Module 10 Aviation Legislation Presentation Day 14 And 15.pdf 423924

Aviation Legislation EASA Module 10

© 20 5 Panasonic Avionics Corporation. Proprietary and Confidential

Table of Content • • • •

Day One : 10.1 Regulatory Framework 10.2 Part-66 Certifying Staff - Maintenance 10.3 Part - 145 Approved Maintenance Organisations

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Day Two : 10.4 JAR-OPS Commercial Air Transportation (Aeroplanes) 10.5 Aircraft Certification Part 21 10.6 Part - M Continuing Airworthiness. 10.7 Applicable National and International Requirements.


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10.1. Regulatory Framework


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Regulatory Bodies International Organisations: • ICAO International Civil Aviation Organisation (Worldwide organisation of authorities). • ECAC European Civil Aviation Conference (European organisation of authorities). • JAA t Aviation Authorities.(European organisation of JAA member authorities) • EASA European Aviation Safety Agency National Authorities (Examples) • LBA Luftfahrt Bundesamt (German authority) • DGAC Direction GEmerale de I"Aviation Civile (French authority) • CAA Civil Aviation Authority (English authority) • FAA Federal Aviation istration (American authority) International Operator Organisations : • lATA Intemational Air Transport Association (Worldwide organisation of operators/airlines) • AEA Association of European Airlines(European organisation of operators/airlines)


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'Role of ICAO ( International Civil Aviation Organization )

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The ICAO is a worldwide union of aviation authorities and a sub organization of the United Nations (UN). Its headquarter is in Montreal, Canada. ICAO was established on 7th December 1944 in Chicago . United States invited 54 nations who met together to form ICAO . lCAO establishes international standards and recommends operating practices and procedures. It covers the technical field of aviation, ICAO develops a code of international air law for 190 countries (at present ).


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'Role of ICAO ( International Civil Aviation Organization ) The Organization is made up of the following : • The ASSEMBLY: it is composed by· the Member States and meets every 3 years to review documents, define policies for future years and approve budgets; • •

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The COUNCIL: it is elected by the Assembly and remains in office for 3 years. It is composed by representatives of 36 countries. The Council is the main governing body; it manages the Agency s work and updates the Annexes with standards and Agency's recommendations, leveraging the expertise of technical directorates;

The SECRETARIAT: it is composed by the permanent framework of professionals; and it is divided into five main divisions: the Air Navigation Bureau, the Air Transport Bureau, the Technical Co-operation Bureau, the Legal Bureau, and the Bureau of istration and Services; The chief officers are the President of the Council and the Secretary General


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'Role of ICAO ( International Civil Aviation Organization ) International CiviI Aviation 0rganization (ICA0 ) annexes: • Annex 1 Personnel Licensing • Annex 2 Rules of the Air • Annex 3 Meteorological Service For lnternationaI Air Navigation • Annex 4 Aeronautical Charts • Annex 5 Units Of !Measurement To Be Used In Air And Ground Operations • Annex 6 0peration Of Aircraft • Annex 7 Aircraft, Nationality and Registration Marks • Annex 8 Airworthiness, of Aircraft • Annex 9 Facilitation • Annex 10 Aeronautical Telecommunications • Annex 11 Air Traffic Control} Flight Information, Alerting Services • Annex 12 Search And Rescue • Annex 13 Aircraft Accident and Incident Investigation • • Annex 14 Aerodromes • • Annex 115 Aeronaucal Information Services • • Annex, 6 Environmental Protection • • Annex 17 Security • • Annex 1 8 The Safe Transport Of Dangerous Goods By Air © 20 5 Panasonic Avionics Corporation. Proprietary and Confidential

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'Role of ICAO ( International Civil Aviation Organization ) •

ICA0 publishes standards and guidance documents which are explanatory of annexes.

lCA0 standards are developed in the following forms: • Standards and Recommended Practices • Procedures for Air Navigation Services • Regional Supplementary Procedures • Guidance Material .


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t Aviation Authorities (JAA)

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t Aviation Authorities (JAA), started in 1970 it is based in Hoofddorp the Netherlands, The t Aviation Authorities (JAA) was. an association body of the European Civil Aviation Conference (ECAC) representing the civil aviation authorities of Member State which signed the "JAA Arrangements , document established in the conference of Cyprus. in Sept 1990. The JAA Member States agreed to cooperate in developing and implementing common safety regulatory standards and procedures .


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t Aviation Authorities (JAA) •

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The did their best to harmonise their practices with the t Aviation Authorities (JAA), this system led to differing interpretations, which adversely affected the efficiency of regulation and increased compliance. A transition to the EASA system and decision-making based on the European Community method will mark a significant improvement in the execution of certification and rulemaking.


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Transfer from JAA to EASA • • •

With the creation of EASA in 2002, the EU transferred the airworthiness regulations away from the JAA. Over time, EASA became responsible for operations and licensing as well. In 2009 the JAA system was disbanded. Only the training organisation (JAA-TO) remains, it mainly provides courses for CAA staff of European countries.


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Role of European commission • • • • • •

The European Parliament: it is the elected body that represents the Europe citizens . It exercises political supervision and takes part in the legislative process. The Council of the European Union (also known as the Council of Ministers): it is the EU's main decision-making body. The EU member states take it in turns to hold the Presidency of the Council for a period of six months. Every Council meeting is attended by one minister from each EU country. The Council has legislative power, ·which it shares with the European Parliament . The European Commission: it is the EUs executive arm. This means that it is the only institution that can propose new laws, on which the European Parliament and Council of the EU then vote.


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Role of EASA (European Aviation Safety Agency ) •

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The Agency was temporarily based in Brussels, but moved to Cologne ( in ), on 2nd November 2004. The European Aviation Safety Agency (EASA) is the European Union's Agency which has the main role of promoting the highest common standards of safety and environmental protection in civil aviation. The agency was established by the European Parliament Basic Regulation n. 1592/2002 issued on 15/07/2002 (replaced by n EC.216/2008 issued on 20/02{2008). This Regulation was done because of the need to provide common rules to the European civil aviation field on: 1 . Safety levels 2. Quality standards 3. Environmental compatibility 4. Goods and services movement 5. Cooperation with third Countries. The EASA has a web site. (www.easa.eu-int)


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EASA 32 Member States • • • • • • • • • • • • • • • • •

Austria Belgium Bulgaria Croatia Cyprus Czech Republic Denmark Estonia Finland Greece Hungary Iceland Ireland Italy Lativa


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Liechtenstein Lithuania Luxembourg Malta Netherland Norway Poland Portugal Romania Slovakia Slovenia Spain Sweden Swtizerland United Kingdom

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Role of EASA (European Aviation Safety Agency ) • Provide advice to the Commission on the following matters: a. The design, production, maintenance and operation of aeronautical products, parts and appliances, as ·well as personnel and organizations involved in the design, production and maintenance of such products, parts and appliances

b. Personnel and organizations involved in the operation of aircraft. • Issue certification , including airworthiness documents such as an Acceptable Means of Compliance (AMC) , as welI as any Guidance Material (GM) for the application of rules • Issue of the Type-Certificates or associated changes. • Issue certificates for parts and appliances. • Issue the appropriate Environmental Certificates.


