S2

S3
B

S1
1. END USER /CLIENT: SATORP
~57747.5001 OVERALL HEIGHT 2. DESIGN BASIS: ASME SEC. VIII, DIV.1, ED. 2023 & AMIS-D-3204 (REV.5)
3. STAMPING REQUIREMENT: YES U-STAMP U2-STAMP
1260 1050 9x@610=5490 1050 840 2350 7x@610=4270 700 1050 700 8x@700=5600 1050 9x@700=6300 1050 9x@700=6300 9400
2 1 4. NATIONAL BOARD REGISTRATION: REQUIRED NOT REQUIRED
5. INSPECTION BY: AI (ABS) CLIENT TPI
B B B B

2:1 ELLIP. HEAD ID 2900

50THK. FIRE PROOFING

2:1 ELLIP. HEAD ID 2200

OPEN TOP & BOTTOM

B

6" HALF PIPE BAFFLE

HYDROTEST CONDITION
35

2-TAILING LUGS
(T.O.G. EL.+300)
P4 6. INTERNAL PRESSURE bar(g) : 6.1 (NOR.) / 6.4 (MAX.)

EL.+17918.182 C.O.G
EMPTY CONDITION

15.3THK. (MIN. A.F.)

11.9THK. (MIN. A.F.)

NOM. THK. = 18mm

NOM. THK. = 14mm A4

EL.+20883.8 C.O.G
STIFFENER RING
T1 T2 7. TEMPERATURE °C : MIN. SEE NOTE 1.16 7A. SERVICE: C3 / C4
B

INSIDE/OUTSIDE

BASE ELEV.
P2 M1 A1 A2 P1 MAX. SEE NOTE 1.16 SEE NOTE 1.17

EL.+38855
A3 B2

(BY OTHERS)
S1

SHELL ID. 2900

8. DENSITY: SEE NOTE 1.18 9. LETHAL SERVICE: NO

EL.+9250
EL.+46990

EL.+46300
EL.+46650

EL.+30450

EL.+29050
SHELL ID. 2200

EL.+37860
10. CYCLIC SERVICE: NO 11. WET SOUR SERVICE: NO
B

TAN LINE
EL. ±0.00
EL.+8050

EL.-2300

EL.-7780

EL.-8143
EL.+220
12. HYDROGEN SERVICE: NO 13. AMINE SERVICE: NO

EL.-500
HOLD
HOLE ON BAFFLE
V1

SIEVE TRAY (#32~#50) SIEVE TRAY (#1~#31) (Ø500) 14. NOMINAL CAPACITY m3 : - 15. NET CAPACITY m3 : -
(BY OTHERS) (BY OTHERS) B
VERTICAL BAFFLE
16. DESIGN PRESSURE bar(g) INTERNAL: 8 (SEE NOTE 1.19)

BASE RING O.D. 3958

SL#4

BASE RING ID. 3378

SL#2 EXTERNAL: - (SEE NOTE 1.19)
AL#14 AL#12 AL#10 AL#8 AL#6 AL#4 AL#2

SKIRT OD. 3538

300

1250
AL#15 8375 17. DESIGN TEMPERATURE °C INTERNAL: 110

B.C.D. 3760
V1 150

#31

#21

#11
#39

#38

#37

#36

#34

#33

#32

#30

#29

#28

#27

#26

#24

#23

#22

#20

#19

#18

#17

#16

#14

#13

#12

#10
#35

#25

#15
#41
EXTERNAL: - (SEE NOTE 1.19)
#50

#49

#48

#47

#46

#45

#44

#43

#42

#1
#9

#8

#7

#6

#5

#4

#3

#2
(BAFFLE HEIGHT)
700

SC#3
18a. MAX. ALLOWABLE WORKING PRESSURE: bar(g) INTERNAL: 9.0
(HOT & CORRODED)

700
AL#16

BC#11
BC#14

BC#13

BC#12

BC#10
LIMITED BY : BOTTOM HEAD

BC#9

BC#8

BC#7

BC#6

BC#4

BC#3

BC#2

SC#4
BC#5
18b. MAX. ALLOWABLE PRESSURE: bar(g)

#40
AL#17

400
300

SC#5
(COLD & NEW) INTERNAL: 13.2
AL#1 SL#3 TYP.
AL#13 AL#11 AL#9 AL#7 AL#5 AL#3 19. MDMT °C @ MAWP bar(g): B -45 @ 9.0
SHELL/HEAD/NOZZLES: 3.0

SC#1
SL#1 SC#2
HLCO +7400
BC#19

BC#18

BC#17

BC#16
BC#15
20. CORROSION ALLOWANCE: mm SKIRT : 1.5

4" HALF PIPE

CC#1
CC#2

LLCO +300
NAME PLATE
50THK./HC(H)
EL.+44240

EL.+5200

EL.+2700
HLL +5800

LLL +1900
DAVIT

INSULATION

NAME PLATE
TOP

EL.-1950
EL.-2300
EL.+40110

EL.+36920

EL.+30900

EL.+23550

EL.+16200

EL.+7800
EL.+8000

EL.+7700

EL.+750
EL.+1600
INTERNALS (WELD/REM):

EL.-8150
EL.-7150
EL.+4950
HEAD : 1.0

(HOLD)
SHELL :
V1

B1 21. JOINT EFFICIENCY: 1.0

B NOZZLE NECK TO FLANGE JOINT : 1.0
M7 22. IMPACT TEST: REQD. NOT REQD. (SEE NOTE 6.6)
1630 50 M2 M3 M4 M5 M6 L3 L7 B3 D1 B
23. PTC: REQD. NOT REQD.

EL.+2450
HOLD S.F.

