Decree No. 66 / 2019 Coll.
Decree amending Decree of the Ministry of Transport and Communications No. 108 / 1997 Coll., implementing Act No. 49 / 1997 Coll., on Civil Aviation and amending and supplementing Act No. 455 / 1991 Coll., on Business Business (Trade Act), as amended
Valid
Order
Effective from 15.03.2019
Text versions:
15.03.2019
07.03.2019
66
DECLARATION
of 28 February 2019
amending Decree No. 108 / 1997 Coll., implementing Act No. 49 / 1997 Coll., on Civil Aviation and amending and supplementing Act No. 455 / 1991 Coll., on Business Business (Trade Act), as amended
The Ministry of Transport provides, pursuant to Section 102 (1) of Act No. 49 / 1997 Coll., on Civil Aviation and on the amendment and amendment of Act No. 455 / 1991 Coll., on Commercial Business (Commercial Act), as amended, as amended, Act No. 146 / 2000 Coll., Act No. 258 / 2002 Coll., Act No. 225 / 2006 Coll., Act No. 301 / 2009 Coll., Act No. 407 / 2010 Coll., Act No. 137 / 2011 Coll., Act No. 127 / 2014 Coll. and Act No. 261 / 2017 Coll., for the implementation of Section 51a (11) and Section 81 (8):
Decree No. 108 / 1997 Coll., implementing Act No. 49 / 1997 Coll., on Civil Aviation, and amending and supplementing Act No. 455 / 1991 Coll., on Business Business (Trade Act), as amended, as amended, as amended, as amended by Decree No. 101 / 1999 Coll., Decree No. 244 / 2003 Coll., Decree No. 359 / 2006 Coll., Decree No. 410 / 2006 Coll., Decree No. 64 / 2010 Coll., Decree No. 314 / 2010 Coll., Decree No. 4 / 2013 Coll., Decree No. 271 / 2014 Coll., Decree No. 9 / 2015 Coll. and Decree No. 2 / 2018 Coll., are amended as follows:
1. footnote 20 shall read:
"(20) Commission Regulation (EU) No 73 / 2010 of 26 January 2010 laying down quality requirements for aeronautical data and aeronautical information for the single European sky, as amended. Regulation (EU) No 996 / 2010 of the European Parliament and of the Council of 20 October 2010 on the investigation and prevention of accidents and incidents in civil aviation and repealing Directive 94 / 56 / EC, as amended. Commission Regulation (EU) No 965 / 2012 of 5 October 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216 / 2008 of the European Parliament and of the Council, as amended. Regulation (EU) No 598 / 2014 of the European Parliament and of the Council of 16 April 2014 on rules and procedures for introducing noise reduction operating restrictions at Union airports in the framework of a balanced approach repealing Directive 2002 / 30 / EC. Regulation (EU) 2018 / 1139 of the European Parliament and of the Council of 4 July 2018 on common rules in the field of civil aviation and establishing a European Union Aviation Safety Agency, amending Regulations (EC) No 2111 / 2005, (EC) No 1008 / 2008, (EU) No 996 / 2010, (EU) No 376 / 2014 and Directive 2014 / 30 / EU of the European Parliament and of the Council and repealing Regulations (EC) No 522 / 2004 and (EC) No 216 / 2008 and Council Regulation (EEC) No 3922 / 91. ';
