Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2313

c) unsafe terrain clearance. 6.9.7 Recommendation.— All turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 5 700 kg or authorized to carry more than nine passengers, should be equipped with a ground proximity warning system which has a forward looking terrain avoidance function. 6.10 Flight recorders Note 1.— Flight recorders comprise two systems, a flight data recorder and a cockpit voice recorder. Note 2.— Combination recorders (FDR/CVR) can only be used to meet the flight recorder equipage requirements as specifically indicated in this Annex. Note 3.— Detailed guidance on flight recorders is contained in Attachment A. 6.10.1 Flight data recorders — types 6.10.1.1 A Type I flight data recorder shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power, configuration and operation. 6.10.1.2 A Type II flight data recorder shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power and configuration of lift and drag devices. 6.10.1.3 The use of engraving metal foil flight data recorders shall be discontinued by 1 January 1995. 6.10.1.4 Recommendation.— The use of analogue flight data recorders using frequency modulation (FM) should be discontinued by 5 November 1998. 28/11/02 No. 22 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 5/11/98 6.10.1.4.1 The use of photographic film flight data recorders shall be discontinued from 1 January 2003. 6.10.1.5 All aeroplanes for which the individual certificate of airworthiness is first issued after 1 January 2005, which utilize data link communications and are required to carry a cockpit voice recorder (CVR), shall record on a flight recorder, all data link communications to and from the aeroplane. The minimum recording duration shall be equal to the duration of the CVR, and shall be correlated to the recorded cockpit audio. 6.10.1.5.1 From 1 January 2007, all aeroplanes which utilize data link communications and are required to carry a CVR, shall record on a flight recorder, all data link communications to and from the aeroplane. The minimum recording duration shall be equal to the duration of the CVR, and shall be correlated to the recorded cockpit audio. 6.10.1.5.2 Sufficient information to derive the content of the data link communications message, and, whenever practical, the time the message was displayed to or generated by the crew shall be recorded. Note.— Data link communications include, but are not limited to, automatic dependent surveillance (ADS), controller-pilot data link communications (CPDLC), data linkflight information services (D-FIS) and aeronautical operational control (AOC) messages. 6.10.1.6 Recommendation.— All aeroplanes of a maximum certificated take-off mass over 5 700 kg, required to be equipped with a flight data recorder and a cockpit voice recorder, may alternatively be equipped with two combination recorders (FDR/CVR). 6.10.1.7 A Type IA flight data recorder shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power, configuration and operation. The parameters that satisfy the requirements for a Type IA flight data recorder are listed in the paragraphs below. The parameters without an asterisk (*) are mandatory parameters which shall be recorded. In addition, the parameters designated by an asterisk (*) shall be recorded if an information data source for the parameter is used by aeroplane systems or the flight crew to operate the aeroplane. 6.10.1.7.1 The following parameters satisfy the requirements for flight path and speed: – Pressure altitude – Indicated airspeed or calibrated airspeed – Air – ground status and each landing gear air-ground sensor when practicable – Total or outside air temperature – Heading (primary flight crew reference) – Normal acceleration – Lateral acceleration – Longitudinal acceleration (body axis) – Time or relative time count – Navigation data*: drift angle, wind speed, wind direction, latitude/longitude – Groundspeed* – Radio altitude* 6.10.1.7.2 The following parameters satisfy the requirements for attitude: – Pitch attitude – Roll attitude – Yaw or sideslip angle* – Angle of attack* 6.10.1.7.3 The following parameters satisfy the requirements for engine power: – Engine thrust/power: propulsive thrust/power on each engine, cockpit thrust/power lever position – Thrust reverse status* – Engine thrust command* – Engine thrust target* – Engine bleed valve position* – Additional engine parameters*: EPR, N1, indicated vibration level, N2, EGT, TLA, fuel flow, fuel cut-off lever position, N3 6.10.1.7.4 The following parameters satisfy the requirements for configuration: – Pitch trim surface