EL.+200
RADIOGRAPHY: (SEE NOTE 6.2)

BC#1
610 L5
20 CONE P3 B B 24. NDT: ULTRASONIC TESTING (SEE NOTE 6.3) VT (SEE NOTE 6.4.6)
B B (SEE NOTE 4.8) PMI (SEE NOTE 6.7) MPI (SEE NOTE 6.4)
18THK. B SHOP (HORZ.): 11.7
25. HYDROSTATIC TEST PRESSURE: bar(g)
FIELD (VERTICAL): B 11.7
2380 3000 3000 2260 3000 3000 1500 3000 2850 1500 3000 3000 3000 3000 3000 3000 3000 740 2648 2298 2588 75
THK.
26 26. PNEUMATIC TEST PRESSURE bar(g): NA
19 18 17 16 15 14 13 12 11 10 9 8 7 6 5 4 3 22 23 24 25 27. MANUFACTURING TOLERANCES: YES SEE TABLE-11
50
PWHT NO
8430x14THK. (SHELL) 38110x18THK. (SHELL) S.F. 8273x20THK. 28. HEAT TREATMENT: PARTIAL PWHT -
47200 TAN TO TAN 8650 (SKIRT) STRESS RELIEVING SEE NOTE - 5
YES PROD. WELD COUPON NO

S2

S3
B3 D1 B DESIGN CODE: IMP. FACTOR: B 1.25
S1 24-M72 ANCHOR
S1

BOLT/NUTS 7.5° SITE CLASS: C

15° B PEAK GROUND ACCELERATION (bedrock) %g 3.0
A4 0° (BY OTHERS)
A2 T1 T2 200 0° TYP. OCCUPANCY CATEGORY: III - B
TRAY#1 REBOILER
0° DESIGN CODE: ASCE 7-05 BASIC WIND SPEED: 145 km/h
A1 SIDE DOWNCOMER PREFERENTIAL
31. WIND LOADING: EXPOSURE FACTOR: C IMP. FACTOR: B 1.15
CL 0°

31
AND SEAL PAN BAFFLE
33

°
0°
#2

6" HALF PIPE BAFFLE

5°
OCCUPANCY CATEGORY: III

45
OPEN TOP & BOTTOM AL#4,6,8,10,12,14 AL#2 32. PAINTING (EXTERNAL/INTERNAL): SEE NOTE-6 33. SURFACE AREA (Sq.m): ~460
L5 30
31

AL#15,17 0° 34. INSULATION : (BY OTHERS) MINERAL FIBER 50 / HC (H)

5°

P2 30 50° 50°
0° 45° P1 35. FIRE PROOFING : (BY OTHERS) CONCRETE 50mm (BOTH SIDES)
7 0°
B1 170 10 65 10 B
10 55 10 41 THK. 38 ~93700 kg
150 36 38 55 THK.
R50 THK. THK. ii. LIFTING WEIGHT ~114200 kg
270° 90° 270° 90° 270° 90° 270° 90° 110
P3 L4 L3 SL#1,3 SL#2,4 TYP. iii. EMPTY WEIGHT B ~141900 kg
100° 7 7 iv. OPERATING WT. : (EMPTY WT.+OPERATING LIQUID) ~185900 kg

50
10
TOP DAVIT 1-EARTH v. HYDROTESTING WT. : (SHOP-NEW) ~385400 kg
V1 AL#1,3 3 3
ARM LUG
250° 39 39 vi. HYDROTESTING WT. : (FIELD-CORRODED) B ~433600 kg

130
2-LIFTING THK. THK.
AL#16

10
TRUNNIONS 2-TAILING LUGS
225° 0 ° REV.

390
290
13

23 ELE. 3 3
5°

40 40
14

5°

130
THK. THK.

13
CL 0°

0
0°

22
DAVIT AL#5,7,9,11,13 37 42

50
°
15

5°
180°
#1

21

0
210°
180° L6

50
50

10
M1 M2 180° 200 DOCUMENT STATUS
170°

0
P4 L7 180° 7 7
M3 M4 M5 M6 A3 B2 190° 10
M7 37 42 THK.
VIEW V1-V1 NAME PLATE 1 : Accpted without comment
B
SCALE 1:50
SECTION S1-S1 SECTION S2-S2 SECTION S3-S3 NAME PLATE BRACKET DETAIL FOR SHELL FOR SKIRT 2 : Accepted with comments
SCALE 1:50 SCALE 1:50 B SCALE 1:50 B
3 : Reject
220 171
164 33 81 DO NOT PAINT 4 : For Information
COMP. RING OD 3958 70 .4 TYP.
THK.

74 934 10 201

1.2
22

14 R2 20 RING OD. 2388

COMP. RING ID 3520 27 29 30 70 NOTE: PERMISSION TO PROCEED DOES NOT CONSTITUTE ACCEPTANCE

23
140 6 199
C25x45°

275

35 5 x 45°

R2
RING ID. 2228 38 OF APPROVAL OF DESIGN DETAILS, CALCULATIONS, ANALYSIS,
14
THK.

ID. 275
THK.

TYP.

HOLE
16

R26 43 TYP. TEST METHODS OR MATERIALS DEVELOPED/SELECTED BY THE

50

12
NPS4

THK.
Ø76 TYP. 8 Ø15 SUPPLIER FROM FULL COMPLIANCE WITH CONTRACTUAL OBLIGATIONS.

14
ROD

45 15
210 Ø26
44 REF.
CH. 25 B B B REF. REVIEW DATE :

75
LINE LINE
Ø107 SKIRT VENT "SV1~4" DETAIL FOR "S03" 179.16° B ENGINEER LEAD ENGINEER
275

275

15
14
400

A A 187 B TYP. DETAIL OF B

14 181 31
97
182 CONICAL CYLINDER DEVELOPMENT 5
32 34 92 DETAIL IN TWO (2) SEGMENTS LADDER/GRAB RUNG STIFF. RING DETAIL EARTHING LUG DETAIL
THK.

91 70
22

THK.

14 70
THK.

70
22

14
22

14 NOZZLES TABLE NOTES:

BASE RING I.D. 3378 135 A) WITH BLIND, BOLTS AND GASKETS. D) WITH VORTEX BREAKER.
THK.

28 16 16 28 89.58°
75

SKIRT O.D. 3558 = = B) WITH BLIND, BOLTS, GASKETS AND DAVIT. E) WITH HALF PIPE BAFFLE
THK. THK. C) XX F) WITH DISTRIBUTOR
24 NOS. M72 ANCHOR BOLT 26
ID. 560

B IFR 08-July-2024 ISSUED FOR REVIEW

ID. 600

70
ID. 720

AB HA MO
1351

3.
AT B.C.D. 3760 EQ. SPACED SA1,2 2 I.D 600 - / 22 - ACCESS HOLE

3
107

BASE RING O.D. 3958 SO3 1 I.D 275 - / 22 B -

A IFR 16-Apr-2024 ISSUED FOR REVIEW FA HA MO
R53.5 SO2 1 I.D 560 - / 22 -
4135
ISSUED REVIEWED APPROVED
DETAIL OF ANCHOR B B B B SO1 1 I.D 720 - / 22 - REV. STEP REV. DATE REVISION DESCRIPTION
BY BY BY
CHAIR SECTION A-A DETAIL FOR "S02" DETAIL FOR "S01" DETAIL FOR "SA1~2" SEGMENT DETAIL B SV1~4 4 4" 80 / 8.56 - VENT HOLE

