CAP 08 CERTIFICATE OF AIRWORTHINESS INDEX
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CAP 08 CERTIFICATE OF AIRWORTHINESS INDEX Section Title Page No. INDEX... i LIST OF ABBREVIATIONS... ii 1. INTRODUCTION... 1 2. SUPPORTING DOCUMENTATION CHECKLIST... 1 2.1 Items Required Once Available... 1 2.2 Items Required at the Time of the Aircraft Inspection... 2 2.3 Items Required Prior to Operation... 4 3. SUPPORTING DOCUMENTATION CHECKLIST FOR THE RENEWAL OF A C OF A... 5 3.1 Items Required at the Time of the Aircraft Renewal Inspection... 5 CAP 08 Rev. N 01 i 01 March 2013
LIST OF ABBREVIATIONS AD AMOC: APU: CVR: DTA: FDR: LOPA: MRI: NAA: SB: SRM: Airworthiness Directive Alternative Means of Compliance Auxiliary Power Unit Cockpit Voice Recorder Damage Tolerant Analysis Flight Data Recorder Layout of Passenger Accommodations Maintenance Requirement Item (e.g. CMR items) National Aviation Authority Service Bulletin Structural Repair Manual CAP 08 Rev. N 01 ii 01 March 2013
1. INTRODUCTION This document is a guide for the person or organisation who will be presenting an aircraft and its associated records to a San Marino Inspector authorised to make a recommendation that the Certificate of Airworthiness be issued or renewed. The person presenting the aircraft and its records would normally be the owner/operator s Airworthiness Coordinator, unless different arrangements are agreed on an individual basis in advance with the Authority. The Airworthiness Coordinator is responsible, prior to the aircraft inspection, for ensuring that the aircraft and its associated records meet Authority standards and requirements. Please contact the Authority if any of the items listed cannot be satisfied. The aircraft must be positioned at an acceptable location, usually an MRO, and have either aircraft or ground power available. It may be necessary to open cowlings and panels to facilitate the inspection. 2. SUPPORTING DOCUMENTATION CHECKLIST 2.1 Items Required Once Available The following items 1 through 2 should be provided to the Authority when available preferably during the aircraft inspection to prevent delays in issuing the Certificates of Registration, Certificate of Airworthiness, Noise Certificates and Designated Airspace approvals. No. Item Requirement Completed An Export C of A, or an equivalent, should be available in the form of: 1. Export Certificate of Airworthiness or Equivalent Document For newly manufactured aircraft (a) For EASA Member State aircraft types, a Statement of Conformity (EASA Form 52). If available, an Export C of A should also be submitted. (b) For aircraft constructed outside of the European Union, an Export C of A issued by the State of Manufacturer is required. For used aircraft (a) A Certificate of Airworthiness for Export issued by the last State of Registry will be required. (b) In some instances National Aviation Authorities do not issue Certificates of Airworthiness for export. In these cases, a current domestic C of A and a statement signed by the last State of Registry confirming that the aircraft and its associated records has been examined, and as this date the aircraft complies with the TCDS and is airworthy. (c) Aircraft imported from an EASA Member State, a Certificate of Airworthiness (C of A) along with a current Airworthiness Review Certificate (ARC). CAP 08 Rev. N 01 1 01 March 2013
2. Deregistration or a Statement of Non-Registration Note : Export C of A or equivalent document issued by the last State of Registry will normally only be considered valid if received by the Authority within 60 days of the date of issue. An aircraft cannot be on more than one Register at any one time. If the aircraft is new and has not been previously registered, then a statement of non-registration is required from the NAA of the State of Manufacturer. For used aircraft a statement of deregistration is required from the NAA of the last State of Registry. 2.2 Items Required at the Time of the Aircraft Inspection The following items 3 through 25 must be available to the Authority Airworthiness Inspector at the time of the aircraft inspection. 3. 4. 5. 6. 7. 8. Type Certificate Data Sheet Manufacturing Certificate of Conformity (applicable to new aircraft) Concessions or design deviations arising during manufacture (applicable to new aircraft) Service Bulletin Status Major Modifications (Supplemental Type Certificates) Other Modifications Confirmation that the Authority accepted Type Certificate Data Sheet is applicable and that the aircraft conforms to it. If the aircraft is new and being delivered from the factory, a copy of the manufacturer s conformity statement should be provided. For EASA Member State types this is an EASA Form 52. For new aircraft, any information on concessions or design deviations should be available to the Authority Inspector to review. Service Bulletin status list detailing SBs embodied or applied and date of embodiment. (separate list for airframe, engine, propeller, APU and equipment) Current list of all Major Modifications STCs) embodied during the life of the aircraft, including any Information for continuing airworthiness, design records and embodiment records. ) A list of all other modifications embodied on the aircraft that are not SBs or STCs, including their method of approval and date of embodiment. ) CAP 08 Rev. N 01 2 01 March 2013
9. 10. 11. 12. 13. 14. 15. 16. Major Repairs (repairs outside of the SRM) Airworthiness Directives Life Limited Parts (LLP) Maintenance Programme Next Due List engines Landing Gear APU Airframe, Engine, APU and Propeller Log Books 17. Weighing Report 18. Weight Schedule 1. Current list of all major repairs embodied during the life of the aircraft including their categorisation if subject to a Damage Tolerant Analysis. 2. The maintenance records associated with any major repairs including their method of approval. 1. Airworthiness Directive status list for the aircraft, engines, APU and equipment, signed and dated at the time of the Authority inspection. The list should state the date of compliance and the means of compliance with the AD. 2. Original records of all accomplished Airworthiness Directives (work orders, certified Task Cards, logbook entries, etc. Current life limited component status list showing when fitted and when the life expires. A list of all the tasks from the Authority accepted Maintenance Programme showing when they were last performed and when they are next due to be performed. The s of the Engines installed should be available for review by the Authority Airworthiness Inspector. The s of the Landing Gears installed should be available for review by the Authority Inspector. The s of the APU installed should be available for review by the Authority Inspector. 