Grain Loading Plan & Stability Booklet
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BIBLIOGRAPHY I
,0' ANT Grain SC,23 OV,
TAIJI
rority nt of public
fs
-
UE
,ffi t'
;"."
i;&
e
FINISHED PLAN
IMO 9478tt82
SHIP NAME
CRANE ISLAND
SHIP N o
522
D.
W.
32,OOO
CLASSIFICATION NK
MT TYPE OPEN HATCH CARGO
GRAIN LOADING PLAN
MANAGER
KANDA SHIPBUILDING CO., LTD.
DESIGN DEPARTMENT
& STABILITY
7,fu
DEPUTY MANAGER
HE +tr
flo'
8
.=.
#i fe
fli
BOOKLET
SCALE
DATE ISSUED
CHIEF
tu
DEPUTY CHIEF IN CHARGE
KURE JAPAN
SHIP
DRAWN BY ,'St
* ,{s
,R. -H.
+t
G.M.
tA
#ot
H
*/1"
DX
fl#
{t a
t6 fr,*
DATE DRAWN
20 October 2009
DRAWING No.
K-36
E atu CIJ(
*t1,
frx
oJ( =&
ffo'
i& ED(
t# EE EEL
E& oJ(
> I
h
H
trl
I
)E
(TOTAL 254 SHEETS WITH
COVER)
( Chapter VI "
PART
Car
r i age
of
Cargoes
'r of
S0LAS
197
4) PAGE
I.
PRINCIPAL PARTICULARS.....
2.
5
GENERAL INFORI',IATION
2-1 lntroduction.....-...-2-2 Regulation to be observed .........---
6
2-3 2-4
1
3.
6
Data & Unit System to be used ...--.-Method of Grain Loading Calculation'......-.-.
7
GRAIN LOADING CALCULATION USING ALLOWABLE GRAIN HEELING
I,l|Oll|ENT
3-1 Flow chart 3-2 STEP-A . Metacentric Height Calculation .......... 3-3 STEP-B : Actual Heel ing Moment Calculation........ 3-4 STEP-C : Al lowable Heel ing Moment 3-5 sample calculation using Al lowable Grain Heel ing Moment 3-6 Table of Allowable Grain Heeling Moment
4. 4-1 4-2
CRAIN LOADING CALCULATION USING STABILITY
Flow
Chart
STEP-D
:
Calculation of Heeling Angle & Residual
Dynamical Stability."..... Stabi I ity Curves from Table of
Cross Curves--...------. Sample Calculation using Stabi I ity DATA FOR EACH CARGO
5.
Curve..
10
.-
1l 14
ig 19
ZO
21
Zz 24 30
STANDARD LOADINC CONDITION
6-1 Blank Sheet 6-2 Stowage Plan-....-... 6-3 Surunary of Loading Table.-.-......... 6-4 Surrnary of Grain Stability Calculation........... 6-5 Standard Loading Condition...........
1.
l0
HOLD
Hold Capacity Table.......-... 5-2 Tables of Volume & Heel ing Moment 5-3 Volumetr ic Heel ing Moment, Volume & KG Diagram.......
5-1
6.
9
CURVE
4-3 Drawing Statical 4-4
g
HYDROSTATIC
TABLE....
36 31
38 41
43 91
Z
PAGE
8.
STABILITY
DATA
8-1 Riehting Lever ( KN ) Table 8-2 Curve of lnflow Angle 8-3 Curve of Deck Edge lmmersion Ang1e..............
9.
14g 166 16g
DATA FOR TANK CAPACITY
9-1 Tank Arrangement ( Tank Surrnary ) ....-....... 9-2 Volume Curves ( with Correction Curve of Free Surface Effect
ll.l
) ...-......-.
1ls
3 PART
IT
( A 10.3
OF INTERNATIONAL GRAIN CODE, END UNTRIMI||ED ) PAGE
1. 2. 2-1
3.
GENERAL INF0RMATI0N
..........
......
te6
.........
197
DATA FOR EACH CARGO HOLD
Hold Capacity Table
(
End-Untrimmed
)...........-.-
STANDARD LOADING CONDITION
3-1 Stowage Plan....-..-. 3-2 Surrnary of Loadine Table..'.-.-.-..-.. 3-3 Surmary of Grain Stabi I ity Calculation..........3-4 Standard Loading Condition...........
200 ZO1
ZO4
206
4
PART
I
chaptervl *carriage of cargoes, of S0LAS 1974
(,I
u)
1.
Principal particulars
Length overall
117.13
t\{
Length between perpend i cu I ar s
168 500
r\{
400
t\{
14. 250
t\|
1A.022
tI|
Breadth Depth
I Fu I I
Fu I
mou I ded
28.
lartaaaaalaltaattala
rnou I ded I
oad dr af t (Sunmer
I
oaded
d i sp
I
,
Ext r eme)
acement
39,671
Deadwe i ght
32, 154.11
Gross tonnage (Register) r . r ! . r r . . r r r r r r
r
Light ship weisht Center of gr av i ty from midship t ' ! t r ' r r r r ' r Center of grav i ty above base line . r . . t ! r . r r
r
. r . ! ! r . . . r r . r . . r r . . . r
.
CIaSS nafne.
' r r . r r . r . . . r r . r . t r !
SymbOl
J,523.11
aft
.
MT
631ttll B.
96
tll
NK
NS*(BCM,
BC_X
II
, GRAB)
,
MNS-
25 Persons
ifiCatiOn
Service
t\JlT
24, 242
Comp I ement
QUal
.82 It|T
r r r . r r r . r . r . r r r . . r . r
ltr.
C.0.
C.
S.0. (85%)
.
.
0cean Go i ng
6,620 kw (9,000 PS) x 125 min-r(RPlrl) 5, 627 kw (7, 650 PS) x 1 18.4 min-r(RPl',l)
speed.
about 14.30 Knots (at designed draft = 9.50m,
C.
S.0. ,15%
Slrl)
Cal I Sign . . . . . r r . r . r r . r r r r . r r r
r
3
nUmbef . . r r r . r r r . . r . ! r . r .
r
39778_PEXT-1
r r ! r . r r r r . r . . r . r r
r
PANAMA
laid r . r . r r r r r . r ! . . r ! . . r . .
r
25 December
LaUnChed ! r . r . r . r . r . . . . r r r . r . r
r
21 July 2009
Del iVefed r . . r r r r t ! . r . r r . . r r r r r
.
4 November 2009
flffiCial
POft Of fegistfy Keel
NK
Class No. 095291
EX53
2001
b
2. 2-1
I
ntroduct
i
GENERAL
I NFORI1ilAI I ON
on
"
Grain Loadins Plan and stabirity Booklet " for this ship has been prepared to enable the master to demonstrate the abi I ity of the ship at all stages of any voyage carrying bulk grain to comply with the stability requirement of chapter vl " carr iage of cargoes " of S0LAS 1g74. ln applying chapter vl of sOLAS rg74, this part I has been prepared in accordance with the " lnternational Grain Code ( Res.MSC.23(SOy -. ;
This
2-2
to be observed
Regulations (1 )
Trinrning of Grain necessary and reasonable trinrming shall be performed to level all free grain surfaces and to minimize the effect of grain shifting. ln any " f illed cornpartment ", the bulk grain shall be trimmed so as to fill all the space under the decks and hatch covers to the maximum extent possible. After loading, all free grain surfaces in" partly fiiled compartment,, shal I be trinuned level and the ship shall be upright before proceeding
All
to
sea.
ln case where the dispensation from trimming of end of fully filled compartment is granted under the provisions of the lnternational
Grain
code, in this case the grain cargo can be loaded with ends untrinmed. ( Refer to Chapter I I in this booklet ) (2)
ntact Stab i I i ty Requ i rements The intact stabi I ity characteristics of any ship carrying bulk grain shall be shown meet, throughout the voyage, at least the following criteria after taking into account the heel ingmoments due to grain shift: (i) the angle of heel due to the shift of grain shall not be greater than 12 degree or the angre at which the deck edge is imrnersed, I
(i
i)
(iii)
is the lesser, inthestatical stabi I itydiagram, thenetor residual
whichever
areabetween
the heeling arm curve and the righting arm curve up to the angle of heel of maximum difference between the ordinates of the two curves, or 40 degrees or the " angle of flooding( 0f) ,,, whichever is the least, shall in ail conditions of loadingnot be less than 0. 075 meter-radians; and the initial metacentric heieht, after correction for the free surface effects of tiquids in tanks, shal I not be less than 0.30 meter.
