- Y Diweddaraf sydd Ar Gael (Diwygiedig)
- Pwynt Penodol mewn Amser (13/07/2009)
- Gwreiddiol (Fel y’i mabwysiadwyd gan yr UE)
Directive 2009/64/EC of the European Parliament and of the Council of 13 July 2009 on the suppression of radio interference produced by agricultural or forestry tractors (electromagnetic compatibility) (codified version) (Text with EEA relevance) (repealed)
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Version Superseded: 09/09/2009
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THE EUROPEAN PARLIAMENT AND THE COUNCIL OF THE EUROPEAN UNION,
Having regard to the Treaty establishing the European Community, and in particular Article 95 thereof,
Having regard to the proposal from the Commission,
Having regard to the opinion of the European Economic and Social Committee(1),
Acting in accordance with the procedure laid down in Article 251 of the Treaty(2),
Whereas:
(1) Council Directive 75/322/EEC of 20 May 1975 on the suppression of radio interference produced by agricultural or forestry tractors (electromagnetic compatibility)(3) has been substantially amended several times(4). In the interests of clarity and rationality the said Directive should be codified.
(2) Directive 75/322/EEC is one of the separate Directives of the EC type-approval system provided for in Council Directive 74/150/EEC of 4 March 1974 on the approximation of the laws of the Member States relating to the type-approval of wheeled agricultural or forestry tractors, as replaced by Directive 2003/37/EC of the European Parliament and of the Council of 26 May 2003 on type-approval of agricultural or forestry tractors, their trailers and interchangeable towed machinery, together with their systems, components and separate technical units(5), and lays down technical prescriptions concerning the suppression of radio interference produced by agricultural or forestry tractors (electromagnetic compatibility). Those technical prescriptions concern the approximation of the laws of the Member States to enable the EC type-approval procedure provided for in Directive 2003/37/EC to be applied in respect of each type of tractor. Consequently, the provisions laid down in Directive 2003/37/EC relating to agricultural and forestry tractors, their trailers and interchangeable towed machinery, together with their systems, components and separate technical units apply to this Directive.
(3) This Directive should be without prejudice to the obligations of the Member States relating to the time-limits for transposition into national law and application of the Directives set out in Annex XII, Part B,
HAVE ADOPTED THIS DIRECTIVE:
For the purposes of this Directive, ‘vehicle’ means any vehicle as defined in Article 2(d) of Directive 2003/37/EC.
1.Member States may not, on grounds relating to electromagnetic compatibility:
refuse to grant EC type-approval or national type-approval in respect of any given type of vehicle,
refuse to grant EC component or technical unit type-approval in respect of any given type of component or separate technical unit,
prohibit the registration, sale or entry into service of vehicles,
prohibit the sale or use of components or separate technical units,
if the vehicles, components or separate technical units comply with the requirements of this Directive.
2.Member States
may not grant EC vehicle type-approval, EC component type-approval or EC separate technical unit type-approval, and
may refuse to grant national type-approval,
for any type of vehicle, component or separate technical unit, if the requirements of this Directive are not fulfilled.
3.Paragraph 2 shall not apply to vehicle types approved before 1 October 2002 pursuant to Council Directive 77/537/EEC of 28 June 1977 on the approximation of the laws of the Member States relating to the measures to be taken against the emission of pollutants from diesel engines for use in wheeled agricultural or forestry tractors(6) or to any subsequent extensions to those approvals.
4.Member States:
shall consider certificates of conformity which accompany new vehicles in accordance with Directive 2003/37/EC to be not valid for the purposes of Article 7(1) of that Directive, and
may refuse the sale and entry into service of new electrical or electronic sub-assemblies as components or separate technical units,
if the requirements of this Directive are not fulfilled.
5.Without prejudice to paragraphs 2 and 4, in the case of replacement parts, Member States shall continue to grant EC type-approval and to permit the sale and entry into service of components or separate technical units intended for use on vehicle types which have been approved before 1 October 2002 pursuant to Directive 75/322/EEC or Directive 77/537/EEC and, where applicable, subsequent extensions to those approvals.
This Directive shall constitute ‘another Community directive’ for the purposes of Article 1(4) of Directive 2004/108/EC of the European Parliament and of the Council of 15 December 2004 on the approximation of the laws of the Member States relating to electromagnetic compatibility(7).
The amendments necessary to adapt to technical progress the requirements of Annexes I to XI shall be adopted in accordance with the procedure referred to in Article 20(3) of Directive 2003/37/EC.
Member States shall communicate to the Commission the text of the main provisions of national law which they adopt in the field covered by this Directive.
Directive 75/322/EEC, as amended by the acts listed in Annex XII, Part A, is repealed, without prejudice to the obligations of the Member States relating to the time-limits for transposition into national law and application of the Directives set out in Annex XII, Part B.
References to the repealed Directive shall be construed as references to this Directive and shall be read in accordance with the correlation table in Annex XIII.
This Directive shall enter into force on the twentieth day following its publication in the Official Journal of the European Union.
It shall apply from 1 January 2010.
This Directive is addressed to the Member States.
Done at Brussels, 13 July 2009.
