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<p>Part-145: Approved Maintenance Organisations (Annex II to EC 2042/2003)Juan Anton</p> <p>Continuing Airworthiness Manager Rulemaking Directorate EASA</p> <p>25 January 2012</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>EC 2042/2003 Article 3Organisations and personnel involved in the continuing airworthiness of aircraft and components, including maintenance, shall comply with the provisions of Part-M and where appropriate those specified in Part-145 and Part-66. As a consequence, Part-M applies also to Part-145 organisations, in particular the following paragraphs: Subpart D: Maintenance standards (maintenance data, performance of maintenance, aircraft defects) Subpart E: Components (installation, maintenance, life limited components, control of unserviceable components)25 January 2012 Slide 2 SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>EC 2042/2003 Article 4</p> <p>Organisations involved in the maintenance of large aircraft or of aircraft used in commercial air transport, and components intended for fitment thereto, shall be approved in accordance with the provisions of Annex II (Part-145).</p> <p>25 January 2012</p> <p>Slide 3</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.10 ScopeRequirements for approval of an organisation for maintenance of aircraft and components</p> <p>Including facilities outside Member State if Identified in exposition Control procedures in place Authority satisfied that they are integral part of the organisation</p> <p>25 January 2012</p> <p>Slide 4</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.20 Terms of approvalA rating: maintenance of aircraft and components (according to aircraft maintenance data) while installed on the aircraft (or temporarily removed to facilitate access)</p> <p>B rating: maintenance on engines/APU and components (according to engine/APU maintenance data) while installed on the engine/APU (or temporarily removed to facilitate access)C rating: maintenance on components other than engine/APU. D1 rating: NDT. Only required when the Part-145 performs NDT for other organisations (issuance of Form 1). This is a rating not related to particular aircraft, engines or components.</p> <p>NOTE: Refer to M.A.502 for more details.25 January 2012 Slide 5 SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.20 Terms of approvalComponent certifying staff is only required for B and C rated organisations. When these organisations need to carry out NDT as part of component maintenance, the NDT should be carried out by personnel qualified in accordance with 145.A.30 (f). These NDT personnel do not need to be certifying staff. The component maintenance, including the NDT, should be released by appropriate component certifying staff. The need for NDT certifying staff qualified in accordance with 145.A.30 (f) and 145.A.35 is only required for D1 rated organisations.</p> <p>25 January 2012</p> <p>Slide 6</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.30 Personnel requirementsAccountable manager Nominated personsAccepted by authority, (EASA Form 4)</p> <p>Quality managerAccepted by authority, (EASA Form 4)</p> <p>Sufficient staffMan hour planning (all functions, also auditing staff). Reviewed and revised at least every 3 months. At least 50% employed staff (not contracted) in every workshop, hangar, flight line and shift, to ensure adequate organisational stability.25 January 2012 Slide 7 SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.30 Personnel requirementsCategoryA licence</p> <p>Release to Service privilegesMinor scheduled line maintenance and simple defect rectification (AMC 145.A.30(g)), personally performed in Part145 organisation. Maintenance on structure, powerplant, and mechanical and electrical systems, avionic line replaceable units (with simple tests). Maintenance on avionic and electrical systems. Base maintenance of entire aircraft in Part-145 organisation.</p> <p>B1/B3 licence</p> <p>B2 licence</p> <p>C licence</p> <p>25 January 2012</p> <p>Slide 8</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.30 Personnel requirements (large aircraft)Cat. CCertifying Base Engineer</p> <p>Base</p> <p>Cat. B1 Cat. B1</p> <p>Cat. B2 Cat. B2</p> <p>Support staff Certifying Technician Certifying Line Mechanic</p> <p>Line</p> <p>Cat. ASimple tasks</p> <p>Mechanic25 January 2012 Slide 9</p> <p>AvionicsSAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.30 Personnel requirements (other than large aircraft)Cat. CorOptional</p> <p>Base</p> <p>Cat. B1/B3 Cat. B1/B3</p> <p>Cat. B2 Cat. B2</p> <p>Certifying Technician Certifying Technician Certifying Line Mechanic</p> <p>Line</p> <p>Cat. ASimple tasks</p> <p>Mechanic25 January 2012 Slide 10</p> <p>AvionicsSAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.30 Personnel requirementsExemptions for certifying staff Facilities outside EU / Line stations outside EU National qualification Conditions in Appendix IV Repetitive pre-flight ADs. Certifying staff authorisation to flight crew (if allowed by the AD). Aircraft operating away from support location. Certifying staff authorisation to commander or flight engineer. Maximum validity 1 year. Aircraft grounded away from base (unforeseen) with no certifying staff available. One-off authorisations. Reported to NAA within 7 days. Rechecked if affect flight safety.