7
2-3
Date &
t
Systern
to be used
(1)
The ship's cargo capacity, tankage, etc., together with vertical & longitudinal centers of gravity and free surface effect ( inertia ) should be taken from the Capacity Table and the Volume Curves ( with correction curves of free surface effect ).
(2)
The ship's Displacement,.Transverse KM, Hydrostatic Table.
(3) 2-4
Un i
Method
etc. should be taken from the
metric system of units is used in all the calculations, unless otherwise special ly stated, in this booklet.
The
of Grain
loading Calculation
This Grain Loading Booklet contains two ways of calculating the intact stability for the purpose of the requirements in the Relevant Regulation ( see 2-2(2) ) , one is a method using the Table or the Curves of Allowable Grain Heeling Moment and the other is to obtain directly the heeling angle and residual dynamical stability from the stability curve, the latter being more accurate in particular.
4
3
. GRAIN LOADING CALCULATION USING ALLOUIABLE GRAIN HEELING MOMENT
Grain loading calculations using IABLE 0F as shown in a flow chart below. For Qu i ck reference, samp I e Ca I cu I at i on ( DEPARTURE ) have been given in 3-5. 3-1
F
I
ALL0WABLE HEELINC IttI0tttIENT Proceed COND I T
I
0N N0. 63
S.
F
.
=44
CF
/tt
ow chart
Start
'13 c.)
!-
(.)
E 'o
C.G. & Trin
Calculation
STEP-A (see 3-2)
o o o
-o E
o = -l'-
a (.
o
# 1]
B
Actual heeling moment calculation
STEP-B (see 3-3)
Allowable hee ling mornent calculation
STEP-C(see 3-4)
h0
(-
T' $ o
J
t*.
o
#
o
d Actual heelins moment Allowable heeling mome
7 3-2
STEP-A
: Metacentric Height Calculation
height is obtained in an usual method of calculation center of gravity and the trim as fol lows.
The metacentric
for
the
(1)
Estimate the weight and their center of gravity of consumables on board and write them into the proper column in the calculation form.
(2)
Decide the weights and their center of gravity of the grain cargoes and others, and write them into the proper columns in the calculation form.
(3)
Decide the
vertical center of gravity(KG) of the loading condition
under
consideration. (4)
Then
the corrected metacentric heieht
from
GoM
can be obtained
:
Gott,l=TKIll-KG-GGo Metacentric Height above Base Line, is read from the Hydrostatic Table. GGo is loss in 0[ll due to Free Surface Effects. ( See also the following paragraph (5).)
where which
(5)
; TK[tl is Transverse
Free Surface Effects Prov i ded a tank i s comp I ete I y f i I I ed wi th I i qu i d, no movement of the I iqu i d is possible and the effect of the liquid on the ship's stability is precisely the same as if tank contained sol id material. when a quantity of I iquid is withdrawn from the tank, the situation changes completely and the stabi I ity of the ship is adversely affected by what is known as the " free surface effects ". This adverse effect on the stabi I ity is referred to as a " loss in GM " or as a " Virtual rise in KG " and is calculated as fol lows : -
Loss in
GM due
Sum
to
of
Fr
Free Surface Effects ee
Su
Displacement
rf ace
( GGo )
Mornents
of ship in
Tons
Tanks where free surface is taken into account, (1) For tanks containing liquid which may be consumed
or discharged during navigation, the expected maximum moment of free surface is to be given. (2) lltlhen liquid in tank is maintained constant at partly f illed condition during navigation, the moment of free surface may be calculated on the basis of actual quantity of the I iquid. The moment of free surface should be calculated by " Specific gravity of liquid x lnertia ", and the inertia of each tank should be referred to " V0LUME CURVES( with [lAX. lT ) or correction curve of free surface effect "
Notes
:
(1)
The corrected metacentric
heieht is shown in this booklet as
"
Go[t{
"
/c 3-3
STEP-B
. Actual Heeling Moment calculation
The heeling moment
(1) (2)
Read
"
is obtained in the following
procedure as shown below.
the weight(T) of grain cargo in each hold from calculation " and write it into the column
STEP-A
calculate the vo I ume
(M3)
volume(M3)
=
WEIGHT(T),
from the foilowing formura.
Stowaee f actor
(CFILF)
x
llle i
sht
(T)
35. 88
(3)
ln case of partly f illed cornpartments, f ind out the Heeling Moment(Ma) ( =1.12 x Trans Heeling Moment ) corresponding to the volume(M3) from " Tables of Volume, center of Gravity & Heeling Moment,, or
"
Heeling Moment, Volume & KG Diagran,,. ln case of filled compartments,find out the Heeling Moment(11r1a) from " SUMMARY TABLE 0F HEELING lrl0MENT FOR FILLED H0LD " of END-TRIMMED or END_UNTR I lllr',lED.
(4)
" Heeling lr{oment(ttl4) " into heeling
]',loment( T-M ) from the it into the column HEELING trr1g1yENT( T-M ). Hee I i ng Moment = 35. g8 x Hee I ne Moment (It{4) ( T-tt{ ) Stowage Factor (CFl11)
Transform
following formula and write
i
3-4
STEP-C
: Al lowable Heel ing Moment
Al lowable Heel ing Moment can be determined by
the fol lowing
procedure.
l)
Correct the KGo by the free surface effect. KGo=KG+66o where ; KG : vertical center of gravity of the ship for the loading condition. GGo r Loss in GoM, i. e. apparent rise of center of gravity.
(2)
the allowable transverse heel ing moment(T*M) from the table of allowable heeling moment at the displacement and the above " KGo,,. For intermediate displacement and " KGo ", the al lowable heel ing moment to be obtained by interpolation. Read
// 3-5
Sample
calculation using al lor,vable grain heel ing moment
( c0NDlTl0N :
1)
N0 61 S F.42
CF/tt
DEPARTURE UNTRTrt4tllED)
At first, the weisht of loading items are investigated and entered in column " WEIGHT ". For instance, from page 206 Itern
We i
LIGHT SHIP
7
ght
,523.
PROVISION
201
CARGO
I
B9
.
st
Con
st ant
Con
i
nvest nvest I nvest I nvest
26
1
92)
34)
.
,
" HEEL
or
The
we
I
CAL
tllOt\JIENT
I
gated
V0LUME CURVES
& KG D I AGRAM " rnoment w i I I be surnmed
NG IIIOIIIENT, VOLUME
ight and vert ica I 39, 611 .82 322, 418. 1
= =
f1t
VERT
i
39, 611 . 82
of each tank or ho l d can be found by the draw i ng "
:-
gated gated i gated i
I
22s. 17
t
nvest i gated
I
1 812
TOTAL
(pages 1 75 (pages 30
an
0. 00
FRESH IlJATER
F.0. & D.0.
namely
11
29904 1g
WATER BALLAST
KG
Notes
0. 00
CONSTANTS
2)
(MT)
1
up.
