DIN EN 4709-001 pdf free download

DIN EN 4709-001-2019 pdf free download.Luft- und Raumfahrt – Unmanned Aircraft Systems – Produktanforderungen und Verifizierung fur die Open Category; Englische Fassung prEN 4709-001:2019.
4.2 Manufacturer’s Instructions on Safe Flight
4.2.1 General
The Manutacturers instructions on Sate Flight shall include the loliowing items:
• user and maintenance manuals (4.2.2) Appendix 1.2 and 1.4;
• an aviation regulation awareness leaflet (4.2.3) Appendix 1.5.
4.2.2 User and maintenance manuals (include instructions and warnings) Each UAS shall be placed on the market with at least the following information:
a) the characteristics of the UA including but not limited to the:
• UA class;
• UA mass (with a description of the reference configuration) and the maximum take-off mass
(MTOM);
• general characteristics of allowed payloads in terms of mass dimensions, interfaces with the UA and other possible restrictions;
• equipment and software to control the UA remotely;
• and a description of the behaviour of the UA in case of a loss of data link
b) deai upeiatioiial instrudioiis;
c) operational limitations (including but not limited to meteorological conditions and day/night operations) and;
d) appropriate description of all the risks related to UAS operations adapted for the age of the user.
Manufacturer’s information and warnings shall be drafted according to EN 62368-1:20 14, F.4 and Clause 5.
4.2.3 Aviation regulation awareness leaflet
Aviation Regulation Information shall be provided on a leaflet by the manufacturer regarding use the UAS in accordance with the applicable regulations on aviation safety, security, privacy and data protection, liability and insurance.
Compliance is checked by inspection of the awareness leaflet provided by the manufacturer against the UAS Class CO Awareness Leaflet related to the regulation on making available on the market of unmanned aircraft intended for use in the ‘open’ category and on third-country UAS operators.
4.3 Follow-Me Mode
4.3.1 General
If provided with a Follow-Me mode, compliance is checked by conducting the test of Subclauses 4.3.2 and 4.3.3 under the following test conditions:
power (MS and confirm proper function per manufacturer instructions;
• system should be fully charged and configured with all available options, or not, whichever is worst case. Confirm test area is free of potential obstacles and safety hazards;
• flight stabilization options should he set to default/ manufacturer’s recommendations. GPS, if any, should be turned off;
• tests require two technicians/engineers. The qualified pilot is responsible for flight during test. The second person is responsible for measurements and to be a spotter;
• pilot the UA to a stable hover with a minimum height of 2 (two) meters, activate the follow-me mode system and conduct the following tests.
4.3.2 Distance measurements
Verif’ that as the remote pilot moves away from the stable UA at a rate within the limits defined by the manufacturer, the UA will keep a distance not exceeding SO m from the pilot. The UA shall also not follow at a distance less than the minimum distance defined by the manufacturer. Three (three) different tests shall be made with the remote pilot moving in different patterns.
4.3.3 Regaining control
Verit’ that the remote pilot is able to regain control of the UA by cancelling follow-me mode or by activating an emergency safe landing procedure that terminates the flight.
4.4 UA Label
The UA shall bear the following label in a visible manner:
Compliance is checked by observation and label permanency per EN 62368-1:2014, F.3.9.DIN EN 4709-001 pdf download.