Damage DOC asdasdasd asdas

MAINITEMCALCULATIONNOTEHPFLAREKODRUMN/S12VZ3602

DAMAGESITEIND.O.C DocumentNumber :AO10012F380000014Revision:00 Status : IFRRev.Date: 16Mar2015

Doc.Type:CAL Discipline:PVV Phase:DE Class:2CTRRef.:0984899MH40TT1EQPCAL000014 System / Subsystem:36 Equipment Type : VZ

VendorName: MMHEATBSDNBHDPONr: 0984899POTitle: SEPARATORSANDCARBONSTEELPROCESSDRUMS(FPSOSNORTHANDSOUTH)

VendorDocumentNumber:MMHEATBM010NS12VZ360204MC

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00 IFR 16-Mar-2015 Issue for Review A.FARIS NGADIRAN NGADIRANRev. Status Date Revision Description Issued by Reviewed by Approved by

KAOMBO

Project

MAIN ITEM CALCULATION NOTE - HP FLARE KO DRUM - N12VZ3602;

S12VZ3602 - DAMAGE SITE IN D.O.C

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Revisionlist:

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TABLEOFCONTENTS

1 INPUTDATA 32 INTERNALPRESSURECALCULATION 173 EXTERNALPRESSURECALCULATION 224 WEIGHTCALCULATION 285 WINDLOADCALCULATION 316 MOTIONLOADCALCULATION 347 CENTEROFGRAVITY 358 SADDLESUPPORT CALCULATION 369 MDMTSUMMARY 6810 VESSELDESIGNSUMMARY 70

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PV Elite Vessel Analysis Program: Input Data Design Internal Pressure (for Hydrotest) 10.0000 bar Design Internal Temperature 115 C Type of Hydrotest UG-99(b) Hydrotest Position Horizontal Projection of Nozzle from Vessel Top 603.00 mm Projection of Nozzle from Vessel Bottom 283.00 mm Minimum Design Metal Temperature -60 C Type of Construction Welded Special Service Air/Water/Steam Degree of Radiography RT 1 Use Higher Longitudinal Stresses (Flag) Y Select t for Internal Pressure (Flag) N Select t for External Pressure (Flag) N Select t for Axial Stress (Flag) N Select Location for Stiff. Rings (Flag) N Consider Vortex Shedding N Perform a Corroded Hydrotest N Is this a Heat Exchanger No User Defined Hydro. Press. (Used if > 0) 0.0000 bar User defined MAWP 10.0000 bar User defined MAPnc 0.0000 bar Load Case 1 NP+EW+WI+FW+BU Load Case 2 NP+EW+EE+FS+BU Load Case 3 IP+OW+WI+FW+BW Load Case 4 IP+OW+EQ+FS+BS Load Case 5 IP+OW+WI+FW+BN Load Case 6 IP+OW+EQ+FS+BU Load Case 7 EP+OW+WI+FW+BW Load Case 8 EP+OW+EQ+FS+BS Load Case 9 EP+OW+WI+FW+BN Load Case 10 EP+OW+EQ+FS+BU Load Case 11 HP+HW+HI Load Case 12 HP+HW+HE Load Case 13 NP+OW+WI+FW+BW Load Case 14 NP+OW+WQ+FS+BS Load Case 15 NP+EW Load Case 16 IP+WE+EW Load Case 17 IP+WF+CW Load Case 18 FS+BS+IP+OW Load Case 19 FS+BS+EP+OW Wind Design Code ASCE-7 2010 Basic Wind Speed [V] 28.100 m/sec Surface Roughness Category D: Flat, unobstructed Importance Factor 1.0 Type of Surface Moderately Smooth

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Base Elevation 32634. mm Percent Wind for Hydrotest 33.0 Using User defined Wind Press. Vs Elev. N Height of Hill or Escarpment H or Hh 0.0000 mm Distance Upwind of Crest Lh 0.0000 mm Distance from Crest to the Vessel x 0.0000 mm Type of Terrain ( Hill, Escarpment ) Flat Damping Factor (Beta) for Wind (Ope) 0.0100 Damping Factor (Beta) for Wind (Empty) 0.0000 Damping Factor (Beta) for Wind (Filled) 0.0000 Seismic Design Code G Loading Seismic Importance Factor 1.000 G Loading Coefficient Gx 0.190 G Loading Coefficient Gz 0.530 G Loading Coefficient Gy -0.180 Percent Seismic for Hydrotest 100.000 Design Nozzle for Des. Press. + St. Head Y Consider MAP New and Cold in Noz. Design N Consider External Loads for Nozzle Des. Y Use ASME VIII-1 Appendix 1-9 N Material Database Year Current w/Addenda or Code Year Configuration Directives: Do not use Nozzle MDMT Interpretation VIII-1 01-37 No Use Table G instead of exact equation for "A" Yes Shell Head Joints are Tapered Yes Compute "K" in corroded condition Yes Use Code Case 2286 No Use the MAWP to compute the MDMT Yes Using Metric Material Databases, ASME II D No Complete Listing of Vessel Elements and Details: Element From Node 10 Element To Node 20 Element Type Spherical Description Left Head Distance "FROM" to "TO" 145.00 mm Inside Diameter 4208.0 mm Element Thickness 14.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 16.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 10.0000 bar Design Temperature Internal Pressure 115 C Design External Pressure 1.0340 bar Design Temperature External Pressure 115 C