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Role of EASA (European Aviation Safety Agency ) • • • • • •

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Approval of Design Organizations Approval of Production 0rganisations located within the territory of the Member States. Approval of Production and Maintenance organizations located outside the territory of the Member State. Monitoring the application of rules by '°‘National Aviation Authorities (NAA) Approval of Airworthiness Directives Define and negotiate bilateral agreements between states (BASA);, previously treated independently by each Member State. The EASA Regulation in not applicable to products/parts/'appliances/staff/organisation involved in military, custom, police organistation or similar.


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Structure of the rules • •

IR 748 /2012: Initial Airworthiness Requirements, This regulation concerns the processes of certification of aeronautical products, production companies and design companies. This regulation also contains Part 21 that establishes the requirements and the procedures for the certification of airplanes products, parts and appliances, production and design organizations.

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IR 2042/2003: Continuing Airworthiness Requirements This regulation concerns the airworthiness and maintenance of a aeronautical products, moreover, the certification of organizations and maintenance staff. It contains the following Annexes (Parts): Annex I Part M: Continuing Airworthiness requirements Annex II Part 145: Maintenance Organisation certification Annex III Part 66: Aircraft, Maintenance License (AML) régulation Annex lV Part 147: Training organization regulation.

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Annexes = Additions


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Aircraft Maintenance Organization approved by EASA Example : • An aircraft which is ed in Bahrain (i.e. A9C -XXX) may only be maintained in Bahrain by a Maintenance Organization which is approved by the Bahrain CAA (i.e Gulf Air Maintenance ) . • With the formation of the JAA / EASA and the resulting mutual recognition a Bahraini ed aircraft may also be maintained by each Maintenance Organization approved by a JAA I EASA member state. • This means also, that an Approved Maintenance Organization in Bahrain may maintain aircraft ed in the JAAIEASA member states.


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EASA Regulation


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Chapter 10.2 Annex III Part 66: Aircraft, Maintenance License (AML) regulation

PART-66 CERTIFYING STAFF


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Structure of the rules IR 2042/2003: Continuing Airworthiness Requirements • It contains the following Annexes (Parts): • Annex I Part M: Continuing Airworthiness requirements • Annex II Part 145: Maintenance Organisation certification • Annex III Part 66: Aircraft, Maintenance License (AML) régulation • Annex lV Part 147: Training organization regulation. Annexes = Additions


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Part 66 Aircraft, Maintenance License • • • •

In Europe, Aircraft Maintenance Certifying Personnel have to comply with the Annex III Part 66 Aircraft, Maintenance License (AML) regulation. Part 66 provides , the requirements for the technical qualification of such personnel, mainly in of knowledge and experience. The certification of personnel who meet these requirements is issued an Aircraft Maintenance License (AML). The Aircraft Maintenance License (AML), , is consistent with the requirements of ICAOs Annex 1 Personnel Licensing..


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Part 66 Aircraft, Maintenance License (AML) • • • • • • • • •

Part 66 is structured in two sections and related appendixes as follow: Section A: contains the technical requirements that must be satisfied for the issue of an aircraft maintenance License Section B: contains the procedures that must be followed by competent authorities. Arppendix l: Basic Knowledge requirements Arppendix ll: Basic Examination Standard Arppend III : Aircraft Type "Training and Examination Standard 0n the Job training Appendix IV: Experience requirements for extending a Part-66 .AML Appendix V: Application Form - EASA Form 19 Appendix VI: Aircraft Maintenance License referred to in Annex Ill (Part-66) – EASA Form 26


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Part 66 , Section A -Technical requirements • • • • •

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Aircraft maintenance licenses include the following categories: Category A - Line Maintenance Certifying Mechanic Category B1 Maintenance Certifying Technician Mechanical Category B2 Maintenance Certifying Technician -.Avionics Category B3 Maintenance Certifying Technician - for the maintenance of pistonengine non- pressurized aeroplanes of less than 2000 kg MT0M (Maximum Take Off Mass ) Category C - Base Maintenance Certifying Engineer.


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Part 66 , Section A -Technical requirements, Application for AML • The application for an aircraft maintenance license, or any extensions (changes) to such license has to be made on an EASA Form 19 and submitted to the competent authority . • When an applicant requests an extension of an AML to the authority of a Member State other than the Member State in which he/she first qualified, the application will be forwarded to the competent authority that issued the license.


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Part 66 , Section A -Technical requirements • •

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The certification privileges of categories are as follows: Category A : aircraft maintenance License permits the holder to issue certificates of release to service (CRS) following minor scheduled line maintenance and simple defect rectification within the limits of tasks specifically endorsed on the authorization. The certification privileges are restricted to work that the license holder has personally performed in the maintenance organisation that issued the certification authorization .•


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Part 66 , Section A -Technical requirements • • • •

Category B1 aircraft maintenance license shalI permit the holder to issue certificates of release to service for the following: 1. Maintenance performed on aircraft s:tructure, power plant and mechanical and eIectricaI systems. 2. Work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting. Note : Category B1 includes the corresponding A subcategory


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Part 66 , Section A -Technical requirements • • • • •

Category B2 : aircraft maintenance license shalI permit the holder: Issue certificates of release to service for following: 1. Maintenance performed on avionic and electrical systems. 2. Electrical and avionics tasks within power plant and mechanical systems, requiring only simple tests to prove their serviceability. Note :The category B2 license does not include any A subcategory.


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Part 66 , Section A -Technical requirements •

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Category B3 Certifying Staff is applicable to piston-engine non-pressurised aeroplanes of 2000 kg MTOM to issue certificates of release to service for the following : 1. maintenance performed on aeroplane structure, powerplant and mechanical and electrical systems 2. work on avionic systems requiring only simple tests to prove their serviceability and not requiring troubleshooting


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Category C aircraft maintenance license shall permit the holder to issue certificates of release to service following base maintenance on aircraft. The privileges apply to the aircraft as a whole. B1 and B2 Staff can also acts as required to a category C to release to service aircraft after base maintenance works on Large Aircraft. In fact, for aircraft classified as Other Than Large not used for commercial transport , technicians of category B are sufficient.