[!lT [vlT-[vl
and KG
VERT
I
CAL
MOII,|ENT
B 13 lll
ll1l
The
3)
effect of free surface of I iquid (l)
sarne dr aw i ng
as above "
V0LUME CURVES "
wi and
I
I be a I so found by the their moment wi I I be
surnmed up.
I
*
D\IIIT
tem
I
xp
.6
51.
1 F. 0. T. * N0. 2 F. 0. T. {< N0. 3 F. 0. T. * NO. 4 F O T * D.O T {< DOT {<
p 1.000
I
(P)
N0.
P/S )
52
0. 980
2408
C
)
1228.
B
0.980
1204
C
)
1228.
B
0. 980
1204
C
)
141
.7
733
P
)
44.1
0.980 0.900
44.
0
2451
S
1
40
900
40
TOTAL
5,
681
tl,lT-tlll
and
GGo=T0TAL I
|1l x:
The tank
x p =
5,68'l
=0.14[VI
39, 611 . 82
containing liquid which may be consumed during navigation.
fz
q
KGo
is calculated by using result of preceding paragraphs
fol lows
:-
KGo=KG+GGo = 8.'13 + 0. 14 = 8.21
5)
The al lowable heel ing moment can be found by the
"
TABLE OF ALLOWABLE GRAIN HEELING lilOlIENT
( pages 15 - 17 ) by interpolation. DISPLACEMENT = 39.677.82 KGo = B.ZJ D
lSP. =
Where:
KGo
=
B.
33, 452 32,589
20
!11
=
1
Where
:-
8.30 32, 5Bg +
KGo
=
1
Where
i,l
D 1
863 841
39,GIT.BZ 617
.82 = 33,
1
000
:-
34,
Allowable Heeling
037
Mornent
+ r
-B7B
= 33,422
x
0. 07
[rllT-[rll
000
33, 430
39, Gll . Bz
x
IFF.
34, 315
000
!1l =
841
IrlT
DISP.= 40, 000
39, 000 KGo = B. 30
"
=
J3, 4ZZ
Sg
as
,rf lrl
6)
actual heelingmoment can be found by the " SU]ttl]rilARY TABLE 0F HEELING ll|0]t|ENT FOR FILLED H0LD " ( paee 23 ) for the filled holds ( No.1,2,4 and 5 hold ), and can be found by " Tables of Volume, Center of Gravity & Heel ing Moment .. The
( pages 24 - 29) or " Heeling Moment, Volume & KG Diagram" ( pases 30 - 34 ) for partly fi I led hold ( No 3 hold ) where the corresponded grain volume are 33% of ful I grain capacity respectively.
Total
heel ing moment lvi I I be summed up as HOLD NAME
fol lows.
HEEL I NG MOtl,lENT
(
UNTR I IlItvlED )
No.1 CARG0 HOLD ( Full ) No.2 CARG0 H0LD ( Full ) No.3 CARG0 H0LD (partly f illed = 3,038. 1 rn3 ) No.4 CARG0 HOLD ( Full ) No.5 CARG0 H0LD ( Full )
1, 179 2, 965 .l
HEEL I NG
42
IllOtllENT
=
CF
2.134 26,51
/LT =
26,51
0. 8543
4x
= 22,lA2
MT/tt,|3
0. 8543
(
22,102 MT-lll
)
the allowable heeling moment ( 33,422 [tllT-M ). ing
moment
are less
than
of
No.3 CARG0 HOLD No.3 CARG0 H0LD (33% Fi I led = 3,038. t rf ) Vo lurne ( m3 ) Trans hee I ing rnornent ( 3097 .5 15018.9 2926. 5 1 4181 .2 D|FF. 171.0 231 .1 Heel
4 m4
[\llT-[\ll
The ship's grain heeling moment
x
731 r
2,965
TOTAL
ST0IIAGE FACTOR
6,
Trans heeling moment = 14,781.2
+
231.7
x
m4 )
( 3,038.1
-
2,926.5
)
171.0 '14,938
Total heeling
1)
moment
= = 1.12
ma
x
14,938 = 16,731
ma
ln this condition : a) The angle of heel due to the shift of grain is not greater than 12 degrees or the angle at which the deck edge is immersed, whichever is the lesser. b) The area or residual dynamical stabi I ity is not less than 0.075 meter-rad i ans. c) The initial metacentric height after correction for the free surface effects of I iquids in tanks, is not less than 0.30meters. Therefore, this condition is compl ied with the lntact Stabi I ity Requirement of lnternational Grain Code.
i /'l rT
3-6
TABLE OF ALLO$IABLE
GRA I
N HEEL I NG MO[\,|ENT
ALLO\/IIABLE HEEL ING
t\llOt\4ENT
This table shows the al lowable maximum heel ing moment due which satisfy fol lowing conditions.
1) 2)
3)
to shift of grain
of heel due to shift of grain (0 i) shal I be not greater than 12 degrees or the angle at which the deck edge inrmersed, whichever is the The angle
lesser.
)
The net or residual area ( Ar between arm curve up to angle of heel of maximum
the heel ing arm curve and the righting difference between the ordinates of (0m), the two curves or 40 degrees or the angle of flooding (0f), whichever is the least, shal I be not less than 0.075 meter-radians. The
ofl
l
initial metacentric height iquids
in
afte r cor rect i on
for the free
tanks (Go[\4) sha I be not less than 0.30 I
surface effects
meters
Statigrl stability curve GoM
Righting arrn curve
Heeling arm
shift
40 0m Heeling angle (deg)
ef
:t.t
TABLE OF ALLOWABLE GRAIN HEELING MOMENT NOTE; VC GO=KG+F.S.C
O
RR.)