For the European Parliament
The President
H.- G. Pöttering
For the Council
The President
E. Erlandsson
ANNEX I | REQUIREMENTS TO BE MET BY VEHICLES AND ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES FITTED TO A VEHICLE | ||
Appendix 1 | Vehicle broadband reference limits: Antenna-vehicle separation: 10 m | ||
Appendix 2 | Vehicle broadband reference limits: Antenna-vehicle separation: 3 m | ||
Appendix 3 | Vehicle narrowband reference limits: Antenna-vehicle separation: 10 m | ||
Appendix 4 | Vehicle narrowband reference limits: Antenna-vehicle separation: 3 m | ||
Appendix 5 | Broadband reference limits of electrical/electronic sub-assembly | ||
Appendix 6 | Narrowband reference limits of electrical/electronic sub-assembly | ||
Appendix 7 | Example of the EC type-approval mark | ||
ANNEX II | Information document No … pursuant to Annex I to Directive 2003/37/EC relating to EC type-approval of an agricultural or forestry tractor concerning electromagnetic compatibility (Directive 2009/64/EC) | ||
Appendix 1 | |||
Appendix 2 | |||
ANNEX III | Information document No … relating to EC type-approval of an electrical/electronic sub-assembly (ESA) with respect to electromagnetic compatibility (Directive 2009/64/EC) | ||
Appendix 1 | |||
Appendix 2 | |||
ANNEX IV | MODEL: EC TYPE-APPROVAL CERTIFICATE ‘VEHICLE’ | ||
Appendix to EC type-approval certificate No … concerning the type-approval of a vehicle with regard to Directive 2009/64/EC | |||
ANNEX V | MODEL: EC TYPE-APPROVAL CERTIFICATE ‘ESA’ | ||
Appendix to EC type-approval certificate No … concerning the type-approval of an electrical/electronic sub-assembly with regard to Directive 2009/64/EC | |||
ANNEX VI | METHOD OF MEASUREMENT OF RADIATED BROADBAND ELECTROMAGNETIC EMISSIONS FROM VEHICLES | ||
Appendix 1 | Figure 1 | TRACTOR TEST AREA | |
Figure 2 | POSITION OF ANTENNA RELATIVE TO TRACTOR | ||
ANNEX VII | METHOD OF MEASUREMENT OF RADIATED NARROWBAND ELECTROMAGNETIC EMISSIONS FROM VEHICLES | ||
ANNEX VIII | METHOD OF TESTING FOR IMMUNITY OF VEHICLES TO ELECTROMAGNETIC RADIATION | ||
Appendix 1 | |||
Appendix 2 | |||
Appendix 3 | Characteristics of test signal to be generated | ||
ANNEX IX | METHOD OF MEASUREMENT OF RADIATED BROADBAND ELECTROMAGNETIC EMISSIONS FROM ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES | ||
Appendix 1 | Electrical/electronic sub-assembly test area boundary | ||
Appendix 2 | Figure 1 | Radiated electromagnetic emissions from an ESA test layout (General plan view) | |
Figure 2 | Radiated electromagnetic emissions from an ESA view of test bench plane of longitudinal symmetry | ||
ANNEX X | METHOD OF MEASUREMENT OF RADIATED NARROWBAND ELECTROMAGNETIC EMISSIONS FROM ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES | ||
ANNEX XI | METHOD(S) OF TESTING FOR IMMUNITY OF ELECTRICAL/ELECTRONIC SUB-ASSEMBLIES TO ELECTROMAGNETIC RADIATION | ||
Appendix 1 | Figure 1 | 150 mm stripline testing | |
Figure 2 | 150 mm stripline testing | ||
Figure 3 | 800 mm stripline testing | ||
Figure 4 | 800 mm stripline dimensions | ||
Appendix 2 | Example of BCI test configuration | ||
Appendix 3 | Figure 1 | TEM cell testing | |
Figure 2 | Design of rectangular TEM cell | ||
Figure 3 | Typical TEM cell dimensions | ||
Appendix 4 | Free field ESA immunity test | ||
Figure 1 | Test layout (general plan view) | ||
Figure 2 | View of test bench plane of longitudinal symmetry | ||
ANNEX XII | PART A: Repealed Directive with list of its successive amendments | ||
PART B: List of time-limits for transposition into national law and application | |||
ANNEX XIII | Correlation table |
‘Vehicle type’ in relation to electromagnetic compatibility means vehicles which do not differ essentially in such respects as:U.K.
An ‘ESA type’ in relation to electromagnetic compatibility means ESAs which do not differ in such essential respects as:U.K.
The following alternative routes to type-approval of a vehicle may be used at the discretion of the vehicle manufacturer.U.K.
A vehicle installation may achieve type-approval directly by following the provisions laid down in point 6. If this route is chosen by a vehicle manufacturer, no separate testing of electrical/electronic systems or ESAs is required.
A vehicle manufacturer may obtain approval for the vehicle by demonstrating to the approval authority that all the relevant (see point 3.1.3) electrical/electronic systems or ESAs have individually been approved in accordance with this Directive and have been installed in accordance with any conditions attached thereto.
Type-approval may be granted to an ESA to be fitted either to any vehicle type or to a specific vehicle type or types requested by the manufacturer. ESAs involved in the direct control of vehicles will normally receive type-approval in conjunction with a vehicle manufacturer.
1 for Germany; 2 for France; 3 for Italy; 4 for the Netherlands; 5 for Sweden; 6 for Belgium; 7 for Hungary; 8 for the Czech Republic; 9 for Spain; 11 for the United Kingdom; 12 for Austria; 13 for Luxembourg; 17 for Finland; 18 for Denmark; 19 for Romania; 20 for Poland; 21 for Portugal; 23 for Greece; 24 for Ireland; 26 for Slovenia; 27 for Slovakia; 29 for Estonia; 32 for Latvia; 34 for Bulgaria; 36 for Lithuania; 49 for Cyprus; 50 for Malta.
It must also include in the vicinity of the rectangle the four-digit sequential number (with leading zeros as applicable) — hereinafter referred to as the ‘base approval number’ — contained in Section 4 of the type-approval number shown on the EC type-approval certificate issued for the type of device in question (see Annex V), preceded by the two figures indicating the sequence number assigned to the most recent major technical amendment to Directive 75/322/EEC, as replaced by this Directive, on the date EC component type-approval was granted.