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Effective Diameter Multiplier 1.2 Material Name [Impact Tested] SA-537 Allowable Stress, Ambient 157.90 MPa Allowable Stress, Operating 157.09 MPa Allowable Stress, Hydrotest 372.33 MPa Material Density 7750.4 kg/m P Number Thickness 31.750 mm Yield Stress, Operating 318.69 MPa UCS-66 Chart Curve Designation Impact Tested External Pressure Chart Name CS-5 UNS Number K12437 Class / Thickness / Grade 2:: 0 ) 4662.2 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 10 Detail Type Nozzle Detail ID U1 Dist. from "FROM" Node / Offset dist 1000.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 10 Detail Type Nozzle

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Detail ID H1 Dist. from "FROM" Node / Offset dist 1500.0 mm Nozzle Diameter 8.0 in. Nozzle Schedule 80 Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 485.59 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 -------------------------------------------------------------------- Element From Node 20 Element To Node 30 Element Type Cylinder Description Shell Distance "FROM" to "TO" 14000. mm Inside Diameter 4200.0 mm Element Thickness 22.000 mm Internal Corrosion Allowance 3.0000 mm Nominal Thickness 22.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 10.0000 bar Design Temperature Internal Pressure 115 C Design External Pressure 1.0340 bar Design Temperature External Pressure 115 C Effective Diameter Multiplier 1.2 Material Name [Impact Tested] SA-537 Efficiency, Longitudinal Seam 1.0 Efficiency, Circumferential Seam 1.0 Element From Node 20 Detail Type Saddle Detail ID Fixed saddle Dist. from "FROM" Node / Offset dist 1400.0 mm Width of Saddle 420.00 mm Height of Saddle at Bottom 2600.0 mm Saddle Contact Angle 130.0 Height of Composite Ring Stiffener 0.0000 mm Width of Wear Plate 440.00 mm Thickness of Wear Plate 22.000 mm Contact Angle, Wear Plate (degrees) 140.0 Element From Node 20 Detail Type Saddle Detail ID Sliding saddle Dist. from "FROM" Node / Offset dist 12600. mm Width of Saddle 420.00 mm Height of Saddle at Bottom 2600.0 mm Saddle Contact Angle 130.0

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Height of Composite Ring Stiffener 0.0000 mm Width of Wear Plate 440.00 mm Thickness of Wear Plate 22.000 mm Contact Angle, Wear Plate (degrees) 140.0 Element From Node 20 Detail Type Platform Detail ID PLAT:[1 OF 1] Dist. from "FROM" Node / Offset dist 0.0000 mm Platform Start Angle (degrees) 0.0 Platform End Angle (degrees) 0.0 Platform Wind Area 5.04E+06 mm Platform Weight 928.00 N Platform Railing Weight 0.02919 N/mm Platform Grating Weight 0.004880 kg/cm Platform Width 4200.0 mm Platform Height 1500.0 mm Platform Clearance or End Offset 76.000 mm Platform Force Coefficient 0.80000001 Ladder Layout Angle 0.0 Ladder Start Elevation -2500.0 mm Ladder End Elevation 4500.0 mm Unit Weight of Ladder 0.05400 N/mm Platform Length (top head platform) 14000. mm Element From Node 20 Detail Type Liquid Detail ID WATER Dist. from "FROM" Node / Offset dist 0.0000 mm Height/Length of Liquid 3010.0 mm Liquid Density 1178.0 kg/m Element From Node 20 Detail Type Ring Detail ID Ring #2 Dist. from "FROM" Node / Offset dist 7145.0 mm Inside Diameter of Ring 4244.0 mm Thickness of Ring 20.000 mm Outside Diameter of Ring 4644.0 mm Material Name SA-537 Height of Section Ring 0.0000 mm Using Custom Stiffener Section No Element From Node 20 Detail Type Ring Detail ID Ring #1 Dist. from "FROM" Node / Offset dist 1400.0 mm Stiffening Ring Moment of Inertia 511.E+06 mm**4 Distance from Shell Surface to Centr 200.00 mm Stiffening Ring Cross Sectional Area 19200. mm Material Name SA-537