DISPLACEMENT (MT) 20000
000 22000 23000
21
24000
25000
I
700
34602
34503
3447 4
34524
34656
7.1 0
34159
33988
3401
7.2A
337 17
34038 33574
3350
730
33215
331 09
3301 5
33507 32998
7.40 7.50 7.60 7.70 7.80 7.90 8.00
32833 32390
32645
32528
32490
34126 33595 33064 32533
321 B0
31 981
32042
32104
31 948
31716
472 309 64
31
472
506 063
32041 31 555 31 068
307 87
30582 30095
29348
8.1 0
29736 29294
30455 29946 29438 28929 28420
3t 551 30999 30446 29893 29340
2881 8
281 87
31 31
3062
1
30179
30323
31
3094 1 3041 0 2987
I
3486 3431 6
33763 3321 0
32657
29 609
27524
27176 26689
26894 26385
na82
26
26203
25877
26 640
607 261 43
257 16
25368
25102
2491 6
26197
2567 8
25230
24571
24364
25755
2521 4
247 43
24859 24351
2381
9.1 0
2531 3
247 49
9.20 9.30 9.40 9.50 9.60 9.70 9.80 9.90
24870 24428
24285 23820
24256 23770
24040 23509 22979 22448
23986
23356 22891 22427 21 963
21 917
21599 21046 20493 1 9940
10.00 10.10
2885
1
28409 27 967
23543 231 01
22659
1
1
4531
4067 1 3602
1
1
8755
1
8834
1
8281
1
8201
17140
7931
7229 6t 20 6212
5985 1 5498 1
15012
14525 1 4038 1 3552 1 3065 12579
1
2651
22152
9263
7738
5703 15194 1 4686 1 4177 1 3668 13160
23258 22705
18732
1
18418
6958
1
9387
17671
16471
1
9713 1 9264
27 128 2657 5
1
18246
1
6024
20281
386
8904
1
17 444
5581
15139 1 4697
I 9391
17782
1
6908 6466
9877
18247
1
11.40 11.50
207 90
20855 20325 1 9794
1871
1
25469
21
1
1
26022
21299
20569 201 05 1 9640 19176
11.00 1 1.10 1 1.20 11.30
261 64
25633
21 8A7
21332
17318 1 6854 1 6389 1 5925 1 5460 1 4996
27 681
21824
20364
17351
10.50 I 0.60 1 0.70
27 403
28234
27756 27225 26694
22310
23283
21034
1
912
227 97
21 498
0.90
10.40
27
28287
23842 23333 22825 22316
2221 6 2177 4
10.80
10.20 10.30
291 22
286 36 281 49 27 662
21337 20850
20889 20447 20005 1 9562 19120 1 8678 1 8235 1 7793
1
31252
1
6
29858 29394 28929 28465 28000 27536 27072
8.20 8.30 8.40 8.50 8.60 8.70 8.80 8.90 9.00
26000
2700a
ALLOWABLE GRAIN HEELING MOMENT (MT-M)
VCGO (M)
6609 1 6078 15547 15017 1 4486 1 3955 1
13424 2893
17729 17176 1 6623 I 6070 15517 1
4964
14411
3858 1 3305 1 2752 1
1
121 99
2363 11832
11646 1 1094
1
121 42
1
1301
11634
1
0770
1
0541
I 988
57 355 0 34582 3491 3 34007 3431 6 33432 3371 B 32857 331 21 32282 32524 31707 31927 31 32 31 330 30557 30733 29982 301 36 29407 29538 2883 1 28941 28256 28344 27681 277 4l 271A6 27150 2653 1 26553 25956 25955 2538 1 25358 24806 247 61 24231 24164 23656 23567 23081 22970 22506 22373 21 931 21775 21 356 21178 20781 20581 20206 9984 9631 9387 9056 8790 8481 81 93 7906 7595 7331 6998 6756 6401 61 81 5804 5606 15207 5031 461 0 4456 1 4012 3881 341 5 3306 281 8 12731 12221 21 55 11624 1 1580 11027 11005 10430 0430 9832 9855 9235 9280 8638
351
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
i
I
ty, { i*r'
TABLE OF ALLOWABLE GRAIN HEELING MOMENT NOTE; VC G0=KG+F.S.C
O
RR.)
DISPLACEMENT (MT) 27000
28000 29000 30000
31
000
32000
33000
34000
ALLOWABLE GRAIN HEELING MOMENT
VCGO
(M) 7.00 7.1 0
7.24
730 7.40 7.50
760 7
.70
780 7.90 8.00
3551 0 3491 3 3431 6 3371 B 331 21
32524 31 927 31
330
307 33 301 36
29538
8.1 0
28941
8.20 8.30 8.40 8.50 8.60 8.70 8.80
28344 27t 4l 21 150
26553 259 55
25358
890
247 61 241 64
9.00
23567
9.1 0
22970 22373 21775 21178
9.20 9.30 9.40 9.50 9.60 9.70 9.80 9.90 10.00 10.10 10.20 10.30 10.40
2058 1 1 9984 1 9387 1 8790 18193 1 7595 1 6998 1
6401
1
5804
I0.50
5207 14610
10 60
14012
0.70
13415 12818 12221
1
10.80
0.90 11.00 1
1.10 11.20 1 1.30 1 1.40 1 1.50
1
1
11624 1 1
1027 0430 9832 9235 8638
4 36351 35294 3571 0 34675 35069 34056 34421 33437 33786 32817 331 44 321 98 32503 31 579 31 862 30960 3122A 30340 30579 29721 29938 29102 29296 28482 28655 27863 2801 3 27244 21372 26625 26731 26005 26089 25386 25448 247 67 24806 24148 24165 23528 23524 22909 22882 22290 22241 21671 21 599 21 051 20958 20432 20317 19813 19675 91 93 9034 8574 8393 7955 17751 17336 17110 16716 16468 6097 15827 15478 I5186 4859 1 4544 1 4239 3903 3620 326 3001 2620 12382 979 11762 337 11143 10696 10524 0055 9904 941 3 9285 8772 8666 81 30 8047 7489
3591
1
1
1
1
3682
1
361 58
35494 3483
1
341 67
33504 32840 32171
31513 30850 301 86
29523 28859 28196
27532 2686
I
26205
25542 2487
B
24215 2355
1
22888 22224 21 561
20897 20234 9570 1 8907
1
18243
1
7580 16916 1 6253 1 5589
1
4926 1 4262
1
1
1
1
1
1
1
1
1
1
3599
1
2935
11
12272 11608
11
1
0945
1
0281
1
961 8
8954 829 1 7 627
6964
37332 37892 36647 37 85 3596 1 36471 35276 35769 34590 3506 33904 34354 3321 I 33646 32533 32938 31 847 32230 31 62 31 523 30476 3081 5 29791 301 07 291 05 29399 28419 28692 27734 27984 21048 2727 6 26362 26569 25671 2586 24991 251 53 24306 24445 23620 23738 22934 23030 22249 22322 21 563 2161 4 24878 20907 20192 201 99 9506 949 8821 8783 81 35 8076 11 449 7368 6764 6660 6078 5952 5393 15245 1 4707 1 4537 1 4021 3829 3336 13122 r 2650 1241 4 11964 11706 11279 10998 0593 029 9908 9583 9222 8875 8536 81 67 785 1 460 71 65 6752 6480 6044 1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
1
7
38509 37179 37050 36320 35590 34860 341 30 33400 32671 31 941 31211 30481 29751 29021 28291 27562 26832 26102 25372 24642 23912 23182 22453 21723 20993 20263 9533 8803 8073 17 344 16614 5884 15154 1 4424 3694 12964 12235 11505 10775 0045 9315 8585 7856 7 126 6396 5666
39 1 92
38440 37688 36936 361 84
35432 34680 33928 3s1 76
32424 31672 30920 301 68
2941 6
28664 27912 27160 26408 25656
24904 24152 23400 22648 21
896
211 44
20392
1
1
1
1
9640 8888
1
1
81 36
1
1
1
17384 16632 I 5881
15129 1
4377
1
3625
12873 12121 11369 10617 9865 9113 836
1
7609 6857 6 1 05
5353
& il
TABLE OF ALLOWABLE GRAIN HEELING MOMENT NOTE; VCG0=KG+F.S.C O RR.) DISPLACEMENT (MT) 41 000 38000 39000 40000 ALLOWABLE GRAIN HEELING MOMENT