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Part 66 , Section A -Technical requirements •

66.A.25 - Basic knowledge requirements for the issue of an AML Category

No M1 M2 M3 M4 M5 M6 M7A M7B M8 M9A M9B M 10 M 11 A

M 11 B M 11 C M 12 M 13 M 14 M 15 M 16 M 17 A M 17 B

Modules Mathematics Physics Electrical Fundamentals Electronic Fundamentals Digital Techniques , Electronic Instrument Systems Materials and Hardware Maintenance Practices Maintenance Practices Basic Aerodynamic Human Factor Human Factor Aviation Legislation Turbine Aeroplane Aerodynamics , Structure and System Turbine Aeroplane Aerodynamics , Structure and System Turbine Aeroplane Aerodynamics , Structure and System Helicopter Aerodynamics Structure and Systems Aircraft Aerodynamics , Structure and System Propulsion Gas Turbine Engine Piston Engine Propeller Propeller


A or B Aeroplane A or B Helicopters with with

B2

B3 Piston Engine less than 2000 Avionics Kg MTOW X X X X X X X X

Turbine Engine X X X X

Piston Engine X X X X

Turbine Engine X X X X

Piston Engine X X X X

X X X

X X X

X X X

X X X

X X X

X X

X X

X X

X X

X X

X

X

X

X

X

X X X X X X

X

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X X X

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66.A.25 - Basic knowledge levels : Level 1: Familiarization with main topics of the subject. Level 2: General knowledge of theoretical and practical aspects of the subject and capacity to apply this knowledge. Level 3: Detailed knowledge of theoretical and practical aspects of the subject.


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Part 66 Experience Requirements • • •

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For category A and subcategories B1.2 and B1.4 ( A/C Piston and Helicopters Piston) i) Three years of practical maintenance experience on operating aircraft, if he has no previous technical training; or ii) Two years of practical maintenance experience on operating aircraft and completion of training considered relevant by the competent authority as a skilled worker, in a technical trade; or iii) One year of practical maintenance experience on operating aircraft and completion of a Part-147 approved basic training course. For category B2 and subcategories B1.1 and B1.3 A/C Turbine and Helicopters Turbine) : Five years of practical maintenance experience on operating aircraft if the applicant has no previous technical training;or Three years of practical maintenance experience on operating aircraft and completion of training considered relevant by the competent authority as a skilled worker, in a technical trade; or Two years of practical maintenance experience on operating aircraft and completion of a Part -147 approved basic training course.


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Part 66 Experience Requirements • •

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For category C with respect to large aircraft: i) three years of experience exercising category B 1.1, B 1.3 or B2 privileges on large aircraft or as Part-145 B1.1, B1.3 or B2 staff, or, a combination of both; or ii) five years of experience exercising category B 1.2 or B1.4 privileges on large aircraft or as Part-145 B1.2 or 81.4 staff,or a combination of both


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Part 66 , Section A -Technical requirements • • •

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66.A.45 –Endorsement with Aircraft Ratings : Type/task training and ratings- Category A The holder of a Category A aircraft maintenance license may only exercise his privileges on a specific aircraft type following the satisfactory completion of the relevant category A Aircraft Task Training carried out by an appropriately approved Part-145 or Part-147 organization. The Task training shall consist of: 1. Practical hands on training 2. Theoretical training as appropriate for each task authorised. Satisfactory completion of training shall be demonstrated by an examination and/or by workplace assessment carried out by an appropriately approved Part 145 or Part-147 organisation.


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Part 66 , Section A -Technical requirements • •

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Category B1 and B2 approved Type training shall be made up of: 1. Theoretical training: detailed theoretical knowledge of the aircraft, its main parts, systems, equipment and applicable components, including training in the documents in use such as technical manuals and maintenance procedures. 2. Practical training element (only cat. B): the practical element should include a cross section of maintenance tasks. The practical training : 4 months for applicants with no previous practical , but this can 'be reduced to a minimum of 2 weeks for applicant with such previous experience


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Part 66 , Section B -Technical requirements Section B: contains the procedures that must be followed by competent authorities • • • • • •

General Issue of an Aircraft Maint License Examinations Conversion of National Qualifications Examination Credits Revocation , suspension or limitation of Aircraft Maint License .


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Part 66 , Section B -Technical requirements •

66.B.500 - Revocation, suspension or imitation of the Aircraft Maintenance License.

Possible causes of revocation, suspension or Limitation of the AML: • Falsification of submitted documentary in order to obtain the aircraft maintenance License and/or the certification privileges • Failing to carry out requested maintenance combined with failure to report such to the organization or person who requested the maintenance • Failing to carry out required maintenance resulting from own inspection combined with failure to report such fact to the organjsation or person for whom the maintenance was intended to be carried out. • Negligent maintenance. • Falsification of the maintenance record. • Issuing a certificate of re{ease to service knowing that the maintenance specified has not been carried out or 'Without [ng that such maintenance has been carded out. • Carrying out maintenance or issuing a certificate of release to service when adversely affected by alcohol or drugs. • Issuing certificate of release to service while not in compliance with this Part.


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Chapter 10.3 Annex II Part 145 Maintenance Organisation certification


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Part 145- Structure • • • • •

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The Part 145 is structured in two sections and related appendixes as follow: Section A.: concerns technical requirements that must be satisfied to approve the Organization and its staff . Section B: contains the procedures that must be followed by competent authorities ( Quality Department i.e DGCA ) . • Appendix I: Authorized Release Certificate- EASA Form 1 • Appendix II Class and Ratings System used for the Approval of Maintenance Organizations referred to in Annex I (Part-M) Subpart F and Annex II (Part-145). • Appendix Ill: Maintenance Organization Approval referred to in Annex II (Part145). • Appendix IV: Conditions for the use of staff not qualified to Part-66 .


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Part 145- Line and Base Maintenance Definition of Line and Base maintenance: • Line Maintenance: Any rnaintenance that is carried out before flight to ensure that the aircraft is fit for the intended flight, it include: • a. Troubleshooting • b, Defect rectification • c. Component replacement with use of external test equipment if required. Component replacement may include cornpones such as engines and propellers. • d. Scheduled maintenance and/or checks including visual inspections • Minor repairs and modifications which do not require extensive disassembly and can be accomplished by simple means..


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Part 145- Line and Base Maintenance • •

For temporary or occasional cases {AD s, SB1 s) the Quality Manager may accept base maintenance tasks to be performed by a line maintenance Base Maintenance: all other maintenance tasks are considered to be Base Maintenance


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Part 145 – Maintenance Organization Exposition •

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MOE (Maintenance Organisation Exposition) is the document or documents that contain the the scope of work in relation to the approval and showing how the organization intends to comply with this Part. The MOE has to be amended as necessary to remain an up-to-date description of the organization. The exposition and any subsequent amendment shall be approved by the competent authority (minor amendments to the exposition may be approved through an exposition procedure called indirect approval).


