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CERTIFICATE OF RELEASE TO SERVICE For PART 66 (PART M Subpart H, M.A.801) CRS Nr.: Registration: OO- Owner: Maintenance location: Manufacturer Type Serial N° Time Time Time since since since new OH last insp. Aircraft Engine 1 2 Propeller1 2 Aircraft MTOW: Maintenance type: Scheduled Unscheduled Repair / Modification Maintenance data (Approved AMP reference, AMP review date and detailed information of used documentation) Calibrated and/or (Tool identification, range and last calibration date) special tools Item Work performed: (Detailed description maintenance carried out, replaced parts, approved repairs/modifications, certificate references, etc….) Nr. (Performance of Complex tasks, as listed in Appendix VII to PART M, are prohibited, except for ELA1 aircraft) 1 2 3 4 5 6 7 Independent inspection performed for item Nr.: Deferred defects/items: Limitations: Certifies that the work specified except as otherwise specified was carried out in accordance with Part-M and in respect to that work the aircraft is considered ready for release to service. Starting Date: Signature: Name Certifying staff: Closing Date: Part 66 licence number: Valid until: CRS Aircraft logbook: Contact: o Copy CAMO o Copy Owner o Copy BCAA Page 1 OF 2 BCAA DOC_C-GEN/CRS-P66-01 01/01/2012 EASA Verordening 2043/2003 Part M Subpart H CERTIFICATE OF RELEASE TO SERVICE – CRS M.A.801 Aircraft certificate of release to service a. a valid ICAO Annex 1 compliant maintenance license for the aircraft type (a) Except for aircraft released to service by a maintenance organisation requiring certification, or; approved in accordance with Annex II (Part-145), the certificate of release to b. a certifying staff authorisation valid for the work requiring certification, issued service shall be issued according to this Subpart; by an ICAO Annex 6 approved maintenance organisation. (b) No aircraft can be released to service unless a certificate of release to service 3. A release in accordance with this paragraph does not affect the controlled is issued at the completion of any maintenance, when satisfied that all environment of the aircraft as long as the M.A.801(d)2 recheck and release has maintenance required has been properly carried out, by: been carried out by an approved maintenance organisation. 1. appropriate certifying staff on behalf of the maintenance organisation approved AMC M.A.801 (f) Aircraft certificate of release to service in accordance with Section A, Subpart F of this Annex (Part M); or 1. The aircraft certificate of release to service should contain the following 2. certifying staff in compliance with the requirements laid down in Annex III (Part- statement: 66), except for complex maintenance tasks listed in Appendix VII to this Annex for (a) ‘Certifies that the work specified except as otherwise specified was carried out which point 1 applies; or in accordance with Part-M and in respect to that work the aircraft is considered 3. by the Pilot-owner in compliance with point M.A.803; ready for release to service’. (c) By derogation from point M.A.801(b)2 for ELA1 aircraft not used in (b) For a Pilot-owner a certificate of release to service should contain the commercial air transport, aircraft complex maintenance tasks listed in Appendix following statement: VII may be released by certifying staff referred to in point M.A.801(b)2; ‘Certifies that the limited pilot-owner maintenance specified except as otherwise (d) By derogation from point M.A.801(b), in the case of unforeseen situations, specified was carried out in accordance with Part M and in respect to that work when an aircraft is grounded at a location where no approved maintenance the aircraft is considered ready for release to service’. organization appropriately approved under this Annex or Annex II (Part-145) and 2. The certificate of release to service should relate to the task specified in the no appropriate certifying staff are available, the owner may authorise any person, manufacturer’s or operator’s instruction or the aircraft maintenance programme with not less than three years of appropriate maintenance experience and holding which itself may cross-refer to a manufacturer’s/operator’s instruction in a the proper qualifications, to maintain according to the standards set out in maintenance manual, Subpart D of this Annex and release the aircraft. The owner shall in that case: service bulletin etc. 1. obtain and keep in the aircraft records details of all the work carried out and of 3. The date such maintenance was carried out should include when the the qualifications held by that person issuing the certification; and maintenance took place relative to any life or overhaul limitation in terms of 2. ensure that any such maintenance is rechecked and released by an date/flying hours/ cycles/landings etc., as appropriate. appropriately authorised person referred to in point M.A.801(b) or an organisation 4. When extensive maintenance has been carried out, it is acceptable for the approved certificate of release to service to summarise the maintenance so long as there is in accordance with Section A, Subpart F of this Annex (Part M), or with Annex II a unique cross-reference to the work-pack containing full details of maintenance (Part-145) at the earliest opportunity but within a period not exceeding seven carried out. days; and Dimensional information should be retained in the work-pack record. 