text: ED Decision 2006/11/R 18/12/2006

text: OJ L 240, 7.9.2002, p.1. Regulation as last amended by

text: Commission Regulation (EC) 1701/2003 of 24 September 2003

text: (OJ L 243, 27.9.2003, p. 5) OJ L 315, 28.11.2003, p. 1 Regulation as amended by

text: Commission Regulation (EC) No 707/2006 of 8 May 2006

text: (OJ L 122, 9.5.2006, p. 17).

text: ED Decision 2006/11/R 18/12/2006

text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“Rulemaking Procedure”), EASA MB/7/03, 27.6.2003.

text: ED Decision 2006/11/R 18/12/2006

identifier: AMC to Part-145 — Amendment 1

amnesord: Part-145 - Maintenance organisation approvals

beslut: ED Decision 2006/011/R

publisher: Europeiska unionens byrå för luftfartssäkerhet

sprak: en

title: AMC to Part-145 — Amendment 1

serie: amc

text: European Aviation Safety Agency

type: rubrik

text: DECISION No 2006/11/R

type: stycke

text: OF THE EXECUTIVE DIRECTOR OF THE AGENCY

text: of 18-12-2006

text: amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY,

text: Having regard to

text: Regulation (EC) No 1592/2002 of 15 July 2002

text: on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the “Agency”), and in particular Articles

text: and

text: thereof.

text: Having regard to the

text: Commission Regulation (EC) No 2042/2003 of 28 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks. (Hereinafter referred to as

text: Commission Regulation (EC) No 2042/2003

text: Whereas:

text: (1) To clarify the meaning of “Officially recognised standard” each time the term is used in

text: Commission Regulation (EC) No 2042/2003

text: (2) National authorities as well as industry requested a definition of the concept of “Officially recognised standard”

text: (3) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance (hereinafter referred to as AMC), as well as any guidance material for the application of the Basic Regulation and its implementing rules.

text: (4) The Agency, pursuant to Article 43 of the Basic Regulation and articles 5(3) and 6 of the Agency rulemaking procedure , has widely consulted interested parties (see: NPA No 1-2006) on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received called CRD

text: HAS DECIDED:

text: Article 1

text: In AMC M.A.402 (b) the following paragraph is added after the first paragraph “In this context officially recognised standard means those standards established or published by an official body whether having legal personality or not, which are widely recognised by the air transport sector as constituting good practice”.

text: Article 2

text: In AMC M.A.606 (f) the following paragraph 11 is added “In this context officially recognised standard means those standards established or published by an official body whether having legal personality or not, which are widely recognised by the air transport sector as constituting good practice”.

text: Article 3

text: In AMC M.A.608 (b) the following paragraph 3 is added “In this context officially recognised standard means those standards established or published by an official body whether having legal personality or not, which are widely recognised by the air transport sector as constituting good practice”.

text: Article 4

text: In AMC 145.A.30 (f ) the following paragraph 11 is added “In this context officially recognised standard means those standards established or published by an official body whether having legal personality or not, which are widely recognised by the air transport sector as constituting good practice”.

text: Article 5

text: In AMC 145.A.40 (b) the following paragraph 3 is added “In this context officially recognised standard means those standards established or published by an official body whether having legal personality or not, which are widely recognised by the air transport sector as constituting good practice”.

text: Article 6

text: This decision shall enter into force on 25 December 2006. It shall be published in the Official Publication of the Agency.

text: Done in Cologne on 18 December 2006.

text: P. GOUDOU

type: vagledning

utgivare: easa


text: ED Decision 2007/002/R 13/03/2007

text: DECISION No 2007/002/R

text: OF THE EXECUTIVE DIRECTOR OF THE AGENCY

text: of 13 March 2007

text: amending Annex II of Decision N° 2003/19/RM of the Executive Director of the Agency of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003 of 20 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.

text: Having regard to

text: Regulation (EC) No 1592/2002

text: of the European Parliament and of the Council of 15 July 2002 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the Basic Regulation), and in particular Articles

text: and

text: thereof,

text: Having regard to the

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks ,

text: (1) Annex II of Acceptable Means of Compliance to Part-145 of Decision 2003/19/RM is required to be up to date to reflect the need of introducing the concept of Critical Design Control Configuration Limitations (CDCCL).

text: (2) To achieve this requirement the text of the Annex II of Acceptable Means of Compliance to Part-145 of Decision 2003/19/RM should be amended accordingly.

text: (3) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance, as well as any guidance material for the application of the Basic Regulation and its implementing rules.

text: OJ L 240, 7.9.2002, p. 1. Regulation as last amended by

text: Regulation (EC) No 1701/2003

text: (OJ L 243, 27.9.2003, p. 5). OJ L 315, 28.11.2003, p. 1. Regulation as amended by

text: Regulation (EC) No 707/2006

text: (OJ L 122, 9.5.2006, p. 17).

text: (4) The Agency, pursuant to Article 43 of the Basic Regulation and Articles 5(3) and 6 of the rulemaking procedure , has widely consulted interested parties on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received .

text: HAS DECIDED:

text: Article 1

text: The Annex II of Acceptable Means of Compliance to Part-145 of Decision

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks, is hereby amended in accordance with the Annex 1 to this Decision.

text: Article 2

text: This Decision shall enter into force on 20 March 2007.

text: Done in Cologne, 13 March 2007

text: P. GOUDOU By delegation C. PROBST

text: Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (“rulemaking procedure”), EASA MB/7/03, 27.6.2003. See: NPA No 22-2005 See: CRD No 22-2005

identifier: AMC to Part-145 — Amendment 2

beslut: ED Decision 2007/002/R

title: AMC to Part-145 — Amendment 2

text: European Aviation Safety Agency

text: Annex 1 to Decision 2007/002/R

text: The following paragraphs of Annex II to Decision 2003/19/RM AMC to Part-145 are amended as follows:

text: AMC 145.A.30(e) Personnel requirements

text: Insert a new paragraph 11:

text: 11. Additional training in fuel tank safety as well as associated inspection standards and maintenance procedures should be required of maintenance organisations’ technical personnel, especially technical personnel involved with the compliance of CDCCL tasks. EASA guidance is provided for training to maintenance organisation personnel in Appendix IV to AMC to 145.A.30(e) and 145.B.10(3). AMC 145.A.42(b) Acceptance of components The EASA Form 1 identifies the eligibility and status of an aircraft component. Block 13 "Remarks" on the EASA Form 1 in some cases contains vital airworthiness related information which may need appropriate and necessary actions. The receiving organisation should be satisfied that the component in question is in satisfactory condition and has been appropriately released to service. In addition, the organisation should ensure that the component meets the approved data/standard, such as the required design and modification standard. This may be accomplished by reference to the manufacturer's parts catalogue or other approved data (i.e. Service Bulletin). Care should also be exercised in ensuring compliance with applicable airworthiness directives, and the status of any life limited parts fitted to the aircraft component as well as Critical Design Configuration Control Limitations. AMC 145.A.45(b) Maintenance data

text: 1. Except as specified in sub-paragraph 5, each maintenance organisation approved under Part-145 should hold and use the following minimum maintenance data relevant to the organisation’s approval class rating. All maintenance related Implementing Rules and associated AMCs , approval specifications and Guidance Material, all applicable national maintenance requirements and notices which have not been superseded by an Agency requirement, procedure or directive and all applicable EASA airworthiness directives plus any non-national airworthiness directive supplied by a contracted non-EU operator or customer as well as Critical Design Configuration Control Limitations. …. AMC 145.A.45(d) Maintenance data The referenced procedure should address the need for a practical demonstration by the mechanic to the quality personnel of the proposed modified maintenance instruction. When satisfied the quality personnel should approve the modified maintenance instruction and ensure that the type certificate or supplementary type certificate holder is informed of the modified maintenance instruction. The procedure should include a paper/electronic traceability of the complete process from start to finish and ensure that the relevant maintenance instruction clearly identifies the modification. Modified maintenance instructions should only be used in the following circumstances; a Where the type certificate / supplementary type certificate holders original intent can be carried out in a more practical or more efficient manner. b Where the type certificate / supplementary type certificate holders original intent cannot be achieved by following the maintenance instructions. For example, where a component cannot be replaced following the original maintenance instructions. c For the use of alternative tools / equipment. Important note: Critical Design Configuration Control Limitations (CDCCL) are airworthiness limitations. Any modification of the maintenance instructions linked to CDCCL constitutes an aircraft modification that should be approved in accordance with Part-21. AMC 145.A.45(g) Maintenance data

text: 1. To keep data up to date a procedure should be set up to monitor the amendment status of all data and maintain a check that all amendments are being received by being a subscriber to any document amendment scheme. Special attention should be given to TC related data such as certification life limited parts, airworthiness limitations and Airworthiness Limitation Items (ALI), etc.

text: 2. …. AMC 145.A.50(a) Certification of maintenance Insert a new paragraph 3

text: 3. At any scheduled or unscheduled maintenance task carried out to a fuel system feature classified as a Critical Design Configuration Control Limitations (CDCCL) and before release to service, the maintenance records shall reflect that the correct configuration is maintained and ensured. This should be done by the marking: “CDCCL task”. AMC 145.A.65(b)(3) Safety and quality policy, maintenance procedures and quality system Insert a new paragraph 4:

text: 4. The maintenance organisation should ensure that when carrying out a modification, repair or maintenance, Critical Design Configuration Control Limitations are not compromised; this will require the development of appropriate procedures where necessary by the maintenance organisation. The maintenance organisation should pay particular attention to possible adverse effects of any wiring change to the aircraft, even a change not specifically associated with the fuel tank system. For example, it should be common practice to identify segregation of fuel gauging system wiring as a Critical Design Configuration Control Limitation. Maintenance organisations can prevent adverse effects associated with wiring changes by standardising maintenance practices through training, rather than by periodic inspection. Training should be provided to end indiscriminate routing and splicing of wire and to provide comprehensive knowledge of critical design features of fuel tank systems that would be controlled by a Critical Design Configuration Control Limitation. EASA guidance is provided for training to maintenance organisation personnel in an Appendix IV to be added to AMC to Part-145. The maintenance of ignition prevention features is necessary for the inherent safety and reliability of an aircraft’s fuel tank system. The aircraft cannot be operated indefinitely with the failure of an ignition prevention feature. The failure will have a direct adverse effect on operational safety. It could prevent the continued safe flight and landing of the aircraft or cause serious or fatal injury to the occupants. The fuel system review required will identify ignition prevention features of the design. The failure of any of these features may not immediately result in an unsafe condition, but it may warrant certain maintenance to support continued airworthiness. AMC 145.A.70(a) Maintenance organisation exposition The following information should be included in the maintenance organisation exposition: The information specified in 145.A.70(a) sub - paragraphs (6) and (12) to (16) inclusive, whilst a part of the maintenance organisation exposition, may be kept as separate documents or on separate electronic data files subject to the management part of said exposition containing a clear cross reference to such documents or electronic data files. The exposition should contain the information, as applicable, specified in this AMC. The information, may be presented in any subject order so long as all applicable subjects are covered. Where an organisation uses a different format, for example, to allow the exposition to serve for more than one approval, then the exposition should contain a cross reference Annex using this list as an index with an explanation as to where in the exposition the subject matter can be found. The exposition should contain information as applicable, on how the maintenance organisation complies with Critical Design Configuration Control Limitations (CDCCL) instructions. The exposition should state how the completion of CDCCL is traced. Insert a new Appendix IV to AMC to Part-145: Fuel Tank Safety training This appendix includes general instructions for providing training on Fuel Tank Safety issues.

text: 1. Levels of training Level 1 Familiarisation training Objectives: The attendant should, after the completion of the training: 1. be familiar with the basic elements of the fuel tank safety issues. 2. be able to give a simple description of the historical background and the elements requiring a safety consideration, using common words and showing examples of non conformities. 3. be able to use typical terms. The familiarisation training should include a presentation of bulletins/notices, short videos or CD material, poster campaigns, etc. Level 2 Detailed training Objectives: The attendant should, after the completion of the training: 1. know the history and the theoretical and practical elements of the subject, have an overview of Special Federal Aviation Regulations (SFARs) from 14 CFR SFAR 88 of the FAA and of JAA TGL 47, be able to give a detailed description of the concept of CDCCL, Airworthiness Limitations Items (ALI) and using theoretical fundamentals and specific examples, 2. have the capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner. 3. have detailed information on how the above items affect the aircraft in the scope of the activity of the organisation or in the fleet. 4. understand and carry out activities with the use of manufacturer and regulatory authority data providing instructions on design and maintenance, such as Service Bulletins, Airworthiness Directives, Aircraft Maintenance Manual, Component Maintenance Manual etc.