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Part 145 – Maintenance Organization Exposition • •

An application for the issue or change of an Maintenance Approval must be made to the competent authority in a EASA Form 2. Organizations applying for several approvals may do so by using a single EASA Form 2.


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Part 145- A.20 - of Approval • • • •

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145.A.20 of Approval: The scope of work specified in the MOE defines the exact limits of approval. The class and Ratings System, used for the Approval of Maintenance Organizations, is based on four categories ( refer to Part IM appendix IV):• Category A class :The approved maintenance organization may carry out maintenance on the aircraft and any component (including engines and/or Auxiliary Power Units), Category B class The approved maintenance organisation may carry out maintenance on the uninstalled engine and/or APU and engine and/or APU components.


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Part 145- A.20 - of Approval •

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Category C class The approved maintenance organisation may carry out maintenance on uninstalled components (excluding engines and APUs) i.e Components Repair shop Category D class The D1 - Non Destructive Testing (NDT) rating is on[y necessary for an approved maintenance organization that carries out NDT as a particular task for another organization


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Part 145- A.25 - Facility requirements •

Facility requirements-working environment

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Facilities are provided appropriate for all planned work, ensuring in particular, protection from the weather elements. Such as Temperature , Dust , Noise and Proper Lighting . Offices accommodation for the certifying staff Storage facilities for components , tools and materials.

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Part 145- A.30 - Personnel requirements able rnanager: • The able manager 'Who has corporate authority for ensuring that all maintenance required by the customer can be financed and carried out to the standard required by MOE . The able manager shall • Ensure that all necessary resources are available to accomplish maintenance • Establish and promote the safety and quality policy. • Demonstrate a basic understanding of Part-145. • The able manager is not required to be necessary knowledgeable in technical matters .


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Part 145- A.30 - Personnel requirements • •

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Maintenance managers: Maintenance managers responsibilities ensuring that the organization complies with Part-145. Individual managers should report to the able manager except in small Part-145 organization. The organization should have, the following managers: Base Maintenance Manager: Is responsible for ensuring that all maintenance carried out in the hangar, plus. any defect rectification is carried out to the design and quallirty standards. Any corrective action resulting from the quality audits monitoring Line Maintenance Manager: is responsible for ensuring that alI maintenance to be carried out on the Line including defect rectification is. carried out to the standards. Any corrective action resulting from the quality audit monitoring


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Part 145- A.30 - Personnel requirements Workshop and Quality manager • Workshop Manager: • Responsible for ensuring that all work on aircraft components is carried out to the standards • Responsible for any corrective action resulting from the quality audits • Quality Manager: • Responsible for monitoring the quality system, and s . • Have direct access to the able manager to ensure that he is kept updated on quality and compliance matters.


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Part 145- A.30 - Personnel requirements •

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The organization shall retain the record for at Least 3 years after the staff have ceased employment with the organization or as soon as the authorization has been with drawn. The maintenance organization shalI provide the staff upon request, ·with a copy of their personal record on leaving the organization.• The staff shall be given access on request to the personal records . The organization shall provide certifying staff with a copy of their certification authorization in either a documented or electronic format.. Certifying staff shall produce their certificate authorization to any authorized person within 24 hours. The minimum age for certifying staff and category B1 and 82 staff is 21 years .


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Part 145.A.50 -Certification of maintenance •

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Certificate of Release to Service (CRS) shall be issued by appropriately authorized certifying staff when it has been verified that all maintenance work has been properly carried out in accordance with the procedures specified In point 145.A.70, and use of the maintenance data and that there are no noncompliances which are known to endanger flight safety. A CRS ( Certificate of Release to Service ) shall be issued before flight at the completion of any maintenance . Where the aircraft operator is. unable to complete alI maintenance work, it may issue a CRS within the approved aircraft limitations. .


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Part 145.A.50 -Certification of maintenance • •

A CRS shall be issued at the completion of any maintenance on a component using the EASA FORM 1 . In the case.of an aircraft grounded at a different Iodation than the primary line or base maintenance stations. due to the non-avilabiity of a component with the appropriate release certificate, it is allowed to temporarily fit a component ·without appropriate release certificate for a period until the aircraft returns provided the component has a suitable release certificate


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Part 145.A.50 -Certification of maintenance • • •

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An EASA Form 1 may be issued for an aircraft component ·which has been: Maintained / Manufactured before Part-145 became effective • Used on an aircraft and removed in a serviceable condition. Examples include leased and loaned aircraft components Removed from aircraft which have been withdrawn from service, or from aircraft which have been involved in accidents, incidents, heavy landings or lightning strikes.


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Part 145.A.60 -Occurrence Reporting • • • • • • • •

The organization shall report to: 1. The competent authority 2. The state of registry; 3. The organization responsible for the design of the aircraft or component : Any condition of the aircraft or component that has resulted or may result in an unsafe condition that hazards seriously the flight safety. The aim of Occurrence Reporting is to identify the factors contributing to incidents,, and to avoid similar errors. The organization shall establish an internal occurrence reporting system to enable the collection and evaluation of such reports, including the assessment . This procedure shall identify adverse trends, corrective actions taken or to be taken to address, deficiences,and include evaluation of all known relevant information relating to such occurrences and a method to circulate the information.


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Part 145.A.60 -Occurrence Reporting • •

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The organization shall make such reports in a form and manner to ensure that they contain all information about the condition and evaluation results. Where the organization is contracted by a commercial operator to carry out maintenance, the organization shall also report to the operator any such condition affecting the operator's aircraft or component. The organization shall produce and submit such reports within 72 hours of the organization identifying the condition .


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Part 145.A.65 - Safety and quality policy •

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145.A.65 - Safety and quality policy ,maintenance procedure and quality system: The organization shall establish a safety and quality policy The primary objectives of quality System are to ensure that it can deliver a safe product and remains in compliance with the following requirements: Independent audits to monitor compliance with required aircraft/aircraft component. Standards and adequacy of the procedures, to ensure that such procedures invoke good maintenance practices, and airworthy aircraft/aircraft components. In the smallest organizations, the independent audit may be contracted to another approved organization or a person with appropriate technical knowledge and proven satisfactory audit expedience. A quality reporting system to the able manager that ensures. proper and timely corrective action is taken


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Part 145.A.65 - Safety and quality policy • • • •

Findings: level 1 finding is any significant non-compliance which lowers the safety standard and hazards seriously the flight safety. level 2 finding is any non-compliance which could lower the safety standard and possibly hazard the flight safety. After receipt of findings .the approved maintenance organization shall define a corrective action· plan to the satisfaction of the competent authority within a period agreed with this authority.


