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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
L U X E M B O U R G
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;
L U X E M B O U R G
1985
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
L U X E M B O U R G
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
L U X E M B O U R G
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
L U X E M B O U R G
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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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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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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SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)
General and Presentation 2-0-1
ACJ B – GENERAL ACJ FSTD A.005 Terminology, Abbreviations 2-B-1
ACJ C – AEROPLANE FSTDS ACJ No. 1 to FSTD Qualification – Application and Inspection 2-C-1 JAR- FSTD A.015 ACJ No. 2 to FSTD Evaluations 2-C-6 JAR- FSTD A.015 ACJ FSTD A.020 Validity of an FSTD Qualification 2-C-10 ACJ No. 1 to Quality System 2-C-10 JAR- FSTD A.025
ACJ No. 2 to BITD Operators Quality System 2-C-17 JAR-FSTD A.025 ACJ No. 3 to Installations 2-C-18 JAR-FSTD A.025 ACJ No. 1 to FSTDs qualified on or after 1 August 2008 2-C-19 JAR-FSTD A.030 Appendix 1 to ACJ No. 1 Validation Test Tolerances 2-C-112 to JAR-FSTD A.030 Appendix 2 to ACJ No. 1 Validation Data Roadmap 2-C-114 to JAR-FSTD A.030 Appendix 3 to ACJ No. 1 Data Requirements for Alternate Engines 2-C-116 to JAR-FSTD A.030 Appendix 4 to ACJ No. 1 Data Requirements for Alternate Avionics 2-C-118 to JAR-FSTD A.030 Appendix 5 to ACJ No. 1 Transport Delay Testing Method 2-C-119 to JAR-FSTD A.030 Appendix 6 to ACJ No. 1 Recurrent Evaluations – Validation Test Data Presentation 2-C-122 to JAR-FSTD A.030 Appendix 7 to ACJ No 1 Applicability 2-C-123 to JAR-FSTD A.030 Appendix 8 to ACJ No 1 General technical Requirements for FSTD Qualification 2-C-125 JAR–FSTD A.030 Levels ACJ No. 2 to Guidance on Design and Qualification of Level “A” 2-C-130 JAR-FSTD A.030 Aeroplane FFSs ACJ No. 3 to Guidance on Design and Qualification of FNPTs 2-C-132 JAR-FSTD A.030 ACJ No. 4 to Guidance on Design and Qualification of BITDs 2-C-136 JAR-FSTD A.030 ACJ No.1 to Engineering Simulator Validation Data 2-C-140 JAR-FSTD A.030(c)(1)
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JAR-FSTD A
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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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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 1-C-29 Initial Issue 01.05.08 1-C-30 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
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2-C-39 Initial Issue 01.05.08 2-C-40 Initial Issue 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
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JAR-FSTD A Paragraph Legend Page
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2-C-102 Initial Issue 01.05.08 2-C-103 Initial Issue 01.05.08 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
L U X E M B O U R G
2001
JAR-FSTD A
P-1 01.05.08
PREAMBLE
JAR–FSTD A Initial Issue JAR–FSTD A comprises 3 Subparts (A, B and C) in Section 1, and 2 Subparts (B and C) in Section 2. JAR-FSTD A is a simple amalgamation of JAR STD 1A, 2A, 3A and 4A into one document. Section 1 Subpart C Terminology and basic regulatory processes combined Table of Standards in Appendix 1 to JAR-FSTD A.030 contains the standard for all devices Section 2 Subpart B Terminology and Abbreviations rationalised and harmonised with Aircraft STD standards documents. Subpart C Regulatory Processes combined. Table of Objective Tests (ACJ to JAR-FSTD A.030) contains the testing requirements for all devices. Table of Functions and Subjective Tests (ACJ to JAR-FSTD A.030) contains the testing requirements for all devices.
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2003
SECTION 1 JAR-FSTD A
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SECTION 1 – REQUIREMENTS
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.
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SECTION 1 JAR–FSTD A
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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.
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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.
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SUBPART B - GENERAL
(JAR-FSTD A.005 continued)
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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.
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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)
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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.
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�
�
�
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.
�
�
�
�
L U X E M B O U R G
2017
1-C-9 01.05.08
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-10
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
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
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
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-12
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
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
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
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-14
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
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
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
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-16
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
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
f Compliance require
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
f Compliance require
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
f Compliance require
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
f Compliance require
d.
L U X E M B O U R G
2025
1-C-17 01.05.08
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
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-18
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
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
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
(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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
01.05.08 1-C-20
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
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
f Compliance require
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
f Compliance require
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
f Compliance require
d. Tests
require
d.