3. notify the organisation responsible for the continuing airworthiness 5. The person issuing the certificate of release to service should use his normal management of the aircraft when contracted in accordance with point M.A.201(e), signature except in the case where a computer release to service system is used. or the competent authority in the absence of such a contract, within seven days of In this latter case the competent authority will need to be satisfied that only the the particular person can electronically issue the release to service. One such issuance of such certification authorisation; method of compliance is the use of a magnetic or optical personal card in (e) In the case of a release to service in accordance with point M.A.801(b)2 or conjunction with a personal identity number (PIN) known only to the individual, point M.A.801(c), the certifying staff may be assisted in the execution of the which is keyed into the computer. maintenance tasks by one or more persons subject to his/her direct and A certification stamp is optional. continuous control 6. At the completion of all maintenance, owners, certifying staff, operators and (f) A certificate of release to service shall contain as a minimum: maintenance organisations should ensure they have a clear, concise, legible 1. basic details of the maintenance carried out; and record of the work performed. 2. the date such maintenance was completed; and 7. In the case of an M.A.801 (b) 2 release to service, certifying staff should retain 3. the identity of the organisation and/or person issuing the release to service, allrecords necessary to prove that all requirements have been met for the including: issuance of a certificate of release to service. (i) the approval reference of the maintenance organisation approved in AMC M.A.801 (g) Aircraft certificate of release to service accordance with Section A, Subpart F of this Annex (Part M) and the certifying 1. Being unable to establish full compliance with sub-paragraph M.A.801 (b) staff issuing such a certificate; or means that the maintenance required by the aircraft owner or M.A. Subpart G (ii) in the case of point M.A.801(b)2 or M.A.801(c) certificate of release to service, organization could not be completed due either to running out of available aircraft the identity and if applicable licence number of the certifying staff issuing such a maintenance downtime for the scheduled check or by virtue of the condition of certificate; the aircraft requiring additional maintenance downtime. 4. the limitations to airworthiness or operations, if any. 2. The aircraft owner or M.A. Subpart G organisation is responsible for ensuring (g) By derogation from paragraph (b) and notwithstanding the provisions of that all required maintenance has been carried out before flight. Therefore an paragraph (h), when the maintenance prescribed cannot be completed, a aircraft owner or M.A. Subpart G organisation should be informed and agree to certificate of release to service may be issued within the approved aircraft the deferment of full compliance with M.A.801 (b). The certificate of release to limitations. Such fact together service may then be issued subject to details of the deferment, including the with any applicable limitations of the airworthiness or the operations shall be aircraft owner or M.A. Subpart G organisation authorisation, being endorsed on entered in the aircraft certificate of release to service before its issue as part of the certificate. the information required in paragraph (f)4; 3. If a certificate of release to service is issued with incomplete maintenance a (h) A certificate of release to service shall not be issued in the case of any known record should be kept stating what action the mechanic, supervisor and certifying noncompliance which endangers flight safety. staff should take to bring the matter to the attention of the relevant aircraft owner AMC M.A.801 (b) Aircraft certificate of release to service of M.A. Subpart G organisation so that the issue may be discussed and resolved A certificate of release to service is necessary before flight, at the completion of with the aircraft owner or M.A. Subpart G organisation. any defect rectification, whilst the aircraft operates a flight between scheduled AMC M.A.801 (h) Aircraft certificate of release to service maintenance checks. ‘Endangers flight safety’ means any instance where safe operation could not be AMC M.A.801 (d) Aircraft certificate of release to service assured or which could lead to an unsafe condition. It typically includes, but is not 1. “3 years of appropriate maintenance experience” means 3 years working in an limited to, significant cracking, deformation, corrosion or failure of primary aircraft maintenance environment on at least some of the aircraft type systems structure, any evidence of burning, electrical arcing, significant hydraulic fluid or corresponding to the aircraft endorsed on the aircraft maintenance license or on fuel leakage and any emergency system or total system failure. An airworthiness the certifying staff authorisation that the person holds. directive overdue for compliance is also considered a hazard to flight safety. 2. “Holding the proper qualifications” means holding either: Page 2 OF 2 BCAA DOC_C-GEN/CRS-P66-01 01/01/2012
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