- Latest available (Revised)
- Original (As adopted by EU)
Commission Directive 2010/22/EU of 15 March 2010 amending, for the purposes of their adaptation to technical progress, Council Directives 80/720/EEC, 86/298/EEC, 86/415/EEC and 87/402/EEC and Directives 2000/25/EC and 2003/37/EC of the European Parliament and of the Council relating to the type-approval of agricultural or forestry tractors (Text with EEA relevance) (repealed)
When the UK left the EU, legislation.gov.uk published EU legislation that had been published by the EU up to IP completion day (31 December 2020 11.00 p.m.). On legislation.gov.uk, these items of legislation are kept up-to-date with any amendments made by the UK since then.
Legislation.gov.uk publishes the UK version. EUR-Lex publishes the EU version. The EU Exit Web Archive holds a snapshot of EUR-Lex’s version from IP completion day (31 December 2020 11.00 p.m.).
This is the original version (as it was originally adopted).
THE EUROPEAN COMMISSION,
Having regard to the Treaty on the Functioning of the European Union,
Having regard to Council Directive 80/720/EEC of 24 June 1980 on the approximation of the laws of the Member States relating to the operating space, access to the driving position and the doors and windows of wheeled agricultural or forestry tractors(1), in particular Article 3 thereof,
Having regard to Council Directive 86/298/EEC of 26 May 1986 on rear-mounted roll-over protection structures of narrow-tracked wheeled agricultural or forestry tractors(2), and in particular Article 12 thereof,
Having regard to Council Directive 86/415/EEC of 24 July 1986 on the installation, location, operation and identification of the controls of wheeled agricultural or forestry tractors(3), and in particular Article 4 thereof,
Having regard to Council Directive 87/402/EEC of 25 June 1987 on roll-over protection structures mounted in front of the driver’s seat in wheeled agricultural or forestry tractors(4), and in particular Article 11 thereof,
Having regard to Directive 2000/25/EC of the European Parliament and of the Council of 22 May 2000 on action to be taken against the emission of gaseous and particulate pollutants by engines intended to power agricultural or forestry tractors and amending Council Directive 74/150/EEC(5), and in particular Article 7 thereof,
Having regard to 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 and repealing Directive 74/150/EEC(6), and in particular points (a) and (b) of Article 19(1) thereof,
Whereas:
(1) As concerns Directive 80/720/EEC, it is appropriate to clarify which windows may be designated as emergency exits.
(2) As concerns Directive 86/415/EEC, in order to improve safety of tractors it is suitable to specify safety requirements for the external controls of the power take-off.
(3) As concerns Directive 86/415/EEC, the use of pictorials according to standards ISO 3767-1:1996 and ISO 3767-2:1996 as symbols for the controls should be allowed in order to adapt Community standards to the standards applied in the framework of controls of wheeled agricultural or forestry tractors worldwide.
(4) As concerns Directive 2000/25/EC, certain additional indications need to be specified in order to be consistent with the introduction of new stage limits (IIIA, IIIB and IV), introduced by Commission Directive 2005/13/EC(7).
(5) As concerns Directive 2003/37/EC, a more precise wording for some points in the information documents should be included for reasons of clarity.
(6) As concerns Directives 2003/37/EC, 86/298/EEC and 87/402/EEC, in view of the fact that OECD Decision C(2005) 1 of the OECD Council was most recently amended by Decision C(2008) 128 of October 2008, it is appropriate to update the references to the OECD codes. For reasons of legal certainty it is necessary to include the relevant texts of such OECD documents in the Directives.
(7) Directives, 80/720/EEC, 86/298/EEC, 86/415/EEC, 87/402/EEC, 2000/25/EC and 2003/37/EC should be amended accordingly.
(8) The measures provided for in this Directive are in accordance with the opinion of the Committee established under Article 20(1) of Directive 2003/37/EC,
HAS ADOPTED THIS DIRECTIVE:
Directive 80/720/EEC is amended in accordance with Annex I to this Directive.
Directive 86/298/EEC is amended in accordance with Annex II to this Directive.
Directive 86/415/EEC is amended in accordance with Annex III to this Directive.
Directive 87/402/EEC is amended in accordance with Annex IV to this Directive.
Directive 2000/25/EC is amended in accordance with Annex V to this Directive.
Directive 2003/37/EC is amended as follows:
in Article 12(4), the words ‘test bulletin’ are replaced by ‘test report’
[concerns only the English version];
Annexes I and II are amended in accordance with Annex VI to this Directive.
1.Member States shall adopt and publish, by 30 April 2011 at the latest, the laws, regulations and administrative provisions necessary to comply with this Directive. They shall forthwith communicate to the Commission the texts of those provisions.
They shall apply those provisions from 1 May 2011, with the exception of Article 5 which they shall apply from the date of entry into force of this Directive.
When Member States adopt those provisions, they shall contain a reference to this Directive or be accompanied by such a reference on the occasion of their official publication. Member States shall determine how such reference is to be made.
2.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.
This Directive shall enter into force on the 20th day following its publication in the Official Journal of the European Union.
This Directive is addressed to the Member States.
Done at Brussels, 15 March 2010.
For the Commission
The President
José Manuel Barroso
Annex I to Directive 80/720/EEC is amended as follows:
point III.4 is deleted;
in point III.5 the following subparagraph is added:
‘Any window of sufficient size may be designated as an emergency exit if they are made of breakable glass and can be broken with a tool provided in the cab for that purpose. Glass referred to in Appendices 3, 4, 5, 6 and 7 of Annex III B to Council Directive 89/173/EEC(8) is not considered to be breakable glass for the purpose of this Directive.’
Directive 86/298/EEC is amended as follows:
in Annex I, point 1 is replaced by the following:
The definitions and requirements of point 1 of Code 7(9) of OECD Decision C(2008) 128 of October 2008, with the exception of point 1.1 (Agricultural and forestry tractors), shall apply, reading as follows:
Roll-over protective structure (safety cab or frame), hereinafter called ‘protective structure’, means the structure on a tractor the essential purpose of which is to avoid or limit risks to the driver resulting from roll-over of the tractor during normal use.
The roll-over protective structure is characterized by the provision of space for a clearance zone large enough to protect the driver when seated either inside the envelope of the structure or within a space bounded by a series of straight lines from the outer edges of the structure to any part of the tractor that might come into contact with flat ground and that is capable of supporting the tractor in that position if the tractor overturns.
The median plane of the wheel is equidistant from the two planes containing the periphery of the rims at their outer edges.
The vertical plane through the wheel axis intersects its median plane along a straight line which meets the supporting surface at one point. If A and B are the two points thus defined for the wheels on the same axle of the tractor, then the track width is the distance between points A and B. The track may be thus defined for both front and rear wheels. Where there are twin wheels, the track is the distance between two planes each being the median plane of the pairs of wheels.
Take the extreme positions of points A and B for the tractor rear axle, which gives the maximum possible value for the track. The vertical plane at right angles to the line AB at its centre point is the median plane of the tractor.
The distance between the vertical planes passing through the two lines AB as defined above, one for the front wheels and one for the rear-wheels.
