Circular Letter MSC/Circ.1026
AMENDMENTS TO THE CODE OF SAFE PRACTICE FOR CARGO STOWAGE AND SECURING (CSS
CODE)
(adopted
on 21 May 2002)
1.
The Maritime Safety Committee, at its seventy-fifth session (15 to 24 May
2002), approved amendments to the Code of Safe Practice for Cargo Stowage and
Securing (CSS Code), as developed by the DSC Sub-Committee at its sixth
session (16 to 20 July 2001) and set out in the Annex.
2.
Member Governments are invited to bring the amendments to the attention of
shipowners, ship operators, shipmasters and crews and all parties concerned.
Annex.
AMENDMENTS TO THE CODE OF SAFE PRACTICE FOR CARGO STOWAGE AND SECURING (CSS
CODE)
ANNEX 13.
METHODS TO ASSESS THE EFFICIENCY OF SECURING ARRANGEMENTS FOR NON-STANDARDIZED
CARGO
1.
In paragraph 1, after the second sentence a new sentence is added as follows:
"A11
lashing assemblies used in the application of the methods described in this
Annex must be attached to fixed securing points or strong supporting structures
marked on the cargo unit or advised as being suitable, or taken as a loop
around the unit with both ends secured to the same side as shown in Annex 5,
Figure 2 of the Code. Lashings going over the top of the cargo unit, which have
no defined securing direction but only act to increase friction by their
pretension, cannot be credited in the evaluation of securing arrangements
under this Annex."
4. STRENGTH OF SECURING EQUIPMENT
2.
In paragraph 4.2, the second sentence in the first sub-paragraph is replaced
by the following text:
"Safe
Working Load (SWL) may be substituted for MSL for securing purposes, provided
this is equal to or exceeds the strength defined by MSL."
3.
In Table 1 (as amended by MSC/Circ.812), "70% of breaking strength" on
the line regarding web lashing is replaced by "50% of breaking
strength".
4.
Existing paragraph 5 is replaced by the following text and re-numbered as
paragraph 6:
"When
using balance calculation methods for assessing the strength of the securing
devices, a safety factor is used to take account of the possibility of uneven
distribution of forces among the devices or reduced capability due to the
improper assembly of the devices or other reasons. This safety factor is used
in the formula to derive the calculated strength (CS) from the MSL and shown in
the relevant method used.
CS
= MSL/safety factor
Notwithstanding
the introduction of such a safety factor, care should be taken to use securing
elements of similar material and length in order to provide a uniform elastic
behaviour within the arrangement."
5.
Existing paragraph 6 is re-numbered as paragraph 5. Existing sub-paragraphs
6.1, 6.2 and 6.3 are re-numbered as 5.1, 5.2 and 5.3 accordingly.
7. ADVANCED CALCULATION METHOD
6.
After Table 3 the following text and formula are added:
"For
length/speed combinations not directly tabulated, the following formula may be
used to obtain the correction factor with v = speed in knots and L - length
between perpendiculars in metres:
This formula
shall not be used for ship lengths less than 50 m or more than 300 m."
7.
Under the existing paragraph 7.2, the following text and a new table are added:
"Friction
contributes towards prevention of sliding. The following friction coefficients
(µ) should be applied.
Table 5
Friction coefficients
Materials in contact |
Friction coefficient, (µ) |
timber-
timber, wet or dray steel-
timber or steel- rubber steel-steel,
dry steel-steel,
wet |
0,4 0,3 0,1 0,0 |
8.
In paragraph 7.2.1, the text from (µ = 0.3 for steel-timber or steel- rubber)
to (µ = 0.0 for steel-steel, wet) is deleted; "table 5" in the
definition of "f" is replaced by "table 6"; and a
formula is added under the definition of CS as follows:
9.
Existing Table 5 is re-numbered as Table 6.
10.
Under the re-numbered Table 6, the following text is added:
"As an
alternative to using Table 6 to determine the forces in a securing arrangement,
the method outlined in paragraph 7.3 can be used to take account of transverse
and longitudinal components of lashing forces."