text: 5. use easily the manufacturer’s documentation from various sources and apply corrective action where appropriate.

text: 6. identify the components or parts or the aircraft subject to FTS from the manufacturer’s documentation, plan the action or apply a Service Bulletin and an Airworthiness Directive. Continuing training The interval between continuing training shall be established by the Maintenance organisation, but should not exceed two years. The continuing training shall include knowledge on evolution of material, tools, documentation and manufacturer’s or competent authority’s directives.

text: 2. The personnel directly involved in Fuel Tank Safety (FTS) systems shall be qualified according to the following table: Organisation Personnel Level of Continuing knowledge training Aircraft and Personnel in aircraft and 2 Yes component component shop maintenance maintenance organisations involved in organisations maintenance task planning, all personnel carrying maintenance tasks on aircraft or components classified as Fuel Tank Safety items, support staff and certifying staff Management, quality assurance 1 Not required personnel and auditors, personnel in charge of stores, and any personnel not directly involved in maintenance activities as required by the organisation NAA Management, inspectors and 1 Not required auditors.

text: 3. General requirements The training shall be carried out at the earliest for the personnel needing level 1 training. Nevertheless, the training for the personnel needing level 2 training has to be carried out before any maintenance task is commenced on an aircraft or a component. The training should be made in appropriate facilities containing examples of components, systems and parts affected by FTS issues and having access to aircraft or component where typical examples of FTS issues can be shown. The use of pictures, films and practical examples of the maintenance on fuel tank system is recommended. The training shall include a representative number of repair and inspections as required by the maintenance programme showing the necessity of using the manufacturer’s data.

text: 4. Characteristics of the training The following characteristics shall be taken into consideration when the level 1 or 2 training programmes are being established: a) understanding of the background and concepts of fuel tank safety as developed during the last 10 years, and b) how in maintenance organisations mechanics can recognise, interpret and handle the improvements that have been made or are being made during fuel tank system maintenance, c) awareness of any hazards working on the Fuel System, and especially with a Flammability Reduction System using nitrogen. a), b) and c) should be introduced in the training programme addressing the following issues: i) The theoretical background behind the fuel tank safety: the explosions of mixtures of fuel and air, the behaviour of those mixtures in an aviation environment, the effects of temperature and pressure, energy needed for ignition etc, the ‘fire triangle’, - Explain 2 concepts to prevent explosions: (1) ignition source prevention and (2) flammability reduction, ii) The major accidents and accident investigations and their conclusions, iii) SFARs from 14 CFR SFAR 88 of the FAA and JAA Internal Policy INT POL 25/12: reason of these documents, and what was the ultimate goal, margins of fuel system safety improvements (from 10-6 to 10-9, in fact improvement by a factor 100- 1000, to identify unsafe conditions and to correct them, to systematically improve fuel tank maintenance), iv) Explain the concepts that are being used: the results of SFAR 88 of the FAA and JAA INT/POL 25/12: modifications, airworthiness limitations and CDCCL, v) Where relevant information can be found by the mechanics and how to use and interpret this information (maintenance manuals, component maintenance manuals) vi) Fuel Tank Safety and Maintenance: fuel tank entry and exit procedures, clean working environment, what is meant by configuration control, wire separation, bonding of components etc, vii) Flammability reduction systems: reason for their presence, their effects, the hazards of an FRS using nitrogen for maintenance, safety precautions in maintenance/working with an FRS, viii) recording maintenance actions, recording measures and results of inspections.


identifier: AMC to Part-145 — Amendment 3

beslut: ED Decision 2009/007/R

title: AMC to Part-145 — Amendment 3

text: ED Decision 2009/007/R 24/03/2009

text: Annex 1 to Decision 2009/007/R

text: AMC to Part145

text: A new AMC 145.A.45(e) is added:

text: AMC 145.A.45(e) Maintenance data

text: The maintenance organisation should transcribe accurately the maintenance data onto such work cards or worksheets or make precise reference to the particular maintenance tasks or tasks contained in such maintenance data making reference to the CDCCL where applicable.

text: Paragraph 3 of AMC 145.A.50(a) is removed as follows: … 3. At any scheduled or unscheduled maintenance task carried out to a fuel system feature classified as a Critical Design Configuration Control Limitations (CDCCL) and before release to service, the maintenance records shall reflect that the correct configuration is maintained and ensured. This should be done by the marking: “CDCCL task”.

text: AMC 145.A.70(a) is amended as follows:

text: AMC 145.A.70(a) Maintenance organisation exposition

text: The following information should be included in the maintenance organisation exposition: The information specified in 145.A.70(a) sub  paragraphs (6) and (12) to (16) inclusive, whilst a part of the maintenance organisation exposition, may be kept as separate documents or on separate electronic data files subject to the management part of said exposition containing a clear cross reference to such documents or electronic data files. The exposition should contain the information, as applicable, specified in this AMC. The information may be presented in any subject order so long as all applicable subjects are covered. Where an organisation uses a different format, for example, to allow the exposition to serve for more than one approval, then the exposition should contain a cross reference Annex using this list as an index with an explanation as to where in the exposition the subject matter can be found. The exposition should contain information as applicable, on how the maintenance organisation complies with Critical Design Configuration Control Limitations (CDCCL) instructions. The exposition should state how the completion of CDCCL is traced. …

text: ED Decision 2009/007/R 24/03/2009

text: Appendix IV Fuel Tank Safety training This appendix includes general instructions for providing training on Fuel Tank Safety issues.

text: A) Effectivity:

text: · Large aeroplanes as defined in Decision 2003/11/RM of the Executive Director of the Agency (CS25) and certified after 1 January 1958 with a maximum type certified passenger capacity of 30 or more or a maximum certified payload capacity of 7500 lbs (3402 kg) cargo or more, and · Large aeroplanes as defined in Decision 2003/11/RM of the Executive Director of the Agency (CS25) which contains CS25 amendment 1 or later in their certification basis.

text: B) Affected organisations:

text: · Part145 approved maintenance organisations involved in the maintenance of aeroplanes specified in paragraph A) and fuel system components installed on such aeroplanes when the maintenance data are affected by CDCCL. · Competent authorities responsible as per 145.B.30 for the oversight of the Part145 approved organisations specified in this paragraph B).

text: C) Persons from affected organisations who should receive training:

text: Phase 1 only: · The group of persons representing the maintenance management structure of the organisation, the quality manager and the staff required to quality monitor the organisation. · Personnel of the competent authorities responsible as per 145.B.30 for the oversight of Part145 approved maintenance organizations specified in paragraph B). Phase 1 + Phase 2 + Continuation training: · Personnel of the Part145 approved maintenance organization required to plan, perform, supervise, inspect and certify the maintenance of aircraft and fuel system components specified in paragraph A).

text: ED Decision 2009/007/R 24/03/2009

text: D) General requirements of the training courses

text: Phase 1 – Awareness The training should be carried out before the person starts to work without supervision but not later than 6 months after joining the organisation. The persons who have already attended the Level 1 Familiarisation course in compliance with ED decision 2007/002/R Appendix IV is already in compliance with Phase 1. Type: Should be an awareness course with the principal elements of the subject. It may take the form of a training bulletin, or other self study or informative session. Signature of the reader is required to ensure that the person has passed the training. Level: It should be a course at the level of familiarisation with the principal elements of the subject. Objectives: The trainee should, after the completion of the training:

text: 1. Be familiar with the basic elements of the fuel tank safety issues.

text: 2. Be able to give a simple description of the historical background and the elements requiring a safety consideration, using common words and showing examples of non conformities.

text: 3. Be able to use typical terms. Content: The course should include:  a short background showing examples of FTS accidents or incidents,  the description of concept of fuel tank safety and CDCCL,  some examples of manufacturers documents showing CDCCL items,  typical examples of FTS defects,  some examples of TC holders repair data  some examples of maintenance instructions for inspection. Phase 2  Detailed training A flexible period may be allowed by the competent authorities to allow organisations to set the necessary courses and impart the training to the personnel, taking into account the organisation’s training schemes/means/practices. This flexible period should not extend beyond 31 December 2010. The persons who have already attended the Level 2 Detailed training course in compliance with ED decision 2007/002/R Appendix IV either from a Part145

text: ED Decision 2009/007/R 24/03/2009

text: maintenance organisation or from a Part147 training organisation are already in compliance with Phase 2 with the exception of continuation training.

text: Staff should have received Phase 2 training by 31 December 2010 or within 12 months of joining the organization, whichever comes later.

text: Type: Should be a more indepth internal or external course. It should not take the form of a training bulletin, or other self study. An examination should be required at the end, which should be in the form of a multi choice question, and the pass mark of the examination should be 75%.

text: Level: It should be a detailed course on the theoretical and practical elements of the subject.

text: The training may be made either:  in appropriate facilities containing examples of components, systems and parts affected by Fuel Tank Safety (FTS) issues. The use of films, pictures and practical examples on FTS is recommended; or  by attending a distance course (elearning or computer based training) including a film when such film meets the intent of the objectives and content here below. An elearning or computer based training should meet the following criteria:  A continuous evaluation process should ensure the effectiveness of the training and its relevance;  Some questions at intermediate steps of the training should be proposed to ensure that the trainee is authorized to move to the next step;  The content and results of examinations should be recorded;  Access to an instructor in person or at distance should be possible in case support is needed. A duration of 8 hours for phase 2 is an acceptable compliance.

text: When the course is provided in a classroom, the instructor should be very familiar with the data in Objectives and Guidelines. To be familiar, an instructor should have attended himself a similar course in a classroom and made additionally some lecture of related subjects.

text: Objectives:

text: The attendant should, after the completion of the training:  have knowledge of the history of events related to fuel tank safety issues and the theoretical and practical elements of the subject, have an overview of the FAA regulations known as SFAR (Special FAR) 88 of the FAA and of JAA Temporary Guidance Leaflet TGL 47, be able to give a detailed description of the concept of fuel tank system ALI (including Critical Design Configuration Control Limitations CDCCL, and using theoretical fundamentals and specific examples;  have the capacity to combine and apply the separate elements of knowledge in a logical and comprehensive manner;

text: ED Decision 2009/007/R 24/03/2009

text: have knowledge on how the above items affect the aircraft;  be able to identify the components or parts or the aircraft subject to FTS from the manufacturer’s documentation,  be able to plan the action or apply a Service Bulletin and an Airworthiness Directive. Content: Following the guidelines described in paragraph E). Continuation training The organisation should ensure that the continuation training is required in each two years period. The syllabus of the training programme referred to in 3.4 of the Maintenance Organisation Exposition (MOE) should include the additional syllabus for this continuation training. The continuation training may be combined with the phase 2 training in a classroom or at distance. The continuing training should be updated when new instruction are issued which are related to the material, tools, documentation and manufacturer’s or competent authority’s directives.

text: E) Guidelines for preparing the content of Phase 2 courses.

text: The following guidelines should be taken into consideration when the phase 2 training programme are being established: a) understanding of the background and the concept of fuel tank safety, b) how the mechanics can recognise, interpret and handle the improvements in the instruction for continuing airworthiness that have been made or are being made regarding the fuel tank system maintenance, c) awareness of any hazards especially when working on the fuel system, and when the Flammability Reduction System using nitrogen is installed. Paragraphs a) b) and c) above should be introduced in the training programme addressing the following issues: i) The theoretical background behind the risk of fuel tank safety: the explosions of mixtures of fuel and air, the behaviour of those mixtures in an aviation environment, the effects of temperature and pressure, energy needed for ignition etc, the ‘fire triangle’,  Explain 2 concepts to prevent explosions: (1) ignition source prevention and (2) flammability reduction, ii) The major accidents related to fuel tank systems, the accident investigations and their conclusions,

text: ED Decision 2009/007/R 24/03/2009

text: iii) SFAR 88 of the FAA and JAA Interim Policy INT POL 25/12: ignition prevention program initiatives and goals, to identify unsafe conditions and to correct them, to systematically improve fuel tank maintenance),

text: iv) Explain the briefly concepts that are being used: the results of SFAR 88 of the FAA and JAA INT/POL 25/12: modifications, airworthiness limitations items and CDCCL,

text: v) Where relevant information can be found and how to use and interpret this information in the instructions for continuing airworthiness (aircraft maintenance manuals, component maintenance manuals, Service Bulletins…)

text: vi) Fuel Tank Safety during maintenance: fuel tank entry and exit procedures, clean working environment, what is meant by configuration control, wire separation, bonding of components etc,

text: vii) Flammability reduction systems when installed: reason for their presence, their effects, the hazards of an FRS using nitrogen for maintenance, safety precautions in maintenance/working with an FRS,

text: viii) Recording maintenance actions, recording measures and results of inspections.