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Stiffening Ring Section Name Fab. Section Height of Section Ring 400.00 mm Using Custom Stiffener Section Yes Stiffener Dimension "A" 20.000 mm Stiffener Dimension "B" 300.00 mm Stiffener Dimension "C" 360.00 mm Stiffener Dimension "D" 20.000 mm Stiffener Dimension "E" 300.00 mm Stiffener Dimension "F" 20.000 mm Element From Node 20 Detail Type Ring Detail ID Ring #3 Dist. from "FROM" Node / Offset dist 12600. mm Stiffening Ring Moment of Inertia 431.E+06 mm**4 Distance from Shell Surface to Centr 222.09 mm Stiffening Ring Cross Sectional Area 17200. mm Material Name SA-537 Stiffening Ring Section Name Fab. Section Height of Section Ring 400.00 mm Using Custom Stiffener Section Yes Stiffener Dimension "A" 20.000 mm Stiffener Dimension "B" 200.00 mm Stiffener Dimension "C" 360.00 mm Stiffener Dimension "D" 20.000 mm Stiffener Dimension "E" 300.00 mm Stiffener Dimension "F" 20.000 mm Element From Node 20 Detail Type Nozzle Detail ID A1 Dist. from "FROM" Node / Offset dist 680.00 mm Nozzle Diameter 36.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 6353.1 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID A2 Dist. from "FROM" Node / Offset dist 3330.0 mm Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3114.8 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID B1 Dist. from "FROM" Node / Offset dist 13425. mm Nozzle Diameter 28.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3686.9 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID B2 Dist. from "FROM" Node / Offset dist 11775. mm Nozzle Diameter 16.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 1242.5 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID A3 Dist. from "FROM" Node / Offset dist 2330.0 mm Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 3114.8 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID A4 Dist. from "FROM" Node / Offset dist 4110.0 mm Nozzle Diameter 10.0 in. Nozzle Schedule 80 Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 654.34 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID F Dist. from "FROM" Node / Offset dist 11930. mm Nozzle Diameter 3.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 126.78 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID D1 Dist. from "FROM" Node / Offset dist 500.00 mm Nozzle Diameter 3.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 161.36 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID D2 Dist. from "FROM" Node / Offset dist 7400.0 mm Nozzle Diameter 3.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 161.36 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID D3 Dist. from "FROM" Node / Offset dist 13000. mm Nozzle Diameter 3.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 161.36 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID M3 Dist. from "FROM" Node / Offset dist 4930.0 mm Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) Y Weight of Nozzle ( Used if > 0 ) 5018.6 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID G1 Dist. from "FROM" Node / Offset dist 4000.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 73.607201 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID G2 Dist. from "FROM" Node / Offset dist 4000.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 145.401 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L1 Dist. from "FROM" Node / Offset dist 8130.0 mm Nozzle Diameter 4.0 in. Nozzle Schedule 160 Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 233.52 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L2 Dist. from "FROM" Node / Offset dist 8830.0 mm Nozzle Diameter 4.0 in. Nozzle Schedule 160 Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 233.52 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L3 Dist. from "FROM" Node / Offset dist 9230.0 mm Nozzle Diameter 4.0 in. Nozzle Schedule 160 Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 233.52 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L4 Dist. from "FROM" Node / Offset dist 9630.0 mm Nozzle Diameter 4.0 in. Nozzle Schedule 160 Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 233.52 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID T1 Dist. from "FROM" Node / Offset dist 1000.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 145.401 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID T2 Dist. from "FROM" Node / Offset dist 6800.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 145.401 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID T3 Dist. from "FROM" Node / Offset dist 13800. mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 145.401 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID P2 Dist. from "FROM" Node / Offset dist 11330. mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L5 Dist. from "FROM" Node / Offset dist 7300.0 mm Nozzle Diameter 3.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 76.397598 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 161.36 N Grade of Attached Flange GR 1.1

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Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID L6 Dist. from "FROM" Node / Offset dist 7300.0 mm Nozzle Diameter 3.0 in. Nozzle Schedule 160 Nozzle Class 150 Layout Angle 140.905 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 173.45 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Nozzle Detail ID M4 Dist. from "FROM" Node / Offset dist 10380. mm Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) Y Weight of Nozzle ( Used if > 0 ) 5018.6 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 20 Detail Type Weight Detail ID INTERNALS Dist. from "FROM" Node / Offset dist 7000.0 mm Miscellaneous Weight 38243. N Offset from Element Centerline 0.0000 mm Element From Node 20 Detail Type Weight Detail ID PIPING Dist. from "FROM" Node / Offset dist 7000.0 mm Miscellaneous Weight 86293. N Offset from Element Centerline 0.0000 mm -------------------------------------------------------------------- Element From Node 30 Element To Node 40 Element Type Spherical Description Right Head Distance "FROM" to "TO" 145.00 mm Inside Diameter 4208.0 mm Element Thickness 14.000 mm Internal Corrosion Allowance 3.0000 mm

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Nominal Thickness 16.000 mm External Corrosion Allowance 0.0000 mm Design Internal Pressure 10.0000 bar Design Temperature Internal Pressure 115 C Design External Pressure 1.0340 bar Design Temperature External Pressure 115 C Effective Diameter Multiplier 1.2 Material Name [Impact Tested] SA-537 Efficiency, Longitudinal Seam 1.0 Efficiency, Circumferential Seam 1.0 Element From Node 30 Detail Type Liquid Detail ID WATER Dist. from "FROM" Node / Offset dist 0.0000 mm Height/Length of Liquid 3155.0 mm Liquid Density 1178.0 kg/m Element From Node 30 Detail Type Nozzle Detail ID M2 Dist. from "FROM" Node / Offset dist 0.0000 mm Nozzle Diameter 24.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 0.0 Blind Flange (Y/N) Y Weight of Nozzle ( Used if > 0 ) 4718.5 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 30 Detail Type Nozzle Detail ID U2 Dist. from "FROM" Node / Offset dist 1000.0 mm Nozzle Diameter 2.0 in. Nozzle Schedule None Nozzle Class 150 Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 94.940 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 Element From Node 30 Detail Type Nozzle Detail ID H2 Dist. from "FROM" Node / Offset dist 1500.0 mm Nozzle Diameter 8.0 in. Nozzle Schedule 80 Nozzle Class 150

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Layout Angle 180.0 Blind Flange (Y/N) N Weight of Nozzle ( Used if > 0 ) 485.59 N Grade of Attached Flange GR 1.1 Nozzle Matl [Impact Tested] SA-350 LF3 PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2014