11.
In paragraph 7.2.3, under the definition of CS a formula is added:
12.
A new paragraph 7.2.4 is added as follows:
"7.2.4 Calculated example
A calculated
example for this method is shown in Appendix l."
13.
A new paragraph 7.3 is added as follows:
"7.3
Balance of forces - alternative method
The balance of
forces described in paragraph 7.2.1 and 7.2.3 will normally furnish a
sufficiently accurate determination of the adequacy of the securing
arrangement. However, this alternative method allows a more precise
consideration of horizontal securing angles.
Securing
devices usually do not have a pure longitudinal or transverse direction in
practice but have an angle β in the horizontal
plane. This horizontal securing angle β is defined in
this Annex as the angle of deviation from the transverse direction. The angle β is to be scaled in the quadrantal mode, i.e.
between 0 and 90°.
Figure 3
- Definition of the vertical and horizontal securing angles α and β
A securing
device with an angle β develops
securing effects both in longitudinal and transverse direction, which can be expressed
by multiplying the calculated strength CS with the appropriate values of Fx
or Fy. The values of Fx and Fy can be obtained
from Table 7.
Table 7
consists of five sets of figures, one each for the friction coefficients µ =
0.4, 0.3, 0.2, 0.1 and 0. Each set of figures is obtained by using the vertical
angle α and horizontal angle β. The value of Fx is obtained when
entering the table with β from the right
while Fy is obtained when entering with β from the left, using the nearest tabular value for α and β. Interpolation
is not required but may be used.
The balance
calculations are made in accordance with the following formulae:
Transverse
sliding:
Fy
≤ µmg+Fy1CS1+...FynCSn
Longitudinal
sliding:
Fx
≤ µ(mg - F2) + Fx1CSl+FxnCSn
Transverse
tipping:
Fya
≤ bmg + 0.9(CS1ñ1 + CS2ñ2
+... + ÑSnñn)
Caution:
Securing
devices, which have a vertical angle a of less than 45° in combination with
horizontal angle β greater than 45°, should not be used
in the balance of transverse tipping in the above formula.
All symbols
used in these formulae have the same meaning as defined in paragraph 7.2 except
Fy and Fx, obtained from Table 7, and CS is as follows:
A calculated
example for this method is shown in Appendix 1.
Table 7
- Fx-values and Fy - values as a function of α, β and µ
