

�

�

�

�

�

�

�

�

�

�

(ii

) Tur

bule

nce

�

�

�

�

�

�

�

�

�

�

(ii

i) O

ther

at

mosph

eric

m

odel

s to

supp

ort

the

requ

ired

train

ing.

�

�

�

�

Ex

ampl

es: G

ener

ic at

mosph

eric

mod

els

of lo

cal w

ind

patte

rns

arou

nd m

ount

ains a

nd st

ructu

res.

.

(iv

) Adj

ustm

ent o

f clo

ud b

ase

and

visi

bilit

y.

�

�

�

�

�

�

�

�

�

(v

) Tempe

ratu

re a

nd b

arom

etric

pre

ssur

e.

�

�

�

�

�

�

�

�

�

�

�

o.1

Rep

rese

ntat

ive

stoppi

ng a

nd d

irect

iona

l con

trol

forc

es fo

r at l

east

the

follo

win

g la

ndin

g su

rface

co

nditi

ons

base

d on

hel

icop

ter r

elat

ed d

ata,

for a

ru

nnin

g la

ndin

g.

(i)

D

ry

(ii

) W

et (s

oft s

urfa

ce a

nd h

ard

surfa

ce)

(ii

i) Ic

y

(iv

) Pa

tchy

Wet

(v

) Pa

tchy

Icy

�

�

p.1

Rep

rese

ntat

ive

brak

e an

d tir

e fa

ilure

dyn

amic

s.

�

�

q.1

Coc

kpit

cont

rol

dyna

mic

s, w

hich

rep

licat

e th

e he

licop

ter

sim

ulat

ed. Fr

ee

resp

onse

of

th

e co

ntro

ls s

hall

mat

ch th

at o

f the

hel

icop

ter

with

in

the

give

n to

lera

nce.

In

itial

an

d up

grad

e ev

alua

tion

will

in

clud

e co

ntro

l fre

e re

spon

se

(cyc

lic,

colle

ctiv

e,

and pe

dal)

mea

sure

men

ts

reco

rded

at

th

e co

ntro

ls. Th

e m

easu

red

resp

onse

s sh

all

corr

espo

nd

to

thos

e of

th

e he

licop

ter

in g

roun

d op

erat

ions

, ho

ver,

clim

b,

�

�

�

�

�

�

�

�

Fo

r hel

icop

ters

with

irre

vers

ible

con

trol s

yste

ms,

m

easu

rem

ents

may

be

obta

ined

on

the

grou

nd.

Eng

inee

ring

valid

atio

n or

hel

icop

ter m

anuf

actu

rer

ratio

nale

will

be

subm

itted

as

just

ifica

tion

for

grou

nd te

st o

r to

omit

a co

nfig

urat

ion.

Fo

r FFS

requ

iring

sta

tic a

nd d

ynam

ic te

sts

at th

e co

ntro

ls, spe

cial

test

fixt

ures

will

not

be

requ

ired

durin

g th

e in

itial

eva

luat

ions

if th

e FSTD

per

ator

’s

QTG

sho

ws

both

test

fixt

ure

resu

lts a

nd a

ltern

ate

L U X E M B O U R G

2076

01.05.08 1-C-16


JAR- FSTD H SECTION 1FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

crui

se, a

nd a

uto-

rota

tion.

test

met

hod

resu

lts, s

uch

as c

ompu

ter d

ata pl

ots,

w

hich

wer

e ob

tain

ed c

oncu

rrent

ly. U

se o

f the

al

tern

ate

met

hod

durin

g in

itial

eva

luat

ion

may

th

en s

atis

fy th

is te

st requ

irem

ent. FT

D L

evel

2

aero

dyna

mic

dat

a ca

n be

repr

esen

tativ

e/ge

neric

an

d ne

ed n

ot n

eces

saril

y be

bas

ed o

n fli

ght t

est

data

.

r.1

(1)

Tran

spor

t del

ay. T

ranspo

rt de

lay

is th

e tim

e be

twee

n co

ntro

l inp

ut a

nd th

e in

divi

dual

ha

rdw

are

(sys

tem

s) re

spon

ses.

As

an a

ltern

ativ

e, a

Lat

ency

test

may

be

used

to

de

mon

stra

te

that

th

e fli

ght

sim

ulat

or

syst

em

does

no

t ex

ceed

th

e pe

rmis

sibl

e de

lay.