2. In Article 16g (1), the word "k 'is inserted after the word" eligible'.
3. in Article 16g (5) and (6):
"(5) Data on obstacles located in and near the territory of an aerodrome eligible for an instrument flight shall be transmitted to the extent specified in Annex 14 to this Regulation and the frequency and characteristics listed in Annex 15 to this Regulation, by:
(a) from a rectangular space around a runway comprising a runway and a prefix, if established, the obstacle data shall be transmitted having a height of 3 m or more above the nearest height of the runway above the sea, measured along the axis of the runway, or for parts relating to the prefix from the altitude nearest to the end of the runway;
(b) the space which is drawn from the end of the space referred to in point (a) in the direction of departure up to 10 km and which is opened by 15% on each side shall be transmitted with data on obstacles which exceed 3 m above the ground and which, at the same time, intersect the area with a gradient of 1,2% from the end of the space referred to in point (a) starting at the height of the runway above the sea in the direction of departure;
(c) the space which is drawn from the outer edge of the spaces referred to in (a) and (b) up to a distance of 10 km from the boundary of the space referred to in (a) shall be provided with obstacle data which exceed 15 m above the ground and which intersect the area with a gradient of 1,2% from the outer edge of the spaces referred to in (a) and (b), starting from which the height of the rectangular space referred to in (a) begins;
(d) from an area which is drawn from the outer edge of the areas referred to in points (a), (b) and (c) to the border of the terminal control area of an aerodrome or to the border of a circular area of 45 km radius centred at the reference point of the aerodrome, if that point is closer, the obstacle data shall be transmitted which exceed 100 m above the ground.
(6) The data on the terrain located in and near the territory of an aerodrome eligible for an instrument flight shall be transmitted to the extent specified in Annex 14 to this Regulation and the frequency and characteristics listed in Annex 15 to this Regulation,
(a) data on the terrain within a circle of 10 km radius from the aerodrome reference point;
(b) terrain data which penetrates a horizontal level of 120 m above the lowest runway height in the area between the outer boundary of the territory referred to in (a); and
1. the limit of the terminal control area of the aerodrome; or
2. the boundary of a circle-shaped area of 45 km radius centred at the aerodrome reference point, if that boundary is closer to that point;
(c) terrain data not exceeding a horizontal level of 120 m above the lowest runway height in the area between the outer boundary of the territory referred to in (a); and
1. the limit of the terminal control area of the aerodrome; or
2. the border of a circle-shaped area of 45 km radius centred at the aerodrome reference point, if that border is closer to that point. ';
4. in Articles 16g (7) and 16h (7), the words "(b)" shall be deleted;
5. In Article 16g (7), the words "the transmission of obstacle and terrain data 'shall be deleted and the words" paragraph 4' shall be replaced by the words "the transmission of terrain data and obstacle data which exceed 100 m above ground, to the extent specified in Annex 14 to this Regulation, and with the frequency and characteristics set out in Annex 15 to this Regulation '.
6. in Paragraph 16g (8), the words "From the territory of an aerodrome eligible for an instrument acceptance, defined by a rectangle of 60 m width on each side of the runway axis and 900 m length from the runway threshold, measured along the extended runway axis against the landing direction, approved" shall be replaced by the words "From the territory of the aerodrome eligible for an instrument acceptance flight and its proximity, defined by a rectangle of 60 m width to each side of the extended runway centreline and within 900 m distance from the runway threshold, measured in the direction of an approved runway approach."
7. In Article 16h (1), the words "in such a format as to allow data exchange 'shall be inserted after the words" obstacles'.
8. in Article 16h (4) and Article 16h (5) of the introductory part of the provision, the words "on the technical data medium" shall be replaced by "via the electronic communications network."
9. in Article 16h (5) (a), the words "defined in accordance with Article 16g (5) (b)" shall be replaced by "a circle of 45 km radius from the reference point of the aerodrome eligible for an instrument flight."
10. in Article 16h (5) (b), the words "defined in accordance with Article 16g (6) (b)" shall be replaced by the words "a circle of 45 km radius from the reference point of the aerodrome eligible for an instrument flight."
11. in Paragraph 16h (6):
"(6) An aerodrome operator eligible for an instrument flight shall transmit to the database administrator, using the electronic communications network in the form and format referred to in paragraph 1, the data referred to in Sections 16g (5) (a) and (b), 16g (6) (a) and 16g (8). ';
12.
Characteristics of individual types of sport flying equipment
(Paragraph 81 (8) of the Law)
(1) The ultra-light glider is a maximum of two-seater non-powered aircraft controlled by aerodynamic means, the maximum take-off mass of which does not exceed 600 kg.
(2) The ultra-light motor glider is a maximum of two-seater aircraft equipped with a propulsion unit whose maximum take-off mass does not exceed 600 kg.