position – Flaps*: trailing edge flap position, cockpit control selection – Slats*: leading edge flap (slat) position, cockpit control selection – Landing gear*: landing gear, gear selector position – Yaw trim surface position* – Roll trim surface position* – Cockpit trim control input position pitch* – Cockpit trim control input position roll* – Cockpit trim control input position yaw* – Ground spoiler and speed brake*: ground spoiler position, ground spoiler selection, speed brake position, speed brake selection – De-icing and/or anti-icing systems selection* – Hydraulic pressure (each system)* – Fuel quantity* – AC electrical bus status* – DC electrical bus status* – APU bleed valve position* – Computed centre of gravity* 6.10.1.7.5 The following parameters satisfy the requirements for operation: – Warnings – Primary flight control surface and primary flight control pilot input: pitch axis, roll axis, yaw axis – Marker beacon passage 28/11/02 No. 22 2007/70/II. szám Annex 6 — Operation of Aircraft Part II 5/11/98 – Each navigation receiver frequency selection – Manual radio transmission keying and CVR/FDR synchronization reference – Autopilot/autothrottle/AFCS mode and engagement status* – Selected barometric setting*: pilot, first officer – Selected altitude (all pilot selectable modes of operation)* – Selected speed (all pilot selectable modes of operation)* – Selected mach (all pilot selectable modes of operation)* – Selected vertical speed (all pilot selectable modes of operation)* – Selected heading (all pilot selectable modes of operation)* – Selected flight path (all pilot selectable modes of operation)*: course/DSTRK, path angle – Selected decision height* – EFIS display format*: pilot, first officer – Multi-function/engine/alerts display format* – GPWS/TAWS/GCAS status*: selection of terrain display mode including pop-up display status, terrain alerts, both cautions and warnings, and advisories, on/off switch position – Low pressure warning*: hydraulic pressure, pneumatic pressure – Computer failure* – Loss of cabin pressure* – TCAS/ACAS (traffic alert and collision avoidance system/airborne collision avoidance system)* – Ice detection* – Engine warning each engine vibration* – Engine warning each engine over temperature* – Engine warning each engine oil pressure low* – Engine warning each engine over speed* – Wind shear warning* – Operational stall protection, stick shaker and pusher activation* – All cockpit flight control input forces*: control wheel, control column, rudder pedal cockpit input forces – Vertical deviation*: ILS glide path, MLS elevation, GNSS approach path – Horizontal deviation*: ILS localizer, MLS azimuth, GNSS approach path – DME 1 and 2 distances* – Primary navigation system reference*: GNSS, INS, VOR/DME, MLS, Loran C, ILS – Brakes*: left and right brake pressure, left and right brake pedal position – Date* – Event marker* – Head up display in use* – Para visual display on* Note 1.— Parameter requirements, including range, sampling, accuracy and resolution, as contained in the Minimum Operational Performance Specification (MOPS) document for Flight Recorder Systems of the European Organization for Civil Aviation Equipment (EUROCAE) or equivalent documents. Note 2.— The number of parameters to be recorded will depend on aeroplane complexity. Parameters without an (*) are to be recorded regardless of aeroplane complexity. Those parameters designated by an (*) are to be recorded if an information source for the parameter is used by aeroplane systems and/or flight crew to operate the aeroplane. 6.10.2 Flight data recorders — duration Types I and II flight data recorders shall be capable of retaining the information recorded during at least the last 25 hours of their operation. 6.10.3 Flight data recorders — aeroplanes for which the individual certificate of airworthiness is first issued on or after 1 January 1989 6.10.3.1 All aeroplanes of a maximum certificated takeoff mass of over 27 000 kg shall be equipped with a Type I flight data recorder. 6.10.3.2 Recommendation.— All aeroplanes of a maximum certificated take-off mass of over 5 700 kg up to and including 27 000 kg should be equipped with a Type II flight data recorder. 6.10.4 Flight data recorders — aeroplanes for which the individual certificate of airworthiness is first issued after 1 January 2005 All aeroplanes of a maximum certificated take-off mass of over 5 700 kg shall be equipped with a Type IA flight data recorder. 6.10.5 Cockpit voice recorders — aeroplanes for which the individual certificate of airworthiness is first issued on or after 1 January 1987 Note.