</p> <p>25 January 2012</p> <p>Slide 11</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.35 Certifying staff and support staffQualification, training and record requirements are the same for certifying staff and for B1 and B2 support staff. All of them must hold a Part-66 licence with the appropriate ratings and have a minimum of 21 years.</p> <p>B1 and B2 support staff do not need to be nominated as certifying staff. May be done if this personnel is used also for line maintenance.</p> <p>25 January 2012</p> <p>Slide 12</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.40 Equipment, tools and materialsAvailable and used (scope of work) Controlled and calibrated (as applicable) Part M.A.402(f) requires verification to ensure that no tools or equipment are left inside aircraft/component</p> <p>25 January 2012</p> <p>Slide 13</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.42 Acceptance of componentsDocumentation needed for components: New components: EASA Form 1 or FAA 8130-3 or TCCA240078 (or TCCA Form One). Maintained components: EASA Form 1 or FAA 8130-3 (dual release) or TCCA24-0078/Form One (dual release) Standard parts and materials (raw / consumable) do not need a Form 1 or equivalent. Certificate of Conformance is enough. Installer must check eligibility of component: Particular attention to modifications and configuration of aircraft, engines, etc.</p> <p>25 January 2012</p> <p>Slide 14</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.42 Acceptance of componentsPMAs can be accepted if: The PMA part is not a critical component". The statement This PMA part is not a critical component should be written in Block 12 of the FAA Form 8130-3; , or The PMA part conforms to design data obtained under a licensing agreement from the holder of the FAA design approval. The statement Produced under licensing agreement from the FAA design approval holder should be written in Block 12 of FAA Form 8130-3; or The PMA part has received an explicit approval by means of a design change or STC from the Agency or, when this approval was granted prior to 28 September 2003, from any of the National Aviation Authorities of the Members States of the European Union. The reference to this authorization should be written in Block 12 of the FAA Form 8130-3.25 January 2012 Slide 15 SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.42 Acceptance of components145.A.42(c) allows fabrication of a restricted range of parts by the Part-145 organisation:</p> <p>Fabricated by the organisation (not by someone else). To be used in the course of undergoing work (not for sale) Within the technical and procedural capabilities of the organisation. In accordance with approved procedures. Using approved data (by TC holder or authority) contained in overhaul or repair manuals, SBs, etc, or as approved by authority. Not eligible for issuance of Form 1. Limited range (bushes, sleeves, shims, control cables, flexible and rigid pipes, electrical cable looms, formed or machined sheel metal panels, secondary structural panels and skin panels).</p> <p>25 January 2012</p> <p>Slide 16</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.45 Maintenance DataHold and use current, available, applicable data in accordance with scope / capability</p> <p>Requirements, directives, CDCCL etc. issued by authority Maintenance / repair instructions issued by TC holder, Part21 organisation or oversight authority. Standards, recognised standard practices. Instructions modified by organisation iaw procedures. May be provided by operator / customer (must be up to date).Part-21 Subpart J Design Organisation may approve minor modifications and minor repairs (major repairs through EASA)</p> <p>25 January 2012</p> <p>Slide 17</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.50 Certification of maintenanceCRS issued by appropriate Certifying Staff on behalf of organisation before flight when All maintenance ordered has been carried out in accordance with MOE procedures, using correct data and no known hazardous non-compliances (see AMC 145.A.50(a) 1.2) New defects / incomplete work orders Communicate rectification to operator Maintenance not completed Operator informed and agrees Inform authority if in doubt Details entered on release certificate Operators agreement endorsed on certificate Issue CRS within aircraft limitations.</p> <p>25 January 2012</p> <p>Slide 18</p> <p>SAMA Information Day (Olten, Switzerland)</p> <p>European Aviation Safety Agency</p> <p>145.A.65 Quality systemIndependent audits Planned to cover all aspects in 12 months. Represent complete maintenance activities. Include product sampling. Small organisations (</p>