B
V1 1 4" 160 / 13.49 150# VENT WN-RF 254 x 15 SEE DWG.
45°±5° S1 1 3" XXS / 15.24 150# UTILITY CONNECTION WN-RF 190 x 18 1670
1 2 45°±5°
4 60° ±5° 6 22a 35° ± 23a A B
45°±5° TY °
5 35° ±5
37.5 P. ° T2 1 2" - / 16.8 300# TEMPERATURE CONTROLLER LWN-RF - 1670
3.2±2
1.6±1

° FA
25 9 11
1.6±1 MT T1 1 2" - / 16.8 300# TEMPERATURE TRANSMITTER LWN-RF - 1670
40° -0

50° -0°

9 13 MT P3,P4 2 2" - / 16.8 300# LWN-RF - 1670

±1
+5°

+5°

T
T

1.6
1.6±1

3.2±2 8 8 FA P2
3.2±2 1 2" - / 16.8 300# LWN-RF - 1320
T
1.6±1

3.2±2
1.6±1
±2

9 9 FC
±1

90° ML
3.2

3.2±2 0° P1 1 2" - / 16.8 300# PRESSURE GAUGE B LWN-RF - 1670

1.6

45°±5°
TYP. BUTT WELD TYP. BUTT WELD TYP. NOZZ. NECK
10
9
11
8
MC M3~7 5 24" - / 14 150# MANHOLE WN-RF 1000 x 18 1820 B AMIRAL
M
THK. ≤ 20 MM THK. > 20 MM TYP. SHELL TO TO SHELL/HEAD 9 12
FC FL M1~2 2 24" - / 14 150# MANHOLE WN-RF 800 x 14 1470 B PROJECT
LONG/CIRC. SEAM LONG/CIRC. SEAM CONE WELD JOINT (WITH R.F PAD) 180° 270° F L7 1 4" XXS / 17.12 300# WN-RF 265 x 18 1720 E
Ø2945 L5,L6 2 2" - / 16.8 300# LWN-RF - 1670 This document is the property of AMIRAL and shall not be disclosed to third parties or reproduced without permission of the owner.
S.F.
50

ID 2900 L3,L4 2 2" - / 16.8 300# LWN-RF - 1670 This document has been generated by an Electronic Document Management System. When printed it is considered as a for information only
LOADS AT BASE EMPTY OPERATING FIELD TEST PASSIVATION ($) copy. The controlled copy is the screen version and it is the holder's responsibilty that he/she holds the latest valid version.
FL L2A~C 3 2" - / 16.8 300# LEVEL GAUGE LWN-RF - 1670
VERTICAL LOAD (WEIGHT) kg 141900 185900 433600 -
L1A~C 3 2" - / 16.8 300# LEVEL GAUGE LWN-RF - 1670
21 SHEAR WIND / EARTHQUAKE kN 223 / 14 223 / 19 112 / - -
R4 9 MOMENT WIND / EARTHQUAKE kNm 6850 / 552 6853 / 746 3427 / - - B
D1 1 4" XXS / 17.12 300# DRAIN WN-RF 235 x 18 SEE DWG.
GENERAL ARRANGEMENT FOR
351.6

8.4 B3 1 14" 80 / 19.05 150# WN-RF 480 x 18 SEE DWG. D

1.6 2 R25 NOZZLE NOZZLE FLANGE FA FL FC F ML MC M MT
( M 1T H LONG. THERMAL SHEAR (µ = 0.1) kN N.A. N.A. N.A. B -
IN
.) K.
A. 23 SADDLE MOVEMENT mm N.A. N.A. N.A. -
NO.
A3 & A4
SIZE RATING
24'' 150#
(kN)
-28.8
(kN)
28.8
(kN)
21.6
(kN)
-
(kN.m)
44.9
(kN.m)
34.6
(kN.m)
-
(kN.m)
51.8
B2
B1
1
1
20"
14"
- / 26
80 / 19.05
150#
150#
TO REBOILER 310-E-2202-A/B
VAPOUR OUTLET TO E-2205
WN-RF
WN-RF
710 x 15
560 x 12
SEE DWG. D
SEE DWG.
LP DEPROPANIZER (310-C-2202 )
3.2

F.
-
°

THK. (# )
° 5
45 ±

B2 20'' 150# -24 24 18 - 31.2 24 - 36 A3,A4 2 24" - / 26 150# FROM REBOILER E-2204-A/B WN-RF 910 x 18 1820
($) SINCE PASSIVATION IS AN OCCASIONAL CONDITION, FOUNDATION CAN BE DESIGNED Doc Type: DRW Discipline: PVE Phase: DE Class: 2 System / Subsystem: NA Equipment Type: VC
CONSIDERING THE SAME LOAD COMBINATION FOR HYDRAULIC TEST WITH REDUCED WIND AND B1 & B3 14'' 150# -16.8 16.8 12.6 - 15.3 11.8 - 17.6 A2 1 12" 80 / 17.48 150# FEED FROM E-2202 WN-RF 475 x 18 1730 F
Y-FORGE RING & 1.6 WITHOUT EARTHQUAKE LOADS ACCORDING TO AMIES-M-001. A2 Contractor Company
23.9

12" 150# -14.4 14.4 10.8 - 11.2 8.6 - 13 A1 1 6" 80 / 10.97 300# REFLUX IN FROM G-2202A/B WN-RF 270 x 14 1380 E
HEAD ID 2680 Document N/A Document SA-AMI-310-1MIS-220201
A1 6" 300# -8.4 8.4 6.3 - 3.3 2.5 - 3.8 ASME REINFORCING
N° OF

SKIRT ID 2923 POSITION NOM. SCHEDULE/ TYPE AND FACING Number : ID :

PRESS. SERVICE PLATE CENTER
Ø2969 D1 4" 300# -5.6 5.6 4.2 - 1.5 1.1 - 1.7 NOZZLE SIZE THICKNESS FLANGE
CLASS (O.D. x THK) LINE
3.2

Vendor
45 ±5

B Y-FORGE DETAIL
Document MISA-2417-2202-001-V Rev.: B Scale: 1: 100 Format : A1 Folio : 1 of 2
° °