The seat index point shall be determined in accordance with ISO 5353:1995
The clearance zone is illustrated in Figures 7.1 and 7.2. The zone is defined in relation to the reference plane and the seat index point (SIP). The reference plane is a vertical plane, generally longitudinal to the tractor and passing through the seat index point and the centre of the steering wheel. Normally the reference plane coincides with the longitudinal median plane of the tractor. This reference plane shall be assumed to move horizontally with the seat and steering wheel during loading but to remain perpendicular to the tractor or the floor of the roll-over protective structure. The clearance zone shall be defined on the basis of sub clauses 1.6.2 and 1.6.3.
The clearance zone for tractors with a non-reversible seat is defined in 1.6.2.1 to 1.6.2.13 below and is bounded by the following planes, the tractor being on a horizontal surface, the seat, where adjustable, adjusted to its rear uppermost position(11), and the steering wheel, where adjustable, adjusted to the mid-position for seated driving:
a horizontal plane A1 B1 B2 A2, (810 + av) mm above the seat index point (SIP) with line B1B2 located (ah–10) mm behind the SIP;
an inclined plane H1 H2 G2 G1, perpendicular to the reference plane, including both a point 150 mm behind line B1B2 and the rearmost point of the seat backrest;
a cylindrical surface A1 A2 H2 H1 perpendicular to the reference plane, having a radius of 120 mm, tangential to the planes defined in 1.6.2.1 and 1.6.2.2 above;
a cylindrical surface B1 C1 C2 B2, perpendicular to the reference plane, having a radius of 900 mm extending forward for 400 mm and tangential to the plane defined in 1.6.2.1 above along line B1B2;
an inclined plane C1 D1 D2 C2, perpendicular to the reference plane, joining the surface defined in 1.6.2.4 above and passing 40 mm from the forward external edge of the steering wheel. In the case of a high steering wheel position, this plane extends forward from line B1B2 tangentially to the surface defined in 1.6.2.4 above;
a vertical plane D1 K1 E1 E2 K2 D2 perpendicular to the reference plane 40 mm forward of the external edge of the steering wheel;
a horizontal plane E1 F1 P1 N1 N2 P2 F2 E2 passing through a point (90–av) mm below the seat index point (SIP);
a surface G1 L1 M1 N1 N2 M2 L2 G2, if necessary curved from the bottom limit of the plane defined in 1.6.2.2 above to the horizontal plane defined in 1.6.2.7 above, perpendicular to the reference plane, and in contact with the seat backrest throughout its length;
two vertical planes K1 I1 F1 E1 and K2 I2 F2 E2 parallel to the reference plane, 250 mm either side of the reference plane, and bounded at the top 300 mm above the plane defined in 1.6.2.7 above;
two inclined and parallel planes A1 B1 C1 D1 K1 I1 L1 G1 H1 and A2 B2 C2 D2 K2 I2 L2 G2 H2 starting from the upper edge of the planes defined in 1.6.2.9 above and joining the horizontal plane defined in 1.6.2.1 above at least 100 mm from the reference plane on the side where the loading is applied;
two portions of vertical planes Q1 P1 N1 M1 and Q2 P2 N2 M2 parallel to the reference plane, 200 mm either side of the reference plane, and bounded towards the top 300 mm above the horizontal plane defined in 1.6.2.7 above;
two portions of I1 Q1 P1 F1 and I2 Q2 P2 F2 of a vertical plane, perpendicular to the reference plane and passing (210–ah) mm in front of the SIP;
two portions I1 Q1 M1 L1 and I2 Q2 M2 L2 of the horizontal plane passing 300 mm above the plane defined in 1.6.2.7 above.
For tractors with a reversible driver’s position (reversible seat and steering wheel), the zone of clearance is the envelope of the two clearance zones defined by the two different positions of the steering wheel and the seat.
:
± 3 mm
except for
:
± 1 mm
:
± 1 mm
:
± 1 mm
:
± 1 %
:
± 2 %
:
± 2°
ah | (mm) | Half of the horizontal seat adjustment |
av | (mm) | Half of the vertical seat adjustment |
B | (mm) | Minimum overall width of the tractor |
B6 | (mm) | Maximum outer width of the protective structure |
D | (mm) | Deflection of the structure at the point of impact (dynamic tests) or at the point of, and in line with, the load application (static tests) |
D′ | (mm) | Deflection of the structure for the calculated energy required |
Ea | (J) | Strain energy absorbed at point when load is removed. Area contained within F-D curve |
Ei | (J) | Strain energy absorbed. Area under F-D curve |
E′i | (J) | Strain energy absorbed after additional loading following a crack or tear |
E′′i | (J) | Strain energy absorbed in overload test in the event of the load having been removed before starting this overload test. Area under F-D curve |
Eil | (J) | Energy input to be absorbed during longitudinal loading |
Eis | (J) | Energy input to be absorbed during side loading |
F | (N) | Static load force |
F′ | (N) | Loading force for calculated energy required, corresponding to E′i |
F-D | Force/deflection diagram | |
Fmax | (N) | Maximum static load force occurring during loading, with the exception of the overload |
Fv | (N) | Vertical crushing force |
H | (mm) | Falling height of the pendulum block (dynamic tests) |
H′ | (mm) | Falling height of the pendulum block for additional test (dynamic tests) |
I | (kgm2) | Tractor reference moment of inertia about the centre line of the rear wheels, whatever the mass of these rear wheels may be |
L | (mm) | Tractor reference wheelbase |
M | (mm) | Tractor reference mass during strength tests, as defined in section 3.1.1.4. of Annex II’ ’ |
Annex II is replaced by the following
The technical requirements for the EC type-approval of rear-mounted roll-over protection structures of narrow-track wheeled agricultural or forestry tractors shall be those set out in point 3 of Code 7 of the OECD Decision C(2008) 128 of October 2008, with the exception of points 3.1.4 (Test report), 3.3.1 (Administrative extensions), 3.4 (Labeling) and 3.6 (Seat belt anchorage performance), reading as follows:
Tests made using special rigs are intended to simulate such loads as are imposed on a protective structure, when the tractor overturns. These tests enable observations to be made on the strength of the protective structure and any brackets attaching it to the tractor and any parts of the tractor which transmit the test load.
Tests may be performed in accordance with the dynamic procedure or the static procedure. The two methods are deemed equivalent.
Note: A complete tractor is not required for the static strength test; however, the protective structure and parts of the tractor to which it is attached represent an operating installation, hereinafter referred to as ‘the assembly’.
Components which may create a hazard in the clearance zone must also be fitted on the tractor (or the assembly) so that they may be examined to see whether the requirements of the Acceptance Conditions in 3.1.3 have been fulfilled. All components of the tractor or the protective structure including weather protective must be supplied or described on drawings.
The reference mass M, used in the formulae to calculate the height of the fall of the pendulum block, the loading energies and the crushing forces, must be at least the mass of the tractor, excluding optional accessories but including coolant, oils, fuel, tools plus the protective structure. Not included are optional front or rear weights, tyre ballast, mounted implements, mounted equipment or any specialised components.