L U X E M B O U R G
2029
1-C-21 01.05.08
SECTION 1 JAR-FSTD AAppendix 1 to JAR-FSTD A.030 (continued)
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
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
f Compliance require
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
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
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
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
f Compliance require
d.
Tests require
d.
L U X E M B O U R G
2033
1-C-25 01.05.08
SECTION 1 JAR-FSTD AAppendix 1 to JAR-FSTD A.030 (continued)
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
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
f Compliance require
d.
g.1
Occulting
- A
minimum
of ten levels
shall
be availa
ble.
�
�
�
�
Occulting shall be
demonstrate
d.
Statement o
f Compliance require
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
SECTION 1 JAR-FSTD AAppendix 1 to JAR-FSTD A.030 (continued)
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
f Compliance require
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
f Compliance require
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
f Compliance require
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
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
SECTION 1 JAR-FSTD AAppendix 1 to JAR-FSTD A.030 (continued)
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
JAR-FSTD A SECTION 1Appendix 1 to JAR-FSTD A.030 (continued)
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
f Compliance require
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
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CONTENTS (general layout)
JAR–FSTD H
HELICOPTER FLIGHT SIMULATION TRAINING DEVICES
FOREWORD
CHECK LIST OF PAGES
PREAMBLE
SECTION 1 – REQUIREMENTS
SUBPART A — APPLICABILITY
SUBPART B — GENERAL
SUBPART C — HELICOPTER FLIGHT SIMULATION TRAINING DEVICES
SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)
ACJ B — GENERAL
ACJ C — HELICOPTER FLIGHT SIMULATION TRAINING DEVICES
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CONTENTS (details)
JAR–FSTD H
HELICOPTER FLIGHT SIMULATION TRAINING DEVICES
Paragraph Page SECTION 1 – REQUIREMENTS
General and Presentation 1-0-1
SUBPART A – APPLICABILITY JAR–FSTD H.001 Applicability 1-A-1
SUBPART B – GENERAL JAR–FSTD H.005 Terminology 1-B-1
SUBPART C – HELICOPTER FLIGHT SIMULATION TRAINING DEVICES JAR–FSTD H.015 Application for FSTD Qualification 1-C-1
JAR–FSTD H.020 Validity FSTD Qualification 1-C-1
JAR–FSTD H.025 Rules governing FSTD Operators 1-C-1
JAR–FSTD H.030 Requirements for FSTDs qualified on or after 1-C-2 1 August 2008
JAR–FSTD H.031 Requirements for FFS qualified on or after 1-C-2 1 April 2001 and before 1 August 2008
JAR–FSTD H.032 Requirements for FTDs qualified on or after 1 January 2004 1-C-3 and before 1 August 2008
JAR–FSTD H.033 Requirements for FNPTs qualified on or after 1 January 2003 1-C-3 and before 1 August 2008
JAR–FSTD H.035 Requirements for FFSs approved or qualified 1-C-3 before 1 April 2001
JAR–FSTD H.036 Requirements for FTDs approved or qualified 1-C-3 before 1 January 2004 JAR–FSTD H.037 Requirements for FNPTs approved or qualified 1-C-4 before 1 January 2003
JAR–FSTD H.040 Changes to qualified FSTDs 1-C-4
JAR–FSTD H.045 Interim FSTD Qualification 1-C-5
JAR–FSTD H.050 Transferability of FSTD Qualification 1-C-5
Appendix 1 to FSTD Standards 1-C-6 JAR–FSTD H.030
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SECTION 2 – ADVISORY CIRCULARS JOINT (ACJ)
General and Presentation 2-0-1
ACJ B – GENERAL ACJ FSTD H.005 Terminology, Abbreviations 2-B-1
ACJ C – HELICOPTER FLIGHT SIMULATION TRAINING DEVICES ACJ No. 1 to FSTD Qualification – Application and Inspection 2-C-1 JAR-FSTD H.015 ACJ No. 2 to FSTD Evaluations 2-C-7 JAR-FSTD H.015
ACJ to Validity of FSTD Qualification 2-C-10 JAR-FSTD H.020
ACJ No. 1 to Quality System 2-C-10 JAR-FSTD H.025 ACJ No. 2 to Installations 2-C-16 JAR-FSTD H.025 ACJ No. 1 to FSTDs qualified on or after 1 August 2008 2-C-17 JAR-FSTD H.030
Appendix 1 to ACJ No. 1 Validation Test Tolerances 2-C-106 to JAR-FSTD H.030
Appendix 2 to ACJ No. 1 Validation Data Roadmap 2-C-108 to JAR-FSTD H.030
Appendix 3 to ACJ No. 1 Rotor Aerodynamic Modeling Techniques 2-C-110 to JAR-FSTD H.030
Appendix 4 to ACJ No. 1 Vibration Platforms for Helicopter FSTDs 2-C-112 to JAR-FSTD H.030
Appendix 5 to ACJ No. 1 Transport Delay Testing Method 2-C-114 to JAR-FSTD H.030
Appendix 6 to ACJ No. 1 Recurrent Evaluations – Validation Test Data Presentation 2-C-117 to JAR-FSTD H.030
Appendix 7 to ACJ No 1 Applicability 2-C-118 to JAR-FSTD H.030
Appendix 8 to ACJ No 1 Visual Display Systems 2-C-119 JAR–FSTD H.030
Appendix 9 to ACJ No 1 General technical Requirements for FSTD Qualification 2-C-122 JAR–FSTD H.030 Levels