Number :
 B
DESCRIPTION MATERIAL NOTES 1. GENERAL / DESIGN: 6.2 ADDITIONALLY RADIOGRAPHY FOR THE VESSEL SHALL BE DONE AS FOLLOWS:
1.1) UNLESS OTHERWISE SPECIFIED ALL DIMENSIONS ARE IN MILLIMETERS. VESSEL SHALL BE FABRICATED AS PER
44 INTERNAL RUNGS 7 SA 516 Gr.70N ROD Ø26 x 1050 LG.
PRESSURE PARTS ASME SECTION VIII DIV.1 ED. 2023 + AMIMS-D-3204 REV.5)
1.2) NOZZLES PROJECTIONS REFERRED FROM EQUIPMENT CENTRELINE TO FLANGE CONTACT FACE. NOZZLE Weld Joint Category Radiography (RT) Ultrasonic (UT) Liquid Penetrant (LP) or Magnetic Particle (MP) 43 EARTHING LUG 1 SS 304L 6THK. x 75 x 201 LG.
SHELLS SA 516 Gr.70N+5S -
PROJECTIONS FOR NOZZLE INSTALLED ON HEADS ARE REFERRED TO EQUIPMENT TANGENT LINE OR R.L. (REF. 42 NAME PL. BRACKET 1 SA 240-304L 10THK. x 67 x 290 LG.
HEADS SA 516 Gr.70N+5S LINE). PROJECTION SHALL BE SUFFICIENT TO ALLOW REMOVAL OF BOLTS THROUGH THE FLANGES WITHOUT A and B 100% 100% 100%
INTERFERENCE WITH THE EXTERNAL SHELL AND/OR INSULATION. 41 NAME PL. BRACKET REPAD 1 SA 516 Gr.70N 10THK. x 110 x 390 LG.
SA 765 Gr.II C 100% 100% 100%
1.3) FOR VERTICAL EQUIPMENT, ALL ELEVATIONS ARE MEASURED FROM BOTTOM TANGENT LINE OR R.L. (REF. LINE). 40 2 SA 240-304L 3THK. x 130 x 150 LG.
STD. L.W.N & W.N FLANGES SA 105N D N/A 100% 100%
FOR ORIENTATION, ORIENTATION PLAN ONLY IS TO BE USED. FOR HORIZONTAL EQUIPMENT, ALL ELEVATIONS
39 NAME PLATE 'ASME' 2 SA 240-304L 3THK. x 130 x 150 LG.
NOZZLE NECKS SA 333 Gr.6 / SA516 Gr.70N ARE MEASURED FROM REFERENCE 0.00 LINE. FOR ORIENTATION, THE FRONT AND SIDE VIEW ALONG WITH
ORIENTATION PLAN ONLY IS TO BE USED. 6.3 ULTRASONIC EXAMINATION: 38 NAME PL. BRACKET 2 SA 240-304L 10THK. x 170 x 390 LG.
NOZZLE FLANGES & BLINDS SA 350 Gr. LF2 CL.1 6.3.1) UT TO BE CARRIED OUT AS PER SECTION 14.3 & TABLE 4 OF AMIMS-D-3204 (REV.5) AS APPLICABLE
1.4) BOLT HOLES IN FLANGES OF NOZZLES AND MANWAYS LOCATED IN HEADS OF EQUIPMENTS SHALL STRADDLE 37 NAME PL. BRACKET 1 SA 240-304L 10THK. x 55 x 290 LG.
REINFORCING PAD SA 516 Gr.70N THE PRINCIPAL CENTERLINES OF THE EQUIPMENT OR LINES PARALLEL THERETO. BOLT HOLES IN FLANGES OF 6.3.2) 100% UT SHALL BE DONE FOR FOLLOWING:
A. BUTT WELDS IN VESSEL SUPPORTS.
B 36 NAME PL. BRACKET REPAD 2 SA 516 Gr.70N 10THK. x 110 x 390 LG.
NOZZLES AND MANWAYS LOCATED IN SHELLS SHALL STRADDLE THE VERTICAL CENTERLINE OF EQUIPMENT.
PIPE / FITTINGS SA 333 Gr.6 / SA 420 Gr.WPL6
1.5) FLANGE TOLERANCES SHALL CONFORM TO ANSI / ASME B16.5 UNLESS OTHERWISE NOTED. FLANGES ≤24" B. FULL PENETRATION WELDS IN EXTERNAL ATTACHMENTS TO PRESSURE RETAINING PARTS 35 PLATE FOR STIFF. RING 1 SA 516 Gr.70N
SA 240 Gr.304L / SA 240 Gr.304L / SS304L ACCORDING TO STD. ASME B16.5; FLANGES >24" ACCORDING TO STD. ASME B16.47 SERIES 'A'; PIPES: CARBON ACCORDING TO REQUIREMENT OF CLAUSE 14.3.1.1(b) OF AMIMS-D-3204 (REV.5) B
STEEL ACCORDING TO ASME B36.10 (SEAMLESS); STAINLESS STEEL PER ASME B36.19; PIPE FITTINGS C. ALL SHELL/HEAD PARENT PLATE MATERIAL PER CLAUSE 14.3.1.1(a) OF AMIMS-D-3204 (REV.5) 34 2 SA 516 Gr.70N 22THK x 182 x 1954 LG.
INTERNALS
ACCORDING TO ASME B16.9; GASKETS (EXTERNAL): ACCORDING TO ASME B16.20/B16.21. 6.3.3 PARENT PLATE UNDER LIFTING TRUNNIONS SHALL BE 100% UT EXAMINED OVER AREA UNDER LIFTING LUGS 33 1 SA 516 Gr.70N 22THK x 171 x 933 LG.
DEMISTER - 1.6) BOLTS SIZES (INCLUDING STUDS AND NUTS), THREADS AND MARKING SHALL CONFORM TO ASME B1.1 WITH PLUS 150mm. TO ENSURE PLATE IS FREE FROM DEFECTS.
32 1 SA 516 Gr.70N 22THK x 181 x 1828 LG.
INTERNAL PIPES / DISTRIBUTORS SA333-6 / SA312 TP304L THREADS CLASS 2A EXTERNAL AND 2B INTERNAL. BOLTS IN 1" DIAMETER AND SMALLER SHALL BE COARSE
THREADS SERIES (UNC), BOLTS OVER 1" DIAMETER SHALL BE 8 THREAD SERIES (8UN). 6.4 MT EXAMINATION: B 31 1 SA 516 Gr.70N 22THK x 187 x 2331 LG.
TRAYS / PACKING 304 S.S 6.4.1) MT TO BE CARRIED OUT ACCORDING TO REQUIREMENT OF SECTION 14.4 & TABLE 4 OF AMIMS-D-3204 (REV.5)
1.7) DESIGN PRESSURE INDICATED AT THE TOP OF THE EQUIPMENT. STATIC HEAD/PRESSURE DROP TO BE ADDED 30 SKIRT VENT 4 SA 333 Gr.6 NPS4, SCH:80 x 164 LG.