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Element Thickness, Pressure, Diameter and Allowable Stress : | | Int. Press | Nominal | Total Corr| Element | Allowable | From| To | + Liq. Hd | Thickness | Allowance | Diameter | Stress(SE)| | | bar | mm | mm | mm | MPa | --------------------------------------------------------------------------- Left Head| 10.365 | 16.000 | 3.0000 | 4208.0 | 157.09 | Shell| 10.348 | 22.000 | 3.0000 | 4200.0 | 157.09 | Right Head| 10.365 | 16.000 | 3.0000 | 4208.0 | 157.09 | Element Required Thickness and MAWP : | | Design | M.A.W.P. | M.A.P. | Minimum | Required | From| To | Pressure | Corroded | New & Cold | Thickness | Thickness | | | bar | bar | bar | mm | mm | ---------------------------------------------------------------------------- Left Head| 10.00000 | 16.0180 | 20.9817 | 14.0000 | 9.95661 | Shell| 10.00000 | 13.7660 | 16.4357 | 22.0000 | 16.9102 | Right Head| 10.00000 | 16.0180 | 20.9817 | 14.0000 | 9.95661 | Minimum 10.000 16.436 MAWP: 10.000 bar, limited by: DESIGN (user specified) Internal Pressure Calculation Results : ASME Code, Section VIII, Division 1, 2013 Spherical Head From 10 To 20 SA-537 at 115 C Left Head Longitudinal Joint: Full Radiography per UW-11(a) Type 1 Circumferential Joint: Full Radiography per UW-11(a) Type 1 Material UNS Number: K12437 Required Thickness due to Internal Pressure [tr]: = (P*R)/(2*S*E-0.2*P) per UG-27 (d) = (10.365*2107.0000)/(2*157.09*1.00-0.2*10.365) = 6.9566 + 3.0000 = 9.9566 mm Max. Allowable Working Pressure at given Thickness, corroded [MAWP]: Less Operating Hydrostatic Head Pressure of 0.365 bar = (2*S*E*t)/(R+0.2*t) per UG-27 (d) = (2*157.09*1.00*11.0000)/(2107.0000+0.2*11.0000) = 16.383 - 0.365 = 16.018 bar Maximum Allowable Pressure, New and Cold [MAPNC]: = (2*S*E*t)/(R+0.2*t) per UG-27 (d) = (2*157.90*1.00*14.0000)/(2104.0000+0.2*14.0000)

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= 20.982 bar Actual stress at given pressure and thickness, corroded [Sact]: = (P*(R + 0.2*t))/(2*E*t) = (10.365*(2107.0000+0.2*11.0000))/(2*1.00*11.0000) = 99.384 MPa Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 0.568 % MDMT Calculations in the Spherical Portion: Note: This Element/Detail was specified as being Impact Tested. Cylindrical Shell From 20 To 30 SA-537 at 115 C Shell Longitudinal Joint: Full Radiography per UW-11(a) Type 1 Circumferential Joint: Full Radiography per UW-11(a) Type 1 Material UNS Number: K12437 Required Thickness due to Internal Pressure [tr]: = (P*R)/(S*E-0.6*P) per UG-27 (c)(1) = (10.348*2103.0000)/(157.09*1.00-0.6*10.348) = 13.9102 + 3.0000 = 16.9102 mm Max. Allowable Working Pressure at given Thickness, corroded [MAWP]: Less Operating Hydrostatic Head Pressure of 0.348 bar = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (157.09*1.00*19.0000)/(2103.0000+0.6*19.0000) = 14.114 - 0.348 = 13.766 bar Maximum Allowable Pressure, New and Cold [MAPNC]: = (S*E*t)/(R+0.6*t) per UG-27 (c)(1) = (157.90*1.00*22.0000)/(2100.0000+0.6*22.0000) = 16.436 bar Actual stress at given pressure and thickness, corroded [Sact]: = (P*(R+0.6*t))/(E*t) = (10.348*(2103.0000+0.6*19.0000))/(1.00*19.0000) = 115.174 MPa Percent Elongation per UCS-79 (50*tnom/Rf)*(1-Rf/Ro) 0.521 % Minimum Design Metal Temperature Results: Note: This Element/Detail was specified as being Impact Tested.

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Spherical Head From 30 To 40 SA-537 at 115 C Right Head Longitudinal Joint: Full Radiography per UW-11(a) Type 1 Circumferential Joint: Full Radiography per UW-11(a) Type 1 Material UNS Number: K12437 Required Thickness due to Internal Pressure [tr]: = (P*R)/(2*S*E-0.2*P) per UG-27 (d) = (10.365*2107.0000)/(2*157.09*1.00-0.2*10.365) = 6.9566 + 3.0000 = 9.9566 mm Max. Allowable Working Pressure at given Thickness, corroded [MAWP]: Less Operating Hydrostatic Head Pressure of 0.365 bar = (2*S*E*t)/(R+0.2*t) per UG-27 (d) = (2*157.09*1.00*11.0000)/(2107.0000+0.2*11.0000) = 16.383 - 0.365 = 16.018 bar Maximum Allowable Pressure, New and Cold [MAPNC]: = (2*S*E*t)/(R+0.2*t) per UG-27 (d) = (2*157.90*1.00*14.0000)/(2104.0000+0.2*14.0000) = 20.982 bar Actual stress at given pressure and thickness, corroded [Sact]: = (P*(R + 0.2*t))/(2*E*t) = (10.365*(2107.0000+0.2*11.0000))/(2*1.00*11.0000) = 99.384 MPa Percent Elong. per UCS-79, VIII-1-01-57 (75*tnom/Rf)*(1-Rf/Ro) 0.568 % MDMT Calculations in the Spherical Portion: Note: This Element/Detail was specified as being Impact Tested. Hydrostatic Test Pressure Results: Pressure per UG99b = 1.3 * M.A.W.P. * Sa/S 13.000 bar Pressure per UG99b[36] = 1.3 * Design Pres * Sa/S 13.000 bar Pressure per UG99c = 1.3 * M.A.P. - Head(Hyd) 20.867 bar Pressure per UG100 = 1.1 * M.A.W.P. * Sa/S 11.000 bar Pressure per PED = 1.43 * MAWP 14.300 bar UG-99(b), Test Pressure Calculation: = Test Factor * MAWP * Stress Ratio = 1.3 * 10.000 * 1.000 = 13.000 bar Horizontal Test performed per: UG-99b