ACJ No. 2 to Guidance on Design & Qualification of Level ‘A’ Helicopter FFS 2-C-127 JAR-FSTD H.030
ACJ No. 3 to Guidance on Design & Qualification of Helicopter FTDs 2-C-129 JAR-FSTD H.030
ACJ No. 4 to Use of Data for Helicopter FTDs 2-C-132 JAR-FSTD H.030
ACJ No. 5 to Guidance on Design & Qualification of Helicopter FNPTs 2-C-133 JAR-FSTD H.030
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ACJ No. 1 to Engineering Simulator Validation Data 2-C-141 JAR-FSTD H.030(c)(1)
ACJ No. 2 to Engineering Simulator Validation Data – Approved Guidelines 2-C-142 JAR-FSTD H.030(c)(1)
ACJ to FSTD H.035 FFS Approved or Qualified before 1 April 2001 2-C-144
ACJ to FSTD H.037 FNPTs Approved or Qualified before 1 January 2003 2-C-145
ACJ to FSTD H.045 New Helicopter FFS/FTD Qualification 2-C-146
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FOREWORD
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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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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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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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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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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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
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SECTION 1 – REQUIREMENTS
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.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.
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SUBPART A - APPLICABILITY SUBPART A - APPLICABILITY
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SECTION 1 JAR-FSTD H
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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.
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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)
L U X E M B O U R G
2063
SECTION 1 JAR-FSTD H
1-C-3 01.05.08
JAR-FSTD H.032 Requirements for Flight Training Devices (FTD) qualified on or after 1 January 2004 and before 1 August 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
(ii) Functions and subjective tests.
(d) FFS that are not recategorised and that do not have a primary reference document used for their testing, shall be qualified by special arrangement. Such FFS will be issued with a Special Category and shall be subjected to functions and subjective tests corresponding to those detailed within this document. In addition any previously recognised validation test shall be used.
JAR–FSTD H.036 Requirements for Flight Training Devices approved or qualified before 1 January 2004
No longer applicable.
INTENTIONALLY LEFT BLANK
JAR-FSTD H.035(a) (continued)
L U X E M B O U R G
2064
JAR-FSTD H SECTION 1
01.05.08 1-C-4
JAR–FSTD H.037 Requirements for Flight Navigation Procedures Trainers approved or qualified before 1 January 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
(ii) Functions and subjective tests.
(d) FNPTs that are not recategorised and that do not have a primary reference document used for their testing shall be qualified by special arrangement. Such FNPTs will be issued with a Special Category and shall be subjected to Functions and Subjective Tests corresponding to those detailed within this document. In addition any previously recognized Validation tests shall be used.
JAR–FSTD H.040 Changes to qualified FSTD
(a) Requirement to notify major changes to a FSTD. The operator of a qualified FSTD shall inform the Authority of proposed major changes such as:
(1) Helicopter modifications which could affect FSTD qualification.
(2) FSTD hardware and or software modifications which could affect the handling qualities, performance or system representations.
(3) Relocation of the FSTD; and
(4) Any deactivation of the FSTD.
The Authority may complete a special evaluation following major changes or when a FSTD appears not to be performing at its initial Qualification Level.
(b) Upgrade of a FSTD. A FSTD may be upgraded to a higher Qualification Level. Special evaluation is required before the award of a higher Level of Qualification.
(1) If an upgrade is proposed the FSTD operator shall seek the advice of the Authority and give full details of the modifications. If the upgrade evaluation does not fall upon the anniversary of the original qualification date, a special evaluation is required to permit the FSTD to continue to qualify even at the previous Qualification Level.
(2) In the case of a FSTD upgrade, an FSTD operator shall run all validation tests for the requested Qualification Level. Results from previous evaluations shall not be used to validate FSTD performance for the current upgrade.
(c) Relocation of a FSTD
(1) In instances where a FSTD is moved to a new location, the Authority shall be advised before the planned activity along with a schedule of related events.
(2) Prior to returning the FSTD to service at the new location the FSTD operator shall perform at least one third of the validation tests and all functions and subjective tests to ensure that the FSTD performance meets its original qualification standard. A copy of the test documentation shall be retained together with the FSTD records for review by the Authority.
(3) An evaluation of the FSTD in accordance with its original JAA qualification criteria shall be at the discretion of the Authority.
(d) Deactivation of a currently qualified FSTD
JAR-FSTD H.040(a) (continued)
L U X E M B O U R G
2065
SECTION 1 JAR-FSTD H
1-C-5 01.05.08
(1) If a FSTD operator plans to remove a FSTD from active status for prolonged periods, the Authority shall be notified and suitable controls established for the period during which the FSTD is inactive.
(2) The FSTD operator shall agree a procedure with the Authority to ensure that the FSTD can be restored to active status at its original Qualification Level.
JAR–FSTD H.045 Interim FSTD Qualification (See ACJ to JAR-FSTD H.045)
(a) In the case of new helicopter programmes, special arrangements shall be made to enable an interim Qualification Level to be achieved.
(b) For Full Flight Simulators, an interim Qualification Level will only be granted at levels A, B or C
(c) Requirements, details relating to the issue, and the period of validity of an interim Qualification Level will be decided by the Authority.
JAR–FSTD H.050 Transferability of FSTD Qualification
When there is a change of FSTD operator:
(a) The new FSTD operator shall advise the Authority in advance in order to agree upon a plan of transfer of the FSTD.
(b) At the discretion of the Authority, the FSTD shall be subject to an evaluation in accordance with its original JAA qualification criteria.
(c) Provided that the FSTD performs to its original standard, its original Qualification Level shall be restored. Revised user approval(s) may also be required.
INTENTIONALLY LEFT BLANK
INTENTIONALLY LEFT BLANK
JAR-FSTD H.040(d) (continued)
L U X E M B O U R G
2066
JAR-FSTD H SECTION 1
01.05.08 1-C-6
Appendix 1 to JAR-FSTD H.030 Flight Simulation Training Device Standards General
This appendix describes the minimum Full Flight Simulator (FFS), Flight Training Device (FTD) and Flight Navigation Procedures Trainer (FNPT) requirements for qualifying devices to the required Qualification Levels. Certain requirements included in this section shall be supported with a statement of compliance (SOC) and, in some designated cases, an objective test. The SOC will describe how the requirement was met. The test results shall show that the requirement has been attained. In the following tabular listing of FSTD standards, statements of compliance are indicated in the compliance column.
For FNPT use in Multi-Crew Co-operation (MCC) training the general technical requirement are expressed in the MCC column with additional systems, instrumentation and indicators as required for MCC training and operation.
For MCC (Multi Crew Co-operation) minimum technical requirements are as for Level II or III, with the following additions or amendments:
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
Appendix 1 to JAR-FSTD H.030 (continued)
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
JAR- FSTD H SECTION 1
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
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
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
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
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
Appendix 1 to JAR-FSTD H.030 (continued)
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
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
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
Appendix 1 to JAR-FSTD H.030 (continued)
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
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
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
Appendix 1 to JAR-FSTD H.030 (continued)
JAR- FSTD H SECTION 1
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
JAR- FSTD H SECTION 1
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
JAR- FSTD H SECTION 1
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
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
Appendix 1 to JAR-FSTD H.030 (continued)
SECTION 1 JAR–FSTD H
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
Appendix 1 to JAR-FSTD H.030 (continued)
JAR- FSTD H SECTION 1
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
SECTION 1 JAR-FSTD H
1-C-27 01.05.08
These standards always refer to the type of helicopter being simulated, except for FNPT, which may be generic. For FNPT, the term “the/a helicopter” is used to represent the aircraft being modelled which can be a specific helicopter type, a family of similar helicopter types or a totally generic helicopter.
Wherever the term runway is used, it includes runways and FATO/TLOF.
INTENTIONALLY LEFT BLANK
Appendix 1 to JAR-FSTD H.030 (continued)
L U X E M B O U R G
2088
JAR-FSTD H SECTION 1
01.05.08 1-C-28
INTENTIONALLY LEFT BLANK
Editeur: Service Central de Législation, 43, boulevard F.-D. Roosevelt, L-2450 Luxembourg
Imprimeur: Association momentanée Imprimerie Centrale / Victor Buck
L U X E M B O U R G