The sequence of tests, without prejudice to the additional tests mentioned in sections 3.2.1.1.6, 3.2.1.1.7, 3.2.2.1.6 and 3.2.2.1.7, is as follows:
impact (dynamic test) or loading (static test) at the rear of the structure (see 3.2.1.1.1 and 3.2.2.1.1);
rear crushing test (dynamic or static test) (see 3.2.1.1.4 and 3.2.2.1.4);
impact (dynamic test) or loading (static test) at the front of the structure (see 3.2.1.1.2 and 3.2.2.1.2);
impact (dynamic test) or loading (static test) at the side of the structure (see 3.2.1.1.3 and 3.2.2.1.3);
crushing at the front of the structure (dynamic or static test) (see 3.2.1.1.5 and 3.2.2.1.5).
after each test in the dynamic test procedure, it shall be free from tears or cracks, as defined in 3.2.1.2.1. If during the dynamic test, significant tears or cracks appear, an additional impact test or crushing test as defined in 3.2.1.1.6 or 3.2.1.1.7 must be performed immediately after the test which caused these tears or cracks to appear;
during static test, at the point when the energy required is attained in each horizontal load test prescribed or in the overload test the force must be greater than 0,8 F;
if during a static test, cracks or tears appear as a result of the application of the crushing force, an additional crushing test as defined in 3.2.2.1.7 must be performed immediately after the crushing test which caused these cracks or tears to appear;
during the tests other than the overload test, no part of the protective structure must enter the clearance zone as defined in 1.6 of Annex I;
during the tests other than the overload test, all parts of the clearance zone shall be secured by the structure, in accordance with 3.2.1.2.2 and 3.2.2.2.2;
during the tests the protective structure must not impose any constraints on the seat structure;
the elastic deflection, measured in accordance with 3.2.1.2.3 and 3.2.2.2.3 shall be less than 250 mm.
The pendulum pivot points must be rigidly fixed so that their displacement in any direction does not exceed 1 per cent of the height of fall.
A rig as shown in Figure 7.7 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide connected to the load-applying mechanism by means of universal joints. Suitable axle stands shall be provided so that the tractor tyres do not bear the crushing force.
The following measuring apparatus is needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, see Figure 7.8).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (see section 3.2.2.2.2).
at start of test, under zero load: ± 2°,
during test, under load: 10° above and 20° below the horizontal. These variations must be kept to a minimum.
If the tractor moves, the entire test shall be repeated, unless the system for measuring the deflections taken into account for plotting the force versus deflection curve is connected to the tractor.
A rig as shown in Figure 7.7 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide, connected to the load-applying mechanism by means of universal joints. Suitable axle stands must be provided so that the tractor tyres do not bear the crushing force.
The following measure devices are also needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, see Figure 7.8).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (section 3.3.2.2.2).
The suspended height of the block shall be adjusted and necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plan parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.1.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed in front of and tight against the rear wheels and then fixed to the ground.
H = 2,165 × 10–8 M L2
or
H = 5,73 × 10–2 I
The pendulum block is then released and strikes the protective structure.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg;
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The suspended height of the pendulum block shall be adjusted and the necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first if the tractor overturned sideways while travelling forward, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plane parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.1.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed behind and tight against the rear wheels and then fixed to the ground.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg;
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
if the protective structure is a rear two-post rollbar, the above formula shall apply,
for other types of protective structure, the height shall be whichever is greater from the formula applied above and that selected below:
H = 2,165 × 10–8 ML2
or
H = 5,73 × 10–2 I
The pendulum block is then released and strikes the protective structure.
With the wire ropes tensioned, the wedging beam shall be placed on the ground, pushed tight against the tyres on the side opposite that which is to receive the impact and then fixed to the ground. It may be necessary to use two beams or wedges if the outer sides of the front and rear tyres are not in the same vertical plane. The prop shall then be placed as indicated in Figure 7.6 against the rim of the most heavily loaded wheel opposite to the point of impact, pushed firmly against the rim and then fixed at its base. The length of the prop shall be such that it makes an angle of 30 ± 3° with the ground when in position against the rim. In addition, its thickness shall, if possible, be between 20 and 25 times less than its length and between 2 and 3 times less than its width. The props shall be shaped at both ends as shown in the details on Figure 7.6.
H = 25 + 0,20 M
for tractors with a reference mass of less than 2 000 kg;
H = 125 + 0,15 M
for tractors with a reference mass of more than 2 000 kg.
if the protective structure is a rear two-post rollbar, the selected height shall be whichever is greater from the formulae applicable above and below:
H = (25 + 0,20 M) (B6 + B) / 2B
for tractor with a reference mass of less than 2 000 kg;
H = (125 + 0,15 M) (B6 + B) / 2B
for tractor with a reference mass of more than 2 000 kg.
for other types of protective structures, the selected height shall be whichever is greater from the formulae applicable above and below:
H = 25 + 0,20 M
for tractor with a reference mass less than 2 000 kg;
H = 125 + 0,15 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
The beam shall be positioned over the rear uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after the cessation of any visually detectable movement of the protective structure.
Where the rear part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the rear of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
The beam shall be positioned across the front uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane. A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after the cessation of any visually detectable movement of the protective structure.
Where the front part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the front of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
If cracks or tears which cannot be considered negligible appear during an impact test, a second, similar test, but with a height of fall of:
H’ = (H × 10–1) (12 + 4a) (1 + 2a)–1
shall be performed immediately after the impact tests causing these tears or cracks to appear, “a” being the ratio of the permanent deformation (Dp) to the elastic deformation (De):
a = Dp / De
as measured at the point of impact. The additional permanent deformation due to the second impact shall not exceed 30 per cent of the permanent deformation due to the first impact.
In order to be able to carry out the additional test, it is necessary to measure the elastic deformation during all the impact tests.
If during a crushing test, significant cracks or tears appear, a second, similar, crushing test, but with a force equal to 1,2 Fv shall be performed immediately after the crushing tests which caused these tears or cracks to appear.
After each test all structural members, joints and fastening systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
Any tears caused by the edges of the pendulum weight are to be ignored.
During each test the protective structure shall be examined to see whether any part it has entered a clearance zone round the driving seat as defined in 1.6.
Furthermore, the clearance zone shall not be outside the protection of the protective structure. For this purpose, it shall be considered to be outside the protection of the structure if any part of it would come in contact with flat ground if the tractor overturned towards the direction from which the test load is applied. For estimating this, the front and rear tyres and track width setting shall be the smallest standard fitting specified by the manufacturer.
The elastic deflection shall be measured (810 + av) mm above the seat index point, in the vertical plane in which the load is applied. For this measurement, any apparatus similar to that illustrated in Figure 7.8 may be used.
After the final crushing test, the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be used.
The load application point shall be that part of the roll-over protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The vertical plane in which the load is applied shall be located at a distance of one third of the external width of the upper part of the structure from the median plane.
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 2,165 × 10–7 M L2
or
Eil = 0,574 × I
Eil = 500 + 0,5 M
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 500 + 0,5 M
if the protective structure is a rear two-post rollbar the preceding formula shall also apply,
for other types of protective structures, the energy shall be whichever is the higher of the above or either of the following as selected:
Eil = 2,165 × 10–7 ML2
or
Eil = 0,574 I
Eis = 1,75 M
Eis = 1,75 M
or
Eis = 1,75 M (B6 + B)/2B
All provisions are identical to those given in 3.2.1.1.4.
All provisions are identical to those given in 3.2.1.1.5.