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Please note that Nozzle, Shell, Head, Flange, etc MAWPs are all considered when determining the hydrotest pressure for those test types that are based on the MAWP of the vessel. Stresses on Elements due to Test Pressure: From To Stress Allowable Ratio Pressure ---------------------------------------------------------------------- Left Head 100.9 372.3 0.271 13.41 Shell 128.8 372.3 0.346 13.41 Right Head 100.9 372.3 0.271 13.41 ---------------------------------------------------------------------- Stress ratios for Nozzle and Pad Materials: Description Pad/Nozzle Ambient Operating ratio ---------------------------------------------------------------------- M1 Nozzle 137.90 137.90 1.000 U1 Nozzle 137.90 137.90 1.000 H1 Nozzle 137.90 137.90 1.000 A1 Nozzle 137.90 137.90 1.000 A2 Nozzle 137.90 137.90 1.000 B1 Nozzle 137.90 137.90 1.000 B2 Nozzle 137.90 137.90 1.000 A3 Nozzle 137.90 137.90 1.000 A4 Nozzle 137.90 137.90 1.000 F Nozzle 137.90 137.90 1.000 D1 Nozzle 137.90 137.90 1.000 D2 Nozzle 137.90 137.90 1.000 D3 Nozzle 137.90 137.90 1.000 M3 Nozzle 137.90 137.90 1.000 G1 Nozzle 137.90 137.90 1.000 G2 Nozzle 137.90 137.90 1.000 L1 Nozzle 137.90 137.90 1.000 L2 Nozzle 137.90 137.90 1.000 L3 Nozzle 137.90 137.90 1.000 L4 Nozzle 137.90 137.90 1.000 T1 Nozzle 137.90 137.90 1.000 T2 Nozzle 137.90 137.90 1.000 T3 Nozzle 137.90 137.90 1.000 P2 Nozzle 137.90 137.90 1.000 L5 Nozzle 137.90 137.90 1.000 L6 Nozzle 137.90 137.90 1.000 M4 Nozzle 137.90 137.90 1.000 M2 Nozzle 137.90 137.90 1.000 U2 Nozzle 137.90 137.90 1.000 H2 Nozzle 137.90 137.90 1.000 ---------------------------------------------------------------------- Minimum 1.000

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Stress ratios for Stiffening Ring Materials: Description Ambient Operating ratio ---------------------------------------------------------------------- Ring #2 157.90 157.09 1.005 Ring #1 157.90 157.09 1.005 Ring #3 157.90 157.09 1.005 ---------------------------------------------------------------------- Minimum 1.005 Stress ratios for Vessel Elements: Description Ambient Operating ratio ---------------------------------------------------------------------- Left Head 157.90 157.09 1.005 Shell 157.90 157.09 1.005 Right Head 157.90 157.09 1.005 ---------------------------------------------------------------------- Minimum 1.005 Elements Suitable for Internal Pressure. PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2014

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External Pressure Calculation Results : ASME Code, Section VIII, Division 1, 2013 Spherical Head From 10 to 20 Ext. Chart: CS-5 at 115 C Left Head Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca Sphere OD D/t Factor A B 11.000 4236.00 385.09 0.0006492 66.66 EMAP = B/((D/t)/2) = 66.6577/(385.0909/2 ) = 3.4614 bar Results for Required Thickness (Tca): Tca Sphere OD D/t Factor A B 6.012 4236.00 704.56 0.0003548 36.43 EMAP = B/((D/t)/2) = 36.4332/(704.5572/2 ) = 1.0341 bar Cylindrical Shell From 20 to Ring #1 Ext. Chart: CS-5 at 115 C Shell Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 2246.33 223.37 0.5293 0.0007855 80.65 EMAP = (4*B)/(3*(D/t)) = (4*80.6549 )/(3*223.3684 ) = 4.8138 bar Results for Required Thickness (Tca): Tca OD SLEN D/t L/D Factor A B 10.362 4244.00 2246.33 409.57 0.5293 0.0003094 31.77 EMAP = (4*B)/(3*(D/t)) = (4*31.7679 )/(3*409.5681 ) = 1.0340 bar Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 9732.71 223.37 2.2933 0.0001689 17.34 EMAP = (4*B)/(3*(D/t)) = (4*17.3410 )/(3*223.3684 ) = 1.0350 bar Cylindrical Shell From Ring #1 to Ring #2 Ext. Chart: CS-5 at 115 C Shell Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 5745.00 223.37 1.3537 0.0002929 30.07

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EMAP = (4*B)/(3*(D/t)) = (4*30.0695 )/(3*223.3684 ) = 1.7947 bar Results for Required Thickness (Tca): Tca OD SLEN D/t L/D Factor A B 15.268 4244.00 5745.00 277.97 1.3537 0.0002100 21.56 EMAP = (4*B)/(3*(D/t)) = (4*21.5611 )/(3*277.9697 ) = 1.0341 bar Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 9734.84 223.37 2.2938 0.0001688 17.34 EMAP = (4*B)/(3*(D/t)) = (4*17.3370 )/(3*223.3684 ) = 1.0347 bar Cylindrical Shell From Ring #2 to Ring #3 Ext. Chart: CS-5 at 115 C Shell Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 5455.00 223.37 1.2853 0.0003091 31.74 EMAP = (4*B)/(3*(D/t)) = (4*31.7396 )/(3*223.3684 ) = 1.8943 bar Results for Required Thickness (Tca): Tca OD SLEN D/t L/D Factor A B 14.950 4244.00 5455.00 283.88 1.2853 0.0002145 22.02 EMAP = (4*B)/(3*(D/t)) = (4*22.0196 )/(3*283.8833 ) = 1.0341 bar Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 9734.19 223.37 2.2936 0.0001689 17.34 EMAP = (4*B)/(3*(D/t)) = (4*17.3382 )/(3*223.3684 ) = 1.0348 bar Cylindrical Shell From Ring #3 to 30 Ext. Chart: CS-5 at 115 C Shell Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca OD SLEN D/t L/D Factor A B 19.000 4244.00 2246.33 223.37 0.5293 0.0007855 80.65 EMAP = (4*B)/(3*(D/t)) = (4*80.6549 )/(3*223.3684 ) = 4.8138 bar Results for Required Thickness (Tca): Tca OD SLEN D/t L/D Factor A B 10.362 4244.00 2246.33 409.57 0.5293 0.0003094 31.77 EMAP = (4*B)/(3*(D/t)) = (4*31.7679 )/(3*409.5681 ) = 1.0340 bar Results for Maximum Stiffened Length (Slen): Tca OD SLEN D/t L/D Factor A B

