時(shí)間：2015-01-22 15:18來源：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. (b) In addition to (a) above, the CVR and CARS shall start to record as early as possible during the cockpit checks prior to engine start at the beginning of the flight until the cockpit checks immediately following engine shutdown at the end of the flight. (c) The CVR shall record on four separate channels, or more, at least the following: (1) Voice communication transmitted from or received in the aircraft by radio; (2) Aural environment on the flight deck; (3) Voice communication of flight crew members on the flight deck using the aircraft’s interphone system, if installed; (4) Digital communications with ATS, unless recorded by the FDR. (d) The CARS shall record on two separate channels, or more, at least the following: (1) Voice communication transmitted from or received in the aeroplane by radio; (2) Aural environment on the flight deck; and (3) Voice communication of flight crewmembers on the flight deck using the aeroplane’s interphone, if installed. (e) The recorder shall be capable of recording on at least four channels simultaneously, except for the recorder in paragraph 7.8.2.2(a)(4) in the preferred channel allocation as follows: (1) Channel 1 – co-pilot headphones and live boom microphone; (2) Channel 2 – pilot headphones and live boom microphone; (3) Channel 3 – area microphone; (4) Channel 4 – time reference plus the third and fourth crewmembers. Note 1: Channel 1 is located closest to the base of the recording head. Note 2: The preferred channel allocation presumes the use of current conventional magnetic tape transport mechanisms and is specified because the outer edges of the tape have a higher risk of damage than the middle. It is not intended to preclude use of alternative recording media where such constraints may not apply. (f) On a tape-based CVR, to ensure accurate time correlation between channels, the recorder shall record in an in-tine format. If a bi-directional configuration is used, the in-line format and channel allocation shall be retained in both directions. ICAO Annex 6, Part II: Appendix 3.1, paragraph 3.1, 3.1.1; 3.1.2;; 3.1.3 ; 3.1.4 ICAO Annex 6, Part III, Appendix 5, paragraph 3, 3.1 ;3.1.1 ;3.1.2 ; 3.1.3 ; 3.1.4 7.8.3.2 AIRCRAFT EQUIPPAGE FOR OPERATIONS (a) No person may operate an aeroplane unless it is equipped with a cockpit voice recorder as listed below: (1) [AAC] All turbine-engined aeroplanes for which the application for a type certificate is first submitted to the appropriate CAA on or after 1 January 2016 and required to be operated by more than one pilot shall be equipped with either a CVR or a CARS. (2) [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 1987 shall be equipped with a CVR. (3) [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 1987, should be equipped with a CVR. (4) [AOC] All aeroplanes of a maximum certificated take-off mass of over 5 700 kg for which the individual certificate of airworthiness is first issued on or after 1 January 2003, shall be equipped with a CVR capable of retaining the information recorded during at least the last two hours of its operation. (5) [AOC] All aeroplanes of a maximum certificated take-off mass of over 5 700 kg for which the individual certificate of airworthiness is first issued on or after 1 January 1987 shall be equipped with a CVR. (6) [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 shall be equipped with a CVR. (7) [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 up to and including 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 a CVR. ICAO Annex 6, Part I: 6.3.2.1 ICAO Annex 6, Part II, Section II: 2.4.16.2.1.1 ICAO Annex 6, Part II, Section III: 3.6.3.2.1; 3.6.3.2.1.1; 3.6.3.2.1.2; 3.6.3.2.1.3 III: 3.6.3.2; 3.6.3.2.1; 3.6.3.2.1.2; 3.6.3.2.1.3; 3.6.3.2.1.4 (b) No person may operate a helicopter unless it is equipped with a cockpit voice recorder as listed below: (1) [AAC] All helicopters of a maximum certificated take-off mass of over 7 000 kg for which the individual certificate of airworthiness is first issued on or after 1 January 1987 shall be equipped with a CVR. For helicopters not equipped with an FDR, at least main rotor speed shall be recorded on the CVR. (2) [AAC] All helicopters of a maximum certificated take-off mass of over 3 180 kg for which the individual certificate of worthiness is first issued on or