Table 7.1 for µ = 0.4
β for Fy |
α |
β for Fx |
|||||||||||||
|
-30 |
-20 |
-10 |
0 |
10 |
20 |
30 |
40 |
45 |
50 |
60 |
70 |
80 |
90 |
|
0 |
0.67 |
0.80 |
0.92 |
1.00 |
1.05 |
1.08 |
1.07 |
1.02 |
0.99 |
0.95 |
0.85 |
0.72 |
0.57 |
0.40 |
90 |
10 |
0.65 |
0.79 |
0.90 |
0.98 |
1.04 |
1.06 |
1.05 |
1.01 |
0.98 |
0.94 |
0.84 |
0.71 |
0.56 |
0.40 |
80 |
20 |
0.61 |
0.75 |
0.86 |
0.94 |
0.99 |
1.02 |
1.01 |
0.98 |
0.95 |
0.91 |
0.82 |
0.70 |
0.56 |
0.40 |
70 |
30 |
0.55 |
0.68 |
0.78 |
0.87 |
0.92 |
0.95 |
0.95 |
0.92 |
0.90 |
0.86 |
0.78 |
0.67 |
0.54 |
0.40 |
60 |
40 |
0.46 |
0.58 |
0.68 |
0.77 |
0.82 |
0.86 |
0.86 |
0.84 |
0.82 |
0.80 |
0.73 |
0.64 |
0.53 |
0.40 |
50 |
50 |
0.36 |
0.47 |
0.56 |
0.64 |
0.70 |
0.74 |
0.76 |
0.75 |
0.74 |
0.72 |
0.67 |
0.60 |
0.51 |
0.40 |
40 |
60 |
0.23 |
0.33 |
0.42 |
0.50 |
0.56 |
0.61 |
0.63 |
0.64 |
0.64 |
0.63 |
0.60 |
0.55 |
0.48 |
0.40 |
30 |
70 |
0.10 |
0.18 |
0.27 |
0.34 |
0.41 |
0.46 |
0.50 |
0.52 |
0.52 |
0.53 |
0.52 |
0.49 |
0.45 |
0.40 |
20 |
80 |
-0.05 |
0.03 |
0.10 |
0.17 |
0.24 |
0.30 |
0.35 |
0.39 |
0.41 |
0.42 |
0.43 |
0.44 |
0.42 |
0.40 |
10 |
90 |
-0.20 |
-0.14 |
-0.07 |
0.00 |
0.07 |
0.14 |
0.20 |
0.26 |
0.28 |
0.31 |
0.35 |
0.38 |
0.39 |
0.40 |
0 |
Table 7.2 for µ = 0.3
β for Fy |
α |
β for Fx |
|||||||||||||
|
-30 |
-20 |
-10 |
0 |
10 |
20 |
30 |
40 |
45 |
50 |
60 |
70 |
80 |
90 |
|
0 |
0.72 |
0.84 |
0.93 |
1.00 |
1.04 |
1.04 |
1.02 |
0.96 |
0.92 |
0.87 |
0.76 |
0.62 |
0.47 |
0.30 |
90 |
10 |
0.70 |
0.82 |
0.92 |
0.98 |
1.02 |
1.03 |
1.00 |
0.95 |
0.91 |
0.86 |
0.75 |
0.62 |
0.47 |
0.30 |
80 |
20 |
0.66 |
0.78 |
0.87 |
0.94 |
0.98 |
0.99 |
0.96 |
0.91 |
0.88 |
0.83 |
0.73 |
0.60 |
0.46 |
0.30 |
70 |
30 |
0.60 |
0.71 |
0.80 |
0.87 |
0.90 |
0.92 |
0.90 |
0.86 |
0.82 |
0.79 |
0.69 |
0.58 |
0.45 |
0.30 |
60 |
40 |
0.51 |
0.62 |
0.70 |
0.77 |
0.81 |
0.82 |
0.81 |
0.78 |
0.75 |
0.72 |
0.64 |
0.54 |
0.43 |
0.30 |
50 |
50 |
0.41 |
0.50 |
0.58 |
0.64 |
0.69 |
0.71 |
0.71 |
0.69 |
0.67 |
0.64 |
0.58 |
0.50 |
0.41 |
0.30 |
40 |
60 |
0.28 |
0.37 |
0.44 |
0.50 |
0.54 |
0.57 |
0.58 |
0.58 |
0.57 |
0.55 |
0.51 |
0.45 |
0.38 |
0.30 |
30 |
70 |
0.15 |
0.22 |
0.28 |
0.34 |
0.39 |
0.42 |
0.45 |
0.45 |
0.45 |
0.45 |
0.43 |
0.40 |
0.35 |
0.30 |
20 |
80 |
0.00 |
0.06 |
0.12 |
0.17 |
0.22 |
0.27 |
0.30 |
0.33 |
0.33 |
0.34 |
0.35 |
0.34 |
0.33 |
0.30 |
10 |
90 |
-0.15 |