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19.000 4244.00 9732.71 223.37 2.2933 0.0001689 17.34 EMAP = (4*B)/(3*(D/t)) = (4*17.3410 )/(3*223.3684 ) = 1.0350 bar Spherical Head From 30 to 40 Ext. Chart: CS-5 at 115 C Right Head Elastic Modulus from Chart: CS-5 at 115 C : 0.205E+06 MPa Results for Maximum Allowable External Pressure (MAEP): Tca Sphere OD D/t Factor A B 11.000 4236.00 385.09 0.0006492 66.66 EMAP = B/((D/t)/2) = 66.6577/(385.0909/2 ) = 3.4614 bar Results for Required Thickness (Tca): Tca Sphere OD D/t Factor A B 6.012 4236.00 704.56 0.0003548 36.43 EMAP = B/((D/t)/2) = 36.4332/(704.5572/2 ) = 1.0341 bar Stiffening Ring Calcs for : Ring #1 , Fab. Section, SA-537 Effective Length of Shell 312.36 mm Area (mm) Distance (mm) Area*Dist Shell: 5934.864 9.5000 56381.203 Ring : 19200.000 219.0000 4204800.000 Total: 25134.863 4261181.000 Centroid of Ring plus Shell = 169.533 mm Inertia Distance A*Dist Shell: 178540.312 160.0327 151994592.000 Ring : 511358976.000 -49.4673 46982696.000 Total: 511537536.000 198977280.000 Available Moment of Inertia, Ring plus Shell 710514624.000 mm**4 Required Stress in Ring plus Shell BREQ 13.83 MPa Required Strain in Ring plus Shell AREQ 0.0001340 Required Moment of Inertia, Ring plus Shell = ( OD * SLEN * (TCA+ARING/SLEN) * AREQ )/ 10.9 = (4244.0000*3995.6670*(19.0000+19200.0000/3995.6670)*0.0001340)/10.9 = 21061522.0000 mm**4 Results for Stiffening Ring Weld Calculations per UG-30 Given Stiffening Ring Fillet Weld Size Wleg 16.000 mm Stiffening Ring Attachment Style CONTINUOUS Location of Stiffening Ring EXTERNAL Radial Pressure Load Pext*Slen 413.18 N /mm The Radial Shear Load V 17535.22 N The First Moment of the Area ( Ring + Shell ) Q 949772.12 mm Weld Shear Flow due to Rad. Shear Load VQ/I 23.44 N /mm The Weld Allowable Stress .55*S 86.40 MPa Minimum Weld Leg Size Min(.25,TCA,TRING) Wldmin 6.35 mm The Weld Allowable Load 2* WLeg*.55*S 2764.53 N /mm

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The Combined Weld Load SRSS of VQ/I and Pext*Slen 413.84 N /mm Stiffening Ring Calcs for : Ring #2, SA-537 Effective Length of Shell 312.36 mm Area (mm) Distance (mm) Area*Dist Shell: 5934.864 9.5000 56381.203 Ring : 4000.000 119.0000 475999.969 Total: 9934.863 532381.188 Centroid of Ring plus Shell = 53.587 mm Inertia Distance A*Dist Shell: 178540.312 44.0872 11535464.000 Ring : 13333320.000 -65.4128 17115356.000 Total: 13511860.000 28650820.000 Available Moment of Inertia, Ring plus Shell 42162652.000 mm**4 Required Stress in Ring plus Shell BREQ 16.70 MPa Required Strain in Ring plus Shell AREQ 0.0001620 Required Moment of Inertia, Ring plus Shell = ( OD * SLEN * (TCA+ARING/SLEN) * AREQ )/ 10.9 = (4244.0000*5600.0005*(19.0000+3999.9998/5600.0005)*0.0001620)/10.9 = 29553394.0000 mm**4 Results for Stiffening Ring Weld Calculations per UG-30 Given Stiffening Ring Fillet Weld Size Wleg 16.000 mm Stiffening Ring Attachment Style CONTINUOUS Location of Stiffening Ring EXTERNAL Radial Pressure Load Pext*Slen 579.07 N /mm The Radial Shear Load V 24575.94 N The First Moment of the Area ( Ring + Shell ) Q 261651.33 mm Weld Shear Flow due to Rad. Shear Load VQ/I 152.51 N /mm The Weld Allowable Stress .55*S 86.40 MPa Minimum Weld Leg Size Min(.25,TCA,TRING) Wldmin 6.35 mm The Weld Allowable Load 2* WLeg*.55*S 2764.53 N /mm The Combined Weld Load SRSS of VQ/I and Pext*Slen 598.82 N /mm Stiffening Ring Calcs for : Ring #3 , Fab. Section, SA-537 Effective Length of Shell 312.36 mm Area (mm) Distance (mm) Area*Dist Shell: 5934.864 9.5000 56381.203 Ring : 17200.000 241.0930 4146799.750 Total: 23134.863 4203181.000 Centroid of Ring plus Shell = 181.682 mm Inertia Distance A*Dist Shell: 178540.312 172.1817 175948144.000 Ring : 430697984.000 -59.4113 60710924.000 Total: 430876512.000 236659072.000 Available Moment of Inertia, Ring plus Shell 667535360.000 mm**4 Required Stress in Ring plus Shell BREQ 14.03 MPa Required Strain in Ring plus Shell AREQ 0.0001360