The electromagnetic radiation generated by the vehicle representative of its type shall be measured using the method described in Annex VI at either of the defined antenna distances. The choice shall be made by the vehicle manufacturer.
The electromagnetic radiation generated by the vehicle representative of its type shall be measured using the method described in Annex VII at either of the defined antenna distances. The choice shall be made by the vehicle manufacturer.
The immunity to electromagnetic radiation of the vehicle representative of its type shall be tested by the method described in Annex VIII.
The electromagnetic radiation generated by the ESA representative of its type shall be measured by the method described in Annex IX.
The electromagnetic radiation generated by the ESA representative of its type shall be measured by the method described in Annex X.
The immunity to electromagnetic radiation of the ESA representative of its type shall be tested by the method(s) chosen from those described in Annex XI.
For vehicles fitted with tyres, the vehicle body/chassis can be considered to be an electrically isolated structure. Significant electrostatic forces in relation to the vehicle's external environment only occur at the moment of occupant entry into or exit from the vehicle. As the vehicle is stationary at these moments, no type-approval test for electrostatic discharge is deemed necessary.
Since during normal driving, no external electrical connections are made to vehicles, no conducted transients are generated in relation to the external environment. The responsibility of ensuring that equipment can tolerate the conducted transients within a vehicle, for example due to load switching and interaction between systems, lies with the manufacturer. No type-approval test for conducted transients is deemed necessary.
Antenna-vehicle separation: 10 m
Frequency — megahertz — logarithmic
See point 6.2.2.1 of Annex I
Antenna-vehicle separation: 3 m
Frequency — megahertz — logarithmic
See point 6.2.2.2 of Annex I
Antenna-vehicle separation: 10 m
Frequency — megahertz — logarithmic
See point 6.3.2.1 of Annex I
Antenna-vehicle separation: 3 m
Frequency — megahertz — logarithmic
See point 6.3.2.2 of Annex I
Frequency — megahertz — logarithmic
See point 6.5.2.1 of Annex I
Frequency — megahertz — logarithmic
See point 6.6.2.1 of Annex I
The ESA bearing the above EC type-approval mark is a device which has been approved in Germany (e1) under the base approval number 0148. The first two digits (02) indicate that the device conforms with the requirements of Directive 75/322/EEC, as amended by Directive 2000/2/EC.
The figures used are only indicative.
The following information, if applicable, must be supplied in triplicate and include a list of contents. Any drawings must be supplied in appropriate scale and in sufficient detail on size A4 or on a folder of A4 format.U.K.
Photographs, if any, must show sufficient detail. Details must be provided of the working of any systems, comportents or technical units with electronic controls.
Means of identification of type, if marked on the vehicle:U.K.
Photograph(s) and/or drawings of a representative vehicle:U.K.
Operating principle:U.K.
Fuel feed:U.K.
Pressure(11) or characteristic diagram … kPa
Injection system:U.K.
Description of system:
Electrical system:U.K.
Generator:U.K.
Type (mechanical hydraulic, electric, etc):U.K.
Glaxing:U.K.
Technical description:
Rear-view mince(s) (position of each):U.K.
Defrosting and demisting:U.K.
Seats and footrests:U.K.
Suppression of radio interference:U.K.
Description of vehicle chosen to represent the type
Body style:
Left or right-hand drive:
Wheelbase:
Component options:
Relevant test report(s) supplied by the manufacturer or approved/recognised laboratories for the purpose of drawing up the EC type-approval certificate.
The following information, if applicable, must be supplied in triplicate and must include a list of contents. Any drawings must be supplied in appropriate scale and in sufficient detail on size A4 or on a folder of A4 format. Photographs, if any, must show sufficient detail.U.K.
If the systems, component or separate technical units (stu) have electronic controls, information concerning their performance must be supplied.
Description of the ESA chosen to represent the type:
Relevant test report(s) supplied by the manufacturer or approved/recognised laboratories for the purpose of drawing up the EC type-approval certificate.
(maximum format: A4 (210 × 297 mm))
EC TYPE-APPROVAL CERTIFICATE
‘VEHICLE’
Communication concerning the:
EC type-approval(13)
extension of EC type-approval(13)
refusal of EC type-approval(13)
withdrawal of EC type-approval(13)
of a type of vehicle with regard to Directive 2009/64/EC.
EC type-approval number:
Reason for extension:
Means of identification of type, if marked on the vehicle/component/separate technical unit(13) (14):U.K.
(for example valid for both left-hand drive and right-hand drive vehicles)
(maximum format: A4 (210 × 297 mm))
EC TYPE-APPROVAL CERTIFICATE
‘ESA’
Communication concerning the:
EC type-approval(15)
extension of EC type-approval(15)
refusal of EC type-approval(15)
withdrawal of EC type-approval(15)
of a type of component/separate technical unit(15) with regard to Directive 2009/64/EC.
EC type-approval number:
Reason for extension:
Means of identification of type, if marked on the vehicle/component/separate technical unit(15) (16):U.K.
Additional informationU.K.
This ESA can be used on any vehicle type with the following restrictions:U.K.
This ESA can only be used on the following vehicle types:U.K.
The measuring equipment shall comply with the requirements of publication No 16-1 (93) of the International Special Committee on Radio Interference (CISPR).
A quasi-peak detector shall be used for the measurement of broadband electromagnetic emissions in this Annex, or if a peak detector is used an appropriate correction factor shall be used depending on the spark pulse rate.
This test is intended to measure the broadband electromagnetic emissions generated by spark-ignition systems and by electric motors (electric traction motors, engines for heating or de-icing systems, fuel pumps, water pumps, etc.) permanently fitted to the vehicle.
Two alternative reference antenna distances are permissible: 10 or 3 m from the vehicle. In either case the requirements of point 3 shall be complied with.