An overload test shall be carried out in all cases where the force decreases by more than 3 per cent during the last 5 per cent of the deflection reached when the energy required is absorbed by the structure (see Figure 7.10).
The overload test involves the gradual increase of the horizontal load by increments of 5 per cent of the initial energy requirement up to a maximum of 20 per cent of energy added (see Figure 7.11).
The overload test is satisfactory if, after each increase by 5, 10, or 15 per cent in the energy required, the force decreases by less than 3 per cent for a 5 per cent increment and remains greater than 0,8 Fmax.
The overload test is satisfactory if, after the structure has absorbed 20 per cent of the added energy, the force exceeds 0,8 Fmax.
Additional cracks or tears and/or entry into or lack of protective of the clearance zone due to elastic deflection are permitted during the overload test. However, after the removal of the load, the structure shall not enter the clearance zone, which shall be completely protected.
If cracks or tears which cannot be considered as negligible appear during a crushing test, a second, similar crushing, but with a force of 1,2 Fv shall be applied immediately after the crushing test which caused the cracks or tears to appear.
After each test all structural members, joints and attachment systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
During each test the protective structure shall be examined to see whether any part of it has entered a clearance zone as defined in 1.6 of Annex I.
In addition, an examination shall be made to determine whether any part of the clearance zone is outside the protection of the structure. For this purpose it is considered to be outside the protection of the roll-over protective structure if any part of it would have come in contact with the ground plane if the tractor had overturned in the direction from which the impact came. For this purpose the front and rear tyres and track setting are assumed to be the smallest specified by the manufacturer.
The elastic deflection shall be measured (810 + av) mm above the seat index point, in the vertical plane in which the load is applied. For this measurement, any apparatus similar to that illustrated in Figure 7.8 may be used.
After the final crushing test, the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be used.
Extension to other tractor models
When technical modifications occur on the tractor, the protective structure or the method of attachment of the protective structure to the tractor, the testing station that has carried out the original test can issue a ‘technical extension report’ in the following cases:
The impact and crushing tests need not be carried out on each model of tractor, provided that the protective structure and tractor comply with the conditions referred to hereunder 3.3.2.1.1 to 3.3.2.1.5.
This procedure has to be followed when the provisions of paragraph 3.3.2.1 are not fulfilled, it may not be used when the method of attachment of the protective structure to the tractor does not remain of the same principle (e.g. rubber supports replaced by a suspension device):
Modifications having no impact on the results of the initial test (e.g. weld attachment of the mounting plate of an accessory in a non-critical location on the structure), addition of seats with different SIP location in the protective structure (subject to checking that the new clearance zone(s) remain(s) within the protection of the deflected structure throughout all tests).
Modifications having a possible impact on the results of the original test without calling into question the acceptability of the protective structure (e.g. modification of a structural component, modification of the method of attachment of the protective structure to the tractor). A validation test can be carried out and the test results will be drafted in the extension report.
The following limits for this type extension are fixed:
no more than 5 extensions may be accepted without a validation test;
the results of the validation test will be accepted for extension if all the acceptance conditions of the Code are fulfilled and:
if the deflection measured after each impact test does not deviate from the deflection measured after each impact test in the original test report by more than ± 7 % (in case of a dynamic test);
if the force measured when the required energy level has been reached in the various horizontal load tests does not deviate from the force measured when the required energy has been reached in the original test by more than ± 7 % and the deflection measured(12) when the required energy level has been reached in the various horizontal load tests does not deviate from the deflection measured when the required energy has been reached in the original test by more than ± 7 % (in case of a static test).
more than one protective structure modifications may be included in a single extension report if they represent different options of the same protective structure, but only one validation test can be accepted in a single extension report. The options not tested shall be described in a specific section of the extension report.
Increase of the reference mass declared by the manufacturer for a protective structure already tested. If the manufacturer wants to keep the same approval number it is possible to issue an extension report after having carried out a validation test (the limits of ± 7 % specified in 3.3.2.2.2.2 are not applicable in such a case).
Steel with an as-rolled thickness less than 2,5 mm and with a carbon content less than 0,2 per cent is considered to meet this requirement.
Structural members of the protective structure made from materials other than steel shall have equivalent low temperature impact resistance.
Minimum Charpy V-notch impact energies
a Indicates preferred size. Specimen size shall be no less than largest preferred size that the material permits. | ||
b The energy requirement at – 20 °C is 2,5 times the value specified for – 30 °C. Other factors affect impact energy strength, i.e. direction of rolling, yield strength, grain orientation and welding. These factors shall be considered when selecting and using steel. | ||
Specimen size | Energy at | Energy at |
---|---|---|
-30 °C | -20 °C | |
mm | J | Jb |
10 × 10a | 11 | 27,5 |
10 × 9 | 10 | 25 |
10 × 8 | 9,5 | 24 |
10 × 7,5a | 9,5 | 24 |
10 × 7 | 9 | 22,5 |
10 × 6,7 | 8,5 | 21 |
10 × 6 | 8 | 20 |
10 × 5a | 7,5 | 19 |
10 × 4 | 7 | 17,5 |
10 × 3,5 | 6 | 15 |
10 × 3 | 6 | 15 |
10 × 2,5a | 5,5 | 14 |
Directive 86/415/EEC is amended as follows:
Annex II is amended as follows:
point 2.4.2.2.3. is replaced by the following:
the following point 2.5 is added:
Annex III is amended as follows:
Under symbol 1 insert ‘ISO 3767-1:1998, symbol 8.18 may be used as alternative’,
Under symbol 3 insert ‘ISO 3767-1:1998, symbol 8.19 may be used as alternative’,
Under symbol 6 insert ‘ISO 3767-2:1991, symbol 7.11 combined with ISO 3767-1:1998, symbol 7.1 to 7.5 may be used as alternative’,
Under symbol 7 insert ‘ISO 3767-2:1991, symbol 7.12 PTO display combined with ISO 3767-1:1991, symbol 7.1 to 7.5 may be used as alternative’.
Directive 87/402/EEC is amended as follows:
In Annex I, point 1 is replaced by the following:
Roll-over protective structure (safety cab or frame), hereinafter called ‘protective structure’, means the structure on a tractor the essential purpose of which is to avoid or limit risks to the driver resulting from roll-over of the tractor during normal use.
The roll-over protective structure is characterized by the provision of space for a clearance zone large enough to protect the driver when seated either inside the envelope of the structure or within a space bounded by a series of straight lines from the outer edges of the structure to any part of the tractor that might come into contact with flat ground and that is capable of supporting the tractor in that position if the tractor overturns.
The median plane of the wheel is equidistant from the two planes containing the periphery of the rims at their outer edges.
The vertical plane through the wheel axis intersects its median plane along a straight line which meets the supporting surface at one point. If A and B are the two points thus defined for the wheels on the same axle of the tractor, then the track width is the distance between points A and B. The track may be thus defined for both front and rear wheels. Where there are twin wheels, the track is the distance between two planes each being the median plane of the pairs of wheels.
Take the extreme positions of points A and B for the tractor rear axle, which gives the maximum possible value for the track. The vertical plane at right angles to the line AB at its centre point is the median plane of the tractor.