(3) An ultra-light aeroplane is a maximum of two-seater motor aircraft controlled by aerodynamic means, the falling speed of which does not exceed 83 km / h and the maximum take-off mass does not exceed 600 kg or 650 kg in the case of ultra-light aeroplanes intended for use on water.
(4) The engine suspension glider is a maximum of two-seater motor aircraft controlled by a change in centre of gravity with the possibility of additional aerodynamic control around one axis, the fall speed of which does not exceed 65 km / h and the maximum take-off mass does not exceed 300 kg for one-seater suspension glider and 450 kg for two-seater suspension glider.
(5) An ultra-light helicopter shall be a maximum of two-seater aircraft powered by rotating load surfaces with a maximum take-off mass of 600 kg or 650 kg in the case of ultra-light helicopters intended for use on water.
(6) The ultra-light vortex is a maximum of two-seater aircraft with rotating carrier surfaces set in motion by an autorotation resulting from forward movement with a maximum take-off mass of 600 kg.
(7) Motor parachute glider is a maximum two-seater aircraft
(a) with an auxiliary engine on the back of a pilot whose maximum take-off mass does not exceed 270 kg and which allows take-off and landing from the pilot's feet; or
(b) a drive on a chassis whose maximum take-off mass does not exceed 300 kg for a single-seat parachute sailplane and 450 kg for a two-seat parachute glider.
(8) The suspension glider shall be a maximum of two-seater non-powered aircraft, the take-off of which is performed by the pilot's rotor or winch and is controlled by a change in centre of gravity with the possibility of additional aerodynamic control around one axis, the maximum empty mass of which does not exceed 40 kg without the clamping device.
(9) The parachute glider is a maximum of two-seater non-powered aircraft, the nature of which is not determined by rigid construction.
(10) A sports parachute is a device used for the descending flight of a person from an aircraft to the ground surface.
(11) The ultra-light balloon is a maximum of two-seater lighter-than-air aircraft with a maximum design capacity not exceeding 1,200 m3 in the case of hot air and 400 m3 in the case of another carrier gas.
(12) The ultra-light airship is a maximum of two-seater lighter-air motor aircraft with a maximum design capacity not exceeding 1 200 m3 in the case of hot air and 400 m3 in the case of other carrier gas.
(13) In the case of an installation of an overall rescue parachute mounted on a dragon of a single-seater suspension glider or of a single-seater parachute, the maximum take-off mass referred to in paragraphs 4 and 7 shall be increased by 15 kg. In the case of an installation of a total rescue parachute mounted on a dragon of a two-seater suspension glider or a two-seater parachute, the maximum take-off mass referred to in paragraphs 4 and 7 shall be increased by 25 kg. ';
13. In Annex No 15, in the section "Field data characteristics', the words" Territory defined under Paragraph 16g (4) 'are replaced by the words "Territory defined under § 16g (4), (6) (c) and (7)'.
14. In Annex No 15, in the section "Field data characteristics', the words" Territory defined under § 16g (5) (a) and (b) 'are replaced by the words "Territory defined under § 16g (6) (a) and (b)'.
15. In Annex No 15, in the part "Obstacle data properties', the words" Territory defined under Paragraph 16g (4) 'are replaced by the words "Territory defined under § 16g (4) and (7)'.
16. In Annex No 15, in the part "Obstacle data properties', the words" Territory defined under § 16g (5) (a) and (b) 'are replaced by the words "Territory defined under § 16g (5)'.
Efficacy
This Regulation shall enter into force on 15 March 2019.
Minister for Transport:
Ing.
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Regulation Information
| Citation | Decree No. 66 / 2019 Coll., amending Decree No. 108 / 1997 Coll., implementing Act No. 49 / 1997 Coll., on Civil Aviation and amending and supplementing Act No. 455 / 1991 Coll., on Business Business, as amended |
|---|---|
| Regulation Type | Order |
| Author | - |
| Collection | Code of Laws |
| Date of Promulgation | 07.03.2019 |
|---|---|
| Effective from | 15.03.2019 |
| Effective until | - |
| Status | Valid |
The regulation text is for informational purposes only.
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