Components removed serviceable from aircraft (AMC No 2 to 145.A.50(d) par 2.6 & 2.7) SOS component Components received from customers for repair and/or overhaul etc. Procedure of treatment of a suspected unapproved part « bogus part Identification Record Notification to the Authority Form used Notification address to EASA Acceptance and incoming inspection of new parts and appliances without an EASA Form 1 for European Light Aircraft (ELA). Reference to EASA Certification Memorandum: EASA CM – 21.A – K – 001 Issue: 1 or later revision 2.3 Storage, Tagging and Release of Aircraft Components and Materials to Aircraft Maintenance Procedures for maintaining satisfactory storage conditions (including segregation) of: Rotable Perishables, raw material Flammable fluids Engines Bulky assemblies Record of position in the store (s) Parts and appliances referred to in point 21.A.307(c) (New parts and appliances without an EASA Form 1 for European Light Aircraft (ELA). Reference to EASA Certification Memorandum: EASA CM – 21.A – K – 001 Issue: 1 or later revision System and procedure to control shelf life / Life limit and AD (Part 2.11) / modification standard Special storage requirements (condition and limitation) e.g.: ESD sensitive devices, rubber Tagging / Labelling system and storage areas Serviceable parts /material Unserviceable Robbery Unsalvageable components (see Part 145.A.42(d) and M.A.505I(d)I and its AMC) Quarantine Batch number Scrap Part 145.A.25 (d), AMC 145.A.25 (d) 1, 2, 3 – Part 145.A.40 (a) – Part 145.A.42(a) / AMC 145.A.42 (a)(b) – Part 145.A.70 (a) 12 – M.A.504(c)(d)I / AMC M.A.504(c)(d)I – 21.A.307(c) / EASA Certification Memorandum: EASA CM – 21.A – K – 001 Issue: 1 or later revision
This paragraph must describe the additional / special procedures of the management of the facilities, materials/ ingredients and tools/ equipment, technical documentations, staff associated to the line maintenance activity of a workshop carrying out base and line maintenance. L2.2 Line Maintenance Procedure related to Servicing / Fuelling / / etc. Technical and maintenance documentation management (control and amendment) Company Technical Procedures / Instructions management Fuel supply quality monitoring (bulk storage / aircraft re-fuelling) Ground de-icing (procedures / monitoring of sub-contractors) Maintenance of ground support equipment Monitoring of sub-contracted ground handling and servicing Part 145.A.70 (a) 12, 15 – Part 145.A.75 (b), (c), (d) L2.3 Line Maintenance Control of Defects and repetitive Defects Reportable defects – PIREPS – Engineering entries – Cabin Procedure on how to deal with defects requiring B1, B2 or B3 certifying staff (AMC 145.A.30 (g)3. Rules for deferring (periods – review – permitted personnel – conformity with MEL /CDL provisions) Awareness of deferred defects carried by aircraft – (monitoring of repetitive defects – Communication with main base) Analysis of tech log (repetitive defects – crew complaints – Analysis and transfer of cabin log items as required) Co-ordination with the operator This paragraph must describe the general procedures followed by the organisation regarding the rectification of defects and repetitive defects recorded during operation of the aircraft. The procedures should also cover the follow up of defects and repetitive defects on behalf of customers/ operators and the Part-145 maintenance organisation. Part 145.A.30 (g) / AMC 145.A.30 (g) - Part 145.A.70 (a) 12, 15 – Part 145.A.75 (b), (c), (d) L2.4 Line Procedure for completion of Technical Log Technical Log system: Taking into account Operator Procedure Completion of Sector Record Page Distribution of copies Certification / Sign-off (Maintenance Statements) Maintenance Duplicate Inspections ETOPS Certification Retention of records Periods Methods and security Part 145.A.70 (a) 12, 15 – Part 145.A.75 (b), (c), (d)
Appendix I 1.9 Scope of Work This paragraph must show the range of work carried out at each approved site within the scope of the approval (EASA Form 3 – Schedule of Approval). This section should also relate to paragraphs 1.8 & 5.3 in such a way that it can be clearly seen which specific tasks are performed at which locations. Aircraft Maintenance Example: Rating TC HOLDER AIRCRAFT MODEL LIMITATION MAINTENANCE Level ** Base Line A1 AIRBUS A300 B2-202 A300 B4-102 Airbus A300 basic model (GE CF6) Up to and including C* checks X X A1 AIRBUS A300 C4-203 Airbus A300 basic model (GE CF6) Daily /weekly / defect rectification X A1 AIRBUS A300 B2-320 Airbus A300 basic model (PW JT9D) Daily/Weekly/defect rectifications X A1 The BOEING COMPANY Boeing 767-200 BOEING 767-200 (PW 4000) Up to C checks* excluding C4C, S4C and multiples X X A2 PILATUS AIRCRAFT PC-12 PC-2/45 PC-12/47E Pilatus PC 12 (PW PT6) Up to and including weekly checks X A2 LAVIA ARGENTINA S.A. (LAVIASA) - Piper PA-25 (Lycoming) Up to and including 100H/Annual checks* X A3 EUROCOPTER AS355 E AS355 F1 AS355 F2 Eurocopter AS 355 (RR Corp 250) Defect rectification, Daily X A4 NIL
NDT task CRS Summary table for the release and qualification of NDT tasks Part-145 organisation Certifying staff required Qualification system Release procedure Release procedure for NDT task Aircraft - Class A The release of the works carried out on aircraft has to be performed by certifying staff holding a Part-66 license Licensing of personnel has to follow Part-66 regulation The release is either in the aircraft technical log or in issuing an aircraft release to service statement A Part-145 organisation holding an A approval rating on a particular aircraft type and having in its approved scope of work NDT for this aircraft type. This organisation needs to have Part-66 certifying staff (B, C) and NDT personnel qualified in accordance with 145.A.30(f) (EN 4179). In this case the NDT qualified staff perform the NDT task and signs the task card / Work Order / Engineering Order for the accomplishment of the task. The aircraft is released by appropriately qualified B1 or C certifying staff as applicable under the organisation’s A rating. Please note that the release of the aircraft would generally include not only the NDT task but also the associated tasks (removal of panels, blankets, wires, etc.). Engines - Class B The release of the works carried out on engines has to be performed by engines certifying staff The certifying staff is qualified in accordance with the procedure established by the organisation. Part-66 license not necessarily required. The release of works performed under class B is done on an EASA Form 1 A Part-145 organisation holding a B-rating approval on a particular engine type and having in its approved scope of work NDT for this engine type. This organisation needs to have “engine” certifying staff (qualified in accordance with company procedures) and NDT personnel qualified in accordance with 145.A.30(f) (EN 4179). In this case the NDT qualified staff perform the NDT task and sign the task card / Work Order / Engineering Order for the accomplishment of the task. The engine certifying