Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1722

f) an electric torch for each crew member station. 6.11 Pressurized aeroplanes when carrying passengers — weather radar Recommendation.— Pressurized aeroplanes when carrying passengers should be equipped with operative weather radar 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 6-9 1/11/01 23/11/06 No. 30 whenever such aeroplanes are being operated in areas where thunderstorms or other potentially hazardous weather conditions, regarded as detectable with airborne weather radar, may be expected to exist along the route either at night or under instrument meteorological conditions. 6.12 All aeroplanes operated above 15 000 m (49 000 ft) — radiation indicator All aeroplanes intended to be operated above 15 000 m (49 000 ft) shall carry equipment to measure and indicate continuously the dose rate of total cosmic radiation being received (i.e. the total of ionizing and neutron radiation of galactic and solar origin) and the cumulative dose on each flight. The display unit of the equipment shall be readily visible to a flight crew member. Note.— The equipment is calibrated on the basis of assumptions acceptable to the appropriate national authorities. 6.13 All aeroplanes complying with the noise certification Standards in Annex 16, Volume I An aeroplane shall carry a document attesting noise certification. When the document, or a suitable statement attesting noise certification as contained in another document approved by the State of Registry, is issued in a language other than English, it shall include an English translation. Note.— The attestation may be contained in any document, carried on board, approved by the State of Registry. 6.14 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. 6.15 Aeroplanes required to be equipped with ground proximity warning systems (GPWS) 6.15.1 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 shall be equipped with a ground proximity warning system. 6.15.2 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 shall be equipped with a ground proximity warning system which has a forward looking terrain avoidance function. 6.15.3 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, for which the individual certificate of airworthiness is first issued on or after 1 January 2004, shall be equipped with a ground proximity warning system which has a forward looking terrain avoidance function. 6.15.4 From 1 January 2007, 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, shall be equipped with a ground proximity warning system which has a forward looking terrain avoidance function. 6.15.5 Recommendation.— All turbine-engined aeroplanes of a maximum certificated take-off mass of 5 700 kg or less and authorized to carry more than five but not more than nine passengers should be equipped with a ground proximity warning system which provides the warnings of 6.15.8 a) and

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