— Cockpit voice recorder performance requirements are as contained in the Minimum Operational Performance Specifications (MOPS) document for Flight Recorder Systems of the European Organization for Civil Aviation Equipment (EUROCAE) or equivalent documents. 6.10.5.1 All aeroplanes of a maximum certificated takeoff mass of over 27 000 kg shall be equipped with a cockpit voice recorder, the objective of which is the recording of the aural environment on the flight deck during flight time. 6.10.5.2 Recommendation.— All aeroplanes of a maximum certificated take-off mass of over 5 700 kg up to and including 27 000 kg should be equipped with a cockpit voice recorder, the objective of which is the recording of the aural environment on the flight deck during flight time. 28/11/02 No. 22 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 5/11/98 6.10.6 Cockpit voice recorders — duration 6.10.6.1 A cockpit voice recorder shall be capable of retaining the information recorded during at least the last 30 minutes of its operation. 6.10.6.2 Recommendation.— A cockpit voice recorder, installed in 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 1990, should be capable of retaining the information recorded during at least the last two hours of its operation. 6.10.6.3 A cockpit voice recorder, installed in 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 2003, shall be capable of retaining the information recorded during at least the last two hours of its operation. 6.10.7 Flight recorders — construction and installation Flight recorders shall be constructed, located and installed so as to provide maximum practical protection for the recordings in order that the recorded information may be preserved, recovered and transcribed. Flight recorders shall meet the prescribed crashworthiness and fire protection specifications. Note.— Industry crashworthiness and fire protection specifications can be found in documents such as the European Organization for Civil Aviation Equipment (EUROCAE) documents ED55 and ED56A. 6.10.8 Flight recorders — operation 6.10.8.1 Flight recorders shall not be switched off during flight time. 6.10.8.2 To preserve flight recorder records, flight recorders shall be de-activated upon completion of flight time following an accident or incident. The flight recorders shall not be re-activated before their disposition as determined in accordance with Annex 13. Note 1.— The need for removal of the flight recorder records from the aircraft will be determined by the investigation authority in the State conducting the investigation with due regard to the seriousness of an occurrence and the circumstances, including the impact on the operation. Note 2.— The pilot-in-command’s responsibilities regarding the retention of flight recorder records are contained in 6.10.9. 6.10.9 Flight recorder records The pilot-in-command shall ensure, to the extent possible, in the event the aeroplane becomes involved in an accident or incident, the preservation of all related flight recorder records, and if necessary the associated flight recorders, and their retention in safe custody pending their disposition as determined in accordance with Annex 13. 6.10.10 Flight recorders — continued serviceability Operational checks and evaluations of recordings from the flight data and cockpit voice recorder systems shall be conducted to ensure the continued serviceability of the recorders. Note.— Procedures for the inspections of the flight data and cockpit voice recorder systems are given in Attachment A. 6.11 Mach number indicator All aeroplanes with speed limitations expressed in terms of Mach number shall be equipped with a Mach number indicator. Note.— This does not preclude the use of the airspeed indicator to derive Mach number for ATS purposes. 6.12 Emergency locator transmitter (ELT) 6.12.1 Except as provided for in 6.12.2, until 1 January 2005 all aeroplanes operated on extended flights over water as described in 6.3.3 b) and when operated on flights over designated land areas as described in 6.4 shall be equipped with one ELT. 6.12.2 All aeroplanes for which the individual certificate of airworthiness is first issued after 1 January 2002, operated on extended flights over water as described in 6.3.3 b) and when operated on flights over designated land areas as described in 6.4 shall be equipped with one automatic ELT. 6.12.3 From 1 January 2005, all aeroplanes operated on extended flights over water as described in 6.3.3 b) and when operated on flights over designated land areas as described in 6.4 shall be equipped with one automatic ELT. 6.12.4 Recommendation.