SUPPORT RINGS & CLIPS - TO THE SAME. AS APPLICABLE.
1.8) THE CALCULATED MAWP OF A VESSEL IN THE HOT AND CORRODED CONDITION SHALL NOT BE LIMITED BY THE 6.4.2) MT TO BE DONE ON WELDS OF LIFTING DEVICES TO ENSURE DEFECT FREE WELDS. PERMANENT MAGNETIC 29 WASHER FOR SKIRT 24 F436 / A36 16THK. x 140 x 140 LG.
OTHER WELDED INTERNALS -
FLANGE RATING. DESIGN LIQUID LEVEL = FULL OF LIQUID. FOR COLUMNS, SAME SHALL BE CONSIDERED AS YOKES ARE NOT PERMITTED. PRODS ARE NOT PERMITED FOR USE ON AIR-HARDENABLE MATERIALS, THAT 28 SKIRT GUSSET PLATE 48 SA 516 Gr.70N 16THK. x 220 x 275 LG.
EXTERNAL ATTACHMENTS HIGHEST LIQUID LEVEL. REQUIRED IMPACT TESTING, AND ON THE FLUID SIDE OF PRESSURIZED COMPONENTS FOR VESSELS IN SOUR
1.9) SET-IN CONSTRUCTION IS MANDATORY FOR ALL THE NOZZLES AND SHALL NOT PROJECT INSIDE THE VESSEL SERVICE. 27 SKIRT COMP. RING 1 SA 516 Gr.70N
STIFFENING RINGS & BRACES SA 516 Gr.70N
EXCEPT FOR PROCESS REASON. 6.4.3) BEVELED EDGES OF WELD PREPARATION FOR CARBON STEEL PLATES WITH THICKNESS 25mm AND THICKER 26 SKIRT BASE RING 1 SA 516 Gr.70N
LIFTING ATTACHMENTS SA 516 Gr.70N 1.10) SPARE PARTS: SEE MATERIAL LIST AND FERROUS ALLOY PLATES SHALL BE MAGNETIC PARTICLE EXAMINED FOR LINEAR DISCONTINUITIES.
B 6.4.4) ALL EDGES PREPARED FOR WELDING AND ALL OPENINGS SHALL BE 100% MT EXAMINED IN ACCORDANCE WITH 25 SKIRT CONE 1 SA 516 Gr.70N .
INSULATION SUPPORTS SA 516 Gr.70N 1.11) NOZZLE FLANGES SEALING SURFACE FINISHING : Ra=3.2~6.4 PER ASME B 16.20.
1.12) BOLTS BELOW OR EQUAL TO 1-1/2” SHALL BE TIGHTENED THROUGH TORQUE KEY. BOLTS OVER 1-1/2” SHALL BE THE ASME SEC VIII DIV.1 24 SKIRT CONE 1 SA 516 Gr.70N .
SUPPORT CLIPS SA 516 Gr.70N
TIGHTENED THROUGH BOLT TENSIONER. BOLT TIGHTENING PROCEDURES SHALL BE PROVIDED BY VENDOR 6.4.5) WET FLUORESCENT MAGNETIC PARTICLE/PT EXAMINATION IS REQUIRED FOR THE FOLLOWING.
23 SKIRT CONE 1 SA 516 Gr.70N .
TRANSITION PLATES SA 516 Gr.70N WITH INSTRUCTIONS FOR BOTH BOLT TENSIONER METHOD AND TORQUE KEY. BOLTS OVER 1-1/2” SHALL HAVE A) PRESSURE CONTAINING WELD JOINTS CATEGORIES A, B, C AND D ACCORDING TO THE REQUIREMENTS OF
AN EXTRA LENGTH EQUAL TO A HEAVY NUT HEIGHT TO ALLOW THE USE OF THE BOLT TENSIONER. BOLTED TABLE-4 OF AMIMS-D-3204 (REV.5), AS APPLICABLE. 22 SKIRT CONE 1 SA 516 Gr.70N 20THK. x 992 x 9389 LG. .
SUPPORT
CONNECTIONS SHALL BE DESIGNED ACCORDINGLY TO PROVIDE REQUIRED CLEARANCES. B)WELDS IN THE VESSEL SUPPORTS AND ATTACHMENT FILLET WELDS 21 Y-FORGE 1 SA 765 Gr. II SEE DETAIL
FORGED RING SA 765 Gr. II 1.13) IN THE CASE OF REMOVABLE INTERNAL PARTS OR ANY INTERNAL THAT CANNOT BE DISMANTLED THAT IS NOT C)INTERNAL AND EXTERNAL ATTACHMENT WELDS TO PRESSURE VESSEL.
SKIRT 20 CONICAL SHELL PLATE 2 SA 516 Gr.70N 18THK. x 1351 x 4135 LG.
SA 516 Gr.70N SUBJECT TO FORCES, THE CORROSION ALLOWANCE SHALL BE PROVIDED ONLY ON ONE SIDE. FOR NON D) AREA WHERE TEMPORARY ATTACHMENTS HAVE BEEN REMOVED.
REMOVABLE INTERNAL PARTS (e.g.: TRAY SUPPORTS, BRACKETS, ETC.), CORROSION ALLOWANCE SHALL BE 6.4.6) VISUAL TEST (VT) SHALL BE DONE FOR FULL JOB. 19 SHELL PLATE (17th COURSE) 1 SA 516 Gr.70N 14THK. x 2380 x 6956 LG.
BASE PLATE SA 516 Gr.70N
TAKEN IN ACCOUNT FOR EACH EXPOSED SURFACE.
6.1. HARDNESS TEST: NONE 18 SHELL PLATE (16th COURSE) 1 SA 516 Gr.70N 14THK. x 3000 x 6956 LG.
BOLTING 1.14) ALL REMOVABLE INTERNALS SHALL BE MANUFACTURED IN PIECES TO PASS THROUGH THE NEAREST MANHOLE.
1.15) ALL MANWAYS SHALL BE EQUIPPED WITH JACK SCREW, CENTERING PINS AND INTERNAL LADDER RUNGS 17 SHELL PLATE (15th COURSE) 1 SA 516 Gr.70N 14THK. x 3000 x 6956 LG.
PRESSURE RETAINING BOLTS & NUTS SA320 Gr.L7 / SA194 Gr.7 B
WHERE APPLICABLE. 6.2. IMPACT TESTING:
16 SHELL PLATE (14th COURSE) 1 SA 516 Gr.70N 18THK. x 2260 x 9167 LG.
INTERNAL BOLTS & NUTS SA193 Gr.B8 / SA194 Gr.8 1.16) THE OPERATING TEMPERATURE OF THE COLUMN 310-C-2202 IS 82 °C AND 5°C AT THE BOTTOM AND TOP 6.6.1) IMPACT TEST FOR VESSEL IS EXEMPTED AS PER UCS 66(a) AND FOR FASTENERS AS PER FIG. UCS 66 NOTE(c).