-0.10 |
-0.05 |
0.00 |
0.05 |
0.10 |
0.15 |
0.19 |
0.21 |
0.23 |
0.26 |
0.28 |
0.30 |
0.30 |
0 |
Table 7.3 for µ = 0.2
β for Fy |
α |
β for Fx |
|||||||||||||
|
-30 |
-20 |
-10 |
0 |
10 |
20 |
30 |
40 |
45 |
50 |
60 |
70 |
80 |
90 |
|
0 |
0.77 |
0.87 |
0.95 |
1.00 |
1.02 |
1.01 |
0.97 |
0.89 |
0.85 |
0.80 |
0.67 |
0.53 |
0.37 |
0.20 |
90 |
10 |
0.75 |
0.86 |
0.94 |
0.98 |
1.00 |
0.99 |
0.95 |
0.88 |
0.84 |
0.79 |
0.67 |
0.52 |
0.37 |
0.20 |
80 |
20 |
0.71 |
0.81 |
0.89 |
0.94 |
0.96 |
0.95 |
0.91 |
0.85 |
0.81 |
0.76 |
0.64 |
0.51 |
0.36 |
0.20 |
70 |
30 |
0.65 |
0.75 |
0.82 |
0.87 |
0.89 |
0.88 |
0.85 |
0.79 |
0.75 |
0.71 |
0.61 |
0.48 |
0.35 |
0.20 |
60 |
40 |
0.56 |
0.65 |
0.72 |
0.77 |
0.79 |
0.79 |
0.76 |
0.72 |
0.68 |
0.65 |
0.56 |
0.45 |
0.33 |
0.20 |
50 |
50 |
0.46 |
0.54 |
0.60 |
0.64 |
0.67 |
0.67 |
0.66 |
0.62 |
0.60 |
0.57 |
0.49 |
0.41 |
0.31 |
0.20 |
40 |
60 |
0.33 |
0.40 |
0.46 |
0.50 |
0.53 |
0.54 |
0.53 |
0.51 |
0.49 |
0.47 |
0.42 |
0.36 |
0.28 |
0.20 |
30 |
70 |
0.20 |
0.25 |
0.30 |
0.34 |
0.37 |
0.39 |
0.40 |
0.39 |
0.38 |
0.37 |
0.34 |
0.30 |
0.26 |
0.20 |
20 |
80 |
0.05 |
0.09 |
0.14 |
0.17 |
0.21 |
0.23 |
0.25 |
0.26 |
0.26 |
0.26 |
0.26 |
0.25 |
0.23 |
0.20 |
10 |
90 |
-0.10 |
-0.07 |
-0.03 |
0.00 |
0.03 |
0.07 |
0.10 |
0.13 |
0.14 |
0.15 |
0.17 |
0.19 |
0.20 |
0.20 |
0 |
Table 7.4 for µ = 0.1
β for Fy |
α |
β for Fx |
|||||||||||||
|
-30 |
-20 |
-10 |
0 |
10 |
20 |
30 |
40 |
45 |
50 |
60 |
70 |
80 |
90 |
|
0 |
0.82 |
0.91 |
0.97 |
1.00 |
1.00 |
0.97 |
0.92 |
0.83 |
0.78 |
0.72 |
0.59 |
0.44 |
0.27 |
0.10 |
90 |
10 |
0.80 |
0.89 |
0.95 |
0.98 |
0.99 |
0.96 |
0.90 |
0.82 |
0.77 |
0.71 |
0.58 |
0.43 |
0.27 |
0.10 |
80 |
20 |
0.76 |
0.85 |
0.91 |
0.94 |
0.94 |
0.92 |
0.86 |
0.78 |
0.74 |
0.68 |
0.56 |
0.42 |
0.26 |
0.10 |
70 |
30 |
0.70 |
0.78 |
0.84 |
0.87 |
0.87 |
0.85 |
0.80 |
0.73 |
0.68 |
0.63 |
0.52 |
0.39 |
0.25 |
0.10 |
60 |
40 |
0.61 |
0.69 |
0.74 |
0.77 |
0.77 |
0.75 |
0.71 |
0.65 |
0.61 |
0.57 |
0.47 |
0.36 |
0.23 |
0.10 |
50 |
50 |
0.51 |
0.57 |
0.62 |
0.64 |
0.65 |
0.64 |
0.61 |
0.56 |
0.53 |
0.49 |
0.41 |
0.31 |
0.21 |
0.10 |
40 |
60 |
0.38 |
0.44 |
0.48 |
0.50 |
0.51 |
0.50 |
0.48 |
0.45 |
0.42 |
0.40 |
0.34 |
0.26 |
0.19 |
0.10 |
30 |
70 |
0.25 |
0.29 |
0.32 |
0.34 |
0.35 |
0.36 |
0.35 |
0.33 |
0.31 |
0.30 |
0.26 |
0.21 |
0.16 |
0.10 |
20 |
SO |
0.10 |
0.13 |
0.15 |
0.17 |
0.19 |