— All aeroplanes should carry an automatic ELT. 24/11/05 No. 24 16A 2007/70/II. szám Annex 6 — Operation of Aircraft Part II 5/11/98 6.12.5 ELT equipment carried to satisfy the requirements of 6.12.1, 6.12.2, 6.12.3 and 6.12.4 shall operate in accordance with the relevant provisions of Annex 10, Volume III. 6.13 Aeroplanes required to be equipped with a pressure-altitude reporting transponder 6.13.1 From 1 January 2003, unless exempted by the appropriate authorities, all aeroplanes shall be equipped with a pressure-altitude reporting transponder which operates in accordance with the relevant provisions of Annex 10, Volume IV. 6.13.2 Recommendation.— All aeroplanes should be equipped with a pressure-altitude reporting transponder which operates in accordance with the relevant provisions of Annex 10, Volume IV. Note.— The provisions in 6.13.1 and 6.13.2 are intended to support the effectiveness of ACAS as well as to improve the effectiveness of air traffic services. Effective dates for carriage requirements of ACAS are contained in Annex 6, Part I, 6.18.1 and 6.18.2. The intent is also for aircraft not equipped with pressure-altitude reporting transponders to be operated so as not to share airspace used by aircraft equipped with airborne collision avoidance systems. To this end, exemptions from the carriage requirement for pressure-altitude reporting transponders could be given by designating airspace where such carriage is not required. 6.14 Aeroplanes required to be equipped with an airborne collision avoidance system (ACAS II) 6.14.1 Recommendation.— All turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 15 000 kg, or authorized to carry more than 30 passengers, for which the individual airworthiness certificate is first issued after 24 November 2005, should be equipped with an airborne collision avoidance system (ACAS II). 6.14.2 All turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 15 000 kg, or authorized to carry more than 30 passengers, for which the individual airworthiness certificate is first issued after 1 January 2007, shall be equipped with an airborne collision avoidance system (ACAS II). 6.14.3 Recommendation.— All turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 5 700 kg but not exceeding 15 000 kg, or authorized to carry more than 19 passengers, for which the individual airworthiness certificate is first issued after 1 January 2008, should be equipped with an airborne collision avoidance system (ACAS II). 6.15 Microphones Recommendation.— All flight crew members required to be on flight deck duty should communicate through boom or throat microphones below the transition level/altitude. 24/11/05 No. 24 16B 2007/70/II. szám ANNEX 6 — PART II 24/11/05 No. 24 CHAPTER 7. AEROPLANE COMMUNICATION AND NAVIGATION EQUIPMENT 7.1 Communication equipment 7.1.1 An aeroplane to be operated in accordance with the instrument flight rules or at night shall be provided with radio communication equipment. Such equipment shall be capable of conducting two-way communication with those aeronautical stations and on those frequencies prescribed by the appropriate authority. Note.— The requirements of 7.1.1 are considered fulfilled if the ability to conduct the communications specified therein is established during radio propagation conditions which are normal for the route. 7.1.2 When compliance with 7.1.1 requires that more than one communication equipment unit be provided, each shall be independent of the other or others to the extent that a failure in any one will not result in failure of any other. 7.1.3 An aeroplane to be operated in accordance with the visual flight rules, but as a controlled flight, shall, unless exempted by the appropriate authority, be provided with radio communication equipment capable of conducting two-way communication at any time during flight with such aeronautical stations and on such frequencies as may be prescribed by the appropriate authority. 7.1.4 An aeroplane to be operated on a flight to which the provisions of 6.3.3 or 6.4 apply shall, unless exempted by the appropriate authority, be provided with radio communication equipment capable of conducting two-way communication at any time during flight with such aeronautical stations and on such frequencies as may be prescribed by the appropriate authority. 7.1.5 The radio communication equipment required in accordance with 7.1.1 to 7.1.4 shall provide for communication on the aeronautical emergency frequency 121.5 MHz. 7.2 Navigation equipment 7.2.1 An aeroplane shall be provided with navigation equipment which will enable it to proceed:

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