xmlns:atom="http://www.w3.org/2005/Atom" xmlns:atom="http://www.w3.org/2005/Atom"
The control conditions specify an altitude, ambient temperature and engine coolant range that determines whether auxiliary emission control strategies may generally or only exceptionally be activated in accordance with point 2.3.
The control conditions specify an atmospheric pressure which is measured as absolute atmospheric static pressure (wet or dry) (‘Atmospheric pressure’)
an altitude not exceeding 500 metres (or equivalent atmospheric pressure of 95,5 kPa);
an ambient temperature within the range 275 K to 303 K (2 °C to 30 °C);
the engine coolant temperature above 343 K (70 °C).
an altitude not exceeding 1 000 metres (or equivalent atmospheric pressure of 90 kPa);
an ambient temperature within the range 275 K to 303 K (2 °C to 30 °C);
the engine coolant temperature above 343 K (70 °C).
the atmospheric pressure greater than or equal to 82,5 kPa;
the ambient temperature within the following range:
equal to or above 266 K (– 7 °C),
less than or equal to the temperature determined by the following equation at the specified atmospheric pressure: Tc = – 0,4514 × (101,3 – Pb) + 311, where: Tc is the calculated ambient air temperature, K and Pb is the atmospheric pressure, kPa;
the engine coolant temperature above 343 K (70 °C).