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Required Moment of Inertia, Ring plus Shell = ( OD * SLEN * (TCA+ARING/SLEN) * AREQ )/ 10.9 = (4244.0000*3850.6665*(19.0000+17200.0000/3850.6665)*0.0001360)/10.9 = 20307274.0000 mm**4 Results for Stiffening Ring Weld Calculations per UG-30 Given Stiffening Ring Fillet Weld Size Wleg 16.000 mm Stiffening Ring Attachment Style CONTINUOUS Location of Stiffening Ring EXTERNAL Radial Pressure Load Pext*Slen 398.18 N /mm The Radial Shear Load V 16898.88 N The First Moment of the Area ( Ring + Shell ) Q1021874.88 mm Weld Shear Flow due to Rad. Shear Load VQ/I 25.87 N /mm The Weld Allowable Stress .55*S 86.40 MPa Minimum Weld Leg Size Min(.25,TCA,TRING) Wldmin 6.35 mm The Weld Allowable Load 2* WLeg*.55*S 2764.53 N /mm The Combined Weld Load SRSS of VQ/I and Pext*Slen 399.02 N /mm External Pressure Calculations | | Section | Outside | Corroded | Factor | Factor | From| To | Length | Diameter | Thickness | A | B | | | mm | mm | mm | | MPa | --------------------------------------------------------------------------- 10| 20| No Calc | 4236.00 | 11.0000 | 0.00064920 | 66.6577 | 20|Ring| 2246.33 | 4244.00 | 19.0000 | 0.00078552 | 80.6549 | Ring|Ring| 5745.00 | 4244.00 | 19.0000 | 0.00029286 | 30.0695 | Ring|Ring| 5455.00 | 4244.00 | 19.0000 | 0.00030912 | 31.7396 | Ring| 30| 2246.33 | 4244.00 | 19.0000 | 0.00078552 | 80.6549 | 30| 40| No Calc | 4236.00 | 11.0000 | 0.00064920 | 66.6577 | External Pressure Calculations | | External | External | External | External | From| To | Actual T. | Required T.|Des. Press. | M.A.W.P. | | | mm | mm | bar | bar | ---------------------------------------------------------------- 10| 20| 14.0000 | 9.01229 | 1.03400 | 3.46142 | 20|Ring| 22.0000 | 13.3621 | 1.03400 | 4.81376 | Ring|Ring| 22.0000 | 18.2679 | 1.03400 | 1.79465 | Ring|Ring| 22.0000 | 17.9498 | 1.03400 | 1.89433 | Ring| 30| 22.0000 | 13.3621 | 1.03400 | 4.81376 | 30| 40| 14.0000 | 9.01229 | 1.03400 | 3.46142 | Minimum 1.795 External Pressure Calculations | | Actual Len.| Allow. Len.| Ring Inertia | Ring Inertia | From| To | Bet. Stiff.| Bet. Stiff.| Required | Available | | | mm | mm | mm**4 | mm**4 |

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------------------------------------------------------------------- 10| 20| No Calc | No Calc | No Calc | No Calc | 20|Ring| 2246.33 | 9732.71 | No Calc | No Calc | Ring|Ring| 5745.00 | 9734.84 | 21.06E+06 | 710.5E+06 | Ring|Ring| 5455.00 | 9734.19 | 29.55E+06 | 42.16E+06 | Ring| 30| 2246.33 | 9732.71 | 20.31E+06 | 667.5E+06 | 30| 40| No Calc | No Calc | No Calc | No Calc | Elements Suitable for External Pressure. PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2014