34000
35000 36000 37000
700 710
391 92
39947
407 83
41 709
421 21
43802
4493
38440
391 73
39
987
40890
41 881
7.20
37 688
391 91
4007 2
41
44267
36 936
38395
42277
.40 7.50 7.60 7.10
361 84
3685
3759
I
39254
42940 42077 41215
431 61
730
38399 37 625
38435
40352
41
43360 42453
35432
3607 7
3761 7
41
35302 34528
39 623
780 790
33176
33754
32424
329 80
39490 38627 37765 36902 36040
40507
34680 33928
802 36006
40640 39733 38826 37919
8.00
3167 2
810
30920
8.20
301 68 2941 6
32206 31 432 30658
VCGO
(M)
1
8.30 8.40
850 860 870 8.80 8.90 9.00 9.1 0
9.20 9.30 9.40
950 9.60 9,70 9.80 9.90 10.00 10.10 10.20 10.30 10.40 10.50 10.60
I0.70 10.80 10.90 11.00 1 1.10 11.20 11.30 11.40 11.50
1
36
3521 0 3441 4 3361
I
36799 35980 351 62
34344
32821
33525
32025 31229 30433
32707 31 889 31 070
29637
34252
26 788
28840 28044 27 248
2861 5 277 97
2601 3
26452
26979
25656
261 61
24152
25239 24465
24859
25342
23400 22648
23691 22917
24063
24524 23706
28664 27
912
27160 26408 25656 24904
29884 29110 28336
27562
21896
221 43
21144
21
20392 1 1
9640 8888 18136
17384
369
23267 22471
22069
20595 1
9821
20082
20432
1
9047
1
9286 1 8490
19614 1 8796 17 977 17159
18273 7498
1
7694
6632
167 24
1
6897
1
5881
1
1
5950
15176
1
4377
1
4402
1
3625
1
3628
12873
1
2854 2080
12121 11369 10617 9865
1
11306 1
0532 9
758
1
5305 1 4509 13713 12916
15522 14704
1
12120 1 1324 1 0528
3886 1 3067
1
12249 1
1431
32 8935
81 57
97
8984 8209 7 435
81 39
6857
6661
61 05
5353
609
6341
10612 97 94 8976
836 7
21251
16101
91 13 1
22887
21675 20878
1
15129
29434
040 40200 39359 3851 I 37678 36838 35997 351 57 3431 7 33476
46080
1
44046
4517 4
392
351 77
38738 37853 36969 36084
3431 4
351 99
[- if^452 3€15l l- 32589 33430 30955 31727 32545
3701 3 361 06 351 99
32636
31 795
4 4 28434 27593 26753 25912 25072 24231
301 1 2927
2339 22551 1
u71A 20870 20029 91 89 8348 7508 6667 15821 1 4987 41 46 13306 12465 11625 10784 9944
546
I
I
34292 33385 32479
30864 30002
31 661
291 39
28277
2989 29007
27 41 4
28122
297 58 2885 1
26551
27 237
27 945
25689
26353 25468 24583 23699
24826 239 64 231 01
30776 1
3151 2 306 65
27038 261 31
25224 24318
22239 21376 20514
2281 4
2341
21929 21045
22504 206 90
1
21597
1
1
9651
201 60
1
1
8788
1
9275
1
9784
1
17926
1
8391
1
8877
1
1
7063
1
7506
1
6201
1
6621
1
5338 4476 13613 12751 11888 11025 9307
1
5737
1
1
4852
1
1
3967
1
2861
1
3083
1
0521
1
1
1017
970 7063
7
61
56
5250
B3OB
8750
622s
6625
4306 2540
04
71 49
4648
5l 30 3264
2841 1211
942
339
649 5644
6547
6024
37 60
1
578
0
0
5887
575
41 65
2032
106
0
0
51 13
4436
2428
503
0
0
0
7
343 1
7
91 7
0
{
iJ
Fr
4,
GRAIN LOADING CALCULATION USING STABILITY
CURVE
Althoueh general ly determined as described in the preceding Chapter the grain loading stabi I ity can be also calculated more accurately, if necessary, using the stabi I ity curve as shown herein.
4-1
F
I
ow
3,
chart
-ci
C.G. & Trirn
0.)
l-
o -o
Ca
'a
STEP-A (see 3-2)
lculation
C
o o 0)
-o E
o = Ja o
;
-()
Actual Heeling Moment Calculation
STEP-B (see 3-3)
B b0
C
T] (tr
o
J
Calc. of Heeling Ang. & Residual Dynamical Stability
l-
o
-s-
P
o
€
12' Edge Immersion
Residual
Area
0.075 (M-Rad.) (tvt-D.g)
= 4.30
STEP-D(see 4-2)
tf
t'4
4-2
STEP-D:
Calculation of Heel ine Angle & Residual Dynamical Stabi I ity
The heel ing angle and
the residual dynamical stabi I ity can be obtained
by the fol lowing figure. Righting arm curve after
corrction for the free surface effects of liquids in tanks T.t
\-/ =l EI
\\
I
angle of heel due grain shift
l-l (III
bol
GoM
to
./
:l
tsl bol rEl Heeling arm
to tra nsverse
idua ll 6yna
m
ica
I
sta b ilit
B
urve due arn
shift which rna be approximately represente by the straigh line AB
d
0m40
0vt
Heeling angle (deg)
i0
= Tota
I Hee I ine Moment Di
sp
I
acement
([tllT-[\ll)
([vIT)
i40 = 0.8 x A
0m is the angle of heel of
difference between the ord i nates of curve, or 40 degrees or the ang I e of
maximum
r ight ing arm curve and heeI ing arm flooding, rlvhichever is the least.
-> dfr
4-3
Drawing
Statical Stabi I ity Curves from Table of Cross
Curves
Statical Stabi I ity Curves ( Righting Arm Curves ) for the purpose as stated in preceding paragraph can be derived from the Righting Lever ( KN ) Table as fol lows.
(l)
The corrected
from
riehtine arm 0 ( Corrected GoZ ) is obtained
:
Corrected
GoZ =
KN
(
frcrn KN Table
)-
KGo
x
sin6
KG
=
Where
KN = KGo = KG = GGo = Q = (2)
Righting lever at assumed
0.0M
KG+GGo
Vertical center of gravity ( fe
) at the loading
condit ion under consideration Loss of G[t,l due to free Surface Effect Angle of incl ination
The Transeverse Metacentric
Heieht (
GoM
) is obtained
from : IVhe r e
KGo = the same as above
(3)
Example; C0NDlTl0N61 S.F.42 CFlIfGRAINL0ADING
KG
=
KGo
=
B. 13tvl KG
+ GGo = 8.21
[y|
xTher efor e,
(1)
e
(" )
Q)
sin0
(3)
(4)
X sin0
(0 = (3)
5
0. 0872
l$l tab le 105
12
0. 2079
2.50
20
0 3420
4. 11
112 283
033 078 134
30
0. 5000
6. 00
4.14
1. 86
40
0 0 0
6428
753
5.32
2.21
7660
B49 B98
633
2. 16
1 16
1. 82
50 60
Then using
8660
KN f rom
KGO
0.12
Corrected
(4)
GOZ
the corrected GoZ values in column (5), a Statical Stability for the ship at this displacement.
Curve can be drawn
?l -t
4-4 Sample Calculatron Usrng Stab:. 11ty
Cunve
I
cr)
*lx I
sl
tLo
3 UHCOCUN IOCU CUFN V Z N O ill(o tr O) aco o_
ZO
LlJ ll
il
CU
N CO
,(-)il
,'
U
l co
cuLo
= T NO il
:,
,,\O ,, CU
C[JI!(D
LU+ tJ
LD
O CU ftl LO
IOX 'N .Z-
/1 t
a
CO
q s-1
-l -l
\dftlss-l
|l.l ,,nloLo
rolv < ol -ls cql I llt
OLfJsiN
(f
OHILD UOO:I
,,
ll
N
(D
og Z H
-J II II I
o
?T?Iq OOrl
.-lvl
r11:? COTO\sCUO
-,1:-,1: ln ln -,1, -,1><
O
.JFV
C]n_u_
Vlocuo9q
LO
:Y o.lco \u cn
Hl-
o_
O
-, 1*
O OOftJ O Ct
X
o
F
Lrn
COCOV
_^. l-r) cu JUuo
!