0.20 |
0.20 |
0.20 |
0.19 |
0.19 |
0.17 |
0.15 |
0.13 |
0.10 |
10 |
90 |
-0.05 |
-0.03 |
-0.02 |
0.00 |
0.02 |
0.03 |
0.05 |
0.06 |
0.07 |
0.08 |
0.09 |
0.09 |
0.10 |
0.10 |
0 |
Table 7.5 for µ = 0.0
β for Fy |
α |
β for Fx |
|||||||||||||
|
-30 |
-20 |
-10 |
0 |
10 |
20 |
30 |
40 |
45 |
50 |
60 |
70 |
80 |
90 |
|
0 |
0.87 |
0.94 |
0.98 |
1.00 |
0.98 |
0.94 |
0.87 |
0.77 |
0.71 |
0.64 |
0.50 |
0.34 |
0.17 |
0.00 |
90 |
10 |
0.85 |
0.93 |
0.97 |
0.98 |
0.97 |
0.93 |
0.85 |
0.75 |
0.70 |
0.63 |
0.49 |
0.34 |
0.17 |
0.00 |
80 |
20 |
0.81 |
0.88 |
0.93 |
0.94 |
0.93 |
0.88 |
0.81 |
0.72 |
0.66 |
0.60 |
0.47 |
0.32 |
0.16 |
0.00 |
70 |
30 |
0.75 |
0.81 |
0.85 |
0.87 |
0.85 |
0.81 |
0.75 |
0.66 |
0.61 |
0.56 |
0.43 |
0.30 |
0.15 |
0.00 |
60 |
40 |
0.66 |
0.72 |
0.75 |
0.77 |
0.75 |
0.72 |
0.66 |
0.59 |
0.54 |
0.49 |
0.38 |
0.26 |
0.13 |
0.00 |
50 |
50 |
0.56 |
0.60 |
0.63 |
0.64 |
0.63 |
0.60 |
0.56 |
0.49 |
0.45 |
0.41 |
0.32 |
0.22 |
0.11 |
0.00 |
40 |
60 |
0.43 |
0.47 |
0.49 |
0.50 |
0.49 |
0.47 |
0.43 |
0.38 |
0.35 |
0.32 |
0.25 |
0.17 |
0.09 |
0.00 |
30 |
70 |
0.30 |
0.32 |
0.34 |
0.34 |
0.34 |
0.32 |
0.30 |
0.26 |
0.24 |
0.22 |
0.17 |
0.12 |
0.06 |
0.00 |
20 |
80 |
0.15 |
0.16 |
0.17 |
0.17 |
0.17 |
0.16 |
0.15 |
0.13 |
0.12 |
0.11 |
0.09 |
0.06 |
0.03 |
0.00 |
10 |
90 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0 |
Remark: Fx
= cos α sin β + µ sin α. Fy
= cos α cos β + µ sin α
14.
The existing text under the heading "Advanced calculation method:
calculated example" with the heading are deleted from section 7 and added
in as new Appendix 1 to the Annex with modifications as following paragraphs 15
and 16.
15.
In new Appendix 1, the words "Advanced calculation method: calculated
example" are replaced by the follows:
"Calculated example 1
(refer to paragraph 7.2,
Balance of forces and moments)"
16.
In new Appendix 1, calculated example 2 is added after calculated example 1 as
follows:
"Calculated example 2
(refer to paragraph 7.3,
Balance of forces - alternative method)
A cargo unit of
68 t mass is stowed on timber (µ = 0.3) in the tween deck at 0.7L of a vessel.
L = 160 m, B = 24 m, ν = = 18 kn and
GM = 1.5 m. Dimensions of the cargo unit are height = 2.4 m and width = 1.8 m.
The external forces are: Fx = = 112 kN, Fy = 312 kN, Fz
= 346 kN.
The top view
shows the overall securing arrangement with eight lashings.