text: The training should include a representative number of examples of defects and the associated repairs as required by the TC / STC holders maintenance data.

text: F) Approval of training

text: For Part145 approved organisations, the approval of the initial and continuation training programme and the content of the examination can be achieved by the change to the MOE exposition. The necessary changes to the MOE to meet the content of this decision should be made and implemented at the time requested by the competent authority.


identifier: AMC to Part 145 — Amendment 8

beslut: ED Decision 2015/016/R

title: AMC to Part 145 — Amendment 8

text: Annex II to Decision 2003/19/RM is amended as follows: The text of the amendment is arranged to show deleted text, new or amended text as shown below: (a) deleted text is marked with strikethrough; (b) new or amended text is highlighted in grey; (c) an ellipsis (…) indicates that the remaining text is unchanged in front of or following the reflected amendment.

text: 1. A new AMC 145.A.50 is introduced in Annex II to Decision 2003/19/RM: AMC 145.A.50 Certification of maintenance after embodiment of a Standard Change or Standard Repair (SC/SR) AMC M.A.801 of the AMC to Part-M contains acceptable means of compliance for the release to service of a SC/SR by an organisation approved in accordance with Part-145.


identifier: AMC to Part 145 — Amendment 9

beslut: ED Decision 2015/024/R

title: AMC to Part 145 — Amendment 9

text: Annex II to ED Decision 2015/0024/R

text: Annex II (Acceptable Means of Compliance to Part-145) to Decision 2003/19/RM is amended as follows: The text of the amendment is arranged to show deleted text, new or amended text as shown below: (a) deleted text is marked with strikethrough; (b) new or amended text is highlighted in grey; (c) an ellipsis (…) indicates that the remaining text is unchanged in front of or following the reflected amendment.

text: A new AMC 145.A.36 is introduced as follows:

text: AMC 145.A.36 Records of airworthiness review staff

text: The following minimum information, as applicable, should be kept on record in respect of each airworthiness review staff: (a) name; (b) date of birth; (c) certifying staff authorisation; (d) experience as certifying staff on ELA1 aircraft; (e) qualifications relevant to the approval (knowledge of relevant parts of Part -M and knowledge of the relevant airworthiness review procedures); (f) scope of the airworthiness review authorisation and personal authorisation reference; (g) date of the first issue of the airworthiness review authorisation; and (h) if appropriate, expiry date of the airworthiness review authorisation.

text: AMC 145.A.55(c) is amended as follows:

text: AMC 145.A.55(c) Maintenance and airworthiness review records

text: AMC 145.A.70(a) is amended as follows:

text: AMC 145.A.70(a) Maintenance organisation exposition

text: PART 0 GENERAL ORGANISATION (Operators within the European Union)

text: PART 1 MANAGEMENT

text: … 1.5 Management organisation chart 1.6 List of certifying staff, and support staff and airworthiness review staff 1.7 Manpower resources …

text: PART 2 MAINTENANCE PROCEDURES

text: … 2.28 Production planning procedures 2.29 Airworthiness review procedures and records for ELA1 aircraft not involved in commercial operations 2.30 Development and approval processing for maintenance programmes for ELA2 aircraft not involved in commercial operations

text: PART L2 ADDITIONAL LINE MAINTENANCE PROCEDURES

text: PART 3 QUALITY SYSTEM PROCEDURES

text: PART 4

text: PART 5

text: PART 6 OPERATORS MAINTENANCE PROCEDURES

text: PART 7 FAA SUPPLEMENTARY PROCEDURES FOR A FAR PART-145 REPAIR STATION

text: PART 8 TRANSPORT CANADA CIVIL AVIATION (TCCA) SUPPLEMENTARY PROCEDURES FOR A TCCA AM573 MAINTENANCE ORGANISATION

text: Part 1: General Name of organisation: Approval reference: Requested approval rating/ EASA Form 3 dated*: FAA FAR 145 Cert No (if applicable): Address of Facility Audited: Audit period: From to Date(s) of Audit: Audit reference(s): Persons interviewed:

text: Competent authority surveyor: Signature(s): Competent authority office: Date of EASA Form 6 part 1 completion: *delete where applicable Part-145 APPROVAL RECOMMENDATION REPORT EASA FORM 6 Part 2: Part-145 Compliance Audit Review The five columns may be labelled and used as necessary to record the approval class and/or product line reviewed. Against each column used of the following Part-145 subparagraphs please either tick () the box if satisfied with compliance or cross (X) the box if not satisfied with compliance and specify the reference of the Part 4 finding next to the box, or enter N/A where an item is not applicable, or N/R when applicable but not reviewed.

text: Para Subject 145.A.25 Facility requirements 145.A.30 Personnel requirements 145.A.35 Certifying Staff and support staff 145.A.36 Records of airworthiness review staff 145.A.40 Equipment, Tools and material 145.A.42 Acceptance of Components 145.A.45 Maintenance Data 145.A.47 Production Planning 145.A.50 Certification of Maintenance 145.A.55 Maintenance Records 145.A.60 Occurrence Reporting 145.A.65 Safety and Quality Policy, maintenance procedures and Quality System 145.A.70 Maintenance Organisation Exposition (see Part 3) 145.A.75 Privileges of the organisation 145.A.80 Limitations on the organisation

text: 145.A.85 Changes to the organisation

text: 145.A.95 Findings

text: Competent surveyor(s): Signature(s):

text: Competent authority office: Date of EASA Form 6 part 2 completion:

text: Part-145 APPROVAL RECOMMENDATION REPORT EASA FORM 6 PART 3: Compliance with 145.A.70 Maintenance organisation exposition Please either tick () the box if satisfied with compliance; or cross (X) if not satisfied with compliance and specify the reference of the Part 4 finding; or enter N/A where an item is not applicable; or N/R when applicable but not reviewed.

text: Part 1 Management

text: 1.1 Corporate commitment by the accountable manager 1.2 Safety and Quality Policy 1.3 Management personnel 1.4 Duties and responsibilities of the management personnel 1.5 Management Organisation Chart 1.6 List of Certifying staff, and support staff and airworthiness review staff (Note: a separate document may be referenced) 1.7 Manpower resources 1.8 General description of the facilities at each address intended to be approved 1.9 Organisations intended scope of work 1.10 Notification procedure to the competent authority regarding changes to the organisation’s activities/approval/location/personnel 1.11 Exposition amendment procedures

text: Part 2 Maintenance Procedures

text: 2.1 Supplier evaluation and subcontract control procedure 2.2 Acceptance/inspection of aircraft components and material from outside contractors 2.3 Storage, tagging, and release of aircraft components and material to aircraft maintenance 2.4 Acceptance of tools and equipment

text: 2.5 Calibration of tools and equipment 2.6 Use of tooling and equipment by staff (including alternate tools) 2.7 Cleanliness standards of maintenance facilities 2.8 Maintenance instructions and relationship to aircraft/aircraft component manufacturers’ instructions including updating and availability to staff 2.9 Repair procedure 2.10 Aircraft maintenance programme compliance 2.11 Airworthiness Directives procedure 2.12 Optional modification procedure 2.13 Maintenance documentation in use and completion of same 2.14 Technical record control 2.15 Rectification of defects arising during base maintenance 2.16 Release to service procedure 2.17 Records for the operator 2.18 Reporting of defects to the competent authority/Operator/Manufacturer 2.19 Return of defective aircraft components to store 2.20 Defective components to outside contractors 2.21 Control of computer maintenance record systems 2.22 Control of manhour planning versus scheduled maintenance work 2.23 Control of critical tasks 2.24 Reference to specific maintenance procedures 2.25 Procedures to detect and rectify maintenance errors 2.26 Shift/task handover procedures 2.27 Procedures for notification of maintenance data inaccuracies and ambiguities to the type certificate holder 2.28 Production planning procedures 2.29 Airworthiness review procedures and records for ELA1 aircraft not involved in commercial operations 2.30 Development and approval processing for maintenance programmes for ELA2 aircraft not involved in commercial operations

text: Part L2 Additional Line Maintenance Procedures

text: L2.1 Line maintenance control of aircraft components, tools, equipment, etc. L2.2 Line maintenance procedures related to servicing/fuelling/de-icing, etc. L2.3 Line maintenance control of defects and repetitive defects

text: L2.4 Line procedure for completion of technical log L2.5 Line procedure for pooled parts and loan parts L2.6 Line procedure for return of defective parts removed from aircraft L2.7 Line procedure for control of critical tasks

text: Part 3 Quality System Procedures

text: 3.1 Quality audit of organisation procedures 3.2 Quality audit of aircraft 3.3 Quality audit remedial action procedure 3.4 Certifying staff qualification and training procedure 3.5 Certifying staff records 3.6 Quality audit personnel 3.7 Qualifying inspectors 3.8 Qualifying mechanics 3.9 Aircraft/aircraft component maintenance tasks exemption process control. 3.10 Concession control for deviation from organisation’s procedures 3.11 Qualification procedure for specialised activities such as NDT, welding etc. 3.12 Control of manufacturers’ and other maintenance working teams 3.13 Human Factors training procedure 3.14 Competence assessment of personnel 3.15 Training procedures for on-the-job training as per Section 6 of Appendix III to Part- 66 (limited to the case where the competent authority for the Part-145 approval and for the Part-66 licence is the same). 3.16 Procedure for the issue of a recommendation to the competent authority for the issue of a Part-66 licence in accordance with 66.B.105 (limited to the case where the competent authority for the Part-145 approval and for the Part-66 licence is the same).

text: Part 4

text: 4.1 Contracting operators 4.2 Operator procedures/paperwork 4.3 Operator record completion

text: Part 5 Appendices

text: 5.1 Sample Documents 5.2 List of subcontractors 5.3 List of Line maintenance locations 5.4 List of Part-145 organisations

text: MOE Reference: MOE Amendment: Competent authority audit staff: Signature(s):

text: Competent authority office: Date of EASA Form 6 part 3 completion:

text: Part-145 APPROVAL RECOMMENDATION REPORT EASA FORM 6 Part 4: Findings Part-145 Compliance status Each level 1 and 2 finding should be recorded whether it has been rectified or not and should be identified by a simple cross-reference to the Part 2 requirement. All non-rectified findings should be copied in writing to the organisation for the necessary corrective action. Part Audit reference(s): L Corrective action E 2 or 3 Findings Date Date V E L ref. Due Closed Reference

text: Part-145 APPROVAL RECOMMENDATION REPORT EASA FORM 6 Part 5: Part-145 Approval or continued approval or change recommendation* Name of organisation: Approval reference: Audit reference(s): The following Part-145 scope of approval is recommended for this organisation: Or, it is recommended that the Part-145 scope of approval specified in EASA Form 3

text: Name of recommending competent authority surveyor: Signature of recommending competent authority surveyor: Competent authority office: Date of recommendation: EASA Form 6 review (quality check) : Date:


text: OJ L 240, 7.9.2002, p. 1. 2 OJ L 315, 28.11.2003, p. 1. 3 Decision of the Management Board concerning the procedure to be applied by the Agency for the issuing of opinions, certification specifications and guidance material (”rulemaking procedure”), EASA MB/7/03, 27.6.2003. 4 See NPA No 6-2005 (http://www.easa.eu.int/doc/Rulemaking/NPA/NPA_06_2005.pdf). 5 See CRD No 6-2005 (http://www.easa.eu.int/doc/Rulemaking/rule_CRD_06_2005.pdf).