after 1 January 1987 should be equipped with a CR. For helicopters not equipped with an FDR, at least main rotor speed shall be recorded on the CVR. (3) [AAC] All helicopters of a maximum certificated take-off mass of over 7 000 kg for which the individual certificate of worthiness is first issued on or after 1 January 1987 should be equipped with a CR. For helicopters not equipped with an FDR, at least main rotor speed shall be recorded on the CVR. ICAO Annex 6, Part III, Section II: 4.3.2.1; 4.3.2.1.1; 4.3.2.1.2; 4.3.2.1.3 ICAO Annex 6, Part III, Section III: 4.7.2.1; 4.7.2.1.1; 4.7.2.1.2; 4.7.2.1.3 7.8.3.3 DISCONTINUATION (a) CVS media not acceptable for use in aircraft registered in [STATE], or operated in commercial air transport operations in [STATE], are— (1) Magnetic tape and wire. ICAO Annex 6, Part I: 6.3.2.2; 6.3.2.2.1; 6.3.2.22 ICAO Annex 6, Part II: Section II: 2.4.16.2.2; 2.4.16.2.2.1; 2.4.16.2.2.2R ICAO Annex 6, Part III, Section II: 4.3.2.2; 4.3.2.2.1; 4.3.2.2.2R ICAO Annex 6, Part III, Section III: 4.7.2.2; 4.7.2.2.1; 4.7.2.2.2 7.8.3.4 DURATION (a) A CVR shall be capable of retaining the information recorded during at least the last— (1) 30 minutes of its operation; or (2) 2 hours, beginning no later than 1 January 2016. ICAO Annex 6, Part I: 6.3.2.3; 6.3.2.3.2; 6.3.2.3.3 ICAO Annex 6, Part II, Section II: 2.4.16.2.3; 2.4.16.2.3.1; 2.4.16.2.3.2; 2.4.16.2.3.3R ICAO Annex 6, Part III, Section II: 4.3.2.3; 4.3.2.3.1; 4.3.2.3.2; 4.3.2.3.3R ICAO Annex 6, Part III, Section II: 4.7.2.3; 4.7.2.3.1; 4.7.2.3.2; 4.7.2.3.3R 7.8.3.5 COCKPIT VOICE RECORDER ALTERNATE POWER (a) [AOC] No person may operate an aeroplane required to be equipped with a CVR unless it is equipped with CVR alternate power that (1) automatically engages and provides ten minutes, plus or minus one minute, of operation whenever aeroplane power to the recorder ceases, either by normal shutdown or by any other loss of power; (2) powers the CVR and its associated cockpit area microphone components, and (3) is located as close as practicable to the alternate power source. (b) [AOC] No person may operate an aeroplane 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 2018 unless is it equipped with an alternate power source, as described in (a) above, that powers– (1) the forward CVR in the case of combination recorders, or (2) at least one CVR. Note 1 – “Alternate” means separate from the power source that normally provides power to the CVR. The use of aeroplane batteries or other power sources is acceptable provided that the requirements are above are met and electrical power to essential and critical loads is not compromised. Note 2 – When the CVR function is combined with other recording functions within the same unit, powering the other functions is allowed. ICAO Annex 6, Part I: 6.3.2.4; 6.3.2.4.1; 6.3.2.4.2; 6.3.2.4.3R and notes 7.8.4 DATA LINK RECORDERS (DLR) AND DATA LINK RECORDING SYSTEMS (DLRS) Note: Data link recorders performance requirements are as contained in the EUROCAE ED-112, Minimum Operational Performance Specifications (MOPS) for Crash Protected Airborne Recorder Systems, or equivalent documents. ICAO Annex 6, Part I: 6.3.3 Note ICAO Annex 6, Part II, Section II: 2.4.16.3 Note 7.8.4.1 APPLICABILITY (a) No person may operate an aeroplane or helicopter for which the individual certificate of airworthiness is first issued on or after 1 January 2016, which utilise any of the data link communications applications listed in IS 7.8.4.1 and are required to carry a CVR, unless the aircraft records on a flight recorder the data link communications messages. (b) No person may operate an aeroplane or helicopter modified on or after 1 January 2016, which utilise any of the data link communications applications listed in IS 7.8.4.1 and are required to carry a CVR, unless the aircraft records on a flight recorder the data link communications messages. (c) No person may operate an aeroplane or helicopter where the aircraft flight path is authorised or controlled through the use of data link messages, unless all data link messages, both uplinks (to the aircraft) and downlinks from the aircraft) are recorded on the aircraft. As far as practicable, the time the messages were displayed to the flight crew and the time of the responses shall be recorded. Note 1: Data link communications are currently conducted by either ATN-based or FANS 1/A-equipped aircraft. |