�

�

�

�

�

�

�

�

�

�

�

For FTD

Lev

el 1

, onl

y in

stru

men

t respo

nse

is

requ

ired

with

in a

max

imum

per

mis

sibl

e de

lay

of

200

milli

seco

nds

For L

evel

'A' &

'B' FFS

and

Lev

el 2

FTD

the

max

imum

per

mis

sibl

e de

lay

is 1

50 m

illise

cond

s

For L

evel

'C' &

‘D’ FFS

and

Lev

el 3

FTD

the

max

imum

per

mis

sibl

e de

lay

is 1

00 m

illise

cond

s

(2

) La

tenc

y. R

elat

ive

resp

onse

of t

he v

isua

l sy

stem

, coc

kpit

inst

rum

ents

and

initi

al m

otio

n sy

stem

resp

onse

sha

ll be

coupl

ed c

lose

ly to

pr

ovid

e in

tegr

ated

sen

sory

cue

s. T

hese

sys

tem

s sh

all r

espo

nd to

abr

upt p

itch,

roll,

and

yaw

inpu

ts a

t the

pilo

t's p

ositi

on w

ithin

the

perm

issi

ble

dela

y, b

ut n

ot b

efor

e th

e tim

e, w

hen

the

helic

opte

r wou

ld re

spon

d un

der t

he s

ame

cond

ition

s. V

isua

l sce

ne c

hang

es fr

om s

tead

y st

ate

dist

urba

nce

shal

l occ

ur w

ithin

the

syst

em

dyna

mic

resp

onse

lim

it bu

t not

bef

ore

the

resu

ltant

mot

ion

onse

t.

�

�

�

�

�

�

�

For FTD

Lev

el 1

and

FN

PT L

evel

I, o

nly

inst

rum

ent

resp

onse

is requ

ired

with

in a

max

imum

per

mis

sibl

e de

lay

of 2

00 m

illise

cond

s

For L

evel

'A' &

'B' FFS

, Lev

el 2

FTD

and

FN

PT

Leve

l II a

nd II

I the

max

imum

per

mis

sibl

e de

lay

is

150

milli

seco

nds

For L

evel

'C' &

'D' FFS

and

Lev

el 3

FTD

the

max

imum

per

mis

sibl

e de

lay

is 1

00 m

illise

cond

s

L U X E M B O U R G

2077

1-C-17 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.1 General

A

B

C

D

1

2 3

I II

III

MCC

s.1

A m

eans

for

qui

ckly

and

effe

ctiv

ely

test

ing

FSTD

pro

gram

min

g an

d ha

rdw

are.

Thi

s m

ay

incl

ude

an a

utom

ated

sys

tem

, w

hich

cou

ld

be u

sed

for

cond

uctin

g at

lea

st a

por

tion

of

the

test

s in

the QTG

.

�

�

�

�

�

Rec

omm

ende

d fo

r FTD

Lev

el 1

,FN

PT L

evel

I an

d II

Auto

mat

ic fl

aggi

ng o

f "ou

t-of-t

oler

ance

" te

sts

resu

lts

is e

ncou

rage

d.

Se

lf-te

stin

g fo

r FST

D h

ardw

are

and pr

ogra

mm

ing

to

dete

rmin

e co

mpl

ianc

e w

ith

the

FSTD

pe

rform

ance

te

sts.

Ev

iden

ce

of

test

ing

shal

l in

clud

e FSTD

num

ber,

date

, tim

e, c

ondi

tions

, to

lera

nces

, an

d th

e appr

opria

te

depe

nden

t va

riabl

es po

rtray

ed

in

compa

rison

w

ith

the

helic

opte

r sta

ndar

d

�

�

�

t.1

A sy

stem

allo

win

g fo

r tim

ely

cont

inuo

us upd

atin

g of

FSTD

har

dwar

e an

d pr

ogra

mm

ing

cons

iste

nt w

ith

helic

opte

r mod

ifica

tions

.

�

�

�

�

�

�

�

u.1

The FSTD

ope

rato

r sh

all

subm

it a Q

ualif

icat

ion

Test

Gui

de in

a fo

rm a

nd m

anne

r acc

epta

ble

to th

e Au

thor

ity. A

reco

rdin

g sy

stem

sha

ll be

pro

vide

d th

at

will

enab

le th

e FSTD

per

form

ance

to b

e co

mpa

red

with

QTG

crit

eria

.