The distance between the vertical planes passing through the two lines AB as defined above, one for the front wheels and one for the rear-wheels.
The seat index point shall be determined in accordance with ISO 5353:1995
The clearance zone (Figure 6.1 in Annex II) is defined on the basis of a vertical reference plane and a reference line:
The reference plane is a vertical plane, generally longitudinal to the tractor and passing through the seat index point and the centre of the steering wheel. Normally the reference plane coincides with the longitudinal median plane of the tractor. This reference plane shall be assumed to move horizontally with the seat and steering wheel during loading but to remain perpendicular to the tractor or the floor of the roll-over protective structure.
The reference line is the line contained in the reference plane that passes through a point located 140 + ah rearward and 90 – av below the seat index point and the first point on the steering wheel rim that it intersects when brought to the horizontal.
The clearance zone for tractors with a non-reversible seat is defined in 1.6.2.1 to1.6.2.11 below and is bounded by the following planes, the tractor being on a horizontal surface, the seat, where adjustable, adjusted to its rear uppermost position(15), and the steering wheel, where adjustable, adjusted to the mid-position for seated driving:
two vertical planes 250 mm on either side of the reference plane, these vertical planes extending 300 mm upwards from the plane defined in 1.6.2.8 below and longitudinally at least 550 mm in front of the vertical plane perpendicular to the reference plane passing (210 – ah) mm in front of the seat index point;
two vertical planes 200 mm on either side of the reference plane, these vertical planes extending 300 mm upwards from the plane defined in 1.6.2.8 below and longitudinally from the surface defined in 1.6.2.11 below to the vertical plane perpendicular to the reference plane passing (210 – ah) mm in front of the seat index point;
an inclined plane perpendicular to the reference plane, parallel with and 400 mm above the reference line, extending backwards to the point where it intersects the vertical plane which is perpendicular to the reference plane and which passes through a point (140 + ah) mm rearward of the seat index point;
an inclined plane, perpendicular to the reference plane which meets the plane defined in 1.6.2.3 above at its rearmost edge and rests on the top of the seat back rest;
a vertical plane perpendicular to the reference plane, passing at least 40 mm forward of the steering wheel and at least 760 – ah forward of the seat index point;
a cylindrical surface with its axis perpendicular to the reference plane, having a radius of 150 mm and tangential to the planes defined in 1.6.2.3 and 1.6.2.5;
two parallel inclined planes passing through the upper edges of the planes defined in 1.6.2.1 above with the inclined plane on the side where the impact is applied no closer than 100 mm to the reference plane above the zone of clearance;
a horizontal plane passing through a point 90 – av below the seat index point;
two portions of the vertical plane perpendicular to the reference plane passing 210 – ah forward of the seat index point, both these part planes joining respectively the rearmost limits of the planes defined in 1.6.2.1 above to the foremost limits of the planes defined in 1.6.2.2 above;
two portions of the horizontal plane passing 300 mm above plane defined in 1.6.2.8 above, both these part planes joining respectively the uppermost limits of the vertical planes defined in 1.6.2.2 above to the lowermost limits of the oblique planes defined in 1.6.2.7 above;
a surface, curved if necessary, whose generating line is perpendicular to the reference plane and rests on the back of the seat backrest.
For tractors with a reversible driver’s position (reversible seat and steering wheel), the clearance zone is the envelope of the two clearance zones defined by the two different positions of the steering wheel and the seat.
:
± 3 mm
:
:
± 1 mm
:
± 1 mm
:
± 1 mm
:
± 1 %
:
± 2 %
:
± 2°
ah | (mm) | Half of the horizontal seat adjustment |
av | (mm) | Half of the vertical seat adjustment |
B | (mm) | Minimum overall width of the tractor |
Bb | (mm) | Maximum outer width of the protective structure |
D | (mm) | Deflection of the structure at the point of impact (dynamic tests) or at the point of, and in line with, the load application (static tests) |
D′ | (mm) | Deflection of the structure for the calculated energy required |
Ea | (J) | Strain energy absorbed at point when load is removed. Area contained within F-D curve |
Ei | (J) | Strain energy absorbed. Area under F-D curve |
E′i | (J) | Strain energy absorbed after additional loading following a crack or tear |
E″i | (J) | Strain energy absorbed in overload test in the event of the load having been removed before starting this overload test. Area under F-D curve |
Eil | (J) | Energy input to be absorbed during longitudinal loading |
Eis | (J) | Energy input to be absorbed during side loading |
F | (N) | Static load force |
F′ | (N) | Loading force for calculated energy required, corresponding to E′i |
F-D | Force/deflection diagram | |
Fi | (N) | Force applied to rear hard fixture |
Fmax | (N) | Maximum static load force occurring during loading, with the exception of the overload |
Fv | (N) | Vertical crushing force |
H | (mm) | Falling height of the pendulum block (dynamic tests) |
H′ | (mm) | Falling height of the pendulum block for additional test (dynamic tests) |
I | (kg.m2) | Tractor reference moment of inertia about the centre line of the rear wheels, whatever the mass of these rear wheels may be |
L | (mm) | Tractor reference wheelbase |
M | (kg) | Tractor reference mass during strength tests, as defined in section 3.2.1.4 in Annex II’ ’ |
Annex II is replaced by the following text:
The technical requirements for the EC type-approval of roll-over protection structures mounted in front of the driver’s seat on narrow-track wheeled agricultural or forestry tractors shall be those set out in point 3 of Code 6(16) of the OECD Decision C(2008) 128 of October 2008, with the exception of points 3.2.4 (Test report), 3.4.1 (Administrative extension), 3.5 (Labelling) and 3.7 (Seat belt anchorage performance), reading as follows:
The protective structure may only be subjected to the strength tests if both the Lateral Stability Test and the Non-Continuous Rolling Test have been satisfactorily completed (see flow diagram as Figure 6.3).
This test is intended to check whether a structure fitted to the tractor for the protection of the driver can satisfactorily prevent continuous roll-over of the tractor in the event of its overturning laterally on a slope with a gradient of 1 in 1,5 (Figure 6.4).
Evidence of non-continuous rolling can be provided in accordance with one of the two methods described in 3.1.4.2 and 3.1.4.3.
A = 235 ± 20
or
B = 335 ± 20
B0 | (m) | Rear tyre width |
B6 | (m) | Width of protective structure between the right and left points of impact |
B7 | (m) | Width of engine bonnet |
D0 | (rad) | Front-axle swing angle from zero position to end of travel |
D2 | (m) | Height of front tyres under full axle load |
D3 | (m) | Height of rear tyres under full axle load |
H0 | (m) | Height of the front-axle pivot point |
H1 | (m) | Height of centre of gravity |
H6 | (m) | Height at the point of impact |
H7 | (m) | Height of engine bonnet |
L2 | (m) | Horizontal distance between the centre of gravity and front axle |
L3 | (m) | Horizontal distance between the centre of gravity and rear axle |
L6 | (m) | Horizontal distance between the centre of gravity and the leading point of intersection of the protective structure (to be preceded by a minus sign if this point lies in front of the plane of the centre of gravity) |
L7 | (m) | Horizontal distance between the centre of gravity and the front corner of the engine bonnet |
Mc | (kg) | Tractor mass used for calculation |
Q | (kgm2) | Moment of inertia about the longitudinal axis through the centre of gravity |
S | (m) | Rear track width |
The sum of the track (S) and tyre (B0) widths must be greater than the width B6 of the protective structure.
the stationary tractor overturns on a slope with a 1/1,5 gradient with a balanced front axle, as soon as the centre of gravity is vertically above the axis of rotation;
the axis of rotation is parallel to the tractor’s longitudinal axis and passes through the centre of the contact surfaces of the downhill front and rear wheel;
the tractor does not slide downhill;
impact on the slope is partly elastic, with a coefficient of elasticity of:
U = 0,2
the depth of penetration into the slope and the deformation of the protective structure together amount to:
T = 0,2 m
no other components of the tractor penetrate into the slope.