H
mca
< tro F a
sl cr)
ttt-)
O ll -J <
a s
O
o
t
CD
ro Ln
O< H+ z tl
il
CU_J
.;)
OO ll
F-tOv
ottrntt CU CT] \r F CU
CUCOss -r (! ro ro ro
FCt Hl _J>
><
a
tx Ct
l ml
ol
tl
(f)t o-r
I
3l
rl
:l
il O -1
?(
5. DATA FOR EACH CARGO HOLD
Z3
5-1
HOLD CAPAC I TY TABLE
TR I illlllED COIVIPARItvlENTS
UNTR
CENTER OF GRAV I TY
I [vltvlED
LOCAT I ON
(FR. No. )
CAPAC
I
IY
HEEL, [!I' T
CAPAC I TY
(ma)
(m3)
(ma)
859.9
5, 374.6
1.119.3
-63. 29
B. 53
(m3)
HEEL,
tvlID.
tlJl
KG
G
(m)
(m)
NO.
1 CARGO HOLD
172-2A3
5, 648. 5
NO.
2
CARGO HOLD
136-1 72
9, 499.
6
2,479.8
9, 256. 2
2, 964.
6
-38.22
B.68
NO.
3
CARGO HOLD
1
00-1 36
9, 499.
6
2,479.8
9,256.2
2,964.
6
-9. 42
B.68
NO.
4
CARGO HOLD
64-1 00
9, 499. 6
2,479.8
g, 256. 2
2, 964.
6
19.38
B. 68
NO.
5
CARGO HOLD
-64
8, 303. 3
2,321
.2
B, 079. g
2,133. 7
46.73
8. 97
IOTAL
NOTE
31
42,450.6
1
0, 626. 5
41
,223,1
1
2, 806.
B
:
1) Grain capacity (EN0 UNTRIltrIt{ED) represents ful I capacity in the untrirrned ends.
minus the volume
of the voids
2) ln order to provide for the vertical shift of the grain in the untrimrned ends, the geometric center of gravity of the hold, as indicated in the above table, shall be used as the KG value for the grain in the hold. 3) Mid.G (L.C.G.) = Longitudinal center of gravity from midship, no sign and minus (-) sign show aft and fore from midship respectively.
4)
KG (V.C.G.) =
Vertical center of gravity
above base tine.
z#
5-2
TABLES OF VOLUME AND HEEL I NG VOLUMETR
1
)
I
C
HEEL I NG ttll0tllENT
l\,lOt\/lENT
AT *PARTLY
F
I
LLED
COMPARTMENT-
the free surface of the bulk grain has not been secured, i t sha I I be assumed that the grain surface after shifting shal I at 25" to the hor i zonta I
When
be
.
2) ln "partly fi lled compartments" the adverse effect of the vertical shift of grain
surfaces shall be taken into account as foilows: hee I
ing
rnornent
ic hee I ing moment curves in the fo I I ow i ng pages ar e shown n the form wh i ch i nc I udes the adverse effect of the vert i ca I shift of gra i n surfaces as stated above.
The vo lurnetr i
t-
Z5 NO.l CARGO HOLD (C) VOLMETRIC HEELING MOMENT TABLE POSITION ULI-AGE
HEIGHT
(M)
VOLUME (Mxx3)
0.00 0.25 0.50
5649.5
0.7 5
5488.2 5434.7 5381.2 5303.0 5210.3
1.00 1.25 1.50 1.75
2.00 2.25 2.50 2.15 3.00 3.25 3.50 3.75 4.00 4.25 4.50 4.15 5.00 5.25 5.50 5,75 6.00 6.25 6.50 6.75 7.00 1.25 7.50 7
.15
8.00 8.25 8.50 8.75 9.00 9.25 9.50 9.7 5
10.00 10.25 10.50 10.75 1 1.00 11.25 1 1.50 I 1.75
5595.1 554't .6
FR.172.50
KG (M) 8.53 8.46 8.39 8.33 8.26 8,1 9 8.1 0
4922.4 4823.5 4723.2
7.99 7.88 7 .16 7.65 7.53 1.42
51 15.9 501 9.9
4621 .6
7.30
4518,8
7.1 B
4414.7
7.06
4309.6 4203.4 4096.2 3988.3
6.94
387 9.8 377 0.7
6.44
3661 .4 3552.1
6.1
3442.e 3333.8 3224.9 31 16.1
3007.4 2898.9 27e0.5 2682.2 257 4.A
2466.2 2358.8 2251 .1
2145.1
2038.8 1932.9 1827.4 1722.3
6.81
6,69 6.56 6.31
I
6.05 5.93
5.80 5.6 7
5.54 5.42 5.29 5.'t 6
5.03
4.90 4.78 4.65 4.52 4.39 4.26 4.14 4.01
1409.5
3.88 3.75 3.63 3.50
1306.1
3-37
'l
203.3
1
100.9
3.24 3.12 2.99 2.86 2.14
1
61 7.6
1
51 3.3
12.15
999.0 897.6 796.1 696.3 596.6
13.00
497.5
13.25
399.0
2.36 2.23
13.50 13.75 'l 4.00
301 .2
2.11
204.A 107.4 11.5
0.0
1.98 1.86 1.73 1.72
NOTE: DEDUCTED
RATE (1.000)
12.00 12.25
12.50
14.25 14.28
2.61
2.49
-
FR.203.00 TRANS. HEEL. MT
W.L.
(M**4)
(M)
.2 6.000 1096.2 't 5.750 1402.6 5.500 1692.1 5.250 1969.2 5.000 2229.9 14.750 2472.0 14.500 2697.1 4.250 2908.4 14.000 31 75.3 13.750 34e5.6 3.500 3789.5 't 3.250 4051.6 3.000 4284.8 12.15A 4485.9 12.500 4657.6 12.250 4801 .9 12.000 4924.6 't 1.750 5036.2 11.500 5137.e 1.250 5231 .9 1.000 5320.8 10.750 5401 .5 10.500 5475.6 10.250 5541 .8 10.000 560'l .1 9.750 5652.6 9.500 56e7.5 9.250 5735.6 9.000 5766.6 8.750 5790.5 8.500 5808.1 8.250 5818.7 8.000 5821.9 7.750 5819.1 7.500 5809.8 7.250 57e5.5 7.000 577 4.5 6.750 5745.8 6.500 5705.7 6.250 5646.5 6.000 5566.5 5.750 5466.6 5.500 5343.2 5.250 5194.8 5.000 501 9.7 4.750 4817.2 4.500 4585.7 4.250 4321 .8 4.000 4023.7 3.750 3689.9 3.500 3319.2 3.250 2909.8 3.000 2459.5 2.750 960.1 2.500 1408.6 2.250 794.1 2.000 86.3 1.750 0.0 1.720
1001
1
1
1 1
1
't
't
1
1
1
?& NO.2 CARGO HOLD
FR.136.50
POSITION
ULLAGE
HEIGHT
(M)
(C) VOLMETRIC HEELING MOMENT TABLE
KG (M)
VOLUME (M*.i.3)
0.00 0.25 0.50 0.7s
9499.6 9376.8 9253.4
1.00 1.25 1.50 1.75
9006.5 8882.9 8740.e 8575.4
8.31
2.00 2.25 2.50
8396. B 8225.1
1.87
8054.8 7883.9 7712.e 7542.0 7371.0
7.61
7240.1 7029.1
6.99 6.86
6858.2 6687.3 6516.3 6345.4 617 4.4 6003.5 5832.6
6.7
2.t5 3.00 3.25 3.50 3.7 5
4.00 4.25 4.50 4.15 5.00 5.25 5.50 5.75
6.00 6.25 6.50 6.75 7.00
5661 .6
7.25
4806.9 4636.0 4465.0
7.50 1
.75
8.00 8.25 8.50 8.75 9.00 9.25 9.50 9.75 10.00 10.25 10.50 10.75 1 1.00 1,25 1 1.50 1 1.75
54s0.7 531e.7 5148.8 4911 .8
10256.8 10981.9
7.4e
7.36 1.24
11
4
141
6.49 6.36 6.24 1
5.99 5.86 5.7 4 5.61
5.4e 5.36 5.24 1
4123.1
4.61
3781 .2
4.4e 4.36 4.24 4.11
27 55.6
3.99 3.86 3.7 4
2584,6
3.61
2413.7 2242.8
3.49 3.36 3,24
2071 .8
3.1
12.00
1900.9 1729.9 't 55e.0
12.25
1
388.1
2.7
12.50
1217
12.15
1046.2
13.00 13.25 13.50 13.75 14.00
875.2
.1
704.3 533.3 362.4 191.5 20.5 0.0
NOTE: DEDUCTED RATE
1
2,99 2.86
4
2.61
2.49 2.36 2.24 2.11
1.99 1.86 1.7
5081
1
3952.2 3610.3 3439.4 3268.4 3097.5 2926.5
29.8
14436.7 147A5.2 14e24.1
6.61
5.1
660.5
12275.9 12834.3 13314.9 13745.9
1
1
14.25 14.28
1
4.99 4.86 4.14
4294.1
(M)
1
1.74
6.1
W.L.