�

�

�

�

�

�

�

�

�

�

�

v.1

FSTD

compu

ter

capa

city

, acc

urac

y, r

esol

utio

n an

d dy

nam

ic r

espo

nse

suffi

cien

t fo

r th

e Q

ualif

icat

ion

Leve

l sou

ght.

�

�

�

�

�

�

�

�

�

�

�

w.1

Dai

ly p

refli

ght

docu

men

tatio

n ei

ther

in

the

daily

lo

g or

in a

loca

tion

easi

ly a

cces

sibl

e fo

r rev

iew

.

�

�

�

�

�

�

�

�

�

�

�

L U X E M B O U R G

2078

01.05.08 1-C-18



FFS

LEVEL

FTD

LEVEL

FNPT

LEVEL

FSTD

STANDA

RDS

1.2 Motion System

A

B

C

D

1

2 3

I II

III

MCC

COMPLIANCE

a.1

Mot

ion

cues

as pe

rcei

ved

by t

he p

ilot

shal

l be

repr

esen

tativ

e of

th

e he

licop

ter,

e.g.

to

uchd

own

cues

sho

uld

be a

fun

ctio

n of

the

sim

ulat

ed r

ate

of

desc

ent.

�

�

�

�

M

otio

n te

sts

to d

emon

stra

te th

at e

ach

axes

ons

et

cues

are

prope

rly p

hase

d w

ith p

ilot i

nput

and

he

licop

ter r

espo

nse.

b.1

A m

otio

n sy

stem

: H

avin

g a

min

imum

of 3

deg

rees

of f

reed

om

(pitc

h, ro

ll, h

eave

) to

acco

mpl

ish

the

requ

ired

task

. 6

degr

ees

of fr

eedo

m s

yner

gist

ic p

latfo

rm

mot

ion

syst

em

�

�

�

�

Th

e in

stru

ctor

's an

d ob

serv

er’s

sea

ts n

eed

not

repr

esen

t tho

se fo

und

in th

e he

licop

ter.

For l

evel

B, a

redu

ced

mot

ion pe

rform

ance

en

velope

is a

ccep

tabl

e.

c.1

A m

eans

of r

ecor

ding

the

mot

ion

resp

onse

tim

e as

requ

ired

�

�

�

�

Se

e pa

ra 1

.1 (r

.1) a

bove

.

L U X E M B O U R G

2079

1-C-19 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.2

Motion System

A

B

C

D

1

2 3

I II

III

MCC

d.1

Spe

cial

ef

fect

s pr

ogra

mm

ing

to

incl

ude

the

follo

win

g:

(1) R

unw

ay r

umbl

e, o

leo

defle

ctio

ns,

effe

cts

of

grou

ndsp

eed

and

unev

en

surfa

ce

char

acte

ristic

s.

(2)

Buf

fet d

ue to

tran

slat

iona

l lift

.

(3)

Buf

fet

durin

g ex

tens

ion

and

retra

ctio

n of

la

ndin

g ge

ar.

(4)

Buf

fet

due

to h

igh

spee

d an

d re

treat

ing

blad

e st

all.

(5)

Buf

fet d

ue to

vor

tex

ring.

(6) R

epre

sent

ativ

e cu

es re

sulti

ng fr

om;

(i)

touc

hdow

n

(ii

) tra

nsla

tiona

l lift

.

(7)

Ant

itorq

ue d

evic

e in

effe

ctiv

enes

s.

(8)

Buf

fet d

ue to

turb

ulen

ce.

�

�

�

�

Fo

r le

vel

A

it m

ay

be

of

a ge

neric

na

ture

su

ffici

ent t

o ac

compl

ish

the

requ

ired

task

s.

See

App

endi

x 4

to A

CJ

No.

1 t

o JAR

-FSTD

H

.030

pa

ra

2.2

on

Vib

ratio

n P

latfo

rms

for

Hel

icop

ter F

STD

s.