The distance between the rear and front axles on both sides of the tractor shall be measured in order to verify there is no steering angle.
The distances between the centre of gravity and the rear axle (L3) or the front axle (L2) shall be calculated from the mass distribution of the tractor between the rear and the front wheels.
The distance from the highest point of the tyre to the ground plane shall be measured (Figure 6.5), and the same method shall be used for the front and rear tyres.
The distance between the centre of gravity and the leading point of intersection of the protective structure shall be measured (Figures 6.6.a, 6.6.b and 6.6.c). If the protective structure is in front of the plane of the centre of gravity, the recorded measure will be preceded by a minus sign (–L6).
The distance between the right and left points of impact of the two vertical posts of the structure shall be measured.
The point of impact is defined by the plane tangent to the protective structure passing through the line made by the top outer points of the front and rear tyres (Figure 6.7).
The vertical distance from the point of impact of the structure to the ground plane shall be measured.
The vertical distance from the point of impact of the engine bonnet to the ground plane shall be measured.
The point of impact is defined by the plane tangent to the engine bonnet and the protective structure passing through the top outer points of the front tyre (Figure 6.7). The measurement shall be made on both sides of the engine bonnet.
The distance between the two points of impact of the engine bonnet as defined previously shall be measured.
The distance from the point of impact of the engine bonnet, as defined previously, to the centre of gravity shall be measured.
The vertical distance between the centre of the front-axle pivot point to the centre of axle of the front tyres (H01) shall be included in the manufacturer’s technical report and shall be checked.
The vertical distance from the centre of the front tyres axle to the ground plane (H02) shall be measured (Figure 6.8).
The height of the front-axle pivot (H0) is the sum of both previous values.
The minimum rear track width fitted with tyres of the largest size, as specified by the manufacturer, shall be measured (Figure 6.9).
The distance between the outer and the inner vertical planes of a rear tyre in its upper part shall be measured (Figure 6.9).
The largest angle defined by the swinging of the front axle from the horizontal position to the maximum deflection shall be measured on both sides of the axle, taking into account any end-stroke shock absorber. The maximum angle measured shall be used.
The tractor mass shall be determined according to the conditions specified in paragraph 3.2.1.4.
Tests made using special rigs are intended to simulate such loads as are imposed on a protective structure, when the tractor overturns. These tests enable observations to be made on the strength of the protective structure and any brackets attaching it to the tractor and any parts of the tractor which transmit the test load.
Tests may be performed in accordance with the dynamic procedure or the static procedure. The two methods are deemed equivalent.
Note: A complete tractor is not required for the static strength test; however, the protective structure and parts of the tractor to which it is attached represent an operating installation, hereinafter referred to as ‘the assembly’.
Components which may create a hazard in the clearance zone must also be fitted on the tractor (or the assembly) so that they may be examined to see whether the requirements of the Acceptance Conditions in 3.2.3 have been fulfilled.
All components of the tractor or the protective structure including weather protective must be supplied or described on drawings.
The reference mass M, used in the formulae to calculate the height of the fall of the pendulum block, the loading energies and the crushing forces, must be at least the mass of the tractor, excluding optional accessories but including coolant, oils, fuel, tools plus the protective structure. Not included are optional front or rear weights, tyre ballast, mounted implements, mounted equipment or any specialised components.
The sequence of tests, without prejudice to the additional tests mentioned in sections 3.3.1.1.6, 3.3.1.1.7, 3.3.2.1.6 and 3.3.2.1.7, is as follows:
impact (dynamic test) or loading (static test) at the rear of the structure
(see 3.3.1.1.1 and 3.3.2.1.1);
rear crushing test (dynamic or static test)
(see 3.3.1.1.4 and 3.3.2.1.4);
impact (dynamic test) or loading (static test) at the front of the structure
(see 3.3.1.1.2 and 3.3.2.1.2);
impact (dynamic test) or loading (static test) at the side of the structure
(see 3.3.1.1.3 and 3.3.2.1.3);
crushing at the front of the structure (dynamic or static test)
(see 3.3.1.1.5 and 3.3.2.1.5).
after each part-test it must be free from cracks or tears within the meaning of 3.3.1.2.1 or 3.2.3.1.2. If, during one of the tests, significant cracks or tears appear, an additional test, in accordance with dynamic tests or static tests, must be applied immediately after the impact or the crushing which caused cracks or tears to appear;
during the tests other than the overload test, no part of the protective structure must enter the clearance zone as defined in 1.6 in Annex I;
during the tests other than the overload test, all parts of the clearance zone shall be secured by the structure, in accordance with 3.3.1.2.2 and 3.3.2.2.2;
during the tests the protective structure must not impose any constraints on the seat structure;
the elastic deflection, measured in accordance with 3.3.1.2.3 and 3.3.2.2.3 shall be less than 250 mm.
The pendulum pivot points must be rigidly fixed so that their displacement in any direction does not exceed 1 per cent of the height of fall.
A rig as shown in Figure 6.14 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide connected to the load-applying mechanism by means of universal joints. Suitable axle stands shall be provided so that the tractor tyres do not bear the crushing force.
The following measuring apparatus is needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, (see Figure 6.15).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (see section 3.3.2.2.2).
at start of test, under zero load: ± 2°,
during test, under load: 10° above and 20° below the horizontal. These variations must be kept to a minimum.
If the tractor moves, the entire test shall be repeated, unless the system for measuring the deflections taken into account for plotting the force versus deflection curve is connected to the tractor.
A rig as shown in Figure 6.14 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide, connected to the load-applying mechanism by means of universal joints. Suitable axle stands must be provided so that the tractor tyres do not bear the crushing force.
The following measuring devices are also needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, (see Figure 6.15).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (section 3.3.2.2.2).
The suspended height of the block shall be adjusted and necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plan parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.2.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed in front of and tight against the rear wheels and then fixed to the ground.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg;
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
The suspended height of the pendulum block shall be adjusted and the necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first if the tractor overturned sideways while travelling forward, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plane parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.2.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed behind and tight against the rear wheels and then fixed to the ground.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg.
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
H = 2,165 × 10-8 M × L2
or
H = 5,73 × 10-2I
The suspended height of the pendulum block shall be adjusted and necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact shall be that part of the protective structure likely to hit the ground first in a sideways overturning accident.
