Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1692

c) current and suitable charts to cover the route of the proposed flight and any route along which it is reasonable to expect that the flight may be diverted. 6.2.4 Marking of break-in points 6.2.4.1 If areas of the fuselage suitable for break-in by rescue crews in emergency are marked on an aeroplane such areas shall be marked as shown below (see figure following). The colour of the markings shall be red or yellow, and if necessary they shall be outlined in white to contrast with the background. 6.2.4.2 If the corner markings are more than 2 m apart, intermediate lines 9 cm × 3 cm shall be inserted so that there is no more than 2 m between adjacent markings. MARKING OF BREAK-IN POINTS (see 6.2.4) Not over 2 m 9 cm 9 cm 9 cm 3 cm 3 cm 3 cm 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 6-3 1/11/01 23/11/06 No. 30 Note.— This Standard does not require any aeroplane to have break-in areas. 6.3 Flight recorders Note 1.— Flight recorders comprise two systems, a flight data recorder (FDR) and a cockpit voice recorder (CVR). 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 D. 6.3.1 Flight data recorders — types 6.3.1.1 A Type I FDR shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power, configuration and operation. 6.3.1.2 Types II and IIA FDRs shall record the parameters required to determine accurately the aeroplane flight path, speed, attitude, engine power and configuration of lift and drag devices. 6.3.1.3 The use of engraving metal foil FDRs shall be discontinued by 1 January 1995. 6.3.1.4 Recommendation.— The use of analogue FDRs using frequency modulation (FM) should be discontinued by 5 November 1998. 6.3.1.4.1 The use of photographic film FDRs shall be discontinued from 1 January 2003. 6.3.1.5 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 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. 6.3.1.5.1 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. 6.3.1.5.2 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), controllerpilot data link communications (CPDLC), data link-flight information services (D-FIS) and aeronautical operational control (AOC) messages. 6.3.1.6 Recommendation.— All aeroplanes of a maximum certificated take-off mass over 5 700 kg, required to be equipped with an FDR and a CVR, may alternatively be equipped with two combination recorders (FDR/CVR). 6.3.1.7 Recommendation.— All multi-engined turbinepowered aeroplanes of a maximum certificated take-off mass of 5 700 kg or less, required to be equipped with an FDR and/or a CVR, may alternatively be equipped with one combination recorder (FDR/CVR). 6.3.1.8 A Type IA FDR 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 FDR 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. 6.3.1.8.1 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* 6.3.1.8.2 The following parameters satisfy the requirements for attitude: – Pitch attitude – Roll attitude – Yaw or sideslip angle* – Angle of attack* 6.3.1.8.3 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* 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 6-4 23/11/06 No. 30 – 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 6.3.1.8.4 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* 6.3.1.8.5 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 – 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, are 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. 6.3.2 Flight data recorders — duration All FDRs shall be capable of retaining the information recorded during at least the last 25 hours of their operation, except for the Type IIA FDR which shall be capable of retaining the information recorded during at least the last 30 minutes of its operation. 6.3.3 Flight data recorders — aeroplanes for which the individual certificate of airworthiness is first issued on or after 1 January 1989 6.3.3.1 All aeroplanes of a maximum certificated take-off mass of over 27 000 kg shall be equipped with a Type I FDR. 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 6-5 1/11/01 23/11/06 No. 30 6.3.3.2 All aeroplanes of a maximum certificated take-off mass of over 5 700 kg, up to and including 27 000 kg, shall be equipped with a Type II FDR. 6.3.3.3 Recommendation.— All multi-engined turbinepowered 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. 6.3.4 Flight data recorders — aeroplanes for which the individual certificate of airworthiness was first issued on or after 1 January 1987 but before 1 January 1989 6.3.4.1 All turbine-engined aeroplanes of a maximum certificated take-off mass of over 5 700 kg, except those in 6.3.4.3, shall be equipped with an FDR which shall record time, altitude, airspeed, normal acceleration and heading. 6.3.4.2 Recommendation.— All turbine-engined aeroplanes of a maximum certificated take-off mass of over 5 700 kg, except those in 6.3.4.3, 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. 6.3.4.3 All turbine-engined aeroplanes of 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. 6.3.5 Flight data recorders — aeroplanes for which the individual certificate of airworthiness was first issued before 1 January 1987 6.3.5.1 All turbine-engined aeroplanes of 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. 6.3.5.2 Recommendation.— All turbine-engined aeroplanes of 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:

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