L U X E M B O U R G

2080

01.05.08 1-C-20



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.2

Motion System

A

B

C

D

1

2 3

I II

III

MCC

e.1

Cha

ract

eris

tic

vibr

atio

ns/b

uffe

ts

that

re

sult

from

ope

ratio

n of

the

hel

icop

ter

and

whi

ch

can

be

sens

ed

in

the

cockpi

t. S

imul

ated

co

ckpi

t vi

brat

ions

to

in

clud

e se

at(s

), fli

ght

cont

rols

an

d in

stru

men

t pa

nel(s

), al

thou

gh

thes

e ne

ed n

ot b

e te

sted

indepe

nden

tly.

�

Sta

tem

ent o

f Compl

ianc

e requ

ired.

Tes

ts

requ

ired

with

rec

orde

d re

sults

whi

ch

allo

w t

he c

ompa

rison

of

rela

tive

ampl

itude

s ve

rsus

frequ

ency

in

the

long

itudi

nal,

late

ral

and

verti

cal a

xes

with

hel

icop

ter

data

.. S

tead

y st

ate

test

s ar

e ac

cept

able

.

See

App

endi

x 4

to A

CJ

No.

1 t

o JAR

-FSTD

H

.030

pa

ra

2.2

on

Vib

ratio

n P

latfo

rms

for

Hel

icop

ter F

STD

s.

L U X E M B O U R G

2081

1-C-21 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FS

TD S

TANDA

RDS

1.3 Visual

Sys

tem

A

B

C

D

1

2 3

I II

III

MCC

a.1

Visu

al s

yste

m c

apab

le o

f mee

ting

all t

he s

tand

ards

of

this

par

agraph

and

the

resp

ectiv

e pa

ragr

aphs

of

valid

atio

n te

sts

as w

ell a

s fu

nctio

ns a

nd s

ubje

ctiv

e te

sts

as app

licab

le t

o th

e Le

vel

of Q

ualif

icat

ion

requ

este

d by

the FSTD

ope

rato

r.

�

�

�

�

�

�

�

�

�

The

choi

ce o

f the

displ

ay s

yste

m a

nd o

f the

fiel

d of

vi

ew requ

irem

ents

sho

uld

fully

con

side

r the

inte

nded

us

e of

the FSTD

. The

bal

ance

bet

wee

n tra

inin

g an

d te

stin

g/ch

ecki

ng

may

in

fluen

ce

the

choi

ce

and

geom

etry

of

the

disp

lay

syst

em.

In a

dditi

on t

he

dive

rse

oper

atio

nal

requ

irem

ents

sh

ould

be

ad

dres

sed.

b.1

Visu

al s

yste

m c

apab

le o

f pr

ovid

ing

at l

east

a 4

5 de

gree

hor

izon

tal

and

30 d

egre

e ve

rtica

l fie

ld o

f vi

ew s

imul

tane

ousl

y fo

r eac

h pi

lot.

�

Vi

sual

sys

tem

cap

able

of pr

ovid

ing

at l

east

a 7

5 de

gree

s ho

rizon

tal a

nd 4

0 de

gree

s ve

rtica

l fie

ld o

f vi

ew s

imul

tane

ousl

y fo

r eac

h pi

lot.

�

“C

ontin

uous

”, cr

oss-

cockpi

t, m

inim

um v

isua

l fie

ld o

f vi

ew pr

ovid

ing

each

pi

lot

with

15

0 de

gree

s ho

rizon

tal a

nd 4

0 de

gree

s ve

rtica

l

�

�

�

�

A

min

imum

of 7

5 de

gree

s ho

rizon

tal f

ield

of v

iew

on

eith

er s

ide

of th

e ze

ro d

egre

e az

imut

h lin

e re

lativ

e to

th

e he

licop

ter f

usel

age

is requ

ired.

b.2

“Con

tinuo

us,”

cros

s-co

ckpi

t, m

inim

um v

isua

l fie

ld o

f vi

ew pr

ovid

ing

each

pi

lot

with

15

0 de

gree

s ho

rizon

tal a

nd 6

0 de

gree

s ve

rtica

l

�

�

A

min

imum

of 7

5 de

gree

s ho

rizon

tal f

ield

of v

iew

on

eith

er s

ide

of th

e ze

ro d

egre

e az

imut

h lin

e re

lativ

e to

th

e he

licop

ter f

usel

age

is requ

ired.

Thi

s w

ill a

llow

an

offs

et p

er s

ide

of th

e ho

rizon

tal f

ield

of v

iew

if

requ

ired

for t

he tr

aini

ng.

