ELM-1950001-MR-Q03-1001-R6

Rajiv Garg/ V. Surange 04.07.10

QUALITY CONTROL PLAN (Q.C.P.)

PAG 1/2

CUSTOMER AND PROJECT NAME PETROFAC X SONATRACH/ANADARKO

PLANT LOCATION EL MERK (ALGERIA)

SERVICE RESIDUE GAS COMPRESSOR

MACHINE/TRAIN COMPOSITION CENTRIFUGAL COMPRESSOR,GAS TURBINE

TOTAL PAGES COMPOSING THIS DOCUMENT 136

JOB DOCUMENT REVISION INDEX

Guerrini, Giorgia Buti, Luca Ricci Alessio 18-May-2010 REVISED WHERE INDICATED 6 6

Guerrini, Giorgia Buti, Luca Ricci Alessio 07-Apr-2010 REVISED WHERE INDICATED 5 5

Guerrini, Giorgia Buti, Luca Ricci Alessio 25-Mar-2010 REVISED WHERE INDICATED 4 4

Guerrini, Giorgia Buti, Luca Ricci Alessio 15-Jan-2010 REVISED WHERE INDICATED 3 3

Calussi, Maurizio Buti, Luca Ricci Alessio 26-Nov-2009 Added PMI Test and tests on UCS page 2

Calussi, Maurizio Buti, Luca Landini Lorenzo 25-Nov-2009 Revised where shown (1) 1

Guerrini, Giorgia Calcaterra Marco Lorenzini Riccardo 30-Jul-2009 ISSUE 0

PREPD CHK APPRD DATE DESCRIPTION REV

JOB

1102487,1102488,1800020,1800021,2991491

ITEM LANG. ANuovoPignoneFirenze

N. SOM5086579 /4 TAV/SH 1/2

This Document is the property of NUOVO PIGNONE. All rights are reserved according to law7221


QCP SOM5086579 /4


N. SOM5086579 /4 DESCRIPTION REV. DESCRIPTION REV.


Introduction Notes

1.1 PURPOSE

THIS DOCUMENT SUMMARIZES THE STANDARD TESTING DONE WITHIN THE MANUFACTURING STAGES FOR THE MAJOR COMPONENTS OF THEPRODUCT IN SUBJECT.THIS IS A REFERENCE DOCUMENT FOR:-DEFINITION OF THE QUALITY DOCUMENTATION TO BE GIVEN TO THE CUSTOMER OR HIS ENGINEERING COMPANY AS MANUFACTURER DATAREPORT (M.D.R.).-DEFINITION OF THE MANUFACTURING OR TESTING PROCEDURES TO BE WITNESSED BY INSPECTORS (IN CASE OF DETAILED QCP FOR A MAJORSUB ITEM IS GIVEN, PRESENT DOCUMENT REPRESENTS THE MASTER LIST FOR CUSTOMER WITNESS/OBSERVED POINTS DEFINITION ON WHICHTEST NOTIFICATION WILL BE GENERATED).

1.2 ACTIVITY OF THE INSPECTOR

THE INSPECTOR MAY SPECIFY THE INSPECTION HE INTENDS TO PERFORM, IN THE SPACE PROVIDED FOR THIS PURPOSE IN THE DOCUMENT.VENDOR HAS THE ABILITY TO PERFORM TEST-ON-LINE WITNESSING BY REMOTE, WITH AN EASY INTERNET ACCESS. THIS CAN BE CONSIDERED ASAN OPTION IN CASE CUSTOMER INSPECTOR CANNOT BE AVAILABLE AT THE TIME OF THE TEST.