The results of measurements shall be expressed in dB microvolts/m (microvol/m) for 120 kHz band width. If the actual band width B (expressed in kHz) of the measuring apparatus differs from 120 kHz, the readings taken in microvolts/m shall be converted to 120 kHz band width through multiplication by a factor 120/B.
Other measuring antennae are allowed within the test area, at a minimum distance of 10 m both from receiving antenna and the vehicle under test, provided that it can be shown that the test results will not be affected.
To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement, measurements shall be taken before and after the main test. If the vehicle is present when ambient measurements are taken, it will be necessary to ensure that any emissions from the vehicle do not affect significantly the ambient measurements, for example by removing the vehicle from the test area, removing the ignition key, or disconnecting the battery. In both of the measurements, the extraneous noise or signal shall be at least 10 dB below the limits of interference given in point 6.2.2.1 or 6.2.2.2 (as appropriate) of Annex I, except for intentional narrowband ambient transmissions.
The engine shall be running at its normal operating temperature and the transmission shall be in neutral. If for practical reasons this cannot be achieved, alternative arrangements mutually agreed between the manufacturer and the test authorities may be made.
Care shall be taken to ensure that the speed setting mechanism does not influence electromagnetic radiations. During each measurement, the engine shall be operated as follows:
Engine type | Method of measurements | |
---|---|---|
Quasi peak | Peak | |
Spark ignition | Engine speed | Engine speed |
One cylinder | 2 500 rpm ± 10 % | 2 500 rpm ± 10 % |
More than one cylinder | 1 500 rpm ± 10 % | 1 500 rpm ± 10 % |
Any antenna may be used provided it can be normalised to the reference antenna. The method described in CISPR publication No 12, Edition 3, Appendix A, may be used to calibrate the antenna.
The phase centre of the antenna shall be 3,00 ± 0,05 m above the plane on which the vehicle rests.
The phase centre of the antenna shall be 1,80 ± 0,05 m above the plane on which the vehicle rests.
The horizontal distance from the tip or other appropriate point of the antenna defined during the normalisation procedure described in point 5.1 to the outer body surface of the vehicle shall be 10,0 ± 0,2 m.
The horizontal distance from the tip or other appropriate point of the antenna defined during the normalisation procedure described in point 5.1 to the outer body surface of the vehicle shall be 3,00 ± 0,05 m.
The antenna shall be located successively on the left and right-hand sides of the vehicle, with the antenna parallel to the plane of longitudinal symmetry of the vehicle, in line with the engine mid-point (see Figure 1 in Appendix 1) and in line with the vehicle mid-point defined as the point on the principal axis of the vehicle midway between the centres of the front and rear axles of the vehicle.
At each of the measuring points, readings shall be taken both with the antenna in a horizontal and in a vertical polarisation (see Figure 2 in Appendix 1).
The maximum of the four readings taken in accordance with points 5.3 and 5.4 at each spot frequency shall be taken as the characteristic reading at the frequency at which the measurements were made.
Las mediciones se efectuarán en la gama de frecuencias que va desde los 30 hasta los 1 000 MHz. A fin de comprobar que se cumplen los requisitos del presente anexo, la autoridad encargada del ensayo efectuará ensayos en hasta 13 frecuencias de dicha gama, por ejemplo 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750 y 900 MHz. En caso de que se rebase el límite durante el ensayo, se deberá comprobar si ello se debe al vehículo y no a la radiación ambiental.U.K.
Spot frequency(MHz) | Tolerance(MHz) |
---|---|
45, 65, 90, 120, 150, 190 and 230 | ±5 |
280, 380, 450, 600, 750 and 900 | ±20 |
The tolerances apply to frequencies quoted and are intended to avoid interference from transmissions operating on or near the nominal spot frequencies during the time of measurement.
The measuring equipment shall comply with the requirements of publication No 16-1 (93) of the International Special Committee on Radio Interference (CISPR).
An average detector or a peak detector shall be used for the measurement of radiated narrowband electromagnetic emissions in this Annex.
The results of measurements shall be expressed in dB microvolts/m (microvolts/m).
Other measuring antennae are allowed within the test area, at a minimum distance of 10 m both from receiving antenna and the vehicle under test, provided that it can be shown that the test results will not be affected.
To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement, ambient measurements shall be taken before and after the main test. It will be necessary to ensure that any emissions from the vehicle do not affect significantly the ambient measurements, for example by removing the vehicle from the test area, removing the ignition key, or disconnecting the battery(ies). In both of the measurements, the extraneous noise or signal shall be at least 10 dB below the limits of interference given in point 6.3.2.1 or 6.3.2.2 (as appropriate) of Annex I, except for intentional narrowband ambient transmissions.
Any antenna may be used provided that it can be normalised to the reference antenna. The method described in the CISPR publication No 12, Edition 3, Appendix A, may be used to calibrate the antenna.
The phase centre of the antenna shall be 3,00 ± 0,05 m above the plane on which the vehicle rests.
The phase centre of the antenna shall be 1,80 ± 0,05 m above the plane on which the vehicle rests.
The horizontal distance from the tip or other appropriate point of the antenna defined during the normalisation procedure described in point 5.1 to the outer body surface of the vehicle shall be 10,0 ± 0,2 m.
The horizontal distance from the tip or other appropriate point of the antenna defined during the normalisation procedure described in point 5.1 to the outer body surface of the vehicle shall be 3,00 ± 0,05 m.
The antenna shall be located successively on the left and right-hand sides of the vehicle with the antenna parallel to the plane of longitudinal symmetry of the vehicle and in line with the engine mid-point (see Figure 2 in Appendix 1 of Annex VI).