RESPECTIVELY. 15 SHELL PLATE (13th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
SA193 Gr.B7 / SA194 Gr.2H / F436 / A36 (H.D.G)
1.17) AS PER PROJECT SERVICE CLASSIFICATION GUIDELINE THE FOLLOWING SERVICES IS FORSEEN TO BE 6.7. IMPACT TESTING: 14 SHELL PLATE (12th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
GASKETS APPLICABLE; 6.7.1) PMI TO BE CARRIED OUT ACCORDING TO REQUIREMENT AMIES-A-206.
-VOC SERVICE 13 SHELL PLATE (11th COURSE) 1 SA 516 Gr.70N 18THK. x 1500 x 9167 LG.
BODY FLANGE GASKETS -
-HAP SERVICE 7. HYDROSTATIC TEST: 12 SHELL PLATE (10th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
NOZZLE FLANGE GASKETS -CMR SERVICE 7.1) HYDROTEST PROCEDURE SHALL BE AS PER DOCUMENT NO. (SA-AMI-000-1MIS-000021)
7.2) GASKET & BOLTING MATERIAL USED DURING HYDROTEST SHALL BE SAME AS SERVICE GASKET. 11 SHELL PLATE (9th COURSE) 1 SA 516 Gr.70N 18THK. x 2850 x 9167 LG.
INTERNAL GASKETS NON-ASBESTOS (GRAPHITE) -LIQUEFIED COMBUSTIBLE GAS SERVICE
-AUTO REFRIGERATION SERVICE. 7.3) HYOROTEST SHALL BE CARRIED OUT WITH CLEAN POTABLE WATER. 10 SHELL PLATE (8th COURSE) 1 SA 516 Gr.70N 18THK. x 1500 x 9167 LG.
1.18) DENSITY OF LIQUID AT OPERATING TEMPERATURE IS: TOP: 559 Kg/m3 ; BOTTOM: 589 Kg/m3 . 7.4) THE TEMPERATURE DURING HYDROTEST SHALL BE AT LEAST 17°C (30°F) ABOVE THE WARMEST MDMT, BUT NOT
9 SHELL PLATE (7th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
1.19) DRY OUT CONDITIONS ARE AS FOLLOWS: TO EXCEED 48C;
TEMPERATURE: 80°C 7.5) MIN. TEMPERATURE SHOULD NOT BE LESS THAN 17°C (30°F). VESSEL SHALL BE THOROUGHLY DRIED & CLEANED 8 SHELL PLATE (6th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
PRESSURE: 7.5 barg 7 SHELL PLATE (5th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
NUMBER TITLE MECHANICAL DESIGN PRESSURE IS AT TOP OF TOWER. DESIGN PRESSURE AT BOTTOM OF TOWER SHALL BE 7.6) . B
B DETERMINED BASED ON TOWER PRESSURE DROP AND BOTTOM LIQUID STATIC HEAD.THE DESIGN PRESSURE 7.7) NO PAINT OR PRIMER SHALL BE APPLIED TO A VESSEL PRIOR TO HYDROSTATIC TESTING. 6 SHELL PLATE (4th COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
MECHANICAL DATA SHEET OF THE TOWER BOTTOM AND ASSOCIATED EQUIPMENT, AND THE DESIGN OF EQUIPMENT SUPPORTS AND THE 7.8) AFTER TESTING, THE VESSEL SHALL BE COMPLETELY DRAINED AND THOROUGHLY DRIED INCLUDING AROUND 5 SHELL PLATE (3rd COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
TOWER FOUNDATION CONSIDER POSSIBLE LIQUID OVERFILLING.DESIGN PRESSURE AT THE BOTTOM OF THE INTERNAL.
4 SHELL PLATE (2nd COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG.
TOWER IS APPROX. 11.0 barg BASED ON LIQUID OVERFILLING AND TOP DESIGN PRESSURE OF 8.0 barg. 7.9) NDT: (PER ASME SEC V) EXAMINATION OF ALL WELDS SHALL INCLUDE A BAND OF BASE METAL AT LEAST 25mm
MATERIAL REQUISITION WIDE ON EACH SIDE OF WELD. 3 SHELL PLATE (1st COURSE) 1 SA 516 Gr.70N 18THK. x 3000 x 9167 LG. .
B
2. SPARE PARTS FOR START UP & COMMISSIONING 2 2:1 ELLIP. HEAD 1 SA 516 Gr.70N .
SUPPLY SPECIFICATION a) GASKET : 200 % (FOR NOZZLES WITH BLIND) 8. SURFACE PREPARATION & PAINTING:
B b) STUD/NUT : 10% (MIN.3 SETS) (FOR NOZZLES WITH BLIND) 8.1) FOR SURFACE PREPARATION & PAINTING DETAIL SEE MISA DOCUMENT NO. (SA-AMI-000-1MIS-000032) B 1 2:1 ELLIP. HEAD 1 SA 516 Gr.70N .
AMIES-W-010 WELDING REQUIREMENT FOR PRESSURE VESSELS c) FOR STUDDED FLANGE SPARE FOR BOLT+NUT REQUIRED = 10% (MIN. 3 NOS) 8.2) EXTERNAL: SHELL AND SKIRT INSULATED PAINTING SYSTEM C, EXTERNAL NON-INSULATED ATTACHMENTS: N°
SPARE FOR INTERNALS SYSTEM C, SKIRT FIREPROOFED: SYSTEM H. PIECES
DESCRIPTION MATERIAL DIMENSIONS NOTES
a) BOLTS, NUTS & WASHERS, 10% or 10 OF EACH SIZE 8.3) INTERNAL: NONE. +
SA-AMI-000-FCON-000279 B STANDARD CONSTRUCTION DRAWINGS FOR PRESSURE VESSELS 8.4) PAINTING REQUIREMENTS: REFERENCE - SA-AMI-000-HECM-218101. SPARES
b) GASKETS, 200%
8.5) GASKET CONTACT SURFACES SHALL NOT BE COATED OR PAINTED. B
SA-AMI-000-FCON-000286 STANDARD CONSTRUCTION DRAWINGS FOR LADDERS & PLATFORMS 3. MATERIAL : 8.6) FOR PAINTING ON EXTERNAL SURFACES FINAL COLOR SHADE: EQUIPMENT : TRAFFIC GREY (RAL7042)