With the wire ropes tensioned, the wedging beam shall be placed on the ground, pushed tight against the tyres on the side opposite that which is to receive the impact and then fixed to the ground. It may be necessary to use two beams or wedges if the outer sides of the front and rear tyres are not in the same vertical plane. The prop shall then be placed as indicated in Figure 6.13 against the rim of the most heavily loaded wheel opposite to the point of impact, pushed firmly against the rim and then fixed at its base. The length of the prop shall be such that it makes an angle of 30 ± 3° with the ground when in position against the rim. In addition, its thickness shall, if possible, be between 20 and 25 times less than its length and between 2 and 3 times less than its width. The props shall be shaped at both ends as shown in the details on Figure 6.13.
H = (25 + 0,20 M) (B6+B) / 2B
for tractor with a reference mass of less than 2 000 kg.
H = (125 + 0,15 M) (B6+B) / 2B
for tractor with a reference mass of more than 2 000 kg.
H = 25 + 0,2 M
for tractor with a reference mass of less than 2 000 kg.
H = 125 + 0,15 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
The beam shall be positioned over the rear uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane. A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after cessation of any visually detectable movement of the protective structure.
Where the rear part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the rear of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
The beam shall be positioned across the front uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane. A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after the cessation of any visually detectable movement of the protective structure.
Where the front part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the front of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
If cracks or tears which cannot be considered negligible appear during an impact test, a second, similar test, but with a height of fall of:
H′ = (H × 10-1) (12 + 4a) (1 + 2a)-1
shall be performed immediately after the impact tests causing these tears or cracks to appear, ‘a’ being the ratio of the permanent deformation (Dp) to the elastic deformation (De):
a = Dp / De
as measured at the point of impact. The additional permanent deformation due to the second impact shall not exceed 30 per cent of the permanent deformation due to the first impact.
In order to be able to carry out the additional test, it is necessary to measure the elastic deformation during all the impact tests.
If during a crushing test, significant cracks or tears appear, a second, similar, crushing test, but with a force equal to 1,2 Fv shall be performed immediately after the crushing tests which caused these tears or cracks to appear.
After each test all structural members, joints and fastening systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
Any tears caused by the edges of the pendulum weight are to be ignored.
During each test the protective structure shall be examined to see whether any part of it has entered the clearance zone round the driving seat as defined in 1.6.
Furthermore, the clearance zone shall not be outside the protection of the protective structure. For this purpose, it shall be considered to be outside the protection of the structure if any part of it would come in contact with flat ground if the tractor overturned towards the direction from which the test load is applied. For estimating this, the front and rear tyres and track width setting shall be the smallest standard fitting specified by the manufacturer.
If the tractor is fitted with a rigid section, a housing or other hard fixture placed behind the driver’s seat, this fixture shall be regarded as a protective point, in the event of sideways or rear overturning. This hard fixture placed behind the driver’s seat shall be capable of withstanding, without breaking or entering the clearance zone, a downward force Fi where:
Fi = 15 M
applied perpendicularly to the top of the frame in the central plane of the tractor. The initial angle of application of force shall be 40° calculated from a parallel to the ground as shown in Figure 6.16. The minimum width of this rigid section shall be 500 mm (see Figure 6.17).
In addition, it shall be sufficiently rigid and firmly attached to the rear of the tractor.
The elastic deflection is measured (810 + av) mm above the index point, in the vertical plane passing through the point of impact. For this measurement, apparatus similar to that illustrated in Figure 6.15 shall be used.
After the final crushing test, the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be used.
The load application point shall be that part of the roll-over protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The vertical plane in which the load is applied shall be located at a distance of 1/3 of the external width of the upper part of the structure from the median plane.
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 500 + 0,5 M
The load application point shall be that part of the roll-over protective structure likely to hit the ground first if the tractor overturned sideways while travelling forward, normally the upper edge.
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 500 + 0,5 M
Eil = 2,165 × 10–7M × L2
or
Eil = 0,574 I
Eis = 1,75 M(B6+B) / 2B
Eis = 1,75 M
All provisions are identical to those given in 3.3.1.1.4.
All provisions are identical to those given in 3.3.1.1.5.
An overload test shall be carried out in all cases where the force decreases by more than 3 per cent during the last 5 per cent of the deflection reached when the energy required is absorbed by the structure (see Figure 6.19).
The overload test involves the gradual increase of the horizontal load by increments of 5 per cent of the initial energy requirement up to a maximum of 20 per cent of energy added (see Figure 6.20).
The overload test is satisfactory if, after each increase by 5, 10, or 15 per cent in the energy required, the force decreases by less than 3 per cent for a 5 per cent increment and remains greater than 0,8 Fmax.
The overload test is satisfactory if, after the structure has absorbed 20 per cent of the added energy, the force exceeds 0,8 Fmax.
Additional cracks or tears and/or entry into or lack of protective of the clearance zone due to elastic deflection are permitted during the overload test. However, after the removal of the load, the structure shall not enter the clearance zone, which shall be completely protected.
If cracks or tears which cannot be considered as negligible appear during a crushing test, a second, similar crushing, but with a force of 1,2 Fv shall be applied immediately after the crushing test which caused the cracks or tears to appear.
After each test all structural members, joints and attachment systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
During each test the protective structure shall be examined to see whether any part of it has entered the clearance zone as defined in 1.6 in Annex I.
Furthermore, the clearance zone shall not be outside the protection of the protective structure. For this purpose, it shall be considered to be outside the protection of the structure if any part of it would come in contact with flat ground if the tractor overturned towards the direction from which the test load is applied. For estimating this, the front and rear tyres and track width setting shall be the smallest standard fitting specified by the manufacturer.
If the tractor is fitted with a rigid section, a housing or other hard fixture placed behind the driver’s seat, this fixture shall be regarded as a protective point, in the event of sideways or rear overturning. This hard fixture placed behind the driver’s seat shall be capable of withstanding, without breaking or entering the clearance zone, a downward force Fi, where:
Fi = 15 M
applied perpendicularly to the top of the frame in the central plane of the tractor. The initial angle of application of force shall be 40° calculated from a parallel to the ground as shown in Figure 6.16. The minimum width of this rigid section shall be 500 mm (see Figure 6.17).
In addition, it shall be sufficiently rigid and firmly attached to the rear of the tractor.
The elastic deflection shall be measured (810+av) mm above the seat index point, in the vertical plane in which the load is applied. For this measurement, any apparatus similar to that illustrated in Figure 6.15 shall be used.
After the final crushing test the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be recorded.
When technical modifications occur on the tractor, the protective structure or the method of attachment of the protective structure to the tractor, the testing station that has carried out the original test can issue a ‘technical extension report’ if the tractor and protective structure satisfied preliminary tests of lateral stability and non-continuous rolling as defined in 3.1.3 and 3.1.4 and if the rear hard fixture as described in paragraph 3.3.1.2.2.2, when fitted, has been tested in accordance with the procedure described in this paragraph (except 3.4.2.2.4) in the following cases:
The impact or loading and crushing tests need not be carried out on each model of tractor, provided that the protective structure and tractor comply with the conditions referred to hereunder 3.4.2.1.1 to 3.4.2.1.5.
This procedure has to be followed when the provisions of paragraph 3.4.2.1 are not fulfilled, it may not be used when the method of attachment of the protective structure to the tractor does not remain of the same principle (e.g. rubber supports replaced by a suspension device):
Modifications having no impact on the results of the initial test (e.g. weld attachment of the mounting plate of an accessory in a non-critical location on the structure), addition of seats with different SIP location in the protective structure (subject to checking that the new clearance zone(s) remain(s) within the protection of the deflected structure throughout all tests).