At each of the measuring points, readings shall be taken both with the antenna in a horizontal and in a vertical polarisation (see Figure 2 in Appendix 1 of Annex VI).
The maximum of the four readings taken in accordance with points 5.3 and 5.4 at each spot frequency shall be taken as the characteristic reading at the frequency at which the measurements are made.
Measurements shall be made throughout the 30 to 1 000 MHz frequency range. This range shall be divided into 13 bands. In each band one spot frequency may be tested to demonstrate that the required limits are satisfied. To confirm that the vehicle meets the requirements of this Annex, the testing authority shall test at one such point in each of the following 13 frequency bands:
30 to 50, 50 to 75, 75 to 100, 100 to 130, 130 to 165, 165 to 200, 200 to 250, 250 to 320, 320 to 400, 400 to 520, 520 to 660, 660 to 820, 820 to 1 000 MHz.
In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the vehicle and not to background radiation.
This test is intended to demonstrate the immunity to degradation in the direct control of the vehicle. The vehicle shall be subject to electromagnetic fields as described in this Annex. The vehicle shall be monitored during the tests.
For the test described in this Annex, field strengths shall be expressed in volts/m.
The test facility shall be capable of generating the field strengths over the frequency ranges defined in this Annex. The test facility shall comply with (national) legal requirements regarding the emission of electromagnetic signals.
Care shall be taken so that the control and monitoring equipment shall not be affected by radiated fields in such a way as to invalidate the tests.
The vehicle shall be in an unladen condition except for necessary test equipment.U.K.
Such testing may only take place if the physical construction of the chamber permits. The antenna location must be noted in the test report.
For the purposes of this Annex the reference point is the point at which the field strength shall be established and shall be defined as follows:U.K.
1,0 ± 0,2 m inside the vehicle, measured from the point of intersection of the windscreen and bonnet (point C in Appendix 1), or
0,2 ± 0,2 m from the centre line of the front axle of the tractor, measured towards the centre of the tractor (point D in Appendix 2),
whichever results in a reference point closer to the antenna,
1,0 ± 0,2 m inside the vehicle, measured from the point of intersection of the windscreen and bonnet (point C in Appendix 1), or
0,2 ± 0,2 m from the centre line of the rear axle of the tractor, measured towards the centre of the tractor (point D in Appendix 2),
whichever results in a reference point closer to the antenna.
The vehicle shall be exposed to electromagnetic radiation in the 20 to 1 000 MHz frequency range.U.K.
27, 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750 and 900 MHz.
The response time of the equipment under test shall be considered and the dwell time shall be sufficient to allow the equipment under test to react under normal conditions. In any case, it shall not be less than two seconds.
At each test frequency, a level of power shall be fed into the field generating device to produce the required field strength at the reference point (as defined in point 5) in the test area with the vehicle absent, the level of forward power, or another parameter directly related to the forward power required to define the field, shall be measured and the results recorded. Test frequencies shall lie in the range 20 to 1 000 MHz. Calibration shall be made, starting at 20, in steps not greater than two per cent of the previous frequency finishing at 1 000 MHz. These results shall be used for type-approval tests unless changes occur in the facilities or equipment which necessitate this procedure being repeated.
The vehicle shall then be introduced into the test facility and positioned in accordance with the requirements of point 5. The required forward power defined in point 7.1.2 at each frequency as defined in point 6.1.1 shall then be applied to the field generating device.
A suitable compact field strength measuring device shall be used to determine the field strength during the calibration phase of the substitution method.
for all field generating devices, 0,5 ± 0,05 m either side of the reference point on a line passing through the reference point and at the same height as the reference point, and perpendicular to the vehicle plane of longitudinal symmetry;
in the case of a TLS, 1,50 ± 0,05 m on a line passing through the reference point at the same height as the reference point and along the line of longitudinal symmetry.
Notwithstanding the condition set out in point 7.2.1, tests shall not be performed at chamber resonant frequencies.
The maximum envelope excursion of the test signal shall equal the maximum envelope excursion of an unmodulated sine wave whose rms value in volts/m is defined in point 6.4.2 of Annex I (see Appendix 3 of this Annex).
The test signal shall be a radio frequency sine wave, amplitude modulated by a 1 kHz sine wave at a modulation depth m of 0,8 ± 0,04.
The modulation depth m is defined as:
=
(maximum envelope excursion – minimum envelope excursion)/(maximum envelope excursion + minimum envelope excursion).
The measuring equipment shall comply with the requirements of publication No 16-1 (93) of the International Special Committee on Radio Interference (CISPR).
A quasi-peak detector shall be used for the measurement of broadband electromagnetic emissions in this Annex, or if a peak detector is used an appropriate correction factor shall be used depending on the interference pulse rate.
This test is intended to measure broadband electromagnetic emissions from ESAs.
The results of measurements shall be expressed in dB microvolts/m (microvolts/m), for 120 kHz band width. If the actual band width B (expressed in kHz) of the measuring apparatus differs from 120 kHz, the readings taken in microvolts/m shall be converted to 120 kHz band width through multiplication by a factor 120/B.
To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement, measurements shall be taken before and after the main test. In both of these measurements, the extraneous noise or signal shall be at least 10 dB below the limits of interference given in point 6.5.2.1 of Annex I, except for intentional narrowband ambient transmissions.
All cables in the loom shall be terminated as realistically as possible and preferably with real loads and actuators.
If extraneous equipment is required for the correct operation of the ESA under test, compensation shall be made for the contribution it makes to the emissions measured.
Any linearly polarised antenna may be used provided it can be normalised to the reference antenna.
The phase centre of the antenna shall be 150 ± 10 mm above ground plane.
The horizontal distance from the phase centre, or tip of the antenna as appropriate, to the edge of the ground plane shall be 1,00 ± 0,05 m. No part of the antenna shall be closer than 0,5 m to the ground plane.
