29 C.F.R. § 1926.1002
Link to an amendment published at 84 FR 21578, May 14, 2019.
(a) General.
(5) The following provisions address requirements for protective enclosures.
(c) Performance requirements.
(d) Test procedures - general.
(4) The following provisions address soil bank test conditions.
(7) Vehicle overturn test - sideways and rearward.
(g) Static test - (1) Test conditions.
(2) Test procedure.
(i) The side-load application shall be at the upper extremity of the frame upright at a 90° angle to the centerline of the vehicle. The side load L shall be applied according to Figure W-16. L and D shall be recorded simultaneously. The test shall be stopped when:
(i) The frame, overhead weather shield, fenders, or other parts in the operator area may be deformed in these tests, but shall not shatter or leave sharp edges exposed to the operator, or violate the dimensions shown in Figures W-16 and W-17, and specified as follows:
D = 2 in. (51 mm) inside of the frame upright to the vertical centerline of the seat;
E = 30 in. (762 mm);
F = Not less than 0 in. (0 mm) and not more than 12 in. (305 mm), measured at the centerline of the seat backrest to the crossbar along the line of load application as shown in Figure W-17; and
G = 24 in. (610 mm).
(j) Definitions applicable to this section.
(3) The following symbols, terms, and explanations apply to this section:
Eis = Energy input to be absorbed during side loading in ft-lb (E′is in J [joules]);
Eis = 723 + 0.4 W ft-lb (E′ is = 100 + 0.12 W′ , J);
Eir = Energy input to be absorbed during rear loading in ft-lb (E′ ir in J);
Eir = 0.47 W ft-lb (E′ ir = 0.14 W′, J);
W = Tractor weight as specified by 29 CFR 1926.1002(e)(1) and (e)(3), in lb (W′ , kg);
L = Static load, lb (kg);
D = Deflection under L, in. (mm);
L-D = Static load-deflection diagram;
Lm-Dm = Modified static load-deflection diagram (Figure W-20). To account for an increase in strength due to an increase in strain rate, raise L in the plastic range L × K;
K = Increase in yield strength induced by higher rate of loading (1.3 for hot, rolled, low-carbon steel 1010-1030). Low carbon is preferable; however, when higher carbon or other material is used, K must be determined in the laboratory. Refer to Norris, C.H., Hansen, R.J., Holley, M.J., Biggs, J.M., Namyet, S., and Minami, J.V., Structural Design for Dynamic Loads, McGraw-Hill, New York, 1959, p. 3;
Lmax = Maximum observed static load;
Load Limit = Point on a continuous L-D curve at which the observed static load is 0.8 Lmax (refer to Figure W-19);
Eu = Strain energy absorbed by the frame, ft-lb (J); area under the Lm-Dm curve;
FER = Factor of energy ratio, FER = EuEis; also, FER = EuEir;
Pb = Maximum observed force in mounting connection under a static load, L, lb (kg);
Pu = Ultimate force capacity of mounting connection, lb (kg);
FSB = Design margin for a mounting connection (PuPb)−1; and
H = Vertical height of lift of 4,410-lb (2,000-kg) weight, in. (H′, mm). The weight shall be pulled back so that the height of its center of gravity above the point of impact is defined as follows: H = 4.92 + 0.00190 W (H′ = 125 + 0.107 W′) (see Figure W-24).
[70 FR 76985, Dec. 29, 2005, as amended at 71 FR 41129, July 20, 2006]