identifier: AMC to Part-147 — AMC Amendment 1

amnesord: Part-147 - Organisations training Part 66 license applicants

beslut: ED Decision 2006/001/R

title: AMC to Part-147 — AMC Amendment 1

text: ED Decision 2006/01/R 16/05/2006

text: European Aviation Safety Agency

text: DECISION No 2006/01/R

text: OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY

text: of 16 May 2006

text: amending Annex VI of Decision No 2003/19/RM of the Executive Director of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to

text: Regulation (EC) No 1592/2002 of 15 July 2002

text: (hereinafter referred to as “the Basic Regulation”) on common rules in the field of civil aviation and establishing a European Aviation Safety Agency (hereinafter referred to as the “Agency”), and in particular Articles

text: and

text: thereof, Having regard to

text: Commission Regulation (EC) No 2042/2003 of 28 November 2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks , Having regard to Decision No 2003/19/RM of the Executive Director of the Agency of 28 November 2003 on acceptable means of compliance and guidance material to

text: Commission Regulation (EC) No 2042/2003

text: on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks,

text: Whereas:

text: (1) The Agency shall issue certification specifications, including airworthiness codes and acceptable means of compliance (hereinafter referred to as “AMC”), as well as any guidance material for the application of the Basic Regulation and its implementing rules.

text: (2) The Agency, pursuant to Article 43 of the Basic Regulation and articles

text: and

text: 3 4 of the EASA rulemaking procedure , has widely consulted interested parties on the matters which are the subject of this Decision and has provided thereafter a written response to the comments received .

text: ED Decision 2006/01/R 16/05/2006

text: (3) AMC 147.A.110 is inserted into Annex VI “Acceptable Means of Compliance to Part-147” to Decision No 2003/19/RM of the Executive Director of the Agency of 28 November 2003 in order to reflect on the minimum dates and information to be kept on record on each instructor, examiner and assessor by the Part-147 approved maintenance training organisation.

text: HAS DECIDED AS FOLLOWS:

text: Article 1

text: Annex VI “Acceptable means of compliance to Part-147” to Decision 2003/19/RM of the Executive Director of the Agency of 28 November 2003 is hereby amended as follows:

text: The following AMC is inserted:

text: AMC 147.A.110 Records of instructors, examiners and assessors

text: 1. The following minimum information relevant to the scope of activity should be kept on record in respect of each instructor, knowledge examiner and practical assessor: (a) Name (b) Date of Birth (c) Personnel Number (d) Experience (e) Qualifications (f) Training history (before entry) (g) Subsequent Training (h) Scope of activity (i) Starting date of employment/contract (j) If appropriate – ending date of employment/contract.

text: 2. The record may be kept in any format but should be under the control of the organisations quality system.

text: 3. Persons authorised to access the system should be maintained at a minimum to ensure that records cannot be altered in an unauthorised manner or that such confidential records become accessible to unauthorised persons.

text: 4. The competent authority is an authorised person when investigating the records system for initial and continued approval or when the competent authority has cause to doubt the competence of a particular person.

text: Article 2

text: This Decision shall enter into force on 16 May 2006.

text: Done in Cologne, 16 May 2006

text: P. GOUDOU


text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation

text: N 262 B Frégate N 262 C Frégate

text: A300 B2-1A A300 B2-1C A300 B2K-3C A300 B2-202 A300 B2-203 A300 B4-2C A300 B4-102 A300 B4-103 A300 B4-203 A300 C4-203 A300 F4-203

text: A300 B4-120 A300 B4-220

text: A300 B4-601 Airbus A300-600 (GE CF6) A300 B4-603 A300 B4-605 R A300 F4-605 R A300 C4-605 R Variant F

text: A300 B4-622 R A300 F4-622 R

text: A300 C4-620

text: A310-308 A310-203 A310-221 A310-203 C

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation AIRBUS A310-204

text: A319-110 series A320-111 A320-210 series A321-110 series A321-210 series

text: A320-230 series A321-130 series A321-230 series

text: A330-300 series

text: A330-320 series

text: A330-340 series 700)

text: A340-310 series

text: A340-640 series 500)

text: One-Eleven 300 series One-Eleven 400 series One-Eleven 500 series AIRCRAFT L-410 M/UVP Turbolet Let L-410 (Walter M601) INDUSTRIES L-410 UVP-E L-410 UVP-E9 L-410 UVP-E20

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation L-410 UVP-E20 CARGO L-410 UVP-E-LW L-410 UVP-LW

text: Avions de PW120) Transport Régional ATR 42-300

text: ATR 42-320

text: ATR 72-102

text: ATR 72-201

text: ATR 72-202

text: ATR 72-211

text: ATR 72-212

text: ATR 42-500 42-500

text: ATR 42-500 42-600

text: ATR 72-212 A 72-500

text: ATR 72-212 A 72-600

text: BAe 146 Series 200

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation BAe 146 Series 300 AVRO 146-RJ70 AVRO 146-RJ85 AVRO 146-RJ100 AVRO 146-RJ115

text: HS.748 Series 2 HS 748 Series 2A HS 748 Series 2B HP.137 Jetstream Mk.1 Jetstream 1 HP.137 (Turbomeca Astazou) HP.137 Jetstream Mk.1 Jetstream 2

text: Jetstream 3101 Jetstream 31 Jetstream 31/32 (Honeywell

text: Jetstream 3201 Jetstream 32/32EP

text: Jetstream 4101

text: THE BOEING B707-100 Long Body Boeing 707/720 (PW JT3D) COMPANY B707-100B Long Body B707-100B Short Body B707-300B Series B707-300C Series B720 B720B

text: B707-200B B707-300 Series

text: B727-100 Series

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation B727C Series THE BOEING B727-100C Series Boeing 727 (PW JT8D) COMPANY B727-200 Series

text: B737-200 B737-200C

text: B737-400 B737-500

text: B737-700 B737-700C B737-800 B737-900 B737-900ER

text: B747-100B B747-100B SUD

text: B747-200C B747-200F B747-300

text: B747-200F B747-200C

text: B747-200F B747-200C

text: B747-400F/SF(BCF)/LCF B747-8I Intercontinental Boeing 747-8 (GE GEnx) B747-8F Freighter

text: B757-200PF B757-300

text: B757-200PF B757-200CB B757-300

text: B777F Freighter

text: Dreamliner 1000)

text: Variant) BD-100-1A10 Challenger 300 Bombardier BD-100-1A10

text: BD-700-1A11 Global 5000

text: CL600-1A11 Challenger 600 Bombardier CL-600-1A11

text: CL-600-2A12 (601 Challenger 601 Bombardier CL-600-2A12/-2B16

text: CL-600-2B16 (601-3A Challenger 601-3A Variant)

text: CL-600-2B16 (601-3R Challenger 601-3R Variant)

text: CL-600-2B16 (CL 604 Challenger-604 Bombardier CL-600-2B16 (variant Variant) (MSN < 5701) CL 604) (GE CF34)

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation CL-600-2B16 (CL 604 Challenger-605 Variant) (MSN > 5701)

text: CL-600-2B19 Regional Jet Series Bombardier CL-600-2B19 (GE

text: CL-600-2C10 Regional Jet Series Bombardier CL-600-2C10/-2D15/-

text: CL-600-2D15 Regional Jet Series 705 CL-600-2D24 Regional Jet Series 900 CL-600-2E25 Regional Jet Series 1000

text: DHC-8-102 DHC-8 Series 100

text: DHC-8-103 DHC-8 Series 100

text: DHC-8-106 DHC-8 Series 100

text: DHC-8-201 DHC-8 Series 200

text: DHC-8-202 DHC-8 Series 200

text: DHC-8-301 DHC-8 Series 300

text: DHC-8-311 DHC-8 Series 300

text: DHC-8-314 DHC-8 Series 300

text: DHC-8-315 DHC-8 Series 300

text: DHC-8-400 DHC-8 Series 400 Bombardier DHC-8-400 (PWC

text: DHC-8-401 DHC-8 Series 400

text: DHC-8-402 DHC-8 Series 400

text: PLC SD3-60 Variant 200

text: SD3-SHERPA Variant 200

text: SD3-60 SHERPA Variant 200

text: C-212-CC Aviocar C-212-CD Aviocar C-212-CE Aviocar C-212-CF Aviocar C-212-DD Aviocar

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation C-212-DF Aviocar C-212-EE Aviocar C-212-VA Aviocar

text: CN-235-200 CN-235-300

text: AIRCRAFT Company 525C Citation Jet CJ4

text: Citation Encore

text: Citation Encore +

text: S550 Citation S/II

text: Citation V

text: Citation Ultra

text: XLS Citation XLS

text: XLS+ Citation XLS+

text: Citation VII

text: AVIATION Fan Jet Falcon (Basic) Fan Jet Falcon 20 (GE CF700) Falcon Fan Jet Falcon Series C Fan Jet Falcon Series D Fan Jet Falcon Series E Fan Jet Falcon Series F

text: Mystère Falcon 20-D5 Mystère Falcon 20-E5 Mystère Falcon 20-F5

text: Mystère Falcon 200 Mystère Falcon 20GF

text: Mystère Falcon 900 F900B

text: Falcon 900EX F900DX Falcon 900EX F900LX

text: Falcon 2000EX F2000DX Falcon 2000EX F2000LX

text: Aerospace GmbH 228-200 series (DORNIER)

text: EMB-120RT Brasilia EMB-120ER Brasilia EMB-120FC Brasilia EMB-120QC Brasilia

text: EMB-135LR EMB-135BJ Legacy 600 Legacy 650 EMB-145 EMB-145ER EMB-145EU EMB-145EP EMB-145LR EMB-145LU EMB-145MP EMB-145MK

text: ERJ 170-100 LR ERJ-170 ERJ 170-200 STD ERJ-175 ERJ 170-200 LR ERJ-175 ERJ 190-100 STD ERJ-190 ERJ 190-100 LR ERJ-190 ERJ-190-100SR ERJ-190 ERJ 190-100 IGW ERJ-190 AR ERJ 190-100 ECJ Lineage 1000

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation ERJ 190-200 STD ERJ-195 ERJ 190-200 LR ERJ-195 ERJ 190-200 IGW ERJ-195 AR

text: MARYLAND AIR INDUSTRIES FH-227

text: FOKKER F27 Mark 100 Friendship SERVICES F27 Mark 200 Friendship F27 Mark 300 Friendship F27 Mark 400 Friendship F27 Mark 500 Friendship F27 Mark 600 Friendship F27 Mark 700 Friendship

text: F27 Mark 0502 Fokker 50 F27 Mark 0604 Fokker 60

text: F28 Mark 1000C Fellowship F28 Mark 2000 Fellowship F28 Mark 3000 Fellowship

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation F28 Mark 3000C Fellowship F28 Mark 3000R Fellowship F28 Mark 3000RC Fellowship FOKKER F28 Mark 4000 Fellowship Fokker F28 Series (RRD Spey) SERVICES F28 Mark 0100 Fokker 100 Fokker 70/100 (RRD Tay) F28 Mark 0070 Fokker 70

text: LP (GALP) c/o Israel Aircraft Industries Astra SPX

text: G100 Gulfstream 100

text: Gulfstream 200 / Galaxy Galaxy 200 Gulfstream (IAI) 200/Galaxy (PWC

text: GULFSTREAM G-159 Gulfstream I Gulfstream G-159 (RRD Dart) AEROSPACE Corporation

text: G-1159A Gulfstream IIB

text: G-1159B Gulfstream III

text: IV/GIV-SP GIV (G300) Gulfstream G300

text: GIV (G400) Gulfstream G400

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation GIV-X (G350) Gulfstream G350

text: GV-SP (G500) Gulfstream G500

text: HAWKER HS.125 series 700 "Hawker Siddeley" BAe 125 Series /700/800

text: Corporation BAe.125 series 800 Hawker 800 DH.125 series 1 "Hawker Siddeley" DH.125 series 3 "Hawker Siddeley" HS.125 series 3 "Hawker Siddeley" HS.125 series F3 "Hawker Siddeley" BH.125 series 400 "Beechcraft Hawker" DH.125 series 400 "Hawker Siddeley" HS.125 series F400 "Hawker Siddeley" BH.125 series 600 "Beechcraft Hawker" HS.125 series 600 "Hawker Siddeley" HS.125 series F600 "Hawker Siddeley"

text: Hawker 750 Hawker 750 BAe 125 Series

text: Hawker 800XP Hawker 800XP

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation Hawker 850XP Hawker 850XP Hawker 900XP Hawker 900XP DH.125 series 1 "Hawker Siddeley" BAe 125 Series (RR Viper) HS.125 series 1 "Hawker Siddeley" DH.125 series 3 "Hawker Siddeley" HS.125 series 3 "Hawker Siddeley" HS.125 series F3 "Hawker Siddeley" DH.125 series 400 "Hawker Siddeley" HS.125 series 400 "Hawker Siddeley" BH.125 series 400 "Beechcraft Hawker" HS.125 series F400 "Hawker Siddeley" BH.125 series 600 "Beechcraft Hawker" HS.125 series 600 "Hawker Siddeley" HS.125 series F600 "Hawker Siddeley"