THE FOLLOWING ACTIVITIES ARE POSSIBLE:

-W (WITNESS POINT): THIS REQUEST SHALL BE APPLIED TO HOLD THE PRODUCTION SCHEDULE AND THE INSPECTION OR TEST SHALL BE CARRIEDOUT WITH THE PURCHASER OR HIS REPRESENTATIVE IN ATTENDANCE.NOTIFICATION MUST BE TRANSMITTED IN ADVANCE AT LEAST THE TIME AS SHOWN ON JOB NOTES PARAGRAPH.THE PRESENCE OF THE INSPECTOR AT THE "W" MANUFACTURING OR TESTING STAGE IS A MANDATORY CONDITION FOR PROCEEDING TOSUBSEQUENT STAGES, UNLESS THE INSPECTOR EXPLICITLY WAIVES THIS RIGHT, INFORMING THE PERTINENT GE O&G REPRESENTATIVE OF HISDECISION IN WRITING.SHOULD THE TEST BE RE-SCHEDULED DUE TO INSPECTOR AVAILABILITY, VENDOR SHALL INFORM THE CUSTOMER OF EVENTUAL ASSOCIATEDDELAY ON THE MANUFACTURING SCHEDULE AND SHALL HAVE THE RIGHT TO EXTEND THE PROJECT ACCORDINGLY.

-O (OPTIONAL OBSERVED POINT): THE PURCHASER SHALL BE NOTIFIED OF THE TIMING OF THE INSPECTION OR TEST; HOWEVER, THE INSPECTIONOR TEST SHALL BE PERFORMED AS SCHEDULED, AND IF THE PURCHASER OR HIS REPRESENTATIVE IS NOT PRESENT, THE VENDOR MAY PROCEEDTO THE NEXT STEP, EVEN IF A FORMAL WAIVE HAS NOT BEEN RECEIVED.NOTIFICATION MUST BE TRANSMITTED IN ADVANCE AT LEAST THE TIME AS SHOWN ON JOB NOTES PARAGRAPH.

TAV/SH 2/3

PAG 2/3


QCP SOM5086579 /4




-R (REVIEW): THIS IS A REQUEST TO REVIEW QUALITY DOCUMENTATION AND, UNLESS OTHERWISE STATED, IT IS ALLOWED WHEN THE FINALDOCUMENTATION DOSSIER HAS BEEN COMPLETED.

-A (APPROVAL): THIS IS A PRELIMINARY APPROVAL REQUEST OF THE QUALITY DOCUMENTATION, AND IT IS MADE IN ADEQUATE ADVANCE, BEFORETHE RELEVANT MANUFACTURING STAGE BEGINS.

1.3 CERTIFICATION

THE CERTIFICATION ISSUED FOR THE TESTS PERFORMED IS LISTED IN THIS DOCUMENT IN THE APPROPRIATE SPACE PROVIDED FOR THISPURPOSE. TYPE OF CERTIFICATES ARE: 2.1, 3.1 AND 3.2 AS PER EN10204 ed.2004 (ITN 07771 IS THE NP INTERNAL REFERENCE DOCUMENT).ABOVE MENTIONED CERTIFICATION WILL BE INCLUDED IN THE MANUFACTURER DATA REPORT (M.D.R.) AS FINAL DOSSIER, ACCORDING TO OIL&GASSTANDARD, DESCRIBED IN THE OTR-MN-06-A-PLANT-01 PROCEDURE.

1.3.1 INTERNAL RECORDS

FOR DETERMINED MANUFACTURING OR TESTING STAGES, BASICALLY THE INTERMEDIATE ONES, NO CERTIFICATION IS ISSUED, BUT AN INHOUSERECORD IS KEPT (TEST PLANS) OF THE TEST AND INSPECTIONS CARRIED OUT, INCLUDING THEIR RESULTS. THIS DOCUMENTATION IS AVAILABLEFOR REVIEW UPON REQUEST AT THE OIL&GAS INSPECTION DEPARTMENT AND USUALLY AT THE SUBSUPPLIER'S PLANTS AS WELL.

-I (INTERNAL RECORD): IS THE SYMBOL THAT IDENTIFIES THIS TYPE OF MANUFACTURING OR TESTING STAGE IN THE DOCUMENT.

