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. (i) a Type II FDR; or (ii) a Class C AIR capable of recording flight path and speed parameters displayed to the pilot(s); or (iii) an ADRS capable of recording the essential parameters defined in the Table in IS 7.8.2.2. Note: Type certificate first issued refers to the date of issuance of the original “Type Certificate” for the aeroplane type, not the date of certification of particular aeroplane variants or derivative models. (2) [AOC] All turbine-engined aeroplanes of a maximum certificated take-off mass of 5 700 kg or less for which the individual certificate of airworthiness is first issued on or after 1 January 2016 shall be equipped with: (i) a Type II FDR; or (ii) a Class C AIR capable of recording flight path and speed parameters displayed to the pilot(s); or (iii) an ADRS capable of recording the essential parameters defined in the Table in IS: 7.8.2.2. (3) [AAC] All aeroplanes of a maximum certificated take-off mass of over 27 000 kg for which the individual certificate of airworthiness is first issued on or after 1 January 1989 shall be equipped with a Type I FDR. (4) [AAC] All aeroplanes of a maximum certificated take-off mass of over 5 700 kg, up to and including 27 000 kg, for which the individual certificate of airworthiness is first issued on or after 1 January 1989, shall be equipped with a Type II FDR. (5) [AOC] All multi-engined turbine-engined aeroplanes of a maximum certificated take-off mass of 5 700 kg or less for which the individual certificate of airworthiness is first issued on or after 1 January 1990 should be equipped with a Type IIA FDR. (6) [AOC] All turbine-engined aeroplanes, for which the individual certificate of airworthiness was first issued on or after 1 January 1987 but before 1 January 1989, with a maximum certificated take-off mass of over 5 700 kg, except those in §7.8.1.2.(h), shall be equipped with an FDR which shall record time, altitude, airspeed, normal acceleration and heading. (7) [AOC] All turbine-engined aeroplanes, for which the individual certificate of airworthiness was first issued on or after 1 January 1987 but before 1 January 1989, with a maximum certificated take-off mass of over 5 700 kg, except those in §7.8.1.2(h), should be equipped with an FDR which shall record time, altitude, airspeed, normal acceleration, heading and such additional parameters as are necessary to determine pitch attitude, roll attitude, radio transmission keying and power on each engine. (8) [AOC] All turbine-engined aeroplanes, for which the individual certificate of airworthiness was first issued on or after 1 January 1987 but before 1 January 1989, with a maximum certificated take-off mass of over 27 000 kg that are of types of which the prototype was certificated by the appropriate national authority after 30 September 1969 shall be equipped with a Type II FDR. (9) [AOC] All turbine-engined aeroplanes, for which the individual certificate of airworthiness was first issued before 1 January 1987, with a maximum certificated take-off mass of over 5 700 kg shall be equipped with an FDR which shall record time, altitude, airspeed, normal acceleration and heading. (10) [AOC] All turbine-engined aeroplanes, for which the individual certificate of airworthiness was first issued before 1 January 1987, with a maximum certificated take-off mass of over 27 000 kg that are of types of which the prototype was certificated by the appropriate national authority after 30 September 1969 should be equipped with an FDR which should record, in addition to time, altitude, airspeed, normal acceleration and heading, such additional parameters as are necessary to meet the objectives of determining: (i) the attitude of the aeroplane in achieving its flight path; and (ii) the basic forces acting upon the aeroplane resulting in the achieved flight path and the origin of such basic forces. (11) [AAC] All aeroplanes of a maximum certificated take-off mass of over 5 700 kg for which the individual certificate of airworthiness is first issued after 1 January 2005 shall be equipped with a Type IA FDR. (12) [AOC] All aeroplanes which are required to record normal acceleration, lateral acceleration and longitudinal acceleration for which the application is for a type certificate is first made to the appropriate CAA on or after 1 January 2016 and which are required to be fitted with an FDR shall record those parameters at a maximum sampling and recording interval of 0.0625 seconds. (13) [AAC] All aeroplanes which are required to record pilot input and/or control surface position of primary controls (pitch, roll, yaw) for which the application for a type certificate is first made to the appropriate CAA on or after 1 January 2016 and which are required to be fitted with an FDR shall record those parameters at a maximum sampling