時間：2015-01-22 15:18來源：藍天飛行翻譯公司 作者：民航翻譯 點擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (2) If the aircraft is away from the station where inspections are normally conducted, an appropriately rated AMT, an AMO or the manufacturer of the aircraft may perform inspections in accordance with the procedures and using the forms of the person who would otherwise perform the inspection. (e) Continuous airworthiness maintenance program inspections (1) Each person performing the inspection program required for an AOC holder’s aircraft or aircraft maintained under a continuous airworthiness maintenance program, shall perform the inspection in accordance with the instructions and procedures set forth in the inspection program. 14 CFR: 43.15; 121.369 5.5.1.8 PERFORMANCE RULES: AIRWORTHINESS LIMITATIONS (a) Each person performing an inspection or other maintenance specified in an airworthiness limitations section of a current manufacturer's maintenance manual, or Instructions for Continued Airworthiness, shall perform the inspection or other maintenance in accordance with that section, or in accordance with specifications approved by the Authority. 14 CFR: 21.50(b); 43.16; 121.369 5.6 MAINTENANCE AND INSPECTION RECORDS AND ENTRIES 5.6.1.1 CONTENT, FORM, AND DISPOSITION OF RECORDS FOR MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, AND MODIFICATION OF AIRCRAFT AND LIFE LIMITED PARTS (a) Each person who maintains, performs preventive maintenance, rebuilds, or modify an aircraft or life limited parts shall, when the work is performed satisfactorily, make an entry in the maintenance record of that equipment as follows— (1) A description (or reference to data acceptable to the Authority) of work performed, including- (i) The total time in services (hours, calendar time and cycles, as appropriate) of the aircraft and all life-limited components; (ii) The current status of compliance with all mandatory continuing airworthiness information; (iii) Appropriate details of modifications and repairs; (iv) Time in service (hours, calendar time and cycles, as appropriate) since last overhaul of the aircraft or its components subject to a mandatory overhaul life; (v) The current status of the aircraft’s compliance with the maintenance program; and the detailed maintenance records to show that all requirements for signing of a maintenance release have been met. (2) Completion date of the work performed; (3) Name, signature, certificate number, and kind of licence held by the person approving the work Note: The signature constitutes the approval for return to service only for the work performed. (b) In addition to the entry required by paragraph (a), major repairs and modifications shall be entered on a form, and the form disposed of, in the manner prescribed in IS: 5.7.1.1, by the person performing the work. ICAO Annex 6: Part I: 8.4.1 ICAO Annex 6, Part II, Section II: 2.6.2: ICAO Annex 6 Part II Section III: 3.11.1 ICAO Annex 6, Part III, Section II: 6.4.1; 6.8.1 ICAO Annex 6, Part III, Section III: 6.2.1 ICAO Annex 6, Part I: 8.4.1 ICAO Annex 6, Part III, Section II: 6.7.1; 6.7.2 ICAO Annex III, Section III: 6.5.1; 6.5.2 14 CFR: 43.9, 121.380 JAR-OPS 1: 1.920 5.6.1.2 CONTENT, FORM AND DISPOSITION OF RECORDS FOR MAINTENANCE, PREVENTIVE MAINTENANCE, OVERHAUL, MODIFICATION AND REBUILDING OF A PRODUCT (a) No person shall approve for return to service any aeronautical product that has undergone maintenance, preventive maintenance, overhaul modification or rebuilding of a product unless— (1) The appropriate maintenance record entry has been made; (2) The repair or modification form authorised by or furnished by the Authority has been executed in a manner prescribed by the Authority; (3) If a repair or modification 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 are appropriately revised and set forth as prescribed. ICAO Annex 6, Part I: 8.1.2; 8.1.3 ICAO Annex 6, Part II, Section II: 2.6.2, 2.6.3 ICAO Annex 6, Part II, Section III: 3.11.1 ICAO Annex 6, Part III, Section II: 6.1.2; 6.1.3 ICAO Annex 6, Part III, Section III: 6.12.; 6.1.3 14 CFR: 43.7; 43.11;145.201; 121.369 (b) Additional entries for overhaul and rebuilding. (1) No person shall describe in any required maintenance entry or form, an aeronautical product as being overhauled or rebuilt unless— (i) It has been disassembled, cleaned, inspected as permitted, repaired as necessary, and reassembled