text: Hawker 1000

text: 300LW Super King Air B300 Super King Air 350

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation B300C Super King Air 350 C

text: 400A Beechjet (Hawker 400XP) 400T Beechjet

text: MU-300 Diamond I/IA

text: MU-300-10 Diamond II

text: 1900C Airliner

text: 1900D Airliner

text: ISRAEL IAI 1121 Jetcommander IAI 1121/1123 (GE CJ610)F AIRCRAFT INDUSTRIES IAI 1121A Jetcommander IAI 1121B Jetcommander IAI 1123 Commodore Jet

text: IAI 1124A Westwind

text: 24B / 24B-A 24C 24D / 24D-A 24E 24F / 24F-A 25 25A 25B 25C

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation 25D 25F

text: Learjet 40 LJ45

text: Upgraded Learjet 60 LJ60XR LOCKHEED 1329-25 JetStar II Lockheed 1329 (Honeywell

text: 1329-23D JetStar

text: 1329-23E JetStar (-8 version)

text: Model L-188 Electra

text: 382B Hercules

text: 382E Hercules

text: 382F Hercules

text: 382G Hercules

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation L-1011-385-1-14 TriStar L-1011-385-1-15 TriStar L-1011-385-3 TriStar McDONNELL DC-8 Series 70 DC-8 (CFM56) DOUGLAS Corporation DC-8 Series 70F

text: DC-8F DC-8 Series 60 DC-8 Series 60F DC-8 Series 10/20/30 DC-8 (PW JT4A)

text: DC-9-20 Series DC-9-30 Series DC-9-40 Series DC-9-50 Series

text: DC-9-82 (MD-82) Series DC-9-83 (MD-83) Series

text: TC holder 2 Aeroplanes Model Commercial 3 Type rating endorsement Designation DC-9-87 (MD-87) Series MD-88

text: DC-10-10F DC-10-15 DC-10-30 DC-10-30F

text: AEROSPACE TPE331) SA227-TT SA227-CC SA227-DC SA227-AC Swearingen Metro SA227-BC Swearingen Metro

text: ZAKLADY LOTNICZE PZL M28 02

text: PZL M28 05

text: Corporation TFE731)

text: NA-265-20 NA-265-30 NA-265-40 NA-265-60 NA-265-65 NA-265-70 NA-265-80 SAAB AB, 340A(SF340A) Saab-Fairchild 340A Saab (SF) 340 (GE CT7) SAAB Aerosystems 340B

text: DHC-7-100 DHC-7-101 DHC-7-102 DHC-7-103 DHC-7-110 DHC-7-111

text: AERO VODOCHODY

text: AIRCRAFT L-410M Turbolet INDUSTRIES L-410 UVP Turbolet

text: L-410 UVP-FG L-410 UVP-E-LW CESSNA AIRCRAFT 425 Corsair / Conquest I Cessna 425 (PWC PT6) Company

text: Citation / Citation I

text: Citation II

text: Citation Jet CJ1

text: 525A Citation Jet CJ2 DORNIER Seastar

text: ECLIPSE AEROSPACE

text: Inc. EMBRAER EMB-110P1 Bandeirante

text: EMB-110P2 Bandeirante de Aeronautica EMB-121A Xingu I

text: EMB-121V Xingu III

text: EXTRA Flugzeugproduktions- EA 400-500 Extra EA-400-500 (RR Corp 250) und Vertiebs GmbH HAWKER 65-90 King Air BEECHCRAFT 65-A90 King Air Corporation 65-A90-1 King Air 65-A90-4 King Air 65-A90-2 King Air B90 King Air

text: C90A King Air C90GT King Air C90GTi King Air E90 King Air F90 King Air H90 King Air

text: HAWKER 200/A200 BEECHCRAFT 200C/A200C Corporation (cont.) 200CT/A200CT 200T B200

text: B200C B200CT B200T B200GT B200CGT 99 99A A99 Airliner A99A Airliner

text: C99 Airliner 100 King Air A100 King Air A100A/C King Air

text: Premier 1, 1A Beech 390 390

text: ISRAEL AIRCRAFT Industries Arava 101B Arava 101B (PWC PT6)

text: M7 AEROSPACE SA226-T SA226-TC

text: SA226-AT SA226-T(B) MITSUBISHI MU-2B Heavy Industries MU-2B-10 MU-2B-20 MU-2B-125

text: MU-2B-35 MU-2B-2540 MU-2B-36 MU-2B-2660 PIAGGIO P.166 DP1

text: Aero Industries

text: P180 Avanti II PT6)

text: PILATUS AIRCRAFT PC-12 PC-12/45

text: PC-12/47 PC-12/47E PIPER AIRCRAFT PA-42-1000 Cheyenne 400LS Piper PA-42 (Honeywell TPE-331) PA-42 Cheyenne III

text: Cheyenne IIIA PA-42-720R

text: REIMS AVIATION

text: SOCATA TBM 700 A TBM 700 B

text: TBM 700 C2 TBM 700 N TBM 850 TWIN COMMANDER 680-T AIRCRAFT 680-V Corporation 680-W 681 690

text: 690C 690D 695 695A 695B VIKING AIR DHC-6-1 Twin Otter (Bombardier) DHC-6-100/110 Twin Otter (De Havilland) DHC-6-200/210 Twin Otter

text: DHC-6- Twin Otter 300/310/320 DHC-6-400 Twin Otter

text: AP68TP600 Viator 250) SF600

text: GOVERNMENT AIRCRAFT FACTORIES Nomad N24A (RR Corp 250) (ASTA) B-N GROUP Ltd. Britten-Norman BN2T Series (Islander) (Britten-Norman) (RR Corp 250) RUAG Aerospace Services GmbH Dornier Do 28 Series (PWC PT6) DORNIER DORNIER Dornier Do 28 (Walter M601)

text: AIRCRAFT INDUSTRIES Let L 200 (LOM) B-N GROUP Britten-Norman BN2 Islander (Lycoming) (Britten-Norman) Britten-Norman BN2A Series Trislander (Lycoming) Britten-Norman BN2B Series (Lycoming) CESSNA AIRCRAFT Company/ Cessna 310/320 Series (Continental) REIMS AVIATION Cessna 335 (Continental) Cessna 336 (Continental) Cessna/Reims-Cessna 337 Series (Continental) (not pressurised) Cessna/Reims-Cessna 337 Series (Continental) (pressurised) Cessna 340 (Continental) Cessna 401/402 (Continental) Cessna 404 (Continental) Cessna 411 (Continental) Cessna 414 (Continental) Cessna 421 (Continental) Cessna T303 (Continental) GENERAL AVIA General Avia F20 Series (Lycoming) Costruzioni Aeronautiche HAWKER BEECHCRAFT Beech 50 Series (Lycoming) Corporation Beech 55 Series (Continental) Beech 56 Series (Lycoming) Beech 58 Series (Continental) Beech 58P (Continental) Beech 58TC (Continental) Beech 60 Series (Lycoming) Beech 65-80 Series (Lycoming) Beech 76 (Lycoming) Beech 95 Series (Lycoming) OMA SUD SPA Sky Technolgies SKYCAR (Lycoming) PIAGGIO Piaggio P166 (Lycoming) Aero Industries PIPER AIRCRAFT Piper PA-23 Aztec (Lycoming) Piper PA-30 Series (Lycoming) Piper PA-31 Series (Lycoming) Piper PA-31P (Lycoming) Piper PA-34 Series (Lycoming) Piper PA-34 Series (Continental) Piper PA-39/40 Series (Lycoming) Piper PA-44 Series (Lycoming) PZL MIELEC PZL-M20 (PZL)

text: TECNAM Costruzioni Aeronautiche Tecnam P92 (Rotax) Tecnam P96/P2002/P2004 (Rotax) THRUSH Aircraft Ayres S2R (PW R-985)

text: TRUE FLIGHT Grumman/American AA-1/-1A Series (Lycoming) Holdings Grumman/American AA-5/AG-5B Series (Lycoming) VULCANAIR Partenavia P.64 (Lycoming)

text: DIAMOND AIRCRAFT Industries Diamond DA42 Series (Thielert) Diamond DA42 Series (Austro Engine)

text: Model Commercial Designation

text: AGUSTA A109E

text: AW109SP A109 A109A

text: A109AII A109C

text: AW139 EH101-500 Series

text: EH101-510 Series

text: EH101-300 AGUSTA AB 212

text: BELL HELICOPTER 212 TEXTRON

text: AGUSTA AB 412 AB 412 EP BELL HELICOPTER CANADA 427

text: 222U 230 Executive

text: HELICOPTERS 234UT

text: EAC S-64F CRANE

text: EUROCOPTER SA 330 F Eurocopter SA 330

text: SA 330 G

text: Model Commercial Designation

text: SA 330 J AS 332 C

text: AS 332 L1

text: AS 332 L2

text: AS 355 E AS 355 F

text: AS 355 F1 AS 355 F2

text: SA 365 N

text: AS 365 N3

text: EC 225 LP

text: SA 365 C

text: SA 365 C3

text: EUROCOPTER BO 105 A DEUTSCHLAND BO 105 C/CBS-4/-5 GMBH BO 105 D/DB BO 105 DB-4

text: BO 105 DBS Series BO 105 LS A-1/A-3

text: BO 105 S EC 135 P1 Series

text: EC 635 P2+ EC 135 T1 Series

text: EC 635 T1 2B) EC 635 T2 Series

text: Model Commercial Designation

text: MBB-BK 117 A Series Eurocopter MBB-BK 117 A/B MBB-BK 117 B (Honeywell LTS 101) Series Eurocopter MBB-BK 117 C1 MBB-BK 117 C1 (Turbomeca Arriel 1) Eurocopter MBB-BK 117 C2 MBB-BK 117 C2 EC145 (Turbomeca Arriel 1) KAMOV KA-32A/T Kamov Ka 32 (Klimov)

text: AS61N AGUSTA AS61NI Agusta AS61N/Sikorsky S-61N S-61N (GE CT58)

text: S-61NM S-58 BT to JT Sikorsky S-58 (PWC PT6T) S-76A Sikorsky S-76A (RR Corp 250) S-76A S-76A+ Sikorsky S-76A SIKORSKY AIRCRAFT S-76A S-76A++ (Turbomeca Arriel 1) S-76B S-76B Sikorsky S-76B (PWC PT6) Sikorsky S-76C S-76C (Turbomeca Arriel 1) S-76C S-76C+ Sikorsky S-76C S-76C S-76C++ (Turbomeca Arriel 2) S-92A Sikorsky S-92A (GE CT7-8)

text: AGUSTA A119 Agusta A119/ Agusta AW119MkII Koala AW119 MkII (PWC PT6)

text: BELL HELICOPTER 214B Bell 214 (Honeywell T5508) TEXTRON 214B-1

text: BELL HELICOPTER CANADA 407 Bell 407 (RR Corp 250)

text: AGUSTA AB 204 B Series

text: AB 205 A1 Agusta AB204, AB205 / Bell 204, 205 BELL HELICOPTER (Honeywell T53) 204B TEXTRON, INC. 205A-1

text: AB 206A AGUSTA AB 206B Agusta AB206 / Bell 206 BELL HELICOPTER (RR Corp 250) TEXTRON CANADA 206 series from A to L LIMITED THE ENSTROM 480 HELICOPTER Enstrom 480 (RR Corp 250) 480B CORPORATION EUROCOPTER AS 350

text: AS 350 B1 Eurocopter AS 350 AS 350 B2 (Turbomeca Arriel 1) Écureuil AS 350 BA

text: AS 350 BB Eurocopter AS 350 AS 350 B3 (Turbomeca Arriel 2B) Eurocopter AS 350 AS 350 D (Honeywell LTS 101)

text: Eurocopter EC 120 EC 120 B Colibri (Turbomeca Arrius 2F)

text: Eurocopter EC 130 EC 130 B4 (Turbomeca Arriel 2B)

text: Eurocopter SA 315B SA 315 B Lama (Turbomeca Artouste)

