時(shí)間：2015-01-22 15:18來(lái)源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (d) When the Authority determines that an airframe or aeronautical product has exhibited an unsafe condition and that condition is likely to exist or to develop in other products of the same type design, the Authority may issue an Airworthiness Directive prescribing inspections and the conditions and limitations, if any, under which those products may continue to be operated. (e) The Authority shall report any airworthiness directives or continuing additional airworthiness requirements that it issues or any malfunction or defect reports to the State of Design. ICAO Annex 8, Part II: Chapter 4: 4.2.3(d)(e)(f); 4.2.4 ICAO Doc. 9388: Chapter 3, Section 2: 2.3.3 14 CFR: 39.1, 39.3, 39.7; 43.3, 91.403(c); 121.363 JAR-OPS 1: 1.890 5.4.1.3 RESPONSIBILITY (a) The owner of an aircraft or, in the case of a leased aircraft, the lessee, shall be responsible for maintaining the aircraft in an airworthy condition by ensuring that— (1) All maintenance, overhaul, modifications and repairs which affect airworthiness are performed as prescribed by the State of Registry; (2) Maintenance personnel make appropriate entries in the aircraft maintenance records certifying that the aircraft is airworthy; (3) The approval for return to service (maintenance release) is completed to the effect that the maintenance work performed has been completed satisfactorily and in accordance with the prescribed methods; and (4) In the event there are open discrepancies, the maintenance release includes a list of the uncorrected maintenance items for which temporary relief of provided in the MEL and these items are made a part of the aircraft permanent record. (b) The owner or operator of an aeroplane over 5, 700 kg maximum certificated take-off mass shall obtain and assess continuing airworthiness information and recommendations available from the organisation responsible for the type design and shall implement resulting actions considered necessary in accordance with a procedure acceptable to the Authority. ICAO Annex 6: Part I: Chapter 8: 8.1.1; 8.1.2; 8.1.3; 8.1.5.2 ICAO Annex 6, Part II Section II: 2.6 ICAO Annex 6, Part II Section III: 3.8.5 ICAO Annex 6, Part III, Section II: 6.1.1; 6.1.2; 6.1.3; 6.1.3 ICAO Annex 6, Part III Section III: 6.1.1; 6.1.2; 6.1.3 14 CFR: 91.403; 91.405; 121.363 JAR-OPS 1: Subpart M 5.4.1.4 MAINTENANCE AND OPERATIONAL EXPERIENCE (a) The owner or operator of an aeroplane over 5, 700 kg maximum certificated take-off mass shall monitor and assess maintenance and operational experience with respect to continuing airworthiness and have a system whereby information on faults, malfunctions, defects and other occurrences that cause or might cause adverse effects on the continuing airworthiness of the aircraft is transmitted to the organisation responsible for the type design of the aircraft. (b) The owner or operator and maintenance organisations shall report to the Authority in respect of aeroplanes over 5,700 kg and helicopters over 3,175 kg maximum certificated take-off mass the service information required by the authority according to the procedure, established by the Authority. (c) The owner or operator and maintenance organisations shall transmit to the organisation responsible for the type design of aircraft respect of aeroplanes over 5, 700 kg and helicopters over 3, 175 kg maximum certificated take-off mass information on faults, malfunction, defects and other occurrences that cause or might cause adverse effect on the continuing airworthiness of the aircraft. ICAO Annex 6: Part 1, 8.5.1 ICAO Annex 8, Part 2, 4.2.3 (f) 5.4.1.5 REPORTING OF FAILURES, MALFUNCTIONS, AND DEFECTS (a) Owners or operators of aircraft over 5,700 kg maximum take-off weight shall report to the Authority any failures, malfunctions, or defects that result in at least the following— (1) Fires during flight and whether the related fire-warning system properly operated; (2) Fires during flight not protected by a related fire-warning system; (3) False fire warning during flight; (4) An engine exhaust system that causes damage during flight to the engine, adjacent structure, equipment, or components; (5) An aircraft component that causes accumulation or circulation of smoke, vapour, or toxic or noxious fumes in the crew compartment or passenger cabin during flight; (6) Engine shutdown during flight because of flameout; (7) Engine shutdown during flight when external damage to the engine or aircraft structure occurs; (8) Engine shutdown during flight due to foreign object ingestion or icing; (9) Shutdown during flight of more than one engine; (10) A propeller feathering malfunction or inability of the system to control overspeed during flight; (11) A fuel or fuel-dumping system failure that affects fuel flow or causes hazardous leakage