1. Introduction
1.1 Where the stability of a Small Workboat is assessed using the righting moment curve
prepared to show compliance of the design with ISO 12217, this curve shall be subject to
verification and, if necessary, correction, as set out below.
1.2 ISO 12217 normally requires the stability to be assessed in the Minimum Operating
Condition. However, where the Loaded Displacement Mass is more than 15% greater than the
former, the stability also has to be assessed in this heavier condition.
1.3 Where data is available for both conditions, the heavier should be used for the
purposes of this Code.
2. Stability Verification Test
2.1 The vessel to be certified shall be subjected to the stability verification test
when as close as practicable to the loading condition used for the righting moment curve
to be checked, as defined in ISO 12217. The purpose of the test is to verify that the
stability of the vessel is adequately described by the righting moment curve of the
“First of Type” used for ISO 12217 assessment. Where this is not adequately
demonstrated, this curve shall be corrected as described below before reassessment of
the stability compliance.
2.2 The test shall be conducted in calm conditions. The vessel shall be heeled to both
port and starboard as much as practicable by the application of a heeling moment
sufficient to produce a heel angle of firstly at least three degrees in either
direction, and secondly at least five degrees, i.e.: two heeling moments and four heel
angles in all. The heeling moments and angles of heel shall be recorded as precisely as
practicable.
2.3 The heeling moments shall be applied using weights that are part of the loaded
condition of the vessel, and moved through a known amount. The righting lever deduced
for that angle of heel is given by:

2.4 Where the weights used to create the heeling moment have to be moved vertically from
their normal location in order to generate the necessary heeling moment, the resulting
measured righting moment should be corrected for the change in the vertical
centre-of-gravity of the craft. The correction = GG1sinϕ, added to the
measured GZ when the weights were raised during the heeling test, where GG1
is the shift in vessel VCG due to the weights moved.
2.5 The First of Type righting moment curve shall be considered acceptable for stability
assessment if the average deviation of the four values obtained at 2.3 and corrected
according to 2.4 below the righting moment curve is equal to or less than 5%. Where the
deviation is above the curve, no limit shall apply.
2.6 Where the average deviation of the four values obtained at 2.3 above from the
righting moment curve is more than 5%, the First of Type righting moment curve shall be
corrected throughout the range of heel angles by an amount equal to GG1sin
ϕ, where ϕ is any heel angle. The value of GG1 used for this
correction shall be obtained as follows:
-
GG1 = { (δ1/sinϕ1) +
(δ2/sinϕ2) +
(δ3/sinϕ3) +
(δ4/sinϕ4) } / 4
-
where: δn = difference in measured GZ from First of Type GZ curve at
angle ϕn, for the four values obtained according to 2.2 and
calculated according to 2.3 and 2.4 above.
2.7 Where the righting moment curve is modified in this way, the stability shall then be
reassessed using the requirements of chapter 11 of the Code.