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Chapter 10.4 AIR OPERATIONS


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EU-OPS- introduction •

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EU operations (OPS) set common technical requirements and istrative procedures applicable to commercial transportation aircraft. An operator shall comply with the applicable airworthiness requirements for aeroplanes operated for the purpose of commercial air transportation. Each airplane (or helicopter) must be operated in compliance and within the approved limitations contained in its Airplane Flight Manual (or Helicopter Flight ManuaI). EU-OPS part 1 prescribe requirements applicable to the operation of any civil airplane by any operator, whose principal place of business and ed office is located in a Member State.


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EU - OPS part 1 • • • • • • • • • • • • •

OPS 1 in subparts that defines specific topics: Subpart A-Applicability and definitions Subpart B -General Subpart C-Operator certification and supervision Subpart O -Operational procedures Subpart E -All weather operations Subpart F-Performance general Subpart G- Performance Class A Subpart H -Performance Class B Subpart I - Performance Class C SubpartJ -Mass and balance Subpart K -Instruments and equipment Subpart L-Communication and navigation equipment


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Subpart M -Aeroplane maintenance Subpart N -Flight crew Subpart 0-Cabin crew Subpart P -Manuals, logs and records Subpart 0-Flight and dutytime limitations and rest requirements Subpart R -Transport of dangerous goods by air Subpart S -Security

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OPS part 1 subpart B • • • •

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MMEL/MEL

OPS part 1 subpart B -OPS 1.030 MMEL/MEL An operator shall establish, for each Aeroplane, a Minimum Equipment List (MEL) approved by the Authority. The MEL shall be based upon, but no less, restrictive than, the relevant Master Minimum Equipment List MMEL An operator shall not operate an Aeroplane other than in accordance with the MEL unless, permitted by the Authority. Any such permission will in no circumstances permit operation outside the constraints of the MMEL. The MMEL is usually issued by a design organization (the Type Certificate holder) and identifies the equipment or functions which may be inoperative for operation. AII the items related to airworthiness, not included must be operative, while a nonsafety-related equipment (for example, galleys) is excluded. The MEL must be approved by the certificating authority (NAA). An MEL is similar in content to the MMIEL except that it is specific to a particular operator and to individual aircraft.


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MEL Page


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OPS part 1 subpart B • • •

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• • •

MMEL/MEL

For each item, the MMEL / MEL specify: 1. The required minimum equipment, function or system for dispatch. 2. The related maintenance action, according to aircraft documentation, indicated with the letter "(M)“. 3. The specific operation procedure that must be accomplished by the flight crew, indicated with the letter "(0)“. 5. The time intervals, which specifies through a letter the allowed period for rectification. Time intervals. letters have the following meaning: .Cat A: no standard interval specified. However, items in this category shall! be rectified in accordance with the conditions stated in the Remarks (or Exceptions) of the MEL. Where a time period is. specified it shall start at 00:01 on the calendar day following the day of discovery. Cat B: the rectification shall be executed within 3 days from discovery Cat C: the rectification shall be executed wthin 10 days. from discovery Cat D: the rectification shall be executed within 120 days from discovery


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OPS part 1 subpart B Configuration Déviation List (CDL) Configuration Déviation List (CDL)• • MMEL / MEL include a section, named Configuration Deviation List (CDL) that is a listing of EASA-approved non-structural external parts that may be missing but the airplane remains airworthy. • To qualify an item onto the CDL, a restrictive set of conditions must be met, Some of these conditions include: • The effect of the missing part upon adjacent structure and systems, • The effect upon airplane performance (for example, the drag penalty imposed upon the airplane when flying with the part missing, and its, effect on operating 'Weights). • The combined effect upon the airplane when more than one CDL item is present on the airplane . • CDL test flights are scheduled into the test plan, and most items on the CDL are qualified during the initial certification of the airplane and. • A list of items, based upon experience with previous designs, is selected during initiail airplane design phase.


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Air Operator Certificate MEA


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Air Operator Certificate


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OPS part 1 subpart C Air Operator Certificate (AOC) Air Operator Certificate (AOC). • The operator must have nominated post holders, acceptable to the Authority, who are responsible for the management and supervision of the following areas: • 1. Flight operations. • 2.. Maintenance system. • 3. Crew training. • 4. Ground operations. • A person may hold more than one of the nominated posts if acceptable to the Authority but, for operators who employ· 21 or more full time staff, a minimum of two persons are required to cover the four areas of responsibility.


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OPS part 1 subpart D Operational Procedures Operational procedures . • The ETOPS rules allows twin-engine aircraft to fly long-distance routes. • Without ETOPS , the maximum distance from an aerodrome for two-engine airplanes is the distance flown in 60 minutes at the One-Engine-lnoperative (OEI) cruise speed. • ETOPS distance may be increased to 120, 180 or more minutes. • Eventually this means that a smaller twin could be used on routes between two c:ity pairs where enger numbers are not economically viable for large aircraft to Operate them.

•

ETOPS : Extended Twin Engine Operations


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OPS part 1 subpart D Occurrence Reporting • • • • • •

Occurrence Reporting (OPS 1.420). Terminology: 1. Incident : is an occurrence, other than an accident, associated with the operation of an aircraft which affects or could affect the safety of operation 2. Serious Incident : is an incident involving circumstances indicating that an accident nearly occurred. 3. Accident" is an occurrence associated with the operation of an aircraft • In case of accident or serious incident, the commander or the operator of an airplane shall submit a report to the authority in the State of the operator within 72 hours of the time when the accident or serious incident occurred.


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Aircraft markings and placards • An aircraft must contain: • The specified marking and placards • Instrument marking and placards required for the safe operation . Each marking and placard prescribed: • Must be displayed in a visible place • Not be easily erased, disfigured or obstructed. • Marking or placards should be placed close to or on the instrument or control with which they are associated. .


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Chapter 10.5 CERTIFICATIOIN OF AIRCRAFT PARTS AND APPLIANCES (PART 21)


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Introduction •

•

•

Regulation (EC) . 216/2008 laying down in article 4 (1) that all aircraft, including its , parts if so designed, constructed or ed in a European Union Member State or ed in a third country but supervised by an operator from a Member State, or even if ed in a third country and supervised by an operator from a third country but with traffic to and from a Member State, must comply with the same rules. For parts and appliances these certification may be issued when specific certifications have proven to meet Airworthiness specifications established to ensure compliance with the essential requirements. All organizations , design products, parts and appliances shall demonstrate their skills as well as to be able to assure the responsibilities associated with the privileges that are recognized through .a process of design organization approval.


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Part 21- Regulation •

The commission regulation (EC) No 748/2012 is laying down implementing rules for the airworthiness and environmental certification of aircraft and related products,parts and appliances, as well as for the certification of design and production organizations..