The antenna shall be placed parallel to a plane which is perpendicular to the ground plane and coincident with the edge of the ground plane along which the principal portion of the harness runs.
At the measuring point, readings shall be taken both with the antenna in a vertical and in a horizontal polarisation.
The maximum of the two readings taken (in accordance with point 5.3) at each spot frequency shall be taken as the characteristic reading at the frequency at which the measurements were made.
Measurements shall be made throughout the 30 to 1 000 MHz frequency range. An ESA is considered as very likely to satisfy the required limits over the whole frequency range if it satisfies them at the following 13 frequencies in the range: 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750 and 900 MHzU.K.
In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the ESA and not to background radiation.
Spot frequency(MHz) | Tolerance(MHz) |
---|---|
45, 65, 90, 120, 150, 190 and 230 | ±5 |
280, 380, 450, 600, 750 and 900 | ±20 |
The tolerances apply to frequencies quoted and are intended to avoid interference from transmissions operating on or near the nominal spot frequencies during the time of measurement.
Level clear area free from electromagnetic reflecting surfaces
Figure 2
Radiated electromagnetic emissions from an ESA view of test bench plane of longitudinal symmetry
The measuring equipment shall comply with the requirements of publication No 16-1 (93) of the International Special Committee on Radio Interference (CISPR).
An average detector or a peak detector shall be used for the measurement of radiated narrowband electromagnetic emissions in this Annex.
The results of measurements shall be expressed in dB microvolts/m (microvolts/m).
To ensure that there is no extraneous noise or signal of a magnitude sufficient to affect materially the measurement, measurements shall be taken before and after the main test. In both of these measurements, the extraneous noise or signal shall be at least 10 dB below the limits of interference given in point 6.6.2.1 of Annex I, except for intentional narrowband ambient transmissions.
The ground plane shall be a metallic sheet with a minimum thickness of 0,5 mm. The minimum size of the ground plane depends on the size of the ESA under test but shall allow for the distribution of the ESA's wiring harness and components. The ground plane shall be connected to the protective conductor of the earthing system. The ground plane shall be situated at a height of 1,0 ± 0,1 m above the test facility floor and shall be parallel to it.
Any linearly polarised antenna may be used provided it can be normalised to the reference antenna.
The phase centre of the antenna shall be 150 ± 10 mm above ground plane.
The horizontal distance from the phase centre, or tip of the antenna as appropriate, to the edge of the ground plane shall be 1,00 ± 0,05 m. No part of the antenna shall be closer than 0,5 m to the ground plane.
The antenna shall be placed parallel to a plane which is perpendicular to the ground plane and coincident with the edge of the ground plane along which the principal portion of the harness runs.
At the measuring point, readings shall be taken both with the antenna in a vertical and in a horizontal polarisation.
The maximum of the two readings taken (in accordance with point 5.3) at each spot frequency shall be taken as the characteristic reading at the frequency at which the measurements were made.
Measurements shall be made throughout the 30 to 1 000 MHz frequency range. This range shall be divided into 13 bands. In each band one spot frequency may be tested to demonstrate that the required limits are satisfied. To confirm that the ESA under test meets the requirements of this Annex, the testing authority shall test one such point in each of the following 13 frequency bands:
30 to 50, 50 to 75, 75 to 100, 100 to 130, 130 to 165, 165 to 200, 200 to 250, 250 to 320, 320 to 400, 400 to 520, 520 to 660, 660 to 820, 820 to 1 000 MHz.
In the event that the limit is exceeded during the test, investigations shall be made to ensure that this is due to the ESA under test and not to background radiation.
Stripline testing: see Appendix 1
Bulk current injection testing: see Appendix 2
TEM cell testing: see Appendix 3
Free field test: see Appendix 4
For the tests described in this Annex, field strengths shall be expressed in volts/m and injected current shall be expressed in milliamps.
27, 45, 65, 90, 120, 150, 190, 230, 280, 380, 450, 600, 750 and 900 MHz
The response time of the equipment under test shall be considered and the dwell time shall be sufficient to allow the equipment under test to react under normal conditions. In any case, it shall not be less than two seconds.
The maximum envelope excursion of the test signal shall equal the maximum envelope excursion of an unmodulated sine wave whose rms value is defined in point 6.4.2 of Annex I (see Appendix 3 of Annex VIII).
The test signal shall be a radio frequency sine wave, amplitude modulated by a 1 kHz sine wave at a modulation depth m of 0,8 ± 0,04.
The modulation depth m is defined as:
=
(maximum envelope excursion — minimum envelope excursion)/(maximum envelope excursion + minimum envelope excursion)
This test method consists of subjecting the wiring harness connecting the components in an ESA to specified field strengths.
At each desired test frequency a level of power shall be fed into the stripline to produce the required field strength in the test area with the ESA under test absent, this level of forward power, or another parameter directly related to the forward power required to define the field, shall be measured and the results recorded. These results shall be used for type-approval tests unless changes occur in the facilities or equipment which necessitate this procedure being repeated. During this process, the position of the field probe head shall be under the active conductor, centred in longitudinal, vertical and transversal directions. The housing of the probe's electronics shall be as far away from the longitudinal stripline axis as possible.
The test method allows the generation of homogeneous fields between an active conductor (the stripline 50 Ω impedance), and a ground plane (the conducting surface of the mounting table), between which part of the wiring harness may be inserted. The electronic controller(s) of the ESA under test shall be installed on the ground plane but outside the stripline with one of its edges parallel to the active conductor of the stripline. It shall be 200 ± 10 mm from a line on the ground plane directly under the edge of the active conductor.U.K.
The distance between any edge of the active conductor and any peripheral device used for measurement shall be at least 200 mm.