Whe

re tr

aini

ng ta

sks

requ

ire e

xten

ded

field

s of

vie

w

beyo

nd th

e 15

0 de

gree

s x

60 d

egre

es, t

hen

such

ex

tend

ed fi

elds

of v

iew

sho

uld

be p

rovi

ded.

b.3

.“Con

tinuo

us” c

ross

coc

kpit,

min

imum

vis

ual f

ield

of

view

pro

vidi

ng e

ach pi

lot w

ith18

0 de

gree

s ho

rizon

tal

and

60 d

egre

es v

ertic

al

�

A m

inim

um o

f 75

degr

ees

of h

oriz

onta

l fie

ld o

f vie

w

on e

ither

sid

e of

zer

o de

gree

s az

imut

h lin

e re

lativ

e to

the

helic

opte

r fus

elag

e is

requ

ired.

Thi

s w

ill a

llow

an

offs

et p

er s

ide

of t

he h

oriz

onta

l fie

ld o

f vi

ew if

requ

ired

for t

he tr

aini

ng.

Whe

re tr

aini

ng ta

sks

requ

ire e

xten

ded

field

s of

vie

w

beyo

nd th

e 18

0 de

gree

s x

60 d

egre

es, t

hen

such

ex

tend

ed fi

elds

of v

iew

sha

ll be

pro

vide

d.

L U X E M B O U R G

2082

01.05.08 1-C-22



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.3 Visual

Sys

tem

A

B

C

D

1

2 3

I II

III

MCC

c.1

A m

eans

of

reco

rdin

g th

e vi

sual

respo

nse

time

for

the

visu

al s

yste

m s

hall

be p

rovi

ded.

�

�

�

�

�

�

�

�

�

d.1

Visu

al c

ues

to a

sses

s ra

te o

f ch

ange

of

heig

ht,

trans

latio

nal d

ispl

acem

ents

and

rate

s, d

urin

g ta

keof

f an

d la

ndin

g.

�

�

Fo

r Lev

el 'A

', Vi

sual

cue

ing

suffi

cien

t to

supp

ort

chan

ges

in app

roac

h pa

th b

y us

ing FATO

pe

rspe

ctiv

e

Vi

sual

cue

s to

ass

ess

rate

of

chan

ge o

f he

ight

, he

ight

AG

L, t

rans

latio

nal

disp

lace

men

ts a

nd r

ates

, du

ring

take

off,

low

al

titud

e/lo

w

airspe

ed

man

oeuv

ring,

hov

er, a

nd la

ndin

g.

�

�

�

�

�

�

�

.

e.1Te

st p

roce

dure

s to

qui

ckly

con

firm

vis

ual

syst

em

colo

ur, R

VR,

focu

s, i

nten

sity

, le

vel

horiz

on,

and

attit

ude

as c

ompa

red

with

the

spec

ified pa

ram

eter

s.

�

�

�

�

�

�

�

�

�

Stat

emen

t of c

ompli

ance

requ

ired.

Test

requ

ired

f.1

A m

inim

um o

f 10

leve

ls o

f occ

ultin

g. T

his

capa

bilit

y sh

ould

be

dem

onst

rate

d by

a v

isua

l mod

el th

roug

h ea

ch c

hann

el.

�

�

�

�

�

�

�

Stat

emen

t of c

ompli

ance

requ

ired.

Test

requ

ired

g.1

Surfa

ce (

Vern

ier)

reso

lutio

n sh

all b

e de

mon

stra

ted

by a

test

pat

tern

of o

bjec

ts s

how

n to

occ

upy

a vi

sual

an

gle

of n

ot g

reat

er th

an 3

arc

min

utes

in th

e vi

sual

di

spla

y us

ed o

n a

scen

e fro

m th

e pi

lot's

eye

poi

nt..

�

�

�

�

�

�

�

Stat

emen

t of c

ompli

ance

requ

ired.

Test

requ

ired

h.1

Ligh

tpoi

nt s

ize

shal

l no

t be

gre

ater

tha

n 6

arc

min

utes

�

�

Th

is is

equ

ival

ent t

o a

light

poi

nt re

solu

tion

of 3

arc

m

inut

es.