3.1) ALL CARBON STEEL MATERIAL SHALL BE IN NORMALIZED AND FULLY KILLED CONDITION. TOP DAVIT : YELLOW (RAL 1021).
3.2) ALL INTERNAL AND EXTERNAL PARTS WELDED TO THE SHELL SHALL BE OF THE SAME MATERIAL, WHICH MATERIALS CERTIFICATION THICKNESSES TOLERANCE
AMIMS-D-3204 (REV.5) MANUFACTURE OF PRESSURE VESSELS
CONSTITUTES THE SECTION OF THE SHELL WHERE THE PARTS WILL BE WELDED. 9. SHIPPING: (SHIPPING & PREPARATION FOR TRANSPORTATION SHALL BE AS PER SEC. 19 OF AMIMS-D-3204 (REV.5) CERTIFICATE EN 10204 3.2 PLATES: ± 0.25 mm
3.3) STUD BOLTS AND NUTS SHALL BE PROTECTED BY SOLID LUBRICANT PASTE SUITABLE FOR HIGH TEMPERATURE 9.1) VESSEL SHALL BE THOROUGHLY CLEANED INSIDE / OUTSIDE.
AMIES-D-001 (REV.5) DESIGN CRITERIA FOR PRESSURE VESSELS CERTIFICATE EN 10204 3.1 PIPES: ± 12.5%
SERVICES. 9.2) FLANGED CONNECTION & OTHER MACHINED SURFACES SHALL BE PROTECTED WITH EASILY REMOVABLE RUST
3.4) ALL MATERIALS EXCEPT CARBON STEEL SHALL BE ALLOY VERIFIED AS PER AMIES-A-206. PREVENTIVE. CERTIFICATE EN 10204 2.2 HEADS: -
B
AMIES-A-004 (REV.3) GENERAL REQUIREMENTS FOR PRESSURE TESTING 3.5) CARBON EQUIVALENT (CE) FOR PLATES AND CUSTOM FORGINGS SHALL BE LIMITED TO 0.43%. 9.3) ALL PAD TELL TALE HOLE 1/4" NPT VENT HOLE SHALL BE PLUGGED WITH STIFF GREASE AFTER TESTING.
3.6) ALL EXTERNAL FASTENERS SHALL BE FLURO-POLYMER COATED 9.4) ALL NOZZLES (WITHOUT BLIND FLANGE) SHALL BE CLOSED USING STEEL COVER + NEOPRENE GASKET USING
3.7) ALL FORGINGS SHALL BE EXAMINED ULTRASONICALLY IN ACCORDANCE WITH ASME SA-388 AND WITH MIN. 4 BOLTS.
AMIES-A-206 (REV.2) POSITIVE MATERIAL IDENTIFICATION
ACCEPTANCE CRITERIA SPECIFIED IN 14.3.1.2 OF AMIMS-D-3204 REV.5 9.5) THE INTERIOR SURFACES OF THE VESSEL SHALL BE PROTECTED FROM CORROSION BY USE OF A
3.8) ALL FORGING SHALL MEET MATERIAL CLEANLINESS C2/R2/S2 RATING, AS DESCRIBED IN ASTM E381. NON-TOXICVAPOR PHASE CORROSION INHIBITOR APPLIED AT 0.3 Kg/m3 OR AS PER APPROVED PRESERVATION
3.9) MATERIAL CERTIFICATION SHALL BE : PROCEDURE.
1) EN 10204:2004 / 3.1 9.6) STENCIL THE FOLLOWING INFORMATION ON THE VESSEL IN MINIMUM 75mm (2.95") HEIGHT LETTERS: ITEM TAG
CONTRACTOR NUMBER a) PRESSURE PARTS (INCLUDING BOLTING) AND DETAILS WELDED TO PRESSURE PARTS (PLATES, FORGINGS, NUMBER, P.O NUMBER, UNIT NUMBER & CG MARKING.
TITLE B TUBES, PIPE), SKIRT, LIFTING TRUNNION ,T LOADS. 9.7) PRIOR TO SHIPPING, VESSEL TO BE COMPLETELY AND THOROUGHLY DRIED AND CLEANED FROM ALL LOOSE
CLIENT NUMBER
B b) PLUGS AND BOLT FLANGES. SCALES, WELD SLAGS, DIRT AND DEBRIS. THE INTERIOR SURFACES OF VESSELS, INCLUDING INTERNALS, SHALL
c) ALL THE INTERNAL PARTS IN CONTACT WITH THE PROCESS FLUID. BE PROTECTED FROM CORROSION BY USE OF A NON-TOXIC VAPOUR PHASE CORROSION INHIBITOR SUCH AS
MISA-2417-2202-001-V d) REMOVABLE AND WELDED INTERNALS. COTEC VCI-309 OR 307 OR EQUIVALENT, (DEPENDING ON THE METALLURGY OF THE VESSEL) APPLIED AT A RATE
GENERAL ARRANGEMENT DRAWING FOR 310-C-2202
SA-AMI-310-1MIS-220201 OF 0.3 KG/M³ OR THE PRODUCT MANUFACTURER RECOMMENDATION
2) EN 10204:2004 / 2.2
MISA-2417-2202-003-V a) FOR ALL REMAINING ELEMENTS INCLUDING GASKETS.
SA-AMI-310-1MIS-220202
SKIRT ACCESS DRAWING FOR 310-C-2202 B IFR 08-July-2024 ISSUED FOR REVIEW AB HA MO
MISA-2417-2202-004-V 4. FABRICATION:-
TEMPLATE AND GAUGE PLATE DETAIL FOR 310-C-2202 4.1) FABRICATION TOLERANCES SHALL BE THE STRINGENT ONE OF THE APPLICABLE CODE, IOGP S-619, PIP HOLD LIST : A IFR 16-Apr-2024 ISSUED FOR REVIEW FA HA MO
SA-AMI-310-1MIS-220203
WITH THE EXCEPTIONS MENTIONED IN CLAUSE 13.1.1 OF AMIMS-D-3204 (REV.5) AND SA-AMI-000-FCON-000279. 1. ELEVATION FROM GROUND.
MISA-2417-2202-005-V 4.2) ANCHOR BOLTS SHALL STRADDLE VESSEL CENTERLINES ON NORTH-SOUTH, EAST-WEST AXIS. 2. ORIENTATION PLAN AND NORTH DIRECTION. ISSUED REVIEWED APPROVED
HYDROTEST AND TRANSPORTATION DRAWING FOR 310-C-2202
SA-AMI-310-1MIS-220204 4.3) ALL REMOVABLE INTERNALS SHALL PASS THROUGH VESSEL MANWAY. B 3. ORIENTATION AND ELEVATION OF NAME PLATE.
REV. STEP REV. DATE REVISION DESCRIPTION
BY BY BY