(M**.4)
1
8.22 8.12 8.00
7.1
FR.172.50 TRANS. HEEL. MT
2778.6 16.000 3241 .2 5.750 15.500 4321 .5 5286.8 15.250 617 2.5 5.000 6e76.1 14.750 7710.5 4.500 8383.1 14.250 9037.9 14.000 9604.8 13.750
8.68 8.59 8.50 8.40
91 29.9
-
4
1.72
(1.000)
.1
15207.4 152e5.7 15362.5
3.500 13.250 13.000 12.750 12.500 12.250 1 2.000 11.750
1
1 1
1.500 1.250
.000 0.750 10.500 10.250 10.000 9.750 9.500 e.250 9.000 8.750 9.500 8.250 8.000 7.750 7.500
11 1
.5 15462.4 15493.7 5512.0 5520.1 15516.3 1s507.4 15493.9 5482.1 15414.7 15456.2 .250 15422.5 7.000 'l 5332.0 6.750 5211 .2 6.500 15018.9 6.250 14787.2 6.000 4506.1 5.750 141 56.6 5.500 137 62.1 5.250 3313.2 5.000 127 88.9 4.750 12207.4 4.500 1565.2 4.250 10855.0 4.000 10069.2 3.750 9205.7 3.500 8258.5 3.250 221 .6 3.000 6088.6 2.15A 4848.8 2.500 3482.2 2.250 1963.6 2.000 213.4 1.750 0.0 1.72A
15421
1
1
1
7
1
1
'l
1
7
27 NO.3 CARGO HOLD POSITION
(C) VOLMETRIC HEELING FR.100.50
ULLAGE
HEIGHT
VOLUME
(M)
(M**s) 9499.6
8.6I
6.8
8.59 8.50 8.40
1.00 1.25 1.50 1.75
9006.5 8882.9 8740.9
2.00 2.25 2.50 2.75 3.00
9253.4 91 29.9
3.25
3.50 3.75 4.00 4.25 4.50 4,75 5.00 5.25 5.50 5.75 6.00 6.25 6.50 6.7s 7.00 7.25 7.50
15.000 14.750
8.12 8.00
7710.5
14.500
857 5.4
8383.1
8396.8
7.87
9037.9 9604.8
14.250 14.000 13.750
8225.t
7.74 7.61
't
0256.9
13.500
1.49 7.36 7.24
10981.9 1 1660.5
13.250
7371 .0
7
.11
7200.1 7029.1
6.99
1227 5.e
668 7.3 651 6.3
6.61
6345.4
6.36
617 4.4
6.24
12834.3 1 3314.9 13745.e 14129.8 14436.1 14705.2 14924.1 15081.2
6003.5 5832.6 5661.6 5490.7 531e.7
6.1
15201 .4
51 48.8
5.4e 5.36 5.24
5295.7 5362.5 15421.5 15462.4 15493.7 15512.0 1 5520.1
5.1
1551 6.3
858.2
6.86 6.7
4
6.4e
1
5.99 5.96 5.7 4 5.61
1
1
1
42s4.1
8.25
4123.1
4.7 4
8.50
3952.2 3781.2 3610.3 343e.4
4,61
15482.1 1547 4.1
4.4e 4.36 4.24
15456.2 15422.5 15332.0
3268.4 3097.5
4.11 3.99
0.00
2926.5
10.25
27 55.6
3.86 3.7 4
10.50 10.75
2584.6
3.61
1
2413.7 2242.8
1
2071 .B
3.49 3.36 3.24
1,00 1.25 1 1.50 11.75
2.00
12.75
3.00
1
3.25
1559.0
2.86 2.7 4
1046.2 875.2 704.3 533.3 362.4 191.5 20.5 0.0
13.50 3.75
14.00 14.25 14.28
NOTE
3.1
388.1 1211 .1
12.50 't
1900.9 1 729.9 'l
12.25
:
15.250
8054.8 7883.e 7712.9 7542.0
8.00
9.50 9.75
15.750 15.500
6976.1
4.99 4.86
9.25
16.000
8.22
.75
9.00
'l
4321 .5
(M)
5286.8 6172.5
6
8.75
1
2118.6 3247.2
W.L.
8.31
4e71.8 4806.9 4636.0 4465.0
J
'l
7
FR.'l 36.50
TRANS. HEEL. MT (M**.4)
KG (M)
0.00 0.25 0.50 0.75
93
-
MOMENT TABLE
15507.4 15493.9
.2 501 8.9
1521 1 't
14781 ,2
4506.1 14156.6
1
1
37 62.1
1
3313.2
127 BB.9
2.4e
12207.4 1565.2 10855.0 10069.2 9205.7 8258.5
2.36
7 221 .6
2.24
1.74
6088.7 4848.8 3482.2 1963.6 213,4
1.12
0.0
1
2.99
2.61
2.11
1.99 1.86
DEDUCTED RATE (1.000)
1
13.000 12.750
12.500 12.250 12.000 1.750 1.500 1.250 1.000
10.750 10.500 10.250 10.000 e.7 50
9.500 9.250 9.000 8.7 50
8.500 8.250 8.000 7.7 s0 7.500 1.250 7.000 6.7 50
6.500 6.250 6.000 5.7 50
5.500 5.250 5.000 4.75A 4.500 4.25A 4.000 3.7 50
s.500 3.250 3.000
2.150 2.500
2.250 2.000 1.750 1.72A
Z8 NO.4 CARGO HOLD (C) VOLMETRIC HEELING MOMENT TABLE
FR.64.50
POSITION
ULLAGE
HEIGHT
(M)
KG (M)
VOLUME (M**c3)
9253.4
8.40
9006.5 8882.9 8740.9 8575.4 8396.8
8.31
5286.8 6112.5
1.00 1.25 1.50 1.75
3.7 5
4.00 4.25 4.50 4.75 5.00 5.25 5.50
7
6.8
4321 .5
6976.1 771 0.5 8383.1
8225.7
7.74
8054.8 7883.9 7712.9 1542.0 7371.0
7.61
7200.1 7029.1
6.99 6.86 6.7 4
651 6.3
6345.4 617 4.4 6003.5 5832.6 5661.6 54e0,7
6.00 6.25 6.50
3247.2
8.22 8.12 8.00 1.81
6858.2 6687.3
5.7 5
7.4s 7.36
1.24 7.1
1
6.61
6.49 6.36
6.24 6.1
1
5.99
5.86 5.7 4
531 e.7
5.61
6.7 5
5148.8
7.00 7.25 7,50 7.75
4e71 .8
5.4e 5.36
4806.9 4636.0 4465.0
8.00
42e4.1
8.25
4123.1
8.50 8.7 5
3952.2 3781.2
9.00
361 0.3
9.25
3439.4 3268.4 3097.5 2926.5 2155.6 2584.6
9.50 e.7 5
10.00 10.25
10.50
2413.7
10.75 1 1.00 11.25 1 1.50 1 1.75
12.00
2242.8 2071.8 'l 900.9 1 729,9 1559.0
12.25
1
12.50
1211
12.75
1046.2
13.00
875.2
13.25
704.3 533.3 362.4 191.5 20.5 0.0
13.50 13.75
14.00 14.25 14.28
NOTE
:
(M)
91 29.9
93
3.00 3.25 3.50
W.L.