text: SA 3180 SA 318 B Alouette-Astazou Eurocopter SA 318 (Turbomeca Astazou) SA 318 C

text: Eurocopter SA 319 SA 319 B Alouette III (Turbomeca Astazou XIV)

text: Eurocopter SA 341 SA 341 G Gazelle (Turbomeca Astazou)

text: Eurocopter SA 342 J SA 342 J Gazelle (Turbomeca Astazou XIV)

text: Eurocopter SA 360 EUROCOPTER SA 360C Dauphin (Turbomeca Astazou XVIIIA) (CONT.) SE 3160 Eurocopter SA 316 B/SA 316 C SA 316 B Alouette III (Turbomeca Artouste) SA 316 C KAMAN AEROSPACE CORPORATION K-1200 Kaman K-1200 (Honeywell T5317)

text: MD HELICOPTERS 369 H series INC. (MDHI) 369 D to FF MD Helicopters 369 Series / SEI NH- S.E.I SERVIZI 500D (RR Corp 250) ELICOTTERISTICI NH-500D ITALIANI MD HELICOPTERS 600N INC. (MDHI) 500N MD Helicopters 500N/600N /AMD500N S.E.I SERVIZI (RR Corp 250) ELICOTTERISTICI AMD-500N ITALIANI PZL-ŚWIDNIK SW-4 PZL SW-4 (RR Corp 250) SCHWEIZER AIRCRAFT 269D Schweizer 269D (RR Corp 250) CORPORATION

text: Model Commercial Designation ANTARES

text: INTERNATIONAL, INC. HELICOPTÈRES

text: GUIMBAL THE ENSTROM F-28 series

text: series CORPORATION SEI (BREDA-NARDI) NH 300C

text: SCHWEIZER AIRCRAFT

text: Model 300C

text: 269B 269C 269C-1 ROBINSON R22 HELICOPTER R22 ALPHA COMPANY

text: R22 MARINER (Lycoming) R44 R44 II

identifier: AMC to Part-66 — Amendment 10

beslut: ED Decision 2011/003/R

title: AMC to Part-66 — Amendment 10

text: Annex to ED Decision 2011/003/R 10/05/2011

text: APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE

text: Amendment 10 (Corrigendum)

text: 10 May 2011

text: The following aircraft type ratings should be used to ensure a common standard throughout the Member States.

text: The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Basic Regulation and its Implementing Rules Regulation 1702/2003, this list is only intended for the maintenance purposes.

text: In order to keep this list current and type ratings consistent, such information should be first passed on to the Agency at part66aml@easa.europa.eu in case a Member State needs to issue a type rating that is not included in this list.

text: Notes:

text: Note 1. For aeroplanes in lists 1 and 2, and helicopters in lists 11, 12 and 13, the table of Appendix I include 3 columns: o column 1: TC holder designation o column 2: aircraft model and, when available, the aircraft commercial designation, o column 3: aircraft designation for endorsement on the Part-66 licence. Only the designations in column 3 should be used for endorsing ratings on Part-66 licences. In the tables of the remaining lists 3 to 10 the TC holder designation is added.

text: Note 2. When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the AML licences may be modified at next renewal or when the licence is re-issued.

text: In the following table, the groups of aircraft are defined as follows:

text: List No. Aircraft: 1 Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating 2 Aeroplanes of 5700 kg and below, requiring type training and individual type rating (A-tr) 3 Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below, eligible for type examinations and manufacturer group ratings 4 Aeroplanes single turbine engine (ASTE) of 5700 kg and below, eligible for type examinations and group ratings 5 Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for type examinations and group ratings 6 Aeroplane single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings 7 Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for

text: type examinations and group ratings 8 Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE- WS), eligible for type examinations and group ratings 9 Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for type examinations and group ratings 10 Aeroplane single piston engine – composite structure (ASPE-CS), eligible for type examinations and group ratings 11 Multi-engine helicopters (MEH), requiring type training and individual type rating 12 Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings 13 Helicopters – Single piston engines (HSPE), eligible for type examinations and group ratings

text: Column 1 includes the TC holder as defined in the TCDS (EASA, FAA or other). For aeroplanes of group 1 and 2 and helicopters, the Column 2 includes the aircraft models as defined in the relevant TCDS (EASA, FAA or other). The following column includes the “commercial designation” when available. Column 3 includes the relevant individual type rating. Only the designations of ratings in column 3 should be used for endorsing individual type ratings on Part-66 licences. Note: aircraft STC data are not included in this table.

text: Changes Corrigendum The subject of the corrigendum of April 2011 in the Annex to the Decision 2010/011/R is to correct the following mistakes: - on page 3, the rating of the Corvette to read SN-601 (PWC JT15D) is corrected; - on page 3, the rating of Airbus A310 (JT9D) which had been erased by mistake is reintroduced; - on page 7 and 8, the ratings of B747 SP are introduced at the right place in the table; - on page 30, the ratings of Aermacchi AL60 were deleted (these ratings were already removed by Decision 2009/016/R); - on page 30, the missing TC holder CESSNA Aircraft Company / Reims Aviation for the Cessna aircraft series is added.

text: Annex to ED Decision 2011/003/R 10/05/2011 List 1

text: 1. Large aircraft (LA). Aeroplanes with a maximum take-off mass of more than 5700 kg, requiring type training and individual type rating

text: AIRBUS N 262 A Frégate Nord 262 (Turbomeca Bastan)

text: AIRBUS SN 601 Corvette Aerospatiale SSN-601 (PWC JT15D) Aerospatiale SN-601 (PWC JT15D) A300 B1 Airbus A300 basic model (GE CF6)

text: A300 B2-320 Airbus A300 basic model (PW JT9D)

text: A300 B4-622 Airbus A300-600 (PW 4000)

text: A300 B4-620 Airbus A300-600 (PW JT9D)

text: A310-304 Airbus A310 (GE CF6)

text: A310-324 Airbus A310 (PW 4000)

text: A310-322 Airbus A310 (PW JT9D)

text: A318-120 series Airbus A318 (PW 6000) A318-110 series Airbus A318/A319/A320/A321 (CFM56)

text: A319-130 series Airbus A319/A320/A321 (IAE V2500)

text: A330-200 series Airbus A330 (GE CF6)

text: A330-220 series Airbus A330 (PW 4000)

text: A330-240 series Airbus A330 (RR RB 211 Trent

text: A340-210 series Airbus A340 (CFM56)

text: A340-540 series Airbus A340 (RR RB 211 Trent

text: A380-840 series Airbus A380 (RR RB 211 Trent 900) A380-860 series Airbus A380 (EA GP7200) A300F4-608ST Beluga Airbus A300-600ST (GE CF6) AIRBUS One-Eleven 200 series Airbus UK (BAC) 1-11 (RRD Spey)

text: L-420 Let L-420 (Walter M601)

text: ALENIA C-27J Alenia C-27 (Allison/RR AE2100)

text: ANTONOV AN-26 Antonov AN26 (Ivchenko AI-24)

text: ATR-GIE ATR 42-200 ATR 42-200/300 series (PWC

text: ATR 72-101 ATR 72-100/200 series (PWC PW120)

text: ATR 42-400 ATR 42-400/500/72-212A (PWC PW120)

text: BAE BAe 146 Series 100 BAe 146/ AVRO 146-RJ (Honeywell SYSTEMS ALF500 Series)

text: HS.748 Series 1 HS748 (RRD Dart)

text: Jetstream 200 Jetstream 200 (Turbomeca Astazou)

text: Jetstream 4100 Jetstream 41 (Honeywell TPE331)

text: BAe ATP ATP (PWC PW120)

text: B707-200 Boeing 707 (PW JT4)

text: B707-400 Series Boeing 707 (RR Conway)

text: B727 Series Boeing 727 (PW JT8D)

text: B737-100 Boeing 737-100/200 (PW JT8D)

text: B737-300 Boeing 737-300/400/500 (CFM56)

text: B737-600 Boeing 737-600/700/800/900 (CFM56)

text: B747-100B Boeing 747-100 (RR RB211 )

text: B747-100 Boeing 747-100 (PW JT9D)

text: B747-200B Boeing 747-200/300 (GE CF6)

text: B747-200B Boeing 747-200/300 (PW JT9D)

text: B747SP Boeing 747SP (PW Jt9D)

text: B747-300 Boeing 747-200/300 (PW JT9D)

text: B747SP Boeing 747SP (PW JT9D)

text: B747-200B Boeing 747-200/300 (RR RB211)

text: B747SP Boeing 747SP (RR RB211)

text: B747-300 Boeing 747-200/300 (RR RB211)

text: B747SP Boeing 747SP (RR RB211)

text: B747-400 Boeing 747-400 (GE CF6)

text: B747-400 Boeing 747-400 (PW 4000)

text: B747-400 Boeing 747-400 (RR RB211)

text: B757-200 Boeing 757-200/300 (PW 2000)

text: B757-200 Boeing 757-200/300 (RR RB211)

text: B767-200 Boeing 767-200/300 (PW 4000)

text: B767-200 Boeing 767-200/300 (PW JT9D)

text: B767-300 Boeing 767-300 (RR RB211)

text: B767-200 Boeing 767-200/300/400 (GE CF6)

text: B777-200 Boeing 777-200/300 (GE 90)

text: B777-200 Boeing 777-200/300 (PW 4000)

text: B777-200 Boeing 777-200/300 (RR RB211 Trent 800)

text: B787-8 Boeing 787-8 (RR RB 211 Trent

text: B787-8 Boeing 787-8 (GEnx)

text: BOMBARDIER CL-215-1A10 Canadair CL-215 (PW R2800) CL-215-6B11 (CL-215T Canadair CL-215 (PWC PW120)

text: CL-215-6B11 (CL-415 Canadair CL-415 (PWC PW123)

text: (Honeywell AS907) BD-700-1A10 Global Express Bombardier BD-700 Series (RRD BR710)

text: (Honeywell ALF502)

text: Variant) (variant CL 601/601-3A/3R) (GE CF34)

text: 100 CF34)

text: 700/701/702 2D24/-2E25 (GE CF34)

text: DHC-8-101 DHC-8 Series 100 Bombardier DHC-8-100/200/300 (PWC PW 120)

text: SHORT SD3-30 Variant 200 Shorts SD3 Series-30/SD3-60 BROTHERS (PWC PT6)

text: EADS CASA C-212-CB Aviocar CASA C-212 (Honeywell TPE331)

text: C-212-DE Aviocar CASA C-212 (PWC PT6)

text: CN-235 CASA CN-235 (GE CT7) EADS CASA CN-235-100 CASA CN-235 (GE CT7)

text: C-295 CASA C-295 (PWC PW127)

text: CESSNA 525B Citation Jet CJ3 Cessna 525B/C (Williams FJ 44)

text: 550 Citation Bravo Cessna 550/560 (PWC PW530/535)

text: 550 Citation II Cessna 550/560 (PWC JT15D)

text: 560XL Citation Excel Cessna 560XL/XLS (PWC PW545)

text: 650 Citation III - VI IV Cessna 650 (Honeywell TFE731)

text: 680 Sovereign Cessna 680 (PWC PW306)

text: 750 Citation X Cessna 750 (RR Corp AE3007C)

text: DASSAULT Falcon 10 Falcon 10 (Honeywell TFE731)

text: Mystère Falcon 20-C5 Falcon 20-5 (Honeywell TFE731)

text: Fan Jet Falcon Series G Falcon 200 (Honeywell ATF 3-6)

text: Mystère Falcon 50 Falcon 50 (Honeywell TFE731)

text: Mystère Falcon 50 F50EX Falcon 50EX (Honeywell TFE731)

text: Mystère Falcon 900 Falcon 900 (Honeywell TFE731)

text: Mystère Falcon 900 F900C Falcon 900C (Honeywell TFE731)

text: Falcon 900EX Falcon 900EX (Honeywell TFE731)

text: Falcon 900EX F900EX EASy Falcon 900EX EASy (Honeywell TFE731)

text: Falcon 2000 Falcon 2000 (CFE 738)

text: Falcon 2000EX Falcon 2000EX (PWC PW308)

text: Falcon 2000EX F2000EX EASy Falcon 2000EX EASy (PWC PW308)

text: Falcon 7X Falcon 7X (PWC PW307A)

text: RUAG 228-100 series Dornier 228 (Honeywell TPE331)

text: 328-100 series Dornier 328-100 (PWC PW119)

text: 328-300 series Dornier 328-300 (PWC PW306)