The wiring harness section of the ESA under test shall be placed in a horizontal attitude between the active conductor and the ground plane (see Figures 1 and 2 in Appendix 1).
The stripline consists of two parallel metallic plates separated by 800 mm. Equipment under test is positioned centrally between the plates and subjected to an electromagnetic field (see Figures 3 and 4 in Appendix 1).
This method can test complete electronic systems including sensors and actuators as well as the controller and wiring loom. It is suitable for apparatus whose largest dimension is less than one-third of the plate separation.
The stripline shall be housed in a screened room (to prevent external emissions) and positioned 2 m away from walls and any metallic enclosure to prevent electromagnetic reflections. RF absorber material may be used to damp these reflections. The stripline shall be placed on non-conducting supports at least 0,4 m above the floor.
A field measuring probe shall be positioned within the central one-third of the longitudinal, vertical and transverse dimensions of the space between the parallel plates with the system under test absent. The associated measuring equipment shall be sited outside the screen room.
At each desired test frequency, a level of power shall be fed into the stripline to produce the required field strength at the antenna. This level of forward power, or another parameter directly related to the forward power required to define the field, shall be used for type-approval tests unless changes occur in the facilities or equipment which necessitate this procedure being repeated.
The main control unit shall be positioned within the central one-third of the longitudinal, vertical and transverse dimensions of the space between the parallel plates. It shall be supported on a stand made from non-conducting material.
The main wiring loom and any sensor/actuator cables shall rise vertically from the control unit to the top ground plate (this helps to maximise coupling with the electromagnetic field). Then they shall follow the underside of the plate to one of its free edges where they shall loop over and follow the top of the ground plate as far as the connections to the stripline feed. The cables shall then be routed to the associated equipment which shall be sited in an area outside the influence of the electromagnetic field, for example: on the floor of the screened room 1 m longitudinally away from the stripline.
This test method allows the testing of vehicle electrical/electronic systems by exposing an ESA to electromagnetic radiation generated by an antenna.
The test shall be performed inside a semi-anechoic chamber on a bench top.U.K.
For large equipment mounted on a metal test stand, the test stand shall be considered a part of the ground plane for testing purposes and shall be bonded accordingly. The faces of the test sample shall be located at a minimum of 200 mm from the edge of the ground plane. 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).
The phase centre of any antenna shall be 150 ± 10 mm above the ground plane on which the ESA under test rests. No parts of any antenna's radiating elements shall be closer than 250 mm to the floor of the facility.
is perpendicular to the ground plane;
bisects the edge of the ground plane and the midpoint of the principal portion of the wiring harness; and
is perpendicular to the edge of the ground plane and the principal portion of the wiring harness.
The field generating device shall be placed parallel to this plane (see Figures 1 and 2 in Appendix 4).
For the purpose of this Annex the reference point is the point at which the field strength shall be established and shall be defined as follows:U.K.
is perpendicular to the ground plane;
is perpendicular to the edge of the ground plane along which the principal portion of the wiring harness runs;
bisects the edge of the ground plane and the midpoint of the principal portion of the wiring harness; and
is coincident with the midpoint of the principal portion of the harness which runs along the edge of the ground plane closest to the antenna;
At each desired test frequency, a level of power shall be fed into the field generating device to produce the required field strength at the reference point (as defined in point 8.3.4 in the test area with the ESA under test absent), this level of forward power, or another parameter directly related to the forward power required to define the field, shall be measured and the results recorded. These results shall be used for type-approval tests unless changes occur in the facilities or equipment which necessitates this procedure being repeated.
A suitable compact field strength measuring device shall be used to determine the field strength during the calibration phase of the substitution method.
The transverse electromagnetic mode (TEM) cell generates homogeneous fields between the internal conductor (septum) and housing (ground plane). It is used for testing ESAs (see Figure 1 in Appendix 3).
|E| = (√(P × Z))/d
=
Electric field (volts/metre)
=
Power flowing into cell (W)
=
Impedance of cell (50 Ω)
=
Separation distance (metres) between the upper wall and the plate (septum).
In order to maintain a homogeneous field in the TEM cell and to obtain repeatable measurement results, the test object shall not be larger than one-third of the cell inside height.
Recommended TEM cell dimensions are given in Appendix 3, Figures 2 and 3.
The TEM cell shall be attached to a co-axial socket panel and connected as closely as possible to a plug connector with an adequate number of pins. The supply and signal leads from the plug connector in the cell wall shall be directly connected to the test object.
The external components such as sensors, power supply and control elements can be connected:
to a screened peripheral;
to a vehicle next to the TEM cell; or
directly to the screened patchboard.
Screened cables must be used in connecting the TEM cell to the peripheral or the vehicle if the vehicle or peripheral is not in the same or adjacent screened room.
This is a method of carrying out immunity tests by inducing currents directly into a wiring harness using a current injection probe. The injection probe consists of a coupling clamp through which the cables of the ESA under test are passed. Immunity tests can then be carried out by varying the frequency of the induced signals.
The ESA under test may be installed on a ground plane as in point 8.2.1 or in a vehicle in accordance with the vehicle design specification.
The injection probe shall be mounted in a calibration jig. Whilst sweeping the test frequency range, the power required to achieve the current specified in point 6.7.2.1 of Annex I shall be monitored. This method calibrates the bulk current injection system forward power versus current prior to testing, and it is this forward power which shall be applied to the injection probe when connected to the ESA under test via the cables used during calibration. It should be noted that the monitored power applied to the injection probe is the forward power.
For an ESA mounted on a ground plane as in point 8.2.1 all cables in the wiring harness shall be terminated as realistically as possible and preferably with real loads and actuators. For both vehicle mounted and ground plane mounted ESAs the current injection probe shall be mounted in turn around all the wires in the wiring harness to each connector and 150 ± 10mm from each connector of the ESA under test electronic control units (ECU), instrument modules or active sensors as illustrated in Appendix 2.