• •

Part 21 is structured in two sections: a. Section A: contains the requirements for the applicants and acquired rights and obliigations b. Section B: contains the procedures for competent authorities.

•


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Part 21 Structure and purpose • • • • • • • • • • • • • • • • • •

Section A and section B are both divided in subparts that defines specific topics:• Subpart A-General Subpart B - Type certificates and restricted type certificates: Subpart C- Not applicable Subpart D -Changes to type certificates and restricted type certificates Subpart E –Supplemental type certificats Subpart F -Production without production organisation approval Subpart G - Production organization approval (POA) Subpart H -Certificate of airworthiness and restricted certificates of Airworthiness Subpart II -Noise certificates Subpart J - Design organization approval (DOA) Subpart K - Parts and appliances Subpart L - Not applicable Subpart M-Repairs Subpart N - Not applicable Subpart O - European Technical Standard Order authorizations (ETSO) Subpart P- Permit to fly Subpart O - identification of products, parts and appliances © 20 5 Panasonic Avionics Corporation. Proprietary and Confidential

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Type Certificate and Supplemental Type Certificate issuing (Part 21 subparts B, D, E) • •

• • • •

•

Any person eligible can apply for a type certificate or restricted type certificate in accordance with Part 21 (21.A.14) The type-certificate and restricted type-certificate are both include the design, the operating limitations, the data sheet for airworthiness and emissions, the applicable type-certification base and environmental! protection requirements Type design changes are classified in two categories: 1. Minor change 2. Major change Only the type-certificate holder may apply for approval of a major change to a design. under this Subpart All other applicant s for a major change to a type design shall apply under Subpart E for a Supplemental Type Certificate STC.


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Production organizations approval for products ,parts and appliances (Part 21 subpart G} • • • • • • • • • • • • •

Exposition – Production Organisation Exposition (POE) The POE shall provide the following information: A statement signed by the able manager confirming that he will be compiling with POE at all times; The title(s) names , duties and responsibilities of managers An organizational chart showing associated chains of responsibility A list of certifying staff A general description of man-power resources; A general description of the facilities located at each address specified in the production organization's certificate of approval; Scope of work relevant to the of approval; The procedure for the organizational changes to the competent authority; The amendment procedure for the production organisation exposition; A description of the quality system and the procedures A list of those outside parties.


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EASA certification specifications CS-23, 25, 27, 29 •

Airworthiness Codes Or Certification Specification Standards

• • • • • • • • • • • • • • •

CS 23 NORMAL. UTILITY. AEROBATIC & COMMUTER AEROPLANES CS 25 LARGE AEROPLANES C2 27 SMALL ROTORCRAFT CS 29 LARGE ROTORCRAFT CS 31 HB HOT AIR BALLOONS CS 34 AIRCRAFT ENGINE EMISSION AN FUEL VENTING CS 36 AIRCRAFT NOSE CS APU AUXLIARV POWER UNITS CS AWO All. WEATHER OPERATIONS CS.. D&FINITIONS & ASIR&VIATCONS CS- EENGINES CS ETSO EUROPEAN TECHNlCAL STAINIOARD ORDERS CS.P PROPELLERS CS·VLA VERY LIGHT AEROPLANES CS-VLR VERY LIGHT ROTORCRAFT


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Certificate of Airworthiness (CofA), •

•

• • • •

•

A Certificate of Airworthiness (CofA), or an airworthiness certificate, is issued for an aircraft by the national aviation authority in the state in which the aircraft is ed. ( i.e DGCA of Lebanon ) The airworthiness certificate proves that the aircraft is airworthy as the aircraft conforms to its type design. ( Aircraft publications such as AMM , IPC , WDM etc.. ) Each airworthiness certificate is issued in one of a number of different categories. A certificate of airworthiness is issued when the aircraft is ed in the name of the owner without expiration date . A yearly currency fee is payable to renew the Certificate of Airworthiness. If this fee is not paid when due, the certificate expires and the owner must apply again for this certificate to be issued. The Certificate of Airworthiness can only remain valid when a certificate of release to service from the maintenance facility declares that the maintenance has been carried out and the aircraft is then certified as being airworthy.


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Certificates of Airworthiness

05/01/04


84

Revision Original

Subpart H Certificate of Airworthiness, restricted certificates of airworthiness and permit to fly • • • • • • • •

The Certificate of Airworthiness. must be accessible and stored with other airworthiness certificate in the cockpit. Permits. to fly shall be issued to aircrafts. According to the following purposes.: a. Development b. Showing compliance with regulations or certification specifications. c. Production flight testing of new production aircraft d. Flying the aircraft for customer acceptance e. Flying the aircraft for Authority acceptance f. Flying the aircraft to a location where maintenance or airworthiness review are to be performed, or to a place of storage


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Permit to Fly

05/01/04


86

Revision Original

Certificate of registration •

•

The certificate of registration must be accessible and stored with other airworthiness certificates in the cockpit. Each aircraft must have its own aircraft registration based on rules and regulation or the respective country the registration.


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Certificate of Registration


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Subpart I Noise certificate • • • •

• •

Any person whose name an aircraft is ed or will be ed shall be eligible as an applicant for a noise certificate An application for a noise certificate shall include: 1. New aircraft: A statement of conformity, the noise information determined in accordance with the applicable noise requirements. 2. Used aircraft: The noise information determined in accordance with the applicable noise requirements, historical records to establish the production., modification, and maintenance standard of the aircraft. a) lf the aircraft remains on the same , the noise certificate shall be transferred together with the aircraft b) if the aircraft moves to the of another Member State, the noise certificate shall be issued upon presentation of the former noise certificate.


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Noise Certificate


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Other documentation weight schedule and radio station license and approval •

• • • • •

The operations manual, specify the principles and methods involved in the loading and in the mass and balance system that meet the requirements of current OPS regulation. The system must cover all types of intended operations. Any weight change has to be recorded and ed in the weight and balance sheet of the aircraft. A scheduled aircraft weighing has to be established. For every flight a weight calculation {load sheet) must be performed and signed 'by the pilot. The aircraft Radio station license must be accessible and stored with other airworthiness certificates in the cockpit.


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Chapter 10.6 Annex I Part M: Continuing Airworthiness requirements


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Introduction •

• • •

•

In Europe, Aircraft Maintenance Organizations have to comply with the Annex I (Part M) of the Regulations document (EC) 2042/2003, The Regulations specifies the conditions to be met by the persons or organizations involved in such continuing airworthiness management. Maintenance organization approval for non commercial and/or small aircraft is treated in subpart F of part M Maintenance of large aircraft, aircraft used for commercial air transport and components thereof shall be carried out by a Part-145 approved maintenance organization. In this case, maintenance organizations have to comply to the Annex II Part 145: Maintenance Organisation certification. Part 145 gives to maintenance organizations the privilege to carry out maintenance, and the subsequent release to service, of large aircraft or of aircraft used for commercial air transport, as well as engines and components installed on them.