MISA-2417-2202-002-V 4.4) INTERNAL AND EXTERNAL WELDED ATTACHMENT PADS SHALL HAVE THEIR CORNERS ROUNDED TO A MINIMUM 4. NOZZLE, TRAY ORIENTATION HOLD.
NAME PLATE DRAWING FOR 310-C-2202 RADIUS OF 50mm AND SHALL BE FULLY SEAL-WELDED, EXCEPT FOR BLANKS SQUARE NUTS USED FOR
SA-AMI-310-1MIS-220205
EXTERNAL INSULATIONS WHERE TACK WELD IS ALLOWED.
MISA-2417-9001-007-V
TOP DAVIT FOR 310-C-2202 4.5) THE PREPARATION OF PLATE EDGES FOR WELDING SHALL BE DONE BY SHEARING, MACHINING, GRINDING OR
SA-AMI-310-1MIS-220206
THERMAL CUTTING.
MISA-2417-2202-008-V 4.6) OUTER EDGE OF WELDS ATTACHING MANWAYS, NOZZLES (WITH AND WITHOUT REINFORCED PADS) AND
DEVELOPMENT DRAWING FOR 310-C-2202
SA-AMI-310-1MIS-220207 OTHERS STRUCTURAL ATTACHMENT (WITH AND WITHOUT REINFORCED PADS), TO PRESSURE-RETAINING
MISA-2417-2202-009-V COMPONENTS SHALL NOT BE CLOSER THAN 50mm (2") (TOE TO TOE) FROM THE ADJACENT EDGE OF ANY OTHER
INSULATION AND FIREPROOFING CLIP DRAWING FOR 310-C-2202 WELD.
SA-AMI-310-1MIS-220210
4.7) 1/4" TELLTALE VENT HOLES DRILLED AND TAPPED FOR 1/4" NPT SHALL BE PROVIDED IN REINFORCING PADS FOR
MISA-2417-2202-015-V WELDED ATTACHMENTS, PER THE FOLLOWING.
EXTERNAL ATTACHMENT DRAWING FOR 310-C-2202
SA-AMI-310-1MIS-220211
4.8) ALL WELDED ATTACHMENT PROVIDED WITH TELL TALE HOLES SHALL BE PNEUMATICALLY TESTED AT MINIMUM
MISA-2417-2202-011-V
SA-AMI-310-1MIS-220230
NOZZLE DETAIL FOR 310-C-2202
4.9)
70kpa PRIOR TO HEAT TREATMENT AND VESSEL PRESSURE TESTING.
ONE HOLE IN SINGLE PIECE REINFORCING PAD. TELLTALE HOLES IN EXTERNAL ATTACHMENT PADS, SHALL BE AMIRAL
MISA-2417-2202-006-V
MANWAY DETAIL FOR 310-C-2202
PLUGGED WITH GREASE, WOODEN PLUGS OR OTHER NON-PRESSURE RETAINING MATERIAL TO PREVENT PROJECT
SA-AMI-310-1MIS-220240 MOISTURE INGRESS BETWEEN THE PAD &. THE VESSEL PRESSURE-RETAINING COMPONENT, VENT / TELLTALE
HOLES IN INTERNAL ATTACHMENT PAD SHALL BE SEAL WELDED.
MISA-2417-2202-012-V This document is the property of AMIRAL and shall not be disclosed to third parties or reproduced without permission of the owner.
WELDED INTERNAL SUPPORT DETAIL FOR 310-C-2202
SA-AMI-310-1MIS-220250 5. HEAT TREATMENT: N/A B This document has been generated by an Electronic Document Management System. When printed it is considered as a for information only
MISA-2417-2202-016-V copy. The controlled copy is the screen version and it is the holder's responsibilty that he/she holds the latest valid version.
LADDER & PLATFORM DRAWING FOR 310-C-2202 NDE, INSPECTION & TESTING :
SA-AMI-310-1MIS-220270
6.1) INSPECTION
6.1.1) PRIOR TO FINAL INSPECTION AND PRESSURE TESTING, THE INSIDE AND OUTSIDE OF THE VESSEL SHALL BE
THOROUGHLY CLEANED OF ALL SLAG, SCALE, DIRT, GRIT, WELD SPATTER, PAINT, OIL, ETC.
6.1.2 )ALL REQUIRED NDE FOR FINAL ACCEPTANCE OF THE VESSEL, PRIOR TO PRESSURE TESTING, SHALL BE
GENERAL ARRANGEMENT FOR
PERFORMED AFTER THE COMPLETION OF ALL WELDING AND REPAIRS. IN VESSELS REQUIRING PWHT, ALL NDE
FILLET WELD LEG. = +2
-0
FOR FINAL ACCEPTANCE SHALL BE PERFORMED AFTER THE FINAL PWHT.
6.1.3) ALL LIFTING ATTACHMENTS SHALL HAVE 100% MPI EXAMINED.
LP DEPROPANIZER (310-C-2202 )
BEVEL ANGLE = ±5° 6.1.4) WELDING & NDE SHALL BE AS PER WELD MAP & NDE PLAN.
= +2 6.1.5) ALL WELDED ATTACHMENTS PROVIDED WITH TELLTALE HOLES SHALL BE PNEUMATICALLY TESTED AT MINIMUM
ROOT GAP -0
Doc Type: DRW Discipline: PVE Phase: DE Class: 2 System / Subsystem: NA Equipment Type: VC
10 kPa PRIOR TO HEAT TREATMENT AND VESSEL PRESSURE TESTING. TELL TALE HOLES MUST NOT BE PLUGGED
FACE WIDTH = +0 DURING THE VESSEL PRESSURE TEST. AFTER TESTING HOLES SHALL BE PLUGGED WITH GREASE, WOODEN Contractor Company
-1
PLUGS OR OTHER NON-PRESSURE RETAINING MATERIAL PRIOR TO SHIPMENT. Document N/A Document SA-AMI-310-1MIS-220201
PERMISSIBLE OUT OF ROUNDNESS = UG-81 OF ASME SECTION VIII, DIV.1 6.1.6) ZERO POINT THICKNESS MEASUREMENT SHALL BE CARRIED OUT FOR ALL VESSELS AS PER APPENDIX III OF Number : ID :

OTHER DIMENSIONAL TOLERANCES = AS PER PIP VEFV1102M AMIMS-D-3204. Vendor

B
Document MISA-2417-2202-001-V Rev.: B Scale: 1: 100 Format : A1 Folio : 2 of 2
BASE PLATE FLATNESS = ±3 B Number :