text: EMBRAER EMB-120 Brasilia Embraer EMB-120 (PWC PW110 Series)

text: EMB-135ER Embraer EMB-135/145 (RR Corp AE3007A)

text: ERJ-170-100 STD ERJ-170 Embraer ERJ-170/190 (GE CF34)

text: EMB-505 Phenom 300 Embraer EMB-505 (PWC PW535) (FOKKER- F-27A to -M Fokker F27 / Fairchild F-27/FH-227 FAIRCHILD) (RRD Dart)

text: F27 Mark 050 Fokker 50 Fokker 50/60 Series (PWC PW 125/127)

text: F28 Mark 1000 Fellowship Fokker F28 Series (RRD Spey)

text: GULFSTREAM 1125 Westwind Astra Gulfstream (IAI) 100/1125/Astra AEROSPACE SPX (Honeywell TFE731)

text: Gulfstream G150 Gulfstream G150 Gulfstream (IAI) G150 (Honeywell TFE731)

text: G-1159 Gulfstream II Gulfstream G-1159 Series (RRD Spey)

text: G-IV/GIV-SP Gulfstream G- Gulfstream G-IV Series (RRD Tay)

text: GIV-X (G450) Gulfstream G450 Gulfstream GIV-X Series (RRD Tay)

text: GV Gulfstream GV Gulfstream GV basic model (RRD BR710)

text: GV-SP (G550) Gulfstream G550 Gulfstream GV-SP Series (RRD BR710)

text: BEECHCRAFT (Honeywell TFE731)

text: 750/800XP/850XP/900XP (Honeywell TFE731)

text: BAe.125 series 1000A/B BAe 125 Series 1000 (PWC PW305)

text: 300 Super King Air Beech 300 Series (PWC PT6)

text: 400 Beechjet Beech 400 / Mitsubishi MU-300 (PWC JT15)

text: 1900 Airliner Beech 1900 (PWC PT6)

text: 4000 Hawker 4000 Hawker 4000 (PWC PW308)

text: IAI 1124 Westwind IAI 1124 (Honeywell TFE731)

text: KELOWNA 440 Convair 580 (RR Corp 501)

text: LEARJET 24 /24A Learjet 24/25 (GE CJ610)

text: 28 Learjet 28/29 (GE CJ610)

text: 31 / 31A Learjet 31 (Honeywell TFE731)

text: 35 / 35A Learjet 35/36 (Honeywell TFE731)

text: Learjet 45 LJ45 Learjet Model 45 (Honeywell TFE731)

text: 55 / 55B / 55C Learjet 55 (Honeywell TFE731) Learjet 60 LJ60 Learjet 60 (PWC PW305)

text: MARTIN TFE731)

text: 1329-23A Lockheed 1329 PW (PW JT12)

text: Model 188C Electra Lockheed 188 (RR Corp 501)

text: 382 Hercules Lockheed 382 (RR Corp 501)

text: 382J Hercules II Lockheed 382 (RR AE2100)

text: L-1011-385-1 TriStar Lockheed L-1011 (RR RB211)

text: DC-8 Series 50 DC-8 (PW JT3D)

text: DC-8 Series 40 DC-8 (RR Conway)

text: DC-9-10 Series DC-9 (PW JT8D)

text: DC-9-81 (MD-81) Series MD-80 Series (PW JT8D)

text: MD-90 Series MD-90 (IAE V2500)

text: 717-200 MD 717-200 (RRD BR700-715)

text: DC-10-10 DC-10/MD-10 (GE CF6)

text: DC-10-40 DC-10 (PW JT9D)

text: MD-11 MD-11 (GE CF6)

text: MD-11 MD-11 (PW 4000)

text: M7 SA227-AT Fairchild SA227 Series (Honeywell

text: SA227-PC Swearingen Metro Fairchild SA227 Series (PWC PT6)

text: POLSKIE PZL M28 00 PZL M 28 (PWC PT6)

text: SABRELINER NA-265-65 Sabreliner NA-265 (Honeywell

text: NA-265-80 Sabreliner NA-265 (GE CF700)

text: NA-265 Sabreliner NA-265 (PW JT12)

text: 2000 Saab 2000 (RR Corp AE2100)

text: TUPOLEV PSC TU 204-120CE Tupolev TU 204 (RR RB211)

text: VIKING AIR DHC-7-1 De Havilland DHC-7 (PWC PT6)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 2

text: 2. Aeroplanes of 5700 kg and below, requiring type training and individual type rating (A-tr)

text: 1 TC Holder 2 Aeroplanes 3 Type rating endorsement Model Commercial Designation

text: Ae 270 Aero Ae-270 (PWC PT6)

text: L-410 UVP-LW Let L-410 LW (Walter M601)

text: 441 Cessna 441 (Honeywell TPE331)

text: Cessna 500 (PWC JT15D) Cessna 500/501/551 (PWC JT15D)

text: Cessna 500/501/551 (PWC JT15D)

text: Cessna 500/501/551 (PWC JT15D)

text: 510 Cessna 510 (PWC PW615)

text: Cessna 525/525A (Williams FJ 44)

text: Seastar CD2 Dornier Seastar CD2 (PWC PT6)

text: EA500 Eclipse EA500 (PWC PW610)

text: Empresa Brasileira Embraer EMB-110 (PWC PT6)

text: EMB-121A1 Xingu II Embraer EMB-121 (PWC PT6)

text: EMB-500 Phenom 100 Embraer EMB-500 (PWC PW617)

text: C90 King Air Beech 90 Series (PWC PT6)

text: Beech 200 Series (PWC PT6)

text: B99 Airliner Beech 99/100 Series (PWC PT6)

text: B100 Beech B100 (Honeywell TPE331)

text: (Williams FJ44)

text: LJ 23 Learjet 23 (GE CJ610)

text: Fairchild SA226 (Honeywell TPE331)

text: Mitsubishi MU-2B (Honeywell

text: Piaggio P166 (PWC PT6)

text: P180 Avanti Piaggio P180 Avanti/Avanti II (PWC

text: Pilatus PC-12 (PWC PT6)

text: PA-42-720 Piper PA-42 (PWC PT6)

text: PA-46-500TP Malibu Meridian Piper PA-46-500TP (PWC PT6)

text: F 406 Caravan II Reims-Cessna F 406 (PWC PT6)

text: TBM 700 C1 Socata TBM 700/850 (PWC PT6)

text: 690A Twin Commander 680/681/690/695 690B Series (Honeywell TPE331)

text: De Havilland DHC-6 (PWC PT6)

text: VULCANAIR AP68TP300 Spartacus Vulcanair AP68TP Series (RR Corp

text: Vulcanair SF600 (RR Corp 250)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 3

text: 3. Aeroplanes multiple turbine engines (AMTE) of 5700 kg and below, eligible for type examinations and manufacturer group ratings

text: TC holder Type rating endorsement

text: M7 AEROSPACE Fairchild SA26-T (PWC PT6) (Fairchild-Swearingen Corp) Fairchild SA26 AT(Honeywell TPE331)

text: PIPER AIRCRAFT Corporation Piper PA-31T Series (PWC PT6)

text: SHORT BROTHERS Shorts SC7 (Honeywell TPE331)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 4

text: 4. Aeroplanes single turbine engine (ASTE) of 5700 kg and below, eligible for type examinations and group ratings

text: TC holder Type rating endorsement AIR TRACTOR Air Tractor AT-302 (Lycoming LTP-101) Air Tractor AT-400/500/600/800 Series (PWC PT6) ZLIN AIRCRAFT INDUSTRIES Zlin Z-37 T Series (Walter M601) ALENIA AERMACCHI Aermacchi SF260TP (RR Corp 250) ALLIED AG CAT Grumman G-164 (PWC PT6) Productions CESSNA AIRCRAFT Company Cessna (Soloy) 206/207 (RR Corp 250) Cessna 208 Series (PWC PT6) Cessna 210 (RR Corp 250) EADS PZL “WARSZAWA-OKECIE” EADS PZL PZL-106 BT (Walter M601) EADS PZL PZL-106 BTU (PWC PT6) EXTRA Flugzeugproduktions- und Vertiebs GmbH Extra EA-400-500 (RR Corp 250) GROB Luft- und Raumfahrt Grob G 520 Series (Honeywell TPE331) MAULE AEROSPACE TECHNOLOGY Maule MX-7 (RR Corp 250) PACIFIC AEROSPACE Corporation PAC 750XL (PWC PT6) PILATUS AIRCRAFT Pilatus PC-6 Series (PWC PT6) Pilatus PC-6 Series (Turbomeca Astazou) Pilatus PC-6 Series (Honeywell TPE 331) THRUSH AIRCRAFT Ayres S2R Series (PWC PT6) VIKING AIR DeHavilland DHC-2 (PWC PT6) (Bombardier) (De Havilland)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 5

text: 5. Aeroplane multiple piston engines – metal structure (AMPE-MS), eligible for type examinations and group ratings

text: TC holder Type rating endorsement AEROSTAR AIRCRAFT Corporation Piper PA-60/61 Series (Lycoming)

text: TC holder Type rating endorsement RUAG Aerospace Services GmbH Do 28/128 Series (Lycoming) SOCATA Grumman GA-7 (Lycoming) STOL AIRCRAFT Corporation Republic UC-1 (Lycoming) TECNAM Tecnam P2006T (Rotax) Costruzioni Aeronautiche TWIN COMMANDER AIRCRAFT Commander 685 (Continental) Corporation Commander 500 Series/680 Series (Lycoming) Rockwell 700 (Lycoming) VULCANAIR Vulcanair P.68 Series (Lycoming) Vulcanair F600A (Lycoming)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 6

text: 6. Aeroplane single piston engine – metal structure (ASPE-MS), eligible for type examinations and group ratings

text: TC holder Type rating endorsement AERO Sp.z.o.o Aero AT-3 (Rotax) AIRCRAFT INDUSTRIES Let Z-37 Series (LOM) AIR TRACTOR Air Tractor AT-250/300 (PW R985) Air Tractor AT-301/401/501 (PW R1340) Air Tractor AT-401 (PZL-3S) Air Transport Group Holdings, Inc Lake C/LA Series (Lycoming) ALENIA AERMACCHI Aermacchi AL60 (Continental) Aermacchi AL60 (Lycoming) SIAI-Marchetti S.205/S.208 (Lycoming) SIAI-Marchetti S.205 (Franklin) Aermacchi SF260 Series (Lycoming) ALLIED AG CAT Grumman G-164 (Continental) Productions Grumman G-164 (Jacobs) Grumman G-164 (PW R Series) APEX Aircraft Robin HR 100 series (Lycoming) (ALPHA) CEAPR Robin HR 100 series (Continental) Robin R 1180 series (Lycoming) Robin R 3000 series (Lycoming) ALPHA AVIATION (APEX Aircraft) Robin HR 200/ R 2000 series (Lycoming) ARV Aviation ARV 1 Super 2 (Hewland)

text: BÖLKOW Bölkow BO 208 (Continental) Bölkow BO 209 (Lycoming) COMMANDER PREMIER AIRCRAFT Commander 112 (Lycoming) CO. Commander 114 (Lycoming) DE HAVILLAND Beagle B.121 series 1 (Continental) Support Beagle B.121 series 2/3 (Lycoming) DYNAC AEROSPACE Corporation Aerocommander 100 (Lycoming) CESSNA Aircraft Company / Reims Cessna 150 Series (Rotax) Aviation Cessna/Reims-Cessna 150/F150 Series (Continental) Cessna/Reims-Cessna 152/F152 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (Lycoming) Cessna/Reims-Cessna 172/F172 Series (Continental) Cessna 172 Series (Thielert) Cessna 175 Series (Lycoming) Cessna 175 Series (Continental) Cessna 177 Series (Lycoming) Cessna 180 Series (Continental) Cessna/Reims-Cessna 182/F182 Series (Lycoming) Cessna/Reims-Cessna 182/F182 Series (Continental) Cessna/Reims-Cessna 182/F182 Series (SMA) Cessna 185 Series (Continental)