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Part M Section A - subpart F - Maintenance Organisations • This subpart includes the following topics: 1. The scope (M.A.601) 2. The application (M.A.602) 3. The extent of approval (M.A.603) 4. The maintenance organization manual (M. A .604) 5. The facilities (M.A.605) 6. The personal requirements (M.A.606) 7. The certifying staff(M.A.607) 8.The components, equipment and tools (M.A.608) 9. The maintenance data (M.A.609)


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Part M Section A - subpart F - Maintenance Organisations 10. The maintenance work orders (M.A.610) 11. The maintenance standards (M.A.611) 12. The aircraft certificate or release to service (M.A.612) 13. The component certificate of release to service (M.A.613) 14. The maintenance records(M.A.614) 15. The privileges of the organization(M.A.615) 16. The organizational review(M.A.616) 17. The changes to the approved maintenance organization (M.A.617) 18. The continued validity of approval (M.A.618) 19. The findings(M.A.619)


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Part M Section A - subpart F - Maintenance Organisations •

•

• • • • • • •

The maintenance organization manual (or Maint Organization Exposition ) has to provide the following information: 1. A statement signed by the able manager to confirm that the organization will continuously work in accordance with Part-M and the MOE manual at all times 2. The organisation's scope of work 3. The title(s) and name(s) of person(s) referred to in M.A.6o6(b) 4. An organization chart showing associated chains of responsibility between the person(s) referred to in M.A .6o6(b) 5. A list of certifying staff with their scope of approval 6.A list of locations where maintenance is carried out, together with a general description of the facilities' 7 Procedures specifying how the maintenance organization ensures compliance with this Part. 8. The maintenance organization manual amendment procedure(s) ..


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Part M Section A - subpart F - Maintenance Organisations • • •

•

•

The extent of maintenance records can be summarized as follow: The approved maintenance organisation shall record all details of work carried out. Records necessary to prove all requirements have been met for issuance of the certificate of release to service including the sub-contractor's release documents shall be retained. The approved maintenance organisation shall provide a copy of each certificate of release to service to the aircraft owner, together with a copy of any specific approved repair/modification data used for repairs/modifications carried out The approved maintenance organization shall retain a copy of all maintenance records and any associated maintenance data for three years from the date the aircraft or aircraft component to 'Which the work relates was released from the approved maintenance organization


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Continuing Airworthiness •

• • • • •

•

Continuing airworthiness ensurs that, all aircraft comply with the airworthiness requirements and are in a condition for safe operation. No aircraft may be operated unless in airworthy condition Two conditions must be met before an aircraft can be consider airworthy": 1.. The aircraft conforms to type design. 2. The aircraft is in condition for safe operation. The first condition is achieved when proper components are installed, in accordance with with drawings, specifications and other data that are part of the Type Certificate, The second condition is refers to the condition of the aircraft with relation to wear and deterioration that occurs during its operative life.


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Continuing Airworthiness • •

•

•

•

Continuing airworthiness includes, eight basic requirements: 1. Design criteria, that provide the necessary accessibility for inspection and let the use of established processes and practices for the accomplishment of maintenance. 2. Maintenance requirements, that involves the preparation by the organization responsible for the type design of the specifications methods, procedures and tasks necessary to maintain the aircraft and publication of this information in a format that can be readily adapted for use by an operator. 3. Company Maintenance Programmed (CMP), as seen as the adoption by each operator of specifications, methods, procedures and tasks using the information provided by the organization responsible for the type design, and preparing that material in the form of a maintenance programme suitable for its operation. 4. Reporting reporting of defects and other significant maintenance and operational information by the operator to the organization responsible for the type design


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Continuing Airworthiness •

• •

•

5. Defect analysis and rectification, The analysis. of defect, accident and other maintenance and operational information by the organization responsible for the type design, the State of Design and the State of Registry and the initiation and transmission of information and recommended or mandatory action to be taken in response to that analyze 6. Local compliance, that oblige the operator to review all service information and take appropriate action 7. Compliance with life limits, that is the accomplishment by the operator of an mandatory requirements concerning the aircraft with particular reference to fatigue life limits and any special tests or inspections required by the certification process or subsequently found necessary to ensure structural integrity 8. Compliance with Structural inspection Program (SIP), with preparatiion of and compliance with Supplemental Structural inspection Programmes and subsequent requirements related to aging aircraft.


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Initial Airworthiness; (Part-21 provisions) related to continuing airworthiness •

•

•

The continuing airworthiness functions, shall be performed in accordance ·with the provisions of Annex I to the Basic Regulation and Annex Part 21 to Commission Regulation (EC) No. 748/2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, in particular its.paragraphs,. 21.A.3 (Failures , Malfuncions and defect ) and 21.A.3B (Airworthiness Directives ), and the related Acceptable e Means of Compliance ("AMC") and Guidance Material 'GM"). ADs, are issued by EASA, The dissemination of airworthiness directives to aircraft owners is a responsibility of the State of Registry and does not belong to the Agency. If an aircraft has outstanding airworthiness directives that !have not been complied with, the aircraft is not considered airworthy.


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Part M - General description •

• •

• •

In Europe, Aircraft Maintenance Organizations have to comply with the Annex I (Part M) of the Regulations document (EC) 2042/2003, which concerns the ,measures to be taken to ensure that airworthiness is maintained, including maintenance. It also specifies the conditions to be met by the persons or organizations involved in such continuing airworthiness management • This regulation establishes common Technical requirements and istrative procedures for ensuring the continuing airworthiness of aircraft, including any component for installation which are: 1. ed in a EASA Member State 2. ed in a third country and used by an operator for which a Member State ensures oversight of operations.