1.4. CONTROL PROCEDURES AND REFERENCE DOCUMENTS

THE ACCEPTANCE CRITERIA DRAWN FROM THE SINGLE PROCEDURES VALID ON ISSUING THIS DOCUMENT ARE AN INTEGRAL PART OF SAIDDOCUMENT AND ARE ENCLOSED FOR REFERENCE.

SHOULD THE TEST RESULTS NOT BE IN COMPLIANCE WITH THE AFOREMENTIONED ACCEPTANCE CRITERIA, IT IS NECESSARY TO REFER TO THEORIGINAL DOCUMENTS, WHICH COULD HAVE BEEN REVISED AFTER ISSUE OF THIS DOCUMENT.

THE DOCUMENTS (SPECIFICATIONS OR DRAWINGS) MENTIONED IN THIS DOCUMENT CAN BE CONSULTED, ON REQUEST, AT NUOVO PIGNONE'SOFFICE AND ARE THE OFFICIAL REFERENCES FOR ALL INTENTS AND PURPOSES.

1.5. "STD/NON-STD" COLUMN

THIS COLUMN IDENTIFIES IF TESTS AND INSPECTIONS OR THEIR ATTRIBUTES ARE STANDARD OR NOT, FOR INTERNAL USE ONLY.

1.6. STRING TEST

TAV/SH 3/4

PAG 3/4


QCP SOM5086579 /4




FOR JOBS WHERE STRING TEST IS APPLICABLE:DUE TO STRING TEST SPECIFIC NATURE THE AVAILABILITY OF CUSTOMER INSPECTOR OR REPRESENTATIVE SHOULD COVER ALL THE NECESSARYTIME TO COMPLETE THE ON GOING TEST (24 HRS/DAY, 7 DAYS/WEEK).GE NP REQUIRES 2-6 DAYS, DEPENDING ON ADVANCE NOTICE REQUIREMENT, TO BE CONSIDERED BY CUSTOMER WHEN BOOKING THEATTENDANCE TO THE TEST. DETAILS TO BE AGREED BEFORE ACTUAL TEST IN BETWEEN OIL&GAS INVOLVED TEAM AND CUSTOMERS/THIRDPARTIES.

1.7 NON-CONFORMITY REPAIRS

1.7.1 NOTIFICATION POLICYWhen a QCP test will origin a non conformance, if no more stringent clauses are agreed into the Contract (including MoM’s), following policies will apply:

Management of nonconformities in manufacturing phase QUA-QMS-04Customer Notification Policy for Centrifugal Cprs. ITN00460Customer Notification Policy for Gas Turbines ITM01200

1.7.2 STANDARD REPAIR PROCEDURESGENP engineering has consolidated standard repair procedures to be used by manufacturing to perform repair without prior engineering approval.The defects categories and application range are listed in the following documents:

Standard repair procedure for Centrifugal Cprs. ITN02240Standard repair procedure for Gas Turbines ITN07762

1.8 ARH DOSSIERS: PLEASE REFER TO SOM5459916 (ELM-BRC-QA-PRC-0001) (1)

1.9REFERENCE TO API 617 SHALL BE CONSIDERED AS API 617 7th EDITION, INCLUDED GENP STD EXCEPTIONS (1)

2.0 LIST OFEQUIPMENTS SUBJECT TO ARH REQUIREMENTS:(1)

Mineral Oil CoolerFuel gas 2-stages scrubber<6>Compressors CasingsAntisurge Control Valve 1st StageAntisurge Control Valve 2nd StageStartingMotor

TAV/SH 4/5

PAG 4/5


QCP SOM5086579 /4




Oil accumulatorMain & stand-by seal gas coalescer filtersSafety Valve ScrubberSafety Valve (Primary Vent)HotBy-Pass