Modifications having a possible impact on the results of the original test without calling into question the acceptability of the protective structure (e.g. modification of a structural component, modification of the method of attachment of the protective structure to the tractor). A validation test can be carried out and the test results will be drafted in the extension report.
The following limits for this type extension are fixed:
no more than 5 extensions may be accepted without a validation test;
the results of the validation test will be accepted for extension if all the acceptance conditions of the Code are fulfilled and:
if the deflection measured after each impact test does not deviate from the deflection measured after each impact test in the original test report by more than ± 7 % (in the case of dynamic tests),
if the force measured when the required energy level has been reached in the various horizontal load tests does not deviate from the force measured when the required energy has been reached in the original test by more than ± 7 % and the deflection measured(18) when the required energy level has been reached in the various horizontal load tests does not deviate from the deflection measured when the required energy has been reached in the original test report by more than ± 7 % (in the case of static tests).
more than one protective structure modifications may be included in a single extension report if the represent different options of the same protective structure, but only one validation test can be accepted in a single extension report. The options not tested shall be described in a specific section of the extension report.
Increase of the reference mass declared by the manufacturer for a protective structure already tested. If the manufacturer wants to keep the same approval number it is possible to issue an extension report after having carried out a validation test (the limits of ± 7 % specified in 3.4.2.2.2.2 are not applicable in such a case).
Modification of the rear hard fixture or addition of a new rear hard fixture. It has to be checked that the clearance zone remains within the protection of the deflected structure throughout all test taking into account the new or modified rear hard fixture. A validation of the rear hard fixture consisting in the test described in 3.3.1.2.2.2 or 3.3.2.2.2.2 has to be carried out and the test results will be drafted in the extension report.
Steel with an as-rolled thickness less than 2,5 mm and with a carbon content less than 0,2 per cent is considered to meet this requirement.
Structural members of the protective structure made from materials other than steel shall have equivalent low temperature impact resistance.
Minimum Charpy V-notch impact energies
a Indicates preferred size. Specimen size shall be no less than largest preferred size that the material permits. | ||
b The energy requirement at – 20 °C is 2,5 times the value specified for – 30 °C. Other factors affect impact energy strength, i.e. direction of rolling, yield strength, grain orientation and welding. These factors shall be considered when selecting and using steel. | ||
Specimen size | Energy at | Energy at |
---|---|---|
-30 °C | -20 °C | |
mm | J | Jb |
10 × 10a | 11 | 27,5 |
10 × 9 | 10 | 25 |
10 × 8 | 9,5 | 24 |
10 × 7,5a | 9,5 | 24 |
10 × 7 | 9 | 22,5 |
10 × 6,7 | 8,5 | 21 |
10 × 6 | 8 | 20 |
10 × 5a | 7,5 | 19 |
10 × 4 | 7 | 17,5 |
10 × 3,5 | 6 | 15 |
10 × 3 | 6 | 15 |
10 × 2,5a | 5,5 | 14 |
Figure 6.3
Flow diagram for determining the continuous roll-over behaviour of a laterally overturning tractor with a front mounted roll-over protective structure (ROPS)
In Annex I, Appendix 4, point 1 Section 2 of Directive 2000/25/EC is replaced by the following:
Directive 2003/37/EC is amended as follows:
In Annex I, model A is amended as follows:
Point 2.4 is replaced by the following:
Unbraked towable mass: …
Independently braked towable mass: …
Inertia-braked towable mass: …
Towable mass when fitted with hydraulic or pneumatic braking: …
Total technically permissible mass(es) of the tractor-trailer combination for each configuration of trailer braking: …
Position of coupling point
Height above ground
Maximum height: …
Minimum height: …
Distance from the vertical plane passing through the axis of the rear axle
Maximum: …
Minimum: …
Maximum static vertical load/technically permissible mass on the coupling point:
of the tractor: …
of the semi-trailer (interchangeable towed machinery) or the centre-axle trailer (interchangeable towed machinery): …’
Point 2.7.2 is replaced by the following:
Length for on-road use (10):
maximum: …
minimum: …
Width for on-road use (11):
maximum: …
minimum: …
Height for on-road use (12):
maximum: …
minimum: …
Forward overhang (13):
maximum: …
minimum: …
Rear overhang (14):
maximum: …
minimum: …
Ground clearance (15):
maximum: …
minimum: …’
In Annex I, Model A, Footnote 15 shall read as follows: ‘Standard ISO 612/-6.8:1978’.
In Annex II, Chapter B, Part II.C is amended as follows:
in the introductory phrase, the words ‘test bulletin’ are replaced by ‘test report’;
(concerns only the English version)
the footnote (*) is replaced by the following:
OECD standard code for the official testing of rear-mounted roll-over protective structures on narrow-track wheeled agricultural and forestry tractors.
For extension tests to test reports that originally used seat reference point (SRP), the required measurements shall be made with reference to SRP instead of SIP and the use of SRP shall be clearly indicated (see Annex 1).
Users are reminded that the seat index point is determined according to ISO 5353 and is a fixed point with respect to the tractor that does not move as the seat is adjusted away from the mid-position. For purposes of determining the clearance zone, the seat shall be placed in the rear and uppermost position.” ’
Permanent + elastic deflection measured at the point when the required energy level is obtained.” ’
OECD standard code for the official testing of front mounted roll-over protective structures on narrow-track wheeled agricultural and forestry tractors.
For extension tests to test reports that originally used seat reference point (SRP), the required measurements shall be made with reference to SRP instead of SIP and the use of SRP shall be clearly indicated (see Annex 1).
Users are reminded that the seat index point is determined according to ISO 5353 and is a fixed point with respect to the tractor that does not move as the seat is adjusted away from the mid-position. For purposes of determining the clearance zone, the seat shall be placed in the rear and uppermost position.” ’
OECD standard code for the official testing of front mounted roll-over protective structures on narrow-track wheeled agricultural and forestry tractors.
The programme and the examples are available on the OECD website.
Permanent + elastic deflection measured at the point when the required energy level is obtained.” ’
The Whole Directive you have selected contains over 200 provisions and might take some time to download. You may also experience some issues with your browser, such as an alert box that a script is taking a long time to run.
Would you like to continue?
The Schedules you have selected contains over 200 provisions and might take some time to download. You may also experience some issues with your browser, such as an alert box that a script is taking a long time to run.
Would you like to continue?
Latest Available (revised):The latest available updated version of the legislation incorporating changes made by subsequent legislation and applied by our editorial team. Changes we have not yet applied to the text, can be found in the ‘Changes to Legislation’ area.
Original (As adopted by EU): The original version of the legislation as it stood when it was first adopted in the EU. No changes have been applied to the text.
Access essential accompanying documents and information for this legislation item from this tab. Dependent on the legislation item being viewed this may include:
Use this menu to access essential accompanying documents and information for this legislation item. Dependent on the legislation item being viewed this may include:
Click 'View More' or select 'More Resources' tab for additional information including:
The data on this page is available in the alternative data formats listed: