Avis d`émission d`une Directive de Navigabilité (AD)* par X l`EASA
Contents
1. Manuel de Maintenance qui n est pas celle approuv e ou pas celle en vigueur en France ou si l AD jointe pr sente une difficult d application li e sa sp cificit nationale exposer le probl me aupr s de la direction des m thodes d OSAC par courriel contact osac aero ou par fax au 01 46 42 65 39 ou aupr s du bureau concern du d partement certification produits de l EASA Cette AD est exigible au titre du r glement Europ en 748 2012 1 11 EASA AIRWORTHINESS DIRECTIVE AD No 2013 0020R4 Date 04 July 2014 Note This Airworthiness Directive AD is issued by EASA acting in accordance with Regulation EC No 216 2008 on behalf of the European Community its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation This AD is issued in accordance with EU 748 2012 Part 21 A 3B In accordance with EC 2042 2003 Annex Part M A 301 the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs Consequently no person may operate an aircraft to which an AD applies except in accordance with the requirements of that AD unless otherwise specified by the Agency EC 2042 2003 Annex Part M A 303 or agreed with the Authority of the State of Registry EC 216 2008 Article 14 4 exemption Design Approval Holder s Names Type Model designation s AMSAFE ANJOU AERONAUTIQUE DAVIS AIRC2. agr s list s au paragraphe R f rence des Documentations de cette AD ou bien contacter le d tenteur de l approbation de conception des ceintures de s curit ou des harnais de s curit pour confirmer que l organisme d entretien ou de r paration a bien t autoris par lui pour assurer cette maintenance ou les r parations 3 Si les ceintures de s curit et les harnais de s curit ont t entretenus ou r par s par un organisme d entretien et ou un atelier non autoris par le d tenteur de l approbation de conception dans les 18 mois apr s l inspection exig e au paragraphe 1 de cette AD d poser les ceintures de s curit et ou les harnais de s curit et les remplacer par des ceintures harnais en tat de navigabilit ou rendre le si ge correspondant inop rant Nota 2 Pour l application de cette AD les ceintures harnais en tat de navigabilit sont des ceintures harnais neufs ou des ceintures harnais ayant t entretenus ou r par s par le d tenteur de l approbation de conception ou par un organisme d entretien et ou un atelier autoris par le d tenteur de l approbation de conception ou des ceintures harnais marqu s EPA 10 11 Nota 3 Les exigences des paragraphes 1 2 et 3 de cette AD n affectent pas les sous ensembles des ceintures de s curit et des harnais de s curit dont le remplacement ou une autre action par exemple nettoyage est accompli conform ment au manuel d entretien quipe
3. be installed on but not limited to the aircraft listed in Appendix 1 of this AD Note 1 This AD is applicable to safety belts and torso restraint systems whose Component Maintenance Manuals CMM explicitly prohibit webbing replacement unless this is accomplished by the design approval holder or by a repair station maintenance organization authorized by the design approval holder TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 2 11 Reason As a result of an investigation on some maintenance organisations EASA was made aware that safety belts and torso restraint systems manufactured by design approval holders have been maintained or repaired by maintenance organisations without holding approved maintenance data In particular the affected restraint systems have been refurbished using webbing materials having mechanical properties significantly different with respect to the materials used to manufacture the original restraint systems e g nylon instead of polyester Based on tests performed in the frame of an EASA approved STC refurbishment of seat belts on dynamically tested seats in compliance with CS 25 562 and during a research project on safety belt performance launched by EASA evidence was gained that different elongation properties of commonly available restraint systems webbing may reduc
4. cette AD exige d inspecter les ceintures de s curit et ou les harnais de s curit install s sur les avions list s dans l annexe 1 de cette AD de v rifier s ils ont t entretenus ou r par s par le d tenteur de l approbation de conception ou par un organisme d entretien et ou un atelier agr par le d tenteur de l approbation de conception et de remplacer les ceintures de s curit et les harnais de s curit concern s par des pi ces en tat de navigabilit La r vision 1 de cette AD a t dit e pour clarifier son applicabilit et faire des corrections l annexe 1 ainsi que de corriger une erreur typographique dans le num ro de document de r f rence d AmSafe Repair Station qui devrait tre le n E512615 Rev A au lieu du n E512165 De plus les documents r f renc s dans le paragraphe Ref Publications de cette AD ont t ajout s dans le fichier compress joint cette AD sur le site http ad easa europa eu La r vision 2 de cette AD est dit e pour introduire une note explicative dans la rubrique Actions et D lais d Application de cette AD et pour amender la d signation des types et des mod les et ajouter un mod le r cemment approuv d un type d avion dans l annexe 1 La r vision 3 de cette AD est dit e pour mettre jour les r f rences des documents de AmSafe et de Schroth La r vision 4 de cette AD est dit e pour amender la section applicabilit pour clarifier les marqua
5. M NG Extra Flugzeugproduktions und Vertriebs Gmbh EA 400 EA 400 400 500 Gomolzig Flugzeug und Maschinenbau GmbH R 90 230RG R 90 230RG Grob Aircraft AG G 120 G 120A 120A I Instytut Lotnictwa I 23 1 23 OMA SUD Sky Technologies S p A SKYCAR SKYCAR Pilatus Aircraft Ltd PC 12 PC 12 12 45 12 47 SOCATA TBM 700 TBM 700 C2 and N variants XtremeAir GmbH XA42 XA41 XA42 ne LOTNICZE Marganski amp Mystowski Sp EM 11C ORKA EM 11C ORKA Z 143 Z 143 L 143 Lsi ZLIN Aircraft a s Z 242 Z 242 L Hoffmann H 40 H 40 172 Skyhawk 172R 172S 182 Skylane 182S 182T T182T 206H Stationair 206H T206H 208 Caravan 208 208B Cessna Aircraft Company 510 Mustang 510 525 CitationJet 525 525A 525B 525C LC40 550FG LC40 550FG LC Series LC41 550FG LC42 550FG Cirrus Design Corporation SR20 22 SR20 SR22 SR22T Eclipse Aerospace Incorporated EA500 EA500 ee Sin EMB 500 Phenom 100 EMB 500 Empresa Brasileira de Aeronautica SA EMB 505 Phenom 300 EMB 505 GA8 Airvan Pty Ltd GA8 GA8 GA8 TC 320 Hawker Beechcraft Corporation 390 390 Premier Premier IA Liberty Aerospace Incorporated XL 2 XL 2 Yes for s n 0007 and 0009 through 0125 that have not been modified per Liberty gross weight increase kit RKI SIL 08 001 Pacific Aerospace Ltd 750XL 750XL TE CAP 00110 003 European Aviation Safety Agenc
6. OSAC Avis d mission d une Directive de Navigabilit AD par l EASA European Aviation Safety Agency autorit primaire d un mat riel tranger Les examens ou modifications d crits ou rappel s ci dessous sont imp ratifs La non application des exigences contenues dans la Directive de Navigabilit cit e ci dessous entra ne l inaptitude au vol de l a ronef concern Envoi 14 2014 du 09 juillet 2014 Directive de Navigabilit de l EASA de r f rence 2013 0020 R4 AMSAFE ANJOU AERONAUTIQUE DAVIS AIRCRAFT PRODUCTS Co SCHROTH SAFETY PRODUCTS GmbH PACIFIC SCIENTIFIC Equipements Ceintures et harnais de s curit Equipements Am nagements Ceintures de s curit Harnais de s curit Inspection Remplacement Cette AD remplace l AD EASA 2013 0020 R3 Nota pour les exploitants et organismes d entretien d a ronefs inscrits au registre fran ais Si l AD jointe invite un contact vers l autorit primaire de l AD contacter le bureau concern du d partement certification produits de l EASA Si pour l ex cution d une t che donn e l AD jointe se r f re une qualification de personnel r pondant une r glementation nationale il est possible de faire intervenir pour cette t che du personnel de qualification quivalente accept e dans l Union Europ enne Si l AD jointe se r f re une donn e de navigabilit ou une instruction pour le maintien de la navigabilit Manuel de Vol
7. RAFT PRODUCTS Co SCHROTH SAFETY PRODUCTS GmbH Safety Belts Torso Restraint Systems PACIFIC SCIENTIFIC E TSOA Numbers Various Foreign AD Not applicable None Revision This AD revises EASA AD 2013 0020R3 dated 21 March 2014 Equipment amp Furnishings Safety Belts Torso Restraint Systems Inspection Replacement Manufacturer s AmSafe Anjou Aeronautique formerly TRW Repa S A formerly L Aiglon Davis Aircraft Products Co Schroth Safety Products GmbH and Pacific Scientific Applicability All part numbers of safety belts and torso restraint systems installed on any aircraft where dynamically tested seats are required in accordance with airworthiness requirements like the European Certification Specifications CS or JAR FAR paragraphs 23 562 25 562 27 562 and 29 562 if safety belts and torso restraint systems have been maintained or repaired after 28 September 2003 by maintenance organizations not holding the applicable maintenance data of the relevant approval holders unless they are marked with European Parts Approval EPA Safety belts and torso restraints system repaired by an organization holding an EASA Design Organization Approval DOA in accordance with Commission Regulation EU No 748 2012 Part 21 Subpart J are not affected by this AD These articles are approved through design changes or STC and are marked with the letters EPA accordingly The affected safety belts and torso restraint systems may
8. copter EC 120 B EC 130 T2 EC225LP Potentially affected for new cabin layouts Eurocopter Deutschland MBB BK117 C 2 EC135 AB139 AW139 AgustaWestland p agna SEAE Compiat Sikorsky S 92A Guimbal Cabri G2 PZL SW 4 MD Helicopters Inc MD900 TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 8 11 TRADUCTION DE COURTOISIE de la DIRECTIVE de NAVIGABILITE de l EASA de r f rence 2013 0020 R4 AMSAFE ANJOU AERONAUTIQUE DAVIS AIRCRAFT PRODUCTS Co SCHROTH SAFETY PRODUCTS GmbH PACIFIC SCIENTIFIC Equipements Ceintures et harnais de s curit CONSTRUCTEUR AmSafe Anjou Aeronautique anciennement TRW Repa S A anciennement L Aiglon Davis Aircraft Products Co Schroth Safety Products GmbH Pacific Scientific APPLICABILITE La pr sente Directive de Navigabilit AD s applique a toutes les r f rences de ceintures de s curit et de harnais de s curit install es sur n importe quel type d a ronef sur lequel les si ges sont test s conform ment aux exigences de navigabilit comme les sp cifications de certification europ enne CS ou JAR FAR paragraphes 23 562 25 562 27 562 et 29 562 si les ceintures de s curit et les harnais de s curit ont t entretenus ou r par s apr s le 28 septembre 2003 par de
9. d file attached to the record of this AD at http ad easa europa eu Revision 2 of this AD was issued to introduce an explanatory note in the AD Required Actions and Compliance Time section and to amend type and model designation and add a recently approved model of one aircraft type in the Appendix 1 Revision 3 of this AD was issued to update AmSafe and Schroth referenced publications Revision 4 of this AD amends the Applicability section to clarify EPA markings to update the Pacific Scientific reference publication and to correct Appendix 1 of the AD Effective Date Revision 4 11 July 2014 Revision 3 28 March 2014 Revision 2 11 July 2013 Revision 1 12 March 2013 Original issue 14 February 2013 Required Action s Required as indicated unless previously accomplished and Compliance Time s 1 Within 6 months after 14 February 2013 the effective date of the original issue of this AD inspect the markings of safety belts and or torso TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 3 11 restraint systems to determine if they have been maintained or repaired by organisations other than the design approval holder A review of the applicable maintenance records is acceptable to identify the safety belts and or torso restraint systems as specified in this paragraph pro
10. e technical content of the requirements in this AD please contact AmSafe Aviation TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 4 11 1043 N 47th Avenue Phoenix Arizona 85043 U S A Telephone 1 602 850 2850 Fax 1 602 850 2812 Anjou Aeronautique 11 rue Marbeuf 75008 Paris France Telephone 40 269 243 918 Fax 33 0 2 41 42 15 77 or 40 269 243 921 Davis Aircraft Products Co Inc 1150 Walnut Avenue Bohemia New York 11716 U S A Telephone 1 631 563 1500 Fax 1 631 563 1117 Pacific Scientific Aviation Services 11700 N W 102nd Rd 6 Miami Florida 33178 U S A Telephone 1 305 477 4711 Fax 1 305 477 9799 Schroth Safety Products GmbH Im Ohl 14 D 59757 Arnsberg Germany Telephone 49 0 29 32 97 42 0 Fax 49 0 29 32 97 42 42 TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 5 11 APPENDIX 1 General Aviation TC HOLDER TYPE MODEL Aero Vodochody a s Ae 270 Ae 270 Aviatech Technical Services OMF 100 OMF 100 160 Costruzioni Aeronautiche TECNAM S r l P2006 P2006T DA 40 DA 40 40D 40F 40NG Diamond Aircraft Industries GmbH DA 42 DA 42 42M 42M NG 42M NG DA 42 Restricted DA 42 M R
11. e the energy absorption capability of the seat restraint system and increase the risk of head injury to the occupant under dynamic crash landing conditions Maintenance or repair of safety belts and torso restraint systems if not assessed and justified in accordance with the dynamic test criteria could therefore result in non compliance with the applicable certification requirements for emergency landing dynamic conditions As aconsequence safety belts and torso restraint system could fail to perform their intended function to protect each occupant during an emergency landing condition and to minimise the effects of survivable accidents For the reasons described above this AD requires to inspect safety belts and or torso restraint systems installed on any aircraft refer to Appendix 1 of this AD to verify if they have been maintained or repaired by the design approval holder or by a repair station maintenance organization authorized by the design approval holder and to replace the affected safety belts and torso restraint systems with serviceable parts Revision 1 of this AD was issued to clarify the Applicability of the AD and make some corrections to Appendix 1 as well as to correct a typographical error in the AmSafe Repair Station Reference Document number which should be No E512615 Rev A instead of E512165 In addition the documents referenced in the Ref Publications section of this AD were added in the compressed zippe
12. ges EPA pour mettre jour les r f rences des documents de Pacific Scientific et pour corriger l annexe 1 de cette AD DATES D ENTREE EN VIGUEUR R vision 4 11 juillet 2014 R vision 3 28 mars 2014 R vision 2 11 juillet 2013 R vision 1 12 mars 2013 Edition originale 14 f vrier 2013 ACTIONS ET DELAIS D APPLICATION Sauf si d j accomplies les actions suivantes sont rendues imp ratives 1 Dans les 6 mois apr s le 14 f vrier 2013 date d entr e en vigueur de l AD originale inspecter les marquages des ceintures de s curit et ou des harnais de s curit pour d terminer s ils ont t entretenus ou r par s par des organismes autres que les d tenteurs de l agr ment de conception Un examen des documents de suivi d entretetien applicables est accept pour identifier les ceintures de s curit et ou les harnais de s curit comme sp cifi s dans ce paragraphe condition que ces documents de suivi soient fiables et que les ceintures de s curit et ou les harnais de s curit concern s peuvent tre de fa on concluante identifi s par cet examen 2 Si les ceintures de s curit et les harnais de s curit ont t entretenus ou r par s par un organisme autre que le d tenteur de l approbation de conception dans le mois apr s l inspection exig e au paragraphe 1 de cette AD v rifier si l organisme est list dans les documents de r f rence des organismes d entretien ou de r paration
13. ment CMM des ceintures harnais de s curit applicable 4 Apr s le 14 f vrier 2013 date d entr e en vigueur de l AD originale ne pas installer de ceinture de s curit ou harnais de s curit sur un a ronef moins qu ils aient t inspect s et corrig s conform ment aux exigences de cette AD DOCUMENTS DE REFERENCE AmSafe Repair Station Reference Document N E512615 Rev B du 16 septembre 2013 Anjou A ronautique 11 Rue Marbeuf 75008 Paris France et ROMTEX ANJOU AERONAUTIQUE Romanian CAA authorisation N RO 145 035 Davis Aircraft Products Co Inc FAA approved repair station D5PR729J et Davis Restraint Systems FAA approved repair station GK3R530L Pacific Scientific Service Information Letter SIL No 25 0303D du 10 octobre 2013 Schroth Service Information Letter SIL SSP 006 R vision C du 15 janvier 2014 ou toute version ult rieure approuv e REMARQUES 11 11
14. s organismes de maintenance n ayant pas les donn es d entretien applicables du d tenteur de l approbation de conception correspondant sauf si ces ceintures de s curit et harnais de s curit sont marqu s avec European Parts Approval EPA Les ceintures de s curit et harnais de s curit r par s par un organisme d tenant un agr ment EASA Design Organization Approval DOA conform ment au R glement Europ en EU No 748 2012 Part 21 sous partie J ne sont pas affect s par cette AD Ces quipements sont approuv s au travers d un changement de conception ou d un STC et sont marqu s en cons quent avec European Parts Approval EPA Les ceintures de s curit et les harnais de s curit concern s peuvent tre install s sur les avions list s dans l appendice 1 de cette AD liste non limitative Nota 1 Cette AD s applique toutes les ceintures de s curit et tous les harnais de s curit dont les manuels d entretien CMM interdisent explicitement le remplacement de la sangle moins que celui ci ne soit effectu par le d tenteur de l approbation de conception ou par un organisme d entretien et ou un atelier autoris par le d tenteur de l approbation de conception RAISON Apr s enqu te dans plusieurs organismes de maintenance l EASA a t inform e que les ceintures de s curit et les harnais de s curit fabriqu s par les d tenteurs de l agr ment de conception ont t entretenus ou r par s par de
15. s organismes de maintenance sans poss der les donn es d entretien approuv es En particulier les harnais de s curit ont t r nov s avec des sangles ayant des propri t s m caniques radicalement diff rentes de celles du mat riau original utilis par le constructeur exemple remplacement du polyester par du nylon Bas s sur des tests effectu s dans le cadre d un STC approuv EASA r novation de ceintures de s curit des si ges conform ment la sp cification de certification CS 25 562 et durant un programme de recherche sur l efficacit des ceintures de s curit lanc par l EASA les r sultats ont mis en vidence que les propri t s d allongement de ces sangles des harnais de s curit r duisent la capacit d absorption de l nergie du harnais de s curit et augmentent le risque de blessure s rieuse la t te pour l utilisateur lors d un accident l atterrissage L entretien ou la r paration des ceintures de s curit et des harnais de s curit si non valu s et accept s selon les crit res de test dynamique peuvent alors tre en non conformit avec les exigences de certification applicables pour des conditions d atterrissage d urgence 9 11 En cons quence les ceintures de s curit et les harnais de s curit peuvent faillir leur but initial de prot ger chaque utilisateur lors d un atterrissage d urgence et de r duire les effets des accidents Pour les raisons d crites ci dessus
16. ts and or torso restraint systems sub assemblies whose replacement or any other action e g cleaning is accomplished in accordance with the applicable safety belts and or torso restraint systems CMM 4 After 14 February 2013 the effective date of the original issue of this AD do not install safety belts or torso restraint systems on any aircraft unless inspected and corrected in compliance with the requirements of this AD Ref Publications AmSafe Repair Station Reference Document N E512615 Rev B dated 16 September 2013 Anjou Aeronautique 11 Rue Marbeuf 75008 Paris France and ROMTEX ANJOU AERONAUTIQUE Romanian CAA authorisation N RO 145 035 Davis Aircraft Products Co Inc FAA approved repair station D5PR729J and Davis Restraint Systems FAA approved repair station GK3R530L Pacific Scientific Service Information Letter SIL No 25 0303D dated 10 October 2013 Schroth Service Information Letter SIL SSP 006 Revision C dated 15 January 2014 Remarks If requested and appropriately substantiated EASA can approve Alternative Methods of Compliance for this AD The original issue of this AD was posted on 27 November 2012 as PAD 12 151 for consultation until 27 December 2012 The Comment Response Document can be found at http ad easa europa eu Enquiries regarding this AD should be referred to Safety Information Section Executive Directorate EASA E mail ADs easa europa eu For any question concerning th
17. vided those records can be relied upon for that purpose and the affected safety belts and or torso restraint systems can be conclusively identified from that review If safety belts and torso restraint systems have been maintained or repaired by an organisation other than the design approval holder within 1 month after the inspection required by paragraph 1 of this AD verify if the organisation is listed among the authorized maintenance or repair organisation reference documents quoted in the Ref Publications section of this AD or alternatively contact the design approval holder of the safety belts and torso restraint systems for confirmation that the maintenance or repair organisation had been authorised by them If the safety belts and or torso restraint systems have been maintained or repaired by a repair station maintenance organization not authorized by the design approval holder within 18 months after the inspection required by paragraph 1 of this AD remove the safety belts and or torso restraint systems and replace them with serviceable parts or make the relevant seat inoperative Note 2 For the purpose of this AD serviceable parts are new parts or parts which have been maintained or repaired by the design approval holder or by a repair station maintenance organization authorized by the design approval holder or parts marked with EPA Note 3 The requirements of paragraphs 1 2 and 3 of this AD do not affect safety bel
18. y All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 6 11 APPENDIX 1 continued Large Aeroplanes TC HOLDER TYPE Ko e 3 8 328 Support Services Dornier 328 A318 A330 Airbus A340 A380 Alenia Aeronautica C 27J AN124 100 Antonov AN 26 BAE Systems Operations Ltd Jetstream 4100 Series Boeing 737 NG 737 600 and 700 146 149 PAX 737 800 and 900 181 189 PAX 747 747 8 767 767 400ER 777 787 Bombardier BD 100 BD 700 CL 600 DHC 8 Series DHC 8 400 Series Cessna Cessna 560 XL Cessna 680 Cessna 750 Dassault Aviation Falcon 2000 2000EX Falcon 7X Embraer EMB 135 145 ERJ 170 ERJ 190 Fokker Services B V Fokker F28 series F28 Mark 0070 Gulfstream Aerospace Corporation GIV X GV GV SP and GVI G150 Gulfstream Aerospace LP G200 Galaxy Hawker Beechcraft Corporation Hawker 4000 Learjet Learjet 45 SAAB AB Saab 2000 Sukhoi Sukhoi RRJ 95 TE CAP 00110 003 European Aviation Safety Agency All rights reserved Proprietary document Copies are not controlled Confirm revision status through the EASA Internet Intranet 7 11 TC HOLDER Bell Helicopter Textron Canada Ltd APPENDIX 1 continued Rotorcraft TYPE 427 MODEL 429 Euro
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