Traduction de «Ground test point » (Anglais → Français) :

ground refuelling point [ ground fuelling point | ground refueling point | ground fueling point ]

ground nadir [ nadir | nadir point | ground plumb point | ground nadir point ]

ground nadir point | ground plumb point | plumb point

ground nadir | ground plumb point

testing point-line signaling | testing point-line signalling

control point | ground control point | picture control point

Ground control point | Picture control point

All leads and cables shall be a minimum of 100 mm from the edge of the ground plane and the distance to the ground plane (from the lowest point of the harness) shall be 50 ± 5 mm above the ground plane. Power shall be applied to the ESA under test via an (5 μ H/50 Ω) artificial network (AN).

For the tests described in Section 3.1 of Annex I to the Directive, the diameter of the sphere is 165 mm. For the tests described in Section 3.2 of Annex I to the Directive, the diameter of the sphere is 165 mm if the lower windscreen frame on the vehicle's centre line is located at a wrap around distance, as defined in point 2.8, of 1500 mm or more from the ground and the diameter of ...[+++] the sphere is 130 mm when this wrap around distance is less than 1500 mm. If the bonnet rear reference line is located at a wrap around distance of more than 2100 mm from the ground, the bonnet rear reference line is defined by the geometric trace of the 2100 mm wrap around distances, as defined in point 2.8.

This activity shall not include: (a) flights performed exclusively for the transport, on official mission, of a reigning Monarch and his immediate family, Heads of State, Heads of Government and Government Ministers, of a country other than a Member State, where this is substantiated by an appropriate status indicator in the flight plan (b) military flights performed by military aircraft and customs and police flights (c) flights related to search and rescue, fire-fighting flights, humanitarian flights and emergency medical service flights authorised by the appropriate competent authority (d) any flights performed exclusively under visual flight rules as defined in Annex 2 to the Chicago Convention (e) flights terminating at the aerodrome f ...[+++]rom which the aircraft has taken off and during which no intermediate landing has been made (f) training flights performed exclusively for the purpose of obtaining a licence, or a rating in the case of cockpit flight crew where this is substantiated by an appropriate remark in the flight plan provided that the flight does not serve for the transport of passengers and/or cargo or for the positioning or ferrying of the aircraft (g) flights performed exclusively for the purpose of scientific research or for the purpose of checking, testing or certifying aircraft or equipment whether airborne or ground-based (h) flights performed by aircraft with a certified maximum take-off mass of less than 5 700 kg (i) flights performed in the framework of public service obligations imposed in accordance with Regulation (EEC) No 2408/92 on routes within outermost regions, as specified in Article 299(2) of the Treaty, or on routes where the capacity offered does not exceed 30 000 seats per year (j) flights which, but for this point, would fall within this activity, performed by a commercial air transport operator operating either:

4.1.1. The test provided for in point 4.2 shall not be required in the case of any exterior mirror of which no part is less than 2 m from the ground, regardless of the adjustment position, when the vehicle is under a load corresponding to its maximum technically permissible mass.