Li

ghtp

oint

siz

e sh

all

not

be g

reat

er t

han

8 ar

c m

inut

es

�

�

�

�

�

�

Th

is is

equ

ival

ent t

o a

light

poi

nt re

solu

tion

of 4

arc

m

inut

es.

L U X E M B O U R G

2083

1-C-23 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.3 Visual

Sys

tem

A

B

C

D

1

2 3

I II

III

MCC

i.1

Day

light

, du

sk,

and

nigh

t vi

sual

sc

enes

w

ith

suffi

cien

t sce

ne c

onte

nt t

o re

cogn

ise

aero

drom

es,

helip

orts

, ter

rain

, and

maj

or la

ndm

arks

aro

und

the

Fina

l App

roac

h an

d Ta

ke-o

ff (F

ATO

) ar

ea a

nd t

o su

cces

sful

ly a

ccompl

ish

low

airspe

ed/lo

w a

ltitu

de

man

oeuv

res

to i

nclu

de l

ift-o

ff, h

over

, tra

nsla

tiona

l lif

t, la

ndin

g an

d to

uchd

own.

�

�

�

�

�

�

�

j.1

A vis

ual d

atab

ase

suffic

ient

to s

uppo

rt th

e requ

irem

ents,

in

cludi

ng

(i)

Spec

ific a

reas

with

in th

e da

taba

se

need

ing h

ighe

r res

olut

ion to

suppo

rt la

ndin

gs, t

ake-

offs

and

gro

und

cush

ion

exer

cises

and

trai

ning

awa

y fro

m a

he

lipor

t. In

cludin

g el

evat

ed h

elipa

d,

helid

ecks

and

conf

ined

are

as

(ii)

For c

ross

-cou

ntry

fligh

ts su

fficie

nt sc

ene

deta

ils to

allo

w fo

r gro

und

to m

ap

navig

atio

n ov

er a

sect

or le

ngth

equ

al to

30

min

utes

at a

n av

erag

e cr

uise

spee

d.

(iii)

For o

ffsho

re a

irbor

ne ra

dar app

roac

hes

(ARA

), ha

rmon

ized

visua

l/rad

ar

repr

esen

tatio

ns o

f inst

allat

ions

.

(iv)

(For

trai

ning

in th

e us

e of

Nig

ht V

ision

G

oggl

es (N

VG) a

visu

al d

ispla

y with

the

abilit

y to

repr

esen

t var

ious

scen

es w

ith

the

requ

ired

leve

ls of

am

bien

t lig

ht/c

olou

r.

�

�

�

�

�

�

�

�

Gen

eric

dat

abas

e is

acc

epta

ble

only

for FTD

s an

d FN

PTs.

Whe

re app

licab

le

Whe

re app

licab

le

Whe

re app

licab

le

L U X E M B O U R G

2084

01.05.08 1-C-24


JAR- FSTD H SECTION 1FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.3 Visual

Sys

tem

A

B

C

D

1

2 3

I II

III

MCC

k.1

Day

light

, tw

iligh

t (du

sk/d

awn)

and

nig

ht v

isua

l capa

bilit

y fo

r sys

tem

brig

htne

ss a

nd c

ontra

st ra

tio

crite

ria a

s appl

icab

le fo

r lev

el o

f qua

lific

atio

n so

ught

.

Nig

ht a

nd D

usk

scen

e

�

�

�

�

�

�

�

�

�

The

ambi

ent l

ight

ing

shou

ld p

rovi

de a

n ev

en le

vel o

f illu

min

atio

n, w

hich

is n

ot d

istra

ctin

g to

the pi

lot.

k.2

The

visu

al s

yste

m s

houl

d be

cap

able

of p

rodu

cing

: Fu

ll col

our p

rese

ntat

ions

.

Full c

olou

r tex

ture

sha

ll be

used

to e

nhan

ce vi

sual

cue

pe

rcep

tion

for i

llum

inat

ed la

nding

surfa

ces .

�

�

�

�

�

�

�

k.3

The

visu

al s

yste

m s

houl

d be

cap

able

of

pr

oduc

ing,

as

a m

inim

um:

(1)

A sc

ene

cont

ent c

ompa

rable

in d

etai

l with

that

pr

oduc

ed b

y 6,0

00 p

olyg

ons f

or d

aylig

ht a

nd 1

000

visib

le lig

ht p

oint

s fo

r nig

ht a

nd d

usk

scen

es fo

r the

en

tire

visua

l sys

tem

.