during flight; (12) An unintended landing gear extension or retraction, or opening or closing of landing gear doors during flight; (13) Brake system components failure that result in loss of brake actuating force when the aircraft is in motion on the ground; (14) Aircraft structure that requires major repair; (15) Cracks, permanent deformation, or corrosion of aircraft structure, if more than the maximum acceptable to the manufacturer or the Authority; (16) Aircraft components or systems malfunctions that result in taking emergency actions during flight (except action to shut down an engine); (17) Each interruption to a flight, unscheduled change of aircraft en route, or unscheduled stop or diversion from a route, caused by known or suspected technical difficulties or malfunctions; (18) Any abnormal vibration or buffeting caused by a structural or system malfunction, defect, or failure; and (19) A failure or malfunction of more than one attitude, airspeed, or altitude instrument during a given operation of the aircraft (b) Owners or operators of aircraft over 5,700 kg maximum take-off weight shall report to the Authority— (1) The number of engines removed prematurely because of malfunction, failure or defect, listed by make and model and the aircraft type in which it was installed; and (2) The number of propeller featherings in flight, listed by type of propeller and engine and aircraft on which it was installed. (i) Each report required by this Subsection shall— (ii) Be made within 3 days after determining that the failure, malfunction, or defect required to be reported has occurred; and (iii) Include as much of the following information as is available and applicable— (iv) Aircraft serial number; (v) When the failure, malfunction, or defect is associated with an article approved under a TSO authorisation, the article serial number and model designation, as appropriate; (vi) When the failure, malfunction or defect is associated with an engine or propeller, the engine or propeller serial number, as appropriate; (vii) Product model; (viii) Identification of the part, component, or system involved, including the part number; and (ix) Nature of the failure, malfunction, or defect (c) The Authority, if it is the Authority of the State of Registry of the aircraft, will submit all such reports upon receipt to the State of Design. (d) The Authority, if it is not the Authority of the State of Registry of the aircraft, will submit all such reports upon receipt to the State of Registry. Note: If the State of Design and the State of Manufacture are different countries, ICAO Annex 8, Part 2, Chapter 4: 4.2.1.1(d) requires the State of Design and the State of Manufacture to have a mutual arrangement for the transmission of continuing airworthiness information for appropriate action on the part of each country. ICAO Annex 8, Part II: Chapter 4: 4.2.3(e),(f) ICAO Doc. 9760 Chapter 2: 2.7 14 CFR: 121.703 5.5 AIRCRAFT MAINTENANCE AND INSPECTION REQUIREMENTS Note: FAA AC 43.13-1B, Acceptable Methods, Techniques, and Practices – Aircraft Inspection and Repair, is an example of an acceptable standard for the inspection and repair of non-pressurised aircraft when there are no manufacturer repair or maintenance instructions. FAA AC 43.13-2A, Acceptable Methods, Techniques and Practices – Aircraft Modifications, contains acceptable methods for modification of non-pressurised aircraft when there are no manufacturer repair or maintenance instructions. 5.5.1.1 APPLICABILITY (a) This Subpart prescribes rules governing the maintenance and inspection of any aircraft having a Certificate of Airworthiness issued by [STATE] or associated aeronautical products. 14 CFR: 43.1 5.5.1.2 GENERAL REQUIREMENTS FOR MAINTENANCE AND INSPECTIONS (a) No person may operate an aircraft unless the aircraft and its components are maintained in accordance with a maintenance program and the aircraft is inspected according to an inspection program approved by the Authority. (b) The maintenance program shall include a description of the aircraft and components and recommended methods for the accomplishment of maintenance tasks. Such information shall include guidance on defect diagnosis. (c) The maintenance program shall include the maintenance tasks and the recommended intervals at which these tasks are to be performed. (d) Maintenance tasks and frequencies that have been specified as mandatory by the State of Design in approval of the type design shall be identified in the maintenance program. (e) The maintenance program shall have a maintenance release process, including signed documentation, in a manner satisfactory to the Authority, indicating that the maintenance performed has been completed satisfactorily. A maintenance release shall contain a certification including— (1) Basic details of the maintenance carried out; |