text: TC holder Type rating endorsement Cessna 188 (Continental) Cessna 206 Series (Continental) Cessna 206 Series (Lycoming) Cessna 207 Series (Continental) Cessna 210 Series (Continental) EVEKTOR Evektor EV-97 (Rotax) FFA ALTENRHEIN AS202 Series (Lycoming) OA7 Optica Series (Lycoming) FLS AEROSPACE Club Sprint/Sprint 160 (Lycoming) FUJI Heavy Industries Fuji FA-200 Series (Lycoming) GARDAN Gardan GY 80 (Lycoming) GENERAL AVIA Costruzioni Aeronautiche General Avia F.22 (Lycoming) GIPPSLAND Aeronautics Gippsland GA8 (Lycoming) HAWKER BEECHCRAFT Corporation Beech 23 Series (Lycoming) Beech A23 (Continental) Beech 24 Series (Lycoming) Beech 33 Series (Continental) Beech 35 Series (Continental) Beech 36 Series (Continental) Beech 77 (Lycoming) S.C.Constructii Aeronautice S.A IAROM IAR-46 (Rotax) IAROM INTERCEPTOR AIRCRAFT Aerocommander 200 (Continental) Corporation LAKE AIRCRAFT Lake 250 (Lycoming) LAVIA ARGENTINA S.A. (LAVIASA) Piper PA-25 Series (Lycoming) MAULE AEROSPACE TECHNOLOGY Maule M4 (Continental) Maule M4 (Franklin) Maule M5 (Lycoming) Maule M5 (Franklin) Maule M5 (Continental) Maule M6 (Lycoming) Maule M7 Series (Lycoming) Maule MX-7 (Lycoming) METEOR Meteor FL53 (Continental) Meteor FL54 (Continental) Meteor FL55 (Lycoming) MOONEY AIRPLANE Company Mooney M20B to M20S/M22 (Lycoming) Mooney M20 (Continental) PILATUS AIRCRAFT Pilatus PC-6 Series (Lycoming) PIPER AIRCRAFT Piper PA-22 Series (Lycoming) Piper PA-24 Series (Lycoming) Piper PA-28 Series (Lycoming) Piper PA-28 Series (Continental) PIPER AIRCRAFT Piper PA-28 Series (Thielert)

text: TC holder Type rating endorsement (cont. Piper PA-32 Series (Lycoming) Piper PA-36 Series (Lycoming) Piper PA-36 Series (Continental) Piper PA-38 Series (Lycoming) Piper PA-46 Series (Continental) Piper PA-46 Series (Lycoming) SKY Int ENTREPRISE Aviat Husky A (Lycoming) EADS PZL "WARSZAWA-OKECIE" PZL-101A Gawron (Ivchenko) PZL-104A Wilga (Ivchenko) PZL-104 Wilga Series (PZL) PZL M 18 (PZL) PZL M 26 (Lycoming) PZL-104 Wilga (Lycoming) REGAL AIR, Inc. REGAL AIR 305 Seris (Continental) REVO, Inc. REVO C/LA-4 Series (Lycoming) SOCATA SOCATA MS 880/885/890 (Continental) SOCATA MS 881 (Potez) SOCATA MS 883/886/887 (Lycoming) SOCATA MS 892/893 / PZL Koliber (Lycoming) SOCATA MS 894 / PZL Koliber (Franklin) SOCATA Rallye 100 (Continental) SOCATA Rallye Series (Continental) SOCATA Rallye 110ST (Lycoming) SOCATA Rallye Series (Lycoming) SOCATA Rallye 150 (Lycoming) SOCATA Rallye 180T (Lycoming) SOCATA Rallye 235 (Lycoming) SOCATA ST10 (Lycoming) SOCATA TB Series (Lycoming) SOCATA TB 9 (Lycoming) SOCATA TB 10 (Lycoming) SOCATA TB 20 (Lycoming) SOCATA TB 21 (Lycoming) SOCATA TB 200 (Lycoming) SYMPHONY AIRCRAFT Industries Symphony OMF-100-160 (Lycoming)

text: Partenavia P.66 (Lycoming)

text: TC holder Type rating endorsement WASSMER CERVA CE43 (Lycoming) CERVA CE44 (Continental) YAKOVLEV Yakovlev YAK-18T (Vedeneyev) Yakovlev YAK-54/55/55M (Vedeneyev) ZLIN AIRCRAFT Zlin Z-42 Series (LOM) (MORAVAN AVIATION) Zlin Z-43 (LOM) Zlin Z-50 (LOM) Zlin Z-50L Series (Lycoming) Zlin Z-26 Series (LOM) Zlin Z-26 Series (Walter Minor/M Avia) Zlin Z-143 L (Lycoming) Zlin Z-242 L (Lycoming) Zlin Z-526 L (Lycoming)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 7

text: 7. Aeroplane multiple piston engines – wooden structure (AMPE-WS), eligible for type examinations and group ratings

text: No aircraft in this list.

text: Annex to ED Decision 2011/003/R 10/05/2011 List 8

text: 8. Aeroplane single piston engine – wooden structure/metal tube-fabric (ASPE- WS), eligible for type examinations and group ratings

text: TC holder Type rating endorsement ALEXANDRIA Aircraft Bellanca 14-19 Series (Continental) Bellanca 17-30/17-31 Series (Continental) APEX CEAPR Robin ATL / ATL S (JPX 4T60) Robin ATL L (Limbach L2000) APEX Dyn’Aero CAP 10 (Lycoming) Robin DR 220 series (Continental) Robin DR 250 series (Lycoming) Robin DR 300 series (Lycoming) APEX CEAPR Robin DR 400 series (Lycoming) Robin DR 400RP (Porsche) Robin DR 400RP (Thielert) AMERICAN CHAMPION Champion 7 Series (Continental) BELLANCA Aircraft Corporation Champion 7 Series (Lycoming) Champion 8 Series (Lycoming) BÖLKOW Klemm K1.107/F.207 (Continental) Bölkow F.207 (Lycoming) MOONEY AIRPLANE Company Mooney M20/M20A (Lycoming) Mooney M18L (Continental) NIPPER Nipper T-66 (Stark) EIS RF 6B (Continental) RENE FOURNIER RF 6B (Lycoming) SCHEIBE Flugzeugbau SF 23 Series (Continental) SKY INTERNATIONAL Pitts S-1 Series (Lycoming) Pitts S-2 Series (Lycoming) Skyfox Aviation Ltd CA25 Series (Rotax) SLINGSBY Aviation Slingsby T67 Series (Lycoming) EIS GmbH RS 180 (Lycoming) SPORTAVIA PUETZER TAYLORCRAFT 2000 Taylorcraft 19 Series (Continental) Taylorcraft F21/F22/F22A Series (Lycoming) VULCANAIR Partenavia P57 (Lycoming) WACO Aircraft Company Waco YMF (Jacobs) WASSMER WA40 Series (Lycoming) WA41 (Lycoming) WA4/21 Series (Lycoming)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 9

text: 9. Aeroplane multiple piston engines – composite structure (AMPE-CS), eligible for type examinations and group ratings

text: TC holder Type rating endorsement

text: Annex to ED Decision 2011/003/R 10/05/2011 List 10

text: 10. Aeroplane single piston engine – composite structure (ASPE-CS), eligible for type examinations and group ratings

text: TC holder Type rating endorsement APEX CAP 20/21 (Lycoming) Dyn’Aero CAP 230 Series (Lycoming) AQUILA Technische Entwicklungen Aquila AT01 (Rotax) Aviation by Excellence AG CESSNA AIRCRAFT Company Cessna C300/C350/C400 (Continental) (COLUMBIA) CIRRUS Design Corporation Cirrus SR20 (Continental) Cirrus SR22 Series (Continental) DIAMOND AIRCRAFT Industries Diamond DA20/DV20 (Rotax) Diamond DA20 (Continental) Diamond DA40 (Lycoming) Diamond DA40 D (Thielert) Diamond DA40 (Austro Engine) AIRCRAFT Design and Certification (WD) D4 Fascination (Rotax) EXTRA Flugzeugproduktions- und Extra EA-300 Series (Lycoming) Vertriebs-GmbH Extra EA-400 (Continental) FFT GYROFLUG SC01 Series (Lycoming) GROB Luft- und Raumfahrt Grob G115/120 Series (Lycoming) INSTYTUT LOTNICTWA Instytut Lotnictwa I-23 Manager (Lycoming) INIZIATIVE INDUSTRIALI ITALIANE III Sky Arrow 650/710 (Rotax) ISSOIRE AVIATION Issoire APM 20/30 (Rotax) LIBERTY AEROSPACE Liberty XL-2 (Continental) Incorporated GOMOLZIG Ruschmeyer R90-230RG (Lycoming) RUSCHMEYER SEASTAR CORP TSC Series (Lycoming) SUKHOI Sukhoi SU-29 (Vedeneyev) Sukhoi SU-31 (Vedeneyev) Sukhoi SU-26 (Vedeneyev) Sukhoi Su-29/31 (MGA) SLINGSBY AVIATION Slingsby T67A/T67B/T67C/T67M Series (Lycoming)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 11

text: 11. Multi-engine helicopters (MEH), requiring type training and individual type rating

text: 1 TC Holder 2 Helicopter 3 Type rating endorsement

text: Agusta A109 Series (PWC

text: Agusta A109 Series (RR Corp 250)

text: A109K2 Agusta A109 (Turbomeca Arriel 1) A109E Agusta A109 Series A109LUH (Turbomeca Arrius 2)

text: Agusta AB139 / AW139 (PWC PT6)

text: Agusta/Westland EH-101

text: (GE CT7)

text: Bell 212 / Agusta AB212 (PWC PT6)

text: 214ST Bell 214ST(GE CT7)

text: 412CF Bell 412 / Agusta AB412 (PWC PT6)

text: Bell 427 (PWC PW207D)

text: 222B Bell 222 (Honeywell LTS 101)

text: 230 230 Utility Bell 230 (RR Corp 250)

text: 427 Bell 427 (PWC PW207D)

text: 429 Bell 429 (PWC PW207D)

text: 430 Bell 430 (RR Corp 250)

text: 234 Boeing 234 (Honeywell 5512)

text: ERICKSON AIR- Erickson S-64

text: (PW JFTD 12)

text: (Turbomeca Turmo)

text: AS 332 L Eurocopter AS 332 (Turbomeca AS 332 C1 Makila 1A/1A1)

text: Eurocopter AS 332 L2

text: (Turbomeca Makila 1A2)

text: Eurocopter AS 355 (RR Corp 250)

text: AS 355 N Eurocopter AS 355 AS 355 NP (Turbomeca Arrius 1) Eurocopter SA 365 N

text: (Turbomeca Arriel 1) SA 365 N1 Eurocopter SA 365 N1, AS 365 N2

text: AS 365 N2 (Turbomeca Arriel 1) Eurocopter AS 365 N3

text: (Turbomeca Arriel 2C) EC 155 B Eurocopter EC 155 EC 155 B1 (Turbomeca Arriel 2)

text: Eurocopter EC 225

text: (Turbomeca Makila 2A)

text: SA 365 C1 Eurocopter SA 365 C Series

text: SA 365 C2 (Turbomeca Arriel 1)

text: SA 366 G1 Dauphin Eurocopter SA 366 G1 Series (Lycoming LTS101)

text: BO 105 series (RR Corp 250)

text: EC 135 P2 Series Eurocopter EC 135 (PWC PW206)

text: EC 135 T2 Series Eurocopter EC 135 (Turbomeca Arrius

text: MD HELICOPTERS, MD Helicopters MD900 (PWC MD900 INC. PW206/207) PZL-ŚWIDNIK W-3A PZL-Swidnik W-3A/W-3AS W-3AS (Rzeszow PZL-10W)

text: Annex to ED Decision 2011/003/R 10/05/2011 List 12

text: 12. Helicopters – Single turbine engine (HSTE), eligible for type examinations and group ratings

text: 1 TC Holder 2 Helicopter 3 Type rating endorsement Model Commercial Designation

text: Annex to ED Decision 2011/003/R 10/05/2011 List 13

text: 13. Helicopters – Single piston engines (HSPE), eligible for type examinations and group ratings

text: SH-4 Silvercraft SH-4 (Franklin)

text: AGUSTA AB 102 Agusta AB 102 (PW S1H4)

text: B-2 Brantly B2 (Lycoming)

text: G2 Cabri Cabri G2 (Lycoming)

text: HELICOPTER Enstrom

text: (Lycoming)

text: CORPORATION 269A Schweizer / Breda Nardi (Hughes)

text: 269/300 (Lycoming)

text: R22 BETA Robinson R22/R44 Series

text: SIKORSKY AIRCRAFT S-58 A to J Sikorsky S-58 (Wright Cyclone)