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Part M - Structure and purpose • • • • • • • • • • • • •

Part M is structured in two sections: Section A: contains the technical requirement's that must be satisfied for the personnel and the organizations (JORAMCO , ADAT etc ), Section B: contains, the procedures that must be followed by competent authorities ( DGCA ) Both Section A and section B are divided in subparts that define specific topics: 1. Subpart A - General 2. Subpart B- ability 3. Subpart C Continuing Airworthiness 4. Subpart D -Maintenance Standards 5. Subpart E-Components 6. Subpart F - Maintenance Organisation. 7. Subpart G -Continuing Airworthiness Management Organsation (CAMO) 8. Subpart H - Certificate of Release to Service (CRS) g. Subpart 1-Aiworthmness Review Certificate


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Part M - Structure and purpose • • • • • • • • •

The Part-M also includes eight appendixes as follow: 1. Appendix I: Continuing Airworthiness Arrangement 2. Appendix II: Authorized Release Certificate- EASA Form 1 3. Appendix Ill: Airworthiness Review Certificate- EASA Form 15 4 Appendix IV:· Class and Ratings System used for the Approval of Maintenance Organizations referred to in Annex I (Part-M) Subpart F and in Annex II (Part-145) 5. Appendix V: Maintenance Organization Approval referred to in Annex I (Part M)Subpart F 6. Appendix VI Continuing Airworthiness Management Organisation Approval referred to in Annex I (Part-M) Subpart G 7. AppendixVII: Complex Maintenance Tasks 8. AppendixVIII: Limited Pilot Owner Maintenance


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Part M Section A - subpart A/B - General/ability • •

•

• • • •

Part M Section A- subpart A-General This Section (M.A.101) establishes the measures to be taken to ensure that airworthiness is maintained, including maintenance. It also specifies the conditions to be met by the persons or organizations involved in such continuing airworthiness management. Part M Section A- subpart B-ability This subpart includes the following topics: 1. The responsibilities' of the owner for the continuing airworthiness of an aircraft (M.A.201) 2. The related occurrence reporting {M.A.202).


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Part M Section A - subpart C - Continuing Airworthiness • •

•

•

An owner or operator shall keep the following records for the periods specified: 1. All detailed maintenance records in respect of the aircraft and any service life limited component fitted thereto, not less than 36 months (3 Years ) after the aircraft or component has been released to service. .2. The total time in service (hours, calendar time, cycles and landings) of the aircraft and all service life-limited components, at least 12 months after the aircraft or component has been permanently withdrawn from service 3. The time in service (hours, calendar time, cycles and landings) as appropriate, since last scheduled maintenance of the component subjected to a service life limit,.


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Part M Section A - subpart C - Continuing Airworthiness • •

•

4. The current status of compliance with maintenance programme 5. The current status of airworthiness directives applicable to the aircraft and components, at least 12 months after the aircraft or component has been permanently withdrawn from service 6. Details of current modifications and repairs to the aircraft, engine(s), propeller(s) and any other component vital to flight safety, at least 12 months after they have been permanently withdrawn from service


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Part M Secticion A - subpart C - Continuing Airworthiness An aircraft technical log system shall contain the following information for each aircraft: • 1. Information about each flight, necessary to ensure continued flight safety • 2. The current aircraft certificate of release to service. • 3. The current maintenance statement giving the aircraft maintenance status of what scheduled and out of phase maintenance is next due except that the competent authority may agree to the maintenance statement being kept elsewhere, • 4. All outstanding deferred defects rectifications that affect the operation of the aircraft. • 5. Any necessary guidance instructions on maintenance arrangements. • 6. An operator shall ensure that the aircraft technical log is retained for 36 months after the date of the last entry.


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Typical Technical Log Page


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Part M Section - subpart D/E/F - Maintenance Standards/ Components/Maintenance Organization Part M Section A - subpart D - Maintenance Standards • 1. The maintenance data (M.A.401) • 2. The performance of maintenance (M.A.402) • 3. The aircraft defects (M.A.403). Part M Section A - subpart E - Components • 1. The installation (M.A.501) • 2. The component maintenance (M.A.502) • 3. The service life limited components (M.A. 50:3) • 4. The control of unserviceably components (MI.A.504). Part M Secti1on A - subpart F - Maintenance Organization • The scope of this Subpart is to establish the requirements to be met by an organization to qualify for the issue or continuation of an approval for the maintenance of aircraft and components not listed in point M.A. 201(9).


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Part M Section A - subpart G - Continuing Airworthiness Management • •

•

This regulation concerns the management of continuing airworthiness of EASA aircraft. Approved 0rganisations can make recommendations to a competent authority that an Airworthiness Review Certificate (EASA Form 15a) may be issued or extend an Airworthiness Review Certificate (EASA Form 15b) under the of their approval. An· application for issue or change of a continuing airworthiness management organization· approval shall be made on a form and in a manner established by the competent authority using the EASA Form 2.


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s545.10 Maintenance Organization Exposition (manual)


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Part M Section A - subpart G - Continuing Airworthiness Management Organization •

•

•

The organization shall appoint an able manager, who has corporate authority for ensuring that at all continuing airworthiness management .activities can be financed and carried out in accordance with this Part. For commercial air transport the able manager shall be the person who also has corporate authority for ensuring that all the operations of the operator can be financed and carried out to the standard required for the issue of an air operator's certificate A person or group of persons shall be nominated with the responsibility of ensuring that the organization is always in compliance with this Subpart . Such person(s) shall be responsible to the able manager


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Part M Section A - subpart G - Continuing Airworthiness Management Organization •

•

•

The able manager shall designate a nominated post holder. This person shall be responsible for the management and supervision of continuing airworthiness activities, pursuant to paragraph (c) The nominated post holder shall not be employed by a Part- 145 approved organization under contract to the operator, unless specifically agreed by the competent authority The organization shall have sufficient appropriately qualified staff for the expected work•


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Part M Section A - subpart G - Continuing Airworthiness Management Organization • • •

• •

The nominated persons shall be able to show relevant knowledge, background and a appropriate experience related to aircraft continuing airworthiness The qualification of all personnel involved in continuing airworthiness management shall be recorded. For organizations extending airworthiness review certificates,the organization shall nominate persons authorized to do so subject to approval by the competent authority The organization shall define and keep updated in the continuing airworthiness management exposition the title(s) and name(s) of person(s) referred to The organization shall establish and control the competence of personnel involved in the continuing airworthiness management , airworthiness review and/or quality audits in accordance with a procedure and to a standard agreed by the competent authority.


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Part M Section A - Subpart G - Continuing Airworthiness Management Organization • •

• •

Every 2 years a complete audit is performed by the competent authority in order to the compliance of the organization During an audit ,finding could be issued by the authority. The findings can be summarized as follow: A level 1 finding is any significant non-compliance with Part-M requirements which lowers the safety standard and hazards seriously the flight safety A level 2 finding is any non-compliance with the Part-M requirements which could lower the safety standard and possibly hazard the flight safety


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Part M Section A - subpart H - Certificate of Release to Service CRS • • • •

This subpart includes the following topics: 1.The aircraft certificate of release to service (M .A.801) 2. The component certificate of release to service (M.A.802) 3.The pilot owner authorization (M .A.803)


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Part M Section A - subpart I -Airworthiness Review Certificate • • • • • •

This subpart includes the following topics: 1.The aircraft airworthiness review (M.A.901) 2.The validity of the airworthiness review certificate (M .A.902) 3.The transfer of aircraft registration within the EU (M.A.903) 4.The airworthiness review of aircraft imported into EU (M.A.904). 5.The findings (M.A.905).


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Chapter 10.7 NATIONAL REGULATIONS


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The End


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