1. All required Log books, including historical Log Books, should be available for the Authority Inspector to review. 2. All Log Book entries should be up to date to include the latest maintenance, flying hours and cycles. 3. Any associated maintenance records (work orders, work packs etc.) including their certification should be made available for review by the Authority Inspector Note: An alternative system to hard copy Log Books may be acceptable to the Authority. The latest weighing report should be made available for review by the Authority Airworthiness Inspector. Note: The aircraft must have been weighed during the preceding 5 years. The Weight Schedule should be available and demonstrate that it contains the latest weighing report and provides details of the variable load (the basic equipment installed) that will then be used to calculate the disposable load of the aircraft prior to flight. CAP 08 Rev. N 01 3 01 March 2013
19. 20. Passenger cabin configuration Maintenance Requirement Items (MRI) A LOPA showing the current passenger cabin configuration including in particular the location and number of any required emergency equipment should be available for review by the Authority Airworthiness Inspector. If applicable, a list of the Maintenance Requirement Items (e.g. CMR items) showing when they were last accomplished and when next due should be provided for review by the Authority Airworthiness Inspector. 21. Flight Test Report (new aircraft) 22. Flight Manual 23. 24. Placards and markings Registration Marks 25. Fireproof Plate For new aircraft, a copy of the production flight test report should be available for review by the Authority Airworthiness Inspector. The applicable Flight Manual/Pilot Operating Handbook should be available, up to date and include any of the required STC supplements. In addition, confirmation from the manufacturer of the latest revision of the Flight Manual should be available. All required placards and markings must be present and legible. The required registration marks must be present and legible. A fireproof plate bearing the San Marino nationality and registration marks must be affixed to the aircraft in a prominent position near the main entrance to the aircraft. 2.3 Items Required Prior to Operation The following items 26 through 33 are not part of the issuance of the Certificate of Airworthiness, but describe the operational requirements that must be met before the first flight on the San Marino aircraft register. The applicant should however make every effort to complete them before the inspection to prevent delays in flying the aircraft. 26. 27. Airspace Approvals Installed Radio Equipment All Airspace approvals should have been applied for in advance of the Authority aircraft inspection. The applicant must be able to demonstrate that the aircraft and its equipment is compliant with the specific configuration and maintenance requirements. All relevant supporting documents must be available for review. 1. A check should be performed to ensure that the radio equipment fitted is the same as that specified on the application form. 2. All required radio equipment must be of a type approved by the FAA or EASA. CAP 08 Rev. N 01 4 01 March 2013
28. ELT Coding 29. 30. Mode S Transponder Coding Flight Data Recorder Any ELTs carried on board must be programmed and appropriately registered. The aircraft transponders must be programmed with the allocated Address. The correct transmission of the allocated Address must be demonstrated to the satisfaction of the Authority prior to flight. For an aircraft >27,000Kg MTWA confirmation that the FDR is recording satisfactorily must be provided. 31. 32. 33. Cockpit Voice Recorder Operational and Emergency Equipment Maintenance Programme For an aircraft >5,700Kg MTWA confirmation that the CVR is recording satisfactorily must be provided. The aircraft should be appropriately equipped for the intended operations. The Maintenance Programme must be accepted by the Authority. 3. SUPPORTING DOCUMENTATION CHECKLIST FOR THE RENEWAL OF A C OF A 3.1 Items Required at the Time of the Aircraft Renewal Inspection The following items 1 through 9 must be available to the Authority Airworthiness Inspector at the time of the aircraft inspection for the renewal of the C of A. 1. 2. 3. Service Bulletin Status Major Modifications (Supplemental Type Certificates) Other Modifications Service Bulletin status list detailing SBs embodied or applied and date of embodiment. (separate list for airframe, engine, propeller, APU and equipment) Current list of all Major Modifications STCs) embodied during the life of the aircraft, including any Information for continuing airworthiness, design records and embodiment records. ) A list of all other modifications embodied on the aircraft that are not SBs or STCs, including their method of approval and date of embodiment. ) CAP 08 Rev. N 01 5 01 March 2013
4. 5. 6. 7. 8. Major Repairs (repairs outside of the SRM) Airworthiness Directives engines Landing Gear APU 3. Current list of all major repairs embodied during the life of the aircraft including their categorisation if subject to a Damage Tolerant Analysis. 4. The maintenance records associated with any major repairs including their method of approval. 3. Airworthiness Directive status list for the aircraft, engines, APU and equipment, signed and dated at the time of the Authority inspection. The list should state the date of compliance and the means of compliance with the AD. 4. Original records of all accomplished Airworthiness Directives (work orders, certified Task Cards, logbook entries, etc. The s of the Engines installed should be available for review by the Authority Airworthiness Inspector. The s of the Landing Gears installed should be available for review by the Authority Inspector. The s of the APU installed should be available for review by the Authority Inspector. 9. Weight Schedule The Weight Schedule should be available and demonstrate that it contains the latest weighing report and provides details of the variable load (the basic equipment installed) that will then be used to calculate the disposable load of the aircraft prior to flight. For the renewal of the C of A the current weight and balance report should be available for inspection. CAP 08 Rev. N 01 6 01 March 2013