(M**4) 217 8.6
9499.6
2.75
TRANS. HEEL. MT
8.68 8.59 8.50
0.00 0.25 0.50 0.75
2.00 2.25 2.50
- FR.100.50
388.1 .1
9037.9 9604.8 10256.9 10981.9 1 1660.5 12275.e 1 2834.3 1 331 4.9 13745.9 1 41 29.8 14436.7 14105.2 14924.7 15081.2 15207.4 152e5.7 15362.5 15421.5 15462.4 't 54e3.7 1 5512.0
5.24
1
5.1
1
1
4.99 4.86 4.14
5520.1 55'l 6.3
15507.4 154e3.e
16.000 15.750 15.500 15.250 'l 5.000 14.750
'14.500
14.250 14.000 13.750 13.500 13.250 13.000 12.7 50
12.500 12.25A 12.000 1 1.750 1 1.500 1 1.250 1 1.000 10.750 10.500 10.250 10.000 9.750 9.500 9.250 9.000 8.750 8.500 8.250 8.000
15482.1 1547 4.1
1,154 7.250
4.11
15456.2 15422.5 15332.0 15211.2
3.99 3.86 3.14
1501 8.9 14187 .2 14506,1
3.61
141 56.6 1 37 62.1
4.61
4.4e 4.36 4.24
3.49 3.36 3.24 3.'l
1
2.99 2. B6
2.7
4
2.61
2.49 2.36 2.24 2.11
1.99 1.86
1.t4 1.12
DEDUCTED RATE (1.000)
13313.2 127 88.9 122A1 .4
1565.2 10855.0 10069.2 9205.7 8258.5
1
7221 .6
6088.7 4848.8 3482.2 1 963.6 213.4 0.0
7.500 7.000 6.750 6.500 6.250 6.000 5.750 5.500 5.250 5.000 4.750 4.500
4.250 4.000 3.750 3.500 3.250 3.000 2.15A 2.500
2.250 2.000 1.750
1.720
Z? NO.s CARGO HOLD (C) VOLMETRIC HEELING MOMENT TABLE POSITION
HEIGHT
(M)
KG (M)
VOLUME
(M**s)
0.00 0.25 0.50 0.75
.00
FR.3'l
ULLAGE
-
FR.64.50 TRANS. HEEL. MT (M*.*+)
B.e7
26'1
8.89
3A41
8075.2
8.7I
't
961 .2
8.70
1.00 1.25 1.50 1.75
1847.3 7 7 33.3
8.60
7601 .7
8.40
7 447 .8
8.28
2.00
1281 .1
8.1 5
2.25
7122.5 6963.5 6904.4 6645.4 6486.4 6327.3 6'l 68.3 6009.3 58s0.2
8.02 7.89 7.16 7.63
1A172.1 10787.1
7.51
1
7.38 7.25
11
5691 .2 5532.1 5373.1 5214.1 5055.1 48e6.1
6.86
4137.2 4578,6 4420.3
6.07
4262.6
5.68 5.55
2.50 2.75
3.00 3.25 3.50 3.75 4.00 4.25 4.50 4.15 5.00 5.25 5.50 5.7s 6.00 6.25
6.50 6.75 7.00
05.4 3948.9 3793.0
41
7.25
7.s0 7.75 8.00
3637.
6.99
1
6.34 6.21
5.e4 5.81
5.41
5.28
8.50 8.75
3023.1
9.00 9.25 9.50 9.75 10.00
2871.0 2119.5 2568.7
5.02 4.88 4.75 4.62 4.49 4.35 4.22 4.09 3.95 3.82 3.68 3.55 3.42 3.28
10.25
2121
10.50
1975.1
10.75 1 1.00 11 .25 1 1.50 11.75 12.00 12.25
1831.0 1688.8 1548.4 1410.0 1213.4 1 138.8 1006.0 815.2
12.50
.1
3.15
3.02 2.89 2.7 6
2.63 2.50
12.15 13.00
7
't
493.9 370.6
2.24
249.5 130.7 14.8
1.99 1.86 1.73 1.12
46.2 619.1
3.25
13.50 1 3.75 14.00 14.25 14.28
NOTE
0.0
:
'l
6.47
5.1 5
2269.0
1
6.60
3483.2 3329.2 31 75.8
241 8.5
1334.4 g1 9.1 12243.6 2602.8 2905.4
13155.3 13339.2 13465.5
6.73
B
8.25
1
8.51
7.12
2.37 2.11
DEDUCTED RATE (1.000)
(M)
0.9 16.000 .2 15.750 4032.4 5.500 15.250 4s21 .3 5741.0 5.000 6486.2 14.750 7164.8 14.500 1784,9 14.25A 8387.7 14.000 8905.9 13.750 9501 .0 13.500
8303.3 8189.1 7
W.L.
3540.9
13556.6 13542.2 13500.2
13.250 13.000 1 2.750 1 2.500 12.25A 12.000 1 1.750 1 1,500 1 1.250 1 1.000 10.750 10.500 10.250 10.000 e.750 e.500 9.250 9.000 8.750 8.500 8.250 8.000 7.750 7.500
13435.1 13349.4 13243.6 13120.8 12982.8 12829.0 12663.8 12492.0 12312.8 12128,4 1e37.4 1733.6 512.0 11272,8 101 4.3 10725.0 1A411 .4 10061.5 e670.6 9248.1 878e.5 8295.1 7758.1 7184.7 6573.7 5e23.7 5233.1 4499.8 3721.0 2892.7 2020.5 103.9 126.2 0.0 1
7.250
1
7.000 6.750 6.500 6.250 6.000 5.750 5.500 5.250 5.000 4.750 4.500 4.250 4.000 3.750 3.500 3.250 3.000
11
1
1
2.150 2.500
2.250 2.000 1.750
1.720
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o o
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7
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z,
(5 e e o o
x. ....rO L-
=.LU
=' lr
=rofr o == C'= Z.a r-{ l-
ltl -l LLI EF J-
z. t t IJ.J -J-
\-/ OOOCIOOe)c>e'OOO F
-C\lc?$lr2
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