(2)

A sc

ene

cont

ent c

ompa

rable

in d

etai

l with

that

pr

oduc

ed b

y 4,0

00 p

olyg

ons f

or d

aylig

ht a

nd 5

000

visib

le lig

ht p

oint

s fo

r nig

ht a

nd d

usk

scen

es fo

r the

en

tire

visua

l sys

tem

(3)

A s

cene

con

tent

compa

rabl

e in

det

ail w

ith

that

pro

duce

d by

6,0

00 p

olyg

ons

for d

aylig

ht

and

7000

vis

ible

ligh

t poi

nts

for n

ight

and

du

sk s

cene

s fo

r the

ent

ire v

isua

l sys

tem

.

�

�

�

�

�

�

�

Stat

emen

t of C

ompl

ianc

e requ

ired.

Test

requ

ired.

Fr

eedo

m o

f app

aren

t qua

ntiz

atio

n an

d ot

her

dist

ract

ing

visu

al e

ffect

s ar

e al

so app

licab

le fo

r Le

vels

A a

nd B

.

l.1

Surfa

ce c

ontra

st ra

tio:

Dem

onst

ratio

n m

odel

Not

less

than

5:1

.

Not

less

than

8:1

�

�

�

�

�

�

�

L U X E M B O U R G

2085

1-C-25 01.05.08



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.3 Visual

Sys

tems

A

B

C

D

1 2

3 I

II III

MCC

l.2

Ligh

tpoi

nt c

ontra

st ra

tio.

Not

less

than

25:

1.

�

�

�

�

m.1

Hig

hlig

ht B

right

ness

. The

min

imum

light

mea

sure

d at

th

e pil

ot's

eye po

sitio

n sh

ould

be

:

14 c

d/m

² (4

ft-L

ambe

rts)

17

cd/m

² (5

ft-La

mbe

rts)

20 c

d/m

² (6

ft-L

ambe

rts)

�

�

�

�

�

�

�

L U X E M B O U R G

2086

01.05.08 1-C-26



FFS

FTD

FNPT

COMPLIANCE

LEVEL

LEVEL

LEVEL

FSTD

STANDA

RDS

1.4

Sound Systems

A

B

C

D

1 2

3 I

II III

MCC

a.1

Sig

nific

ant

fligh

t dec

k so

unds

, an

d th

ose,

whi

ch

resu

lt fr

om p

ilot

actio

ns c

orre

spon

ding

to

thos

e of

the

helic

opte

r sh

all b

e pr

ovid

ed.

�

�

�

�

�

�

�

�

�

�

Fo

r FT

D l

evel

1 a

s appr

opria

te f

or t

he s

yste

m

train

ing

requ

ired.

Stat

emen

t of C

ompl

ianc

e requ

ired

for FFS

.

a.2

Sou

nds

due

to e

ngin

es, t

rans

mis

sion

and

rot

ors

shou

ld b

e av

aila

ble

�

b.1

Sou

nd o

f pr

ecip

itatio

n, w

inds

hiel

d w

iper

s, t

he

soun

d re

sulti

ng f

rom

a b

lade

str

ike

and

a cr

ash

cond

ition

w

hen

oper

atin

g th

e he

licop

ter

in

exce

ss o

f lim

itatio

ns.

�

�

�

�

C

rash

sou

nds

may

be

gene

ric

Stat

emen

t of C

ompl

ianc

e or

Dem

onst

ratio

n of

repr

esen

tativ

e so

unds

requ

ired.

c.1R

ealis

tic a

mpl

itude

and

frequ

ency

of

cockpi

t ac

oust

ic e

nviro

nmen

t.

�

Obj

ectiv

e st

eady

-sta

te te

sts

requ

ired

d.1Th

e vo

lum

e co

ntro

l sh

all

have

an

indi

catio

n of

so

und

leve

l set

ting

whi

ch m

eets

all qu

alifi

catio

n requ

irem

ents

.

�

�

�

�

L U X E M B O U R G

2087


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.



L U X E M B O U R G

2088


01.05.08 1-C-28


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

Imprimeur: Association momentanée Imprimerie Centrale / Victor Buck

L U X E M B O U R G