TAV/SH 5/6

PAG 5/6


QCP SOM5086579 /4




Table of ContentsJOBNOTES Job Notes pagina/page 10

ABBR Abbreviations pagina/page 13

1005000 INLET PLENUM pagina/page 14

1010000 EXHAUST PLENUM pagina/page 15

1035000 INLET CASING pagina/page 16

1060000 AXIAL COMPRESSOR CASING pagina/page 17

1080000 AXIAL COMPRESSOR DISCHARGE CASING pagina/page 18

1120000 TURBINE CASING pagina/page 19

1215000 TURBINE EXHAUST CASING (CASTING PART) pagina/page 20

1220000 TURBINE EXHAUST CASING (FABRICATED PART) pagina/page 21

1260000 COMBUSTION CHAMBER CASING pagina/page 22

1270000 COMBUSTION CHAMBER CAP & LINER pagina/page 23

1330000 TRANSITION PIECE pagina/page 24

1420000 N.2-3 BEARING SUPPORT pagina/page 25

1440000 N.4 BEARING SUPPORT pagina/page 26

1655000 HIGH PRESSURE ROTOR pagina/page 27

1680000 LOW PRESSURE ROTOR pagina/page 28

1760000 GAS TURBINE pagina/page 29

2005000 CASING FORGED STEEL: BCL ; NOZZLES FORGED STEEL: BCL pagina/page 30

2010000 COVER/S FORGED STEEL (WITHOUT WELDS): BCL pagina/page 31

2020000 FABRICATED CASING FOR BCL pagina/page 32

2040000 FORGED STEEL COUNTER CASING : BCL pagina/page 33

TAV/SH 6/7

PAG 6/7


QCP SOM5086579 /4




2100000 DIAPHRAGMS CAST IRON : BCL pagina/page 34

2105000 DIAPHRAGMS FORGED ; BCL pagina/page 35

2120000 DIAPHRAGMS MACHINED pagina/page 36

2185000 IMPELLER/S FORGED STEEL : BCL \ EDM pagina/page 37

2205000 SHAFT FORGED STEEL CC pagina/page 38

2215000 COMPRESSOR ROTOR pagina/page 39

2225000 STUD BOLTS (standard configurations ) pagina/page 40

2235000 FORGED STEEL HOUSING FOR TILTING PAD JOURNAL BEARING pagina/page 41

2240000 PLATE STEEL JOURNAL PAD pagina/page 42

2245000 BEARING ASSEMBLY (JOURNAL AND/OR THRUST) pagina/page 43

2250000 DRY GAS SEAL pagina/page 44

2260000 CENTRIFUGAL COMPRESSOR pagina/page 45

5005000 LOAD COUPLINGS (INCLUDING TORQUEMETER) pagina/page 47

5010000 AUXILIARY COUPLING pagina/page 48

5020000 LOAD GEAR pagina/page 49

5025000 GT AUXILIARY GEAR pagina/page 51

5040000 GT AUXILIARY BASEPLATES (INCLUDING OIL TANK) pagina/page 52

5045000 GT MAIN BASEPLATES AND COMPRESSOR BASEPLATES pagina/page 53

5050000 CRITICAL PIPING SERVICE: HYDRAULIC OIL, SEAL GAS (1st AND 2nd CLASSES OF SPEC. FOR LINES) pagina/page 54

5055000 NON CRITICAL PIPING SERVICE: SEAL/FUEL GAS, LUBE OIL, AIR, WATER, ATM. DRAINS&VENTS (3rd AND 4thCLASSES OF SPEC FOR LINES) pagina/page 55

5070000 LV ELECTRIC MOTORS A.C. pagina/page 56

5075000 LV ELECTRIC MOTORS A.C. dedicated to VENTILATION FANS pagina/page 57

5080000 LV ELECTRIC MOTOR D.C. pagina/page 58

TAV/SH 7/8

PAG 7/8


QCP SOM5086579 /4




5090000 VOLUMETRIC PUMPS (HYDR. OIL MAIN, RATCHET OIL, LUBE OIL MAIN) pagina