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Element and Detail Weights | | Element | Element | Corroded | Corroded | Extra due | From| To | Metal Wgt. | ID Volume |Metal Wgt. | ID Volume | Misc % | | | kgm | m | kgm | m | kgm | --------------------------------------------------------------------------- 10| 20| 3714.12 | 21.0154 | 3021.87 | 21.1026 | 185.706 | 20| 30| 31662.7 | 189.381 | 27364.5 | 189.922 | 1583.14 | 30| 40| 3714.12 | 21.0154 | 3021.87 | 21.1026 | 185.706 | --------------------------------------------------------------------------- Total 39090 231.41 33408 232.13 1954 Weight of Details | | Weight of | X Offset, | Y Offset, | From|Type| Detail | Dtl. Cent. |Dtl. Cent. | Description | | kgm | mm | mm | ------------------------------------------------- 10|Liqd| 21386.4 | -701.333 | 526.500 | WATER 10|Nozl| 499.213 | -2104.00 | ... | M1 10|Nozl| 10.1659 | -1851.17 | ... | U1 10|Nozl| 51.9955 | -1475.40 | ... | H1 20|Sadl| 2109.18 | 1400.00 | 2328.00 | Fixed saddle 20|Sadl| 2109.18 | 12600.0 | 2328.00 | Sliding saddle 20|Plat| 99.3678 | 6924.00 | ... | PLAT:[1 OF 1] 20|Liqd| 175248. | 7000.00 | 595.000 | WATER 20|Ring| 454.468 | 7145.00 | ... | Ring #2 20|Ring| 2279.62 | 1400.00 | ... | Ring #1 20|Ring| 2061.59 | 12600.0 | ... | Ring #3 20|Nozl| 680.273 | 680.000 | 2557.20 | A1 20|Nozl| 333.526 | 3330.00 | 2404.80 | A2 20|Nozl| 394.785 | 13425.0 | 2455.60 | B1 20|Nozl| 133.044 | 11775.0 | 2303.20 | B2 20|Nozl| 333.526 | 2330.00 | 2404.80 | A3 20|Nozl| 70.0648 | 4110.00 | 2236.52 | A4 20|Nozl| 13.5756 | 11930.0 | 2138.10 | F 20|Nozl| 17.2776 | 500.000 | 2138.10 | D1 20|Nozl| 17.2776 | 7400.00 | 2138.10 | D2 20|Nozl| 17.2776 | 13000.0 | 2138.10 | D3 20|Nozl| 537.378 | 4930.00 | 2404.80 | M3 20|Nozl| 10.1659 | 4000.00 | 2125.40 | G1 20|Nozl| 10.1659 | 4000.00 | 2125.40 | G2 20|Nozl| 25.0049 | 8130.00 | 2157.15 | L1 20|Nozl| 25.0049 | 8830.00 | 2157.15 | L2 20|Nozl| 25.0049 | 9230.00 | 2157.15 | L3 20|Nozl| 25.0049 | 9630.00 | 2157.15 | L4 20|Nozl| 10.1659 | 1000.00 | 2125.40 | T1 20|Nozl| 10.1659 | 6800.00 | 2125.40 | T2 20|Nozl| 10.1659 | 13800.0 | 2125.40 | T3 20|Nozl| 10.1659 | 11330.0 | 2125.40 | P2

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20|Nozl| 17.2776 | 7300.00 | 2138.10 | L5 20|Nozl| 18.5722 | 7300.00 | 2144.45 | L6 20|Nozl| 537.378 | 10380.0 | 2404.80 | M4 20|Wght| 3900.00 | 7000.00 | ... | INTERNALS 20|Wght| 8800.00 | 7000.00 | ... | PIPING 30|Liqd| 21386.4 | 846.333 | 526.500 | WATER 30|Nozl| 505.244 | 2249.00 | ... | M2 30|Nozl| 10.1659 | 1996.17 | ... | U2 30|Nozl| 51.9955 | 1620.40 | ... | H2 Total Weight of Each Detail Type Total Weight of Saddles 4218.4 Total Weight of Platforms 99.4 Total Weight of Liquid 218021.1 Total Weight of Stiffeners 4795.7 Total Weight of Nozzles 4411.0 Total Weight of Weights 12700.0 --------------------------------------------------------------- Sum of the Detail Weights 244245.6 kgm Weight Summation Fabricated Shop Test Shipping Erected Empty Operating ------------------------------------------------------------------------------ 41045.5 54470.6 41045.5 54470.6 41045.5 58469.9 4218.4 236907.3 4218.4 ... 4218.4 218021.1 4411.0 ... 4411.0 ... 99.4 ... ... ... ... 99.4 ... ... 4795.7 ... 4795.7 ... ... 12700.0 ... ... ... ... 4795.7 -3900.0 ... ... ... ... 4411.0 ... ... ... ... ... 3900.0 ... ------------------------------------------------------------------------------ 54470.6 291377.9 54470.6 58469.9 58469.9 285291.1 kgm Miscellaneous Weight Percent: 5.0 % Note that the above value for the miscellaneous weight percent has been applied to the shells/heads/flange/tubesheets/tubes etc. in the weight calculations for metallic components. Weight Summary Fabricated Wt. - Bare Weight W/O Removable Internals 54470.6 kgm Shop Test Wt. - Fabricated Weight + Water ( Full ) 291377.9 kgm Shipping Wt. - Fab. Wt + Rem. Intls.+ Shipping App. 54470.6 kgm Erected Wt. - Fab. Wt + Rem. Intls.+ Insul. (etc) 58469.9 kgm Ope. Wt. no Liq - Fab. Wt + Intls. + Details + Wghts. 58469.9 kgm

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Operating Wt. - Empty Wt + Operating Liq. Uncorroded 285291.1 kgm Oper. Wt. + CA - Corr Wt. + Operating Liquid 279324.2 kgm Field Test Wt. - Empty Weight + Water (Full) 291477.2 kgm Outside Surface Areas of Elements | | Surface | From| To | Area | | | mm | ---------------------------- 10| 20| 30.17E+06 | 20| 30| 186.7E+06 | 30| 40| 30.17E+06 | ------------------------------- Total 247002080.000 mm PV Elite is a trademark of Intergraph CADWorx & Analysis Solutions, Inc. 2014

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Input Values: Wind Design Code ASCE-7 2010 Basic Wind Speed [V] 28.100 m/sec Surface Roughness Category D: Flat, unobstructed Importance Factor 1.0 Type of Surface Moderately Smooth Base Elevation 32634. mm Percent Wind for Hydrotest 33.0 Using User defined Wind Press. Vs Elev. N Height of Hill or Escarpment H or Hh 0.0000 mm Distance Upwind of Crest Lh 0.0000 mm Distance from Crest to the Vessel x 0.0000 mm Type of Terrain ( Hill, Escarpment ) Flat Damping Factor (Beta) for Wind (Ope) 0.0100 Damping Factor (Beta) for Wind (Empty) 0.0000 Damping Factor (Beta) for Wind (Filled) 0.0000 Wind Analysis Results Static Gust-Effect Factor, Operating Case [G]: = min(0.85, 0.925((1 + 1.7 * gQ * Izba

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