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. (e) The certification of release to service shall reference the data specified in the manufacturer's maintenance instructions or instructions for continued airworthiness. (f) Where instructions include a requirement to insure that a dimension or test figure is within a specific tolerance as opposed to a general tolerance, the dimension or test figure shall be recorded unless the instruction permits the use of GO/NO gauges. It is not normally sufficient to state that the dimension or the test figure is within tolerance. (g) The date such maintenance was carried out shall include when the maintenance took place relative to any life or overhaul limitation in terms of date/flying hours/cycles/landings etc., as appropriate. (h) When extensive maintenance has been carried out, it is acceptable for the certification of release to service to summarise the maintenance as long as there is a cross-reference to the work package containing full details of maintenance carried out. Dimensional information shall be retained in the work package record. (i) The person issuing the release to service shall use a full signature and preferably a certification stamp except in the case where a computer release to service system is used. In this latter case, the Authority will need to be satisfied that only the particular person can electronically issue the release to service. (j) When a part of component is released to service, the AMO shall complete Model CAA Form AAT as contained in IS: 6.5.1.7. Note: One such method of compliance with item (c)(6) is the use of a magnetic or optical personal card in conjunction with a personal identity number (PIN) which is keyed into the computer and known only to the individual. Note: An aeronautical product which has been maintained off the aircraft requires the issue of a certification of release to service (Model CAA Form AAT) for such maintenance and another certification of release to service of the aircraft in regard to maintenance being properly accomplished on the aircraft. The release to service of the aircraft will typically be made by the AMO in the aircraft technical log maintenance records section. ICAO Doc 9760, Third Edition (2013), Part III, Chapter 10: 10.9 FAA Order 8130.21G; FAA Form 8130-3 14 CFR: 43.5 EASA: 145.A.50 6.5.1.8 MAINTENANCE RECORDS (a) The AMO shall record, in a form acceptable to the Authority, all details for maintenance work performed. (b) The AMO shall provide a copy of each certification of release to service to the aircraft operator, together with a copy of any specific airworthiness data used for repairs/alterations performed. (c) The AMO shall retain a copy of all detailed maintenance records and any associated airworthiness data for two years from the date the aircraft or aeronautical product to which the work relates was released from the AMO. Note: 14 CFR and JAR require retaining maintenance records for two years. ICAO Annex 6, Part I: 8.7.6.2 requires a minimum period of one year. (d) Each person who maintains, performs preventive maintenance, rebuilds, or modifies an aircraft/aeronautical product shall make an entry in the maintenance record of that equipment: (1) A description and reference to data acceptable to the Authority of work performed. (2) The date of completion of the work performed. (3) The name of the person performing the work if other than the person specified in this subsection. (4) If the work performed on the aircraft/aeronautical product has been performed satisfactorily, the signature, certificate number, and kind of certificate held by the person approving the work. (5) The authorised signature, the AMO certificate number, and kind of licence held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof. (6) The signature constitutes the approval for return to service only for the work performed. (7) In addition to the entry required by this paragraph, major repairs and major alterations shall be entered on a form, and the form disposed of by the person performing the work, in the manner prescribed by the Authority in Part 5: 5.7.1.1. (e) No person shall describe in any required maintenance entry or form an aircraft or aeronautical component as being overhauled unless— (1) Using methods, techniques, and practices acceptable to the Authority, it has been disassembled, cleaned, inspected as permitted, repaired as necessary, and reassembled; and (2) It has been tested in accordance with approved standards and technical data, or in accordance with current standards and technical data acceptable to the Authority, which have been developed and documented by the holder of the type certificate, supplemental type certificate, or a material, part, process, or appliance approval under a TSO. (f) No person may describe in any required maintenance entry or form, an aircraft or other aeronautical product as being rebuilt unless it has been— (1) Disassembled, cleaned, inspected as permitted; (2) Repaired as necessary; and (3) Reassembled and tested to the same tolerances and limits as a new item, using either new parts or used parts that either conform to new part tolerances and limits, or to approved oversized or undersized dimensions. (g) No person may approve for return to service any aircraft or aeronautical product that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless— (1) The appropriate maintenance record entry has been made; and (2) The repair or alteration form authorised by or furnished by the Authority has been executed in a manner prescribed by the Authority; (h) If a repair or alteration results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual, those operating limitations or flight data shall be appropriately revised and set forth as prescribed by the Authority. (i) Maintenance record entries for inspections. The person approving or disapproving for return to service an aircraft/aeronautical product, after any inspection performed in accordance with this regulation, shall make an entry in the maintenance record of that equipment containing the following information— (1) The type of inspection and a brief description of the extent of the inspection; (2) The date of the inspection and aircraft total time in service; (3) The authorised signature, the AMO certificate number, and kind of licence held by the person approving or disapproving for return to service the aircraft, airframe, aircraft engine, propeller, appliance, component part, or portions thereof; (4) If the aircraft is found to be airworthy and approved for return to service, the following or a similarly worded statement—I certify that this aircraft has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition; (5) If the aircraft is not approved for return to service because of needed maintenance, non-compliance with the applicable specifications, airworthiness directives, or other approved data, the following or a similarly worded statement—I certify that this aircraft has been inspected in accordance with (insert type) inspection and a list of discrepancies and unairworthy items dated (date) has been provided for the aircraft owner or operator; and (6) If an inspection is conducted under an inspection programme provided for in this regulation, the entry shall identify the inspection programme accomplished, and contains a statement that the inspection was performed in accordance with the inspections and procedures for that particular programme. (j) Listing of discrepancies. If the person performing any inspection required by this regulation finds that the aircraft is not airworthy or does not meet the applicable type certificate data sheet, airworthiness directives, or other approved data upon which its airworthiness depends, that person shall give the owner or lessee a signed and dated list of those discrepancies. ICAO Annex 6, Part 1, 8.7.6.1; 8.7.6.2 ICAO Doc 9760, Third Edition (2013), Part III: Chapter 10: 10.8 14 CFR: 145.219 EASA: 145.A.55 6.5.1.9 AIRWORTHINESS DATA- INSTRUCTIONS FOR CONTINUED AIRWORTHINESS (a) The AMO shall be in receipt of all airworthiness data appropriate to support the work performed from the Authority, the aircraft/aeronautical product design organisation, and any other approved design organisation in the State of Manufacture or State of Design, as appropriate. Note: The Authority may classify data from another authority or organisation as mandatory and may require the AMO to hold such data. (b) Where the AMO modifies airworthiness data specified in paragraph (a) to a format or presentation more useful for its maintenance activities, the AMO shall submit to the Authority an amendment to the AMO Procedures Manual for any such proposed alterations for acceptance. (c) All airworthiness data used by the AMO shall be kept current and made available to all personnel who require access to that data to perform their duties. (d) The IS: 6.5.1.9 contains detailed requirements concerning airworthiness data. ICAO Doc 9760, Third Edition (2013), Part III: Chapter 10: 10.6.2.1 14 CFR: 145.109(d) EASA: 145.A. 45 6.5.1.10 REPORTING OF UNAIRWORTHY CONDITIONS (a) The AMO shall report to the Authority and the aircraft design organisation of the State of Design any identified condition that could present a serious hazard to the aircraft. (b) Reports shall be made on a form and in a manner prescribed by the Authority and contain all pertinent information about the condition known to the AMO. The report shall contain at least the following items— |
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