using methods, techniques, and practices acceptable to the Authority; and (ii) 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 manufacturing approval. (2) No person shall describe in any required maintenance entry or form an aircraft or other aeronautical product as being rebuilt unless it has been disassembled, cleaned, inspected as permitted, repaired as necessary, reassembled, and tested to the same tolerances and limits as a new item, using either new parts or used parts that conform to new part tolerances and limits. (c) If the maintenance, preventive maintenance, overhaul, modification or rebuilding of a product is performed by an AMO, the AMO shall complete an airworthiness approval tag (CAA form) as prescribed in Part 6. ICAO Annex 6, Part I: 8.4.1(c);8.6 ICAO Annex 6, Part II, Section II: 2.6.2(c), 2.6.3 ICAO Annex 6: Part III: Section II: 6.4.1(c);6.4 ICAO Annex 6, Part III, Section III: 6.2.1(c); 6.4 14 CFR: 43.2 5.6.1.3 CONTENT, FORM, AND DISPOSITION OF RECORDS OF INSPECTIONS FOR RETURN TO SERVICE (a) Inspection record entries. The person approving or disapproving the return to service of an aeronautical product after any inspection performed in accordance with Part 8, shall make an entry in the maintenance record of that equipment containing the following information— (1) Type of inspection and a brief description of the extent of the inspection; (2) Date of the inspection and aircraft or component total time in service; (3) Signature, the licence number, and kind of licence held by the person approving or disapproving for return to service the aeronautical product; (4) If the aircraft or component is found to be airworthy and approved for return to service, the following or a similarly worded statement— “I certify that this aircraft/ component has been inspected in accordance with (insert type) inspection and was determined to be in airworthy condition”; (5) If the aircraft or component 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/component 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 program provided for in Part 8, the person performing the inspection shall make an entry identifying the inspection program accomplished, and containing a statement that the inspection was performed in accordance with the inspections and procedures for that particular program. (b) Listing of discrepancies. The person performing any inspection required in Part 8 who find 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, shall give the owner/operator a signed and dated list of those discrepancies. ICAO Annex 6, Part I: 8.1.2; 8.1.3 ICAO Annex 6, Part II, Section II: 2.6.4 ICAO Annex 6, Part II, Section III: 3.8.5 ICAO Annex 6, Part III, Section II: 6.1.2; 6.1.3 ICAO Annex 6, Part III, Section III: 6.12.; 6.1.3 14 CFR: 43.11 MODEL CIVIL AVIATION REGULATIONS PART 5 — IMPLEMENTING STANDARDS [STATE] VERSIONS 2.8 NOVEMBER 2014 PART 5 — IMPLEMENTING STANDARDS IS: 5.1.1.2 MODIFICATION, REPAIRS AND PREVENTIVE MAINTENANCE IS: 5.1.1.2(A)(8) MAJOR MODIFICATIONS (a) Airframe Major Modifications. Major modifications include modifications to the listed aircraft parts, or the listed types of modifications (when not included in the applicable manufacturer specifications or type certificate data sheet (TCDS)— (1) Wings. (2) Tail surfaces. (3) Fuselage. (4) Engine mounts. (5) Control system. (6) Landing gear. (7) Hull or floats (8) Elements of an airframe including spars, ribs, fittings, shock absorbers, bracing, cowlings, fairings, and balance weights. (9) Hydraulic and electrical actuating system of components. (10) Rotor blades. (11) Changes to the empty weight or empty balance which result in an increase in the maximum Certified weight or centre of gravity limits of the aircraft. (12) Changes to the basic design of the fuel, oil, cooling, heating, cabin pressurisation, electrical, hydraulic, de-icing, or exhaust systems. (13) Changes to the wing or to fixed or movable control surfaces which affect flutter and vibration characteristics. (b) Powerplant Major Modifications. Major powerplant modifications, even when not listed in the applicable engine specifications, include— (1) Conversion of an aircraft engine from one approved model to another, involving any changes in compression ratio, propeller reduction gear, impeller gear ratios or the substitution of major engine parts which requires extensive rework and testing of the engine. |