and recording interval of 0.125 seconds. Note: For aeroplanes with control systems in which movement of a control surface will back drive the pilot’s control, “or” applies. For aeroplanes with control systems in which movement of a control surface will not back drive the pilot’s control, “and” applies. In aeroplanes with independent moveable surfaces, each surface needs to be recorded separately. In aeroplanes with independent pilot input on primary controls, each pilot input on primary controls needs to be recorded separately. (b) No person may operate the following helicopter unless it is equipped with a flight data recorder capable of recording the aural environment of the flight deck during flight time. (1) [AAC] All helicopters with a maximum certificated take-off mass of over 3 180 kg for which the individual certificate of airworthiness is first issued on or after 1 January 2016 shall be equipped with a Type IVA FDR. (2) [AAC] All helicopter with a certificated takeoff mass of over 7 000 kg, or having a passenger seating configuration of more than nineteen, for which the individual certificate of airworthiness is first issued on or after 1, January 1989 shall be equipped with a Type IV FDR. (3) [AAC] All helicopters with a maximum certificated take-off mass of over 3 180 kb, up to and including 7 000 kg, for which the individual certificate of airworthiness is first issued on or after 1 January 1989 shall be equipped with a Type V FDR. (4) [AOC] All turbine-engined helicopter of a maximum certificated take-off mass of over 2 250 kg, up to and including 3 180 kb for which the which the application for a type certificate is first made to the appropriate CAA on or after 1 January 2018, unless is it equipped with: (i) A Type IVA FDR; or (ii) A Class C AIR capable of recording fight path and speed parameters displayed to the pilot(s); or (iii) An ADRS capable of recording the essential parameters in the Table in IS: 7.8.2.2. (5) [AOC] All turbine-engined helicopter of a maximum certificated take-off mass of over 3 180 kg or less for which the individual certificate of airworthiness is first issued on or after 1 January 2018, unless is it equipped with: (i) A Type IVA FDR; or (ii) A Class C AIR capable of recording fight path and speed parameters displayed to the pilot(s); or (iii) An ADRS capable of recording the essential parameters in the Table in IS: 7.8.2.2. ICAO Annex 6, Part 1: 6.3.1.2.1; 6.3.1.2.2R; 6.3.1.2.3; 6.3.1.2.4; 6.3.1.2.5; 6.3.1.2.6; 6.3.1.2.7; 6.3.1.2.8; 6.3.2.1.9; 6.3.1.2.10R; 6.3.1.2.11; 6.3.2.1.12; 6.3.1.2.13 ICAO Annex 6, Part II, Section II: 2.4.16.1.2.1; 2.4.16.2.2 ICAO Annex 6, Part II, Section III: 3.6.3.1.1.1; 3.6.3.2.2.1; 3.6.3.1.1.3 ICAO Annex 6, Part III, Section II: 4.3.1.2; 4.3.1.2.1; 4.3.1.2.3; 4.3.1.2.4;4.3.1.2.5R ICAO Annex 6, Part III, Section III: 4.7.1.2; 4.7.1.2.1; 4.7.1.2.2; 4.7.1.2.3 7.8.2.3 DISCONTINUATION (a) Flight data recorder media not acceptable for use in aircraft registered in [STATE], or operated in commercial air transport operations in [STATE], are – (1) Engraving metal foil; (2) Photographic film; (3) Analogue data using frequency modulation (FM); (4) Magnetic tape. ICAO Annex 6, Part I: 6.3.1.3 ICAO Annex 6, Part II,2.4.16.1.3; 2.4.16.1.3.1; 2.4.16.1.3.2R; 2.4.16.1.3.3; 2.4.16.1.3.4; 2.4.16.1.3.5R; ICAO Annex 6, Part III, Section II: 4.3.1.3; 4.3.1.3.1; 4.3.1.3.2; 4.3.1.3.3; 4.3.1.3.4; 4.3.1.3.5; 4.3.1.3.6 ICAO Annex 6, Part III, Section III: 4.7.1.3; 4.7.1.3.1; 4.7.1.3.2; 4.7.1.3.3; 4.7.1.3.4; 4.7.1.3.5; 4.7.1.3.6 7.8.2.4 DURATION (a) FDRs shall be capable of retaining the information recorded during the last-- (1) Type I and II -- 25 hours of operation. (2) Type IIA – 30 minutes of operation. (3) Type IV, IVA and V – 10 hours of operation. ICAO Annex 6, Part I: 6.3.1.4 ICAO Annex 6, Part II, 2.4.16.1.4 ICAO Annex 6, Part III, Section II: 4.3.1.4 ICAO Annex 6, Part III, Section III: 4.7.1.4 7.8.3 COCKPIT VOICE RECORDERS (CVR) AND COCKPIT AUDIO RECORDING SYSTEMS (CARS) Note 1: CVR performance requirements are as contained in the EUROCAE ED-112, Minimum Operational Performance Specification (MOPS) for Crash Protected Airborne Recorder Systems, or equivalent documents. Note 2: CARS performance requirements are as contained in the EUROCAE ED-155, Minimum Operational Performance Specification (MOPS) for Lightweight Flight Recording Systems, or equivalent documents. ICAO Annex 6, Part I: 6.3.2 Notes ICAO Annex 6, Part II, Section II: 2.4.16.2 Notes ICAO Annex 6, Part III, Section II: 4.3.2 Note ICAO Annex 6, Part III, Section III: 4.7.2 Note 7.8.3.1 SIGNALS TO BE RECORDED – CVR AND CARS (a) The CVR, and CARS as applicable to aeroplanes, shall start to record prior to the aircraft moving under its own power and record continuously until the termination of the flight when the aircraft is no longer capable of moving under its own power. |