For an ESA under test mounted on a ground plane as in point 8.2.1, a wiring harness shall be connected between an artificial network (AN) and the principal electronic control unit (ECU). This harness shall run parallel to the edge of the ground plane and 200 mm minimum from its edge. This harness shall contain the power feed wire which is used to connect the vehicle battery to this ECU and the power return wire if used on the vehicle.
The distance from the ECU to the AN shall be 1,0 ± 0,1 m or shall be the harness length between the ECU and the battery as used on the vehicle, if known, whichever is the shorter. If a vehicle harness is used then any line branches which occur in this length shall be routed along the ground plane but perpendicular away from the edge of the ground plane. Otherwise the ESA under test wires which are in this length shall break out at the AN.
=
Ground plate
=
Main loom and sensor/actuator cables
=
Wooden frame
=
Driven plate
=
Insulator
=
Test object
=
DUT
=
RF measuring probe (optional)
=
RF injection probe
=
Artificial network
=
Shielded room filter network
=
Power source
=
DUT interface: stimulation and monitoring equipment
=
Signal generator
=
Broadband amplifier
=
RF 50 Ω directional complex
=
RF power level measuring device or equivalent
=
Spectrum analyser or equivalent (optional)
=
Outer conductor, shield
=
Inner conductor (septum)
=
Insulator
=
Input
=
Insulator
=
Door
=
Socket panel
=
Test object power supply
=
Terminating resistance 50 Ω
=
Insulation
=
Test object (maximum height one third of distance between cell floor and septum)
The following table shows the dimensions for constructing a cell with specified upper frequency limits:
Upper frequency(MHz) | Cell form factorW: b | Cell form factorL/W | Plate separationb (cm) | SeptumS (cm) |
---|---|---|---|---|
200 | 1,69 | 0,66 | 56 | 70 |
200 | 1,00 | 1,00 | 60 | 50 |
Typical TEM cell dimensions
Council Directive 75/322/EEC | |
Council Directive 82/890/EEC | only as regards the reference to Directive 75/322/EEC in Article 1(1) |
Directive 97/54/EC of the European Parliament and of the Council | only as regards the reference to Directive 75/322/EEC in the first indent of Article 1 |
Commission Directive 2000/2/EC | Article 1 and Annex only |
Commission Directive 2001/3/EC | Article 2 and Annex II only |
Point I.A.13 of Annex II to the 2003 Act of Accession | |
Council Directive 2006/96/EC | only as regards the reference to Directive 75/322/EEC in Article 1 and Annex, point A.12. |
a In conformity with Article 2 of Directive 2000/2/EC: 1.With effect from 1 January 2001, Member States may not, on grounds relating to electromagnetic compatibility:
if the vehicles, components or separate technical units comply with the requirements of Directive 75/322/EEC, as amended by this Directive. 2.With effect from 1 October 2002, Member States:
for any type of vehicle component or separate technical unit, if the requirements of Directive 75/322/EEC, as amended by this Directive, are not fulfilled. 3.Paragraph 2 shall not apply to vehicle types approved before 1 October 2002 pursuant to Council Directive 77/537/EEC“b nor to any subsequent extensions to these approvals. 4.With effect from 1 October 2008, Member States:
if the requirements of this Directive are not fulfilled. 5.Without prejudice to paragraphs 2 and 4, in the case of replacement parts, Member States shall continue to grant EC type-approval and to permit the sale and entry into service of components or separate technical units intended for use on vehicle types which have been approved before 1 October 2002 pursuant to Directive 75/322/EEC or Directive 77/537/EEC and, where applicable, subsequent extensions to these approvals.”. | ||
Directive | Time-limit for transposition | Date of application |
---|---|---|
75/322/EEC | 21 November 1976 | — |
82/890/EEC | 21 June 1984 | — |
97/54/EC | 22 September 1998 | 23 September 1998 |
2000/2/EC | 31 December 2000a | — |
2001/3/EC | 30 June 2002 | — |
2006/96/EC | 31 December 2006 | — |
Directive 75/322/EEC | Directive 2000/2/EC | This Directive |
---|---|---|
Article 1 | Article 1 | |
Article 2 | Article 2 | |
Article 4 | Article 3 | |
Article 5 | Article 4 | |
Article 6(1) | — | |
Article 6(2) | Article 5 | |
— | Article 6 | |
— | Article 7 | |
Article 7 | Article 8 | |
Annex I | Annex I | |
Annex IIA | Annex II | |
Annex IIB | Annex III | |
Annex IIIA | Annex IV | |
Annex IIIB | Annex V | |
Annex IV | Annex VI | |
Annex V | Annex VII | |
Annex VI | Annex VIII | |
Annex VII | Annex IX | |
Annex VIII | Annex X | |
Annex IX | Annex XI | |
— | Annex XII | |
— | Annex XIII |
Opinion of the European Parliament of 19 February 2008 (not yet published in the Official Journal) and Council Decision of 22 June 2009.
See Annex XII, Part A.
If applicable.
For example: radio telephone and citizens' band radio.
Delete as appropriate.
Indicate tolerance.
Delete where not applicable.
Delete where not applicable.
If the means of identification of type contains characters not relevant to describe the vehicle, component or separate technical unit types covered by this type-approval certificate such characters shall be represented in the documentation by the symbol: ‘?’ (for example ABC??123??).
Delete where not applicable.
If the means of identification of type contains characters not relevant to describe the vehicle, component or separate technical unit types covered by this type-approval certificate such characters shall be represented in the documentation by the symbol: ‘?’ (for example ABC??123??).
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