Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 1728

e) excessive descent below the instrument glide path. 23/11/06 No. 30 2007/70/II. szám Annex 6 — Operation of Aircraft Part I 1/11/01 6-10 23/11/06 No. 30 6.16 Aeroplanes carrying passengers — cabin crew seats 6.16.1 Aeroplanes for which the individual certificate of airworthiness is first issued on or after 1 January 1981 All aeroplanes shall be equipped with a forward or rearward facing (within 15 degrees of the longitudinal axis of the aeroplane) seat, fitted with a safety harness for the use of each cabin crew member required to satisfy the intent of 12.1 in respect of emergency evacuation. 6.16.2 Aeroplanes for which the individual certificate of airworthiness was first issued before 1 January 1981 Recommendation.— All aeroplanes should be equipped with a forward or rearward facing (within 15 degrees of the longitudinal axis of the aeroplane) seat, fitted with a safety harness for the use of each cabin crew member required to satisfy the intent of 12.1 in respect of emergency evacuation. Note.— Safety harness includes shoulder straps and a seat belt which may be used independently. 6.16.3 Cabin crew seats provided in accordance with 6.16.1 and 6.16.2 shall be located near floor level and other emergency exits as required by the State of Registry for emergency evacuation. 6.17 Emergency locator transmitter (ELT) 6.17.1 Except as provided for in 6.17.2, until 1 January 2005 all aeroplanes operated on long-range over-water flights as described in 6.5.3 shall be equipped with at least two ELT(S). 6.17.2 All aeroplanes for which the individual certificate of airworthiness is first issued after 1 January 2002, operated on long-range over-water flights as described in 6.5.3, shall be equipped with at least two ELTs, one of which shall be automatic. 6.17.3 From 1 January 2005, all aeroplanes operated on long-range over-water flights as described in 6.5.3 shall be equipped with at least two ELTs, one of which shall be automatic. 6.17.4 Except as provided for in 6.17.5, until 1 January 2005 aeroplanes on flights over designated land areas as described in 6.6 shall be equipped with at least one ELT(S). 6.17.5 All aeroplanes for which the individual certificate of airworthiness is first issued after 1 January 2002, on flights over designated land areas as described in 6.6, shall be equipped with at least one automatic ELT. 6.17.6 From 1 January 2005, aeroplanes on flights over designated land areas as described in 6.6 shall be equipped with at least one automatic ELT. 6.17.7 Recommendation.— All aeroplanes should carry an automatic ELT. 6.17.8 ELT equipment carried to satisfy the requirements of 6.17.1, 6.17.2, 6.17.3, 6.17.4, 6.17.5, 6.17.6 and 6.17.7 shall operate in accordance with the relevant provisions of Annex 10, Volume III. 6.18 Aeroplanes required to be equipped with an airborne collision avoidance system (ACAS II) 6.18.1 From 1 January 2003, 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 an airborne collision avoidance system (ACAS II). 6.18.2 From 1 January 2005, all turbine-engined aeroplanes of a maximum certificated take-off mass in excess of 5 700 kg or authorized to carry more than 19 passengers shall be equipped with an airborne collision avoidance system (ACAS II). 6.18.3 Recommendation.— All aeroplanes should be equipped with an airborne collision avoidance system (ACAS II). 6.18.4 An airborne collision avoidance system shall operate in accordance with the relevant provisions of Annex 10, Volume IV. 6.19 Aeroplanes required to be equipped with a pressure-altitude reporting transponder All aeroplanes shall be equipped with a pressure-altitude reporting transponder which operates in accordance with the relevant provisions of Annex 10, Volume IV. Note.— This provision is intended to improve the effectiveness of air traffic services as well as airborne collision avoidance systems. 6.20 Microphones All flight crew members required to be on flight deck duty shall communicate through boom or throat microphones below the transition level/altitude. 2007/70/II. szám Chapter 6 Annex 6 — Operation of Aircraft 6-11 1/11/01 23/11/06 No. 30 6.21 Turbo-jet aeroplanes — forward-looking wind shear warning system 6.21.1 Recommendation.— All turbo-jet 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 forward-looking wind shear warning system. 6.21.2 Recommendation.— A forward-looking wind shear warning system should be capable of providing the pilot with a timely aural and visual warning of wind shear ahead of the aircraft, and the information required to permit the pilot to safely commence and continue a missed approach or go-around or to execute an escape manoeuvre if necessary. The system should also provide an indication to the pilot when the limits specified for the certification of automatic landing equipment are being approached, when such equipment is in use. 6.22 All aeroplanes operated by a single pilot under the instrument flight rules (IFR) or at night For approval in accordance with 4.9.1, all aeroplanes operated by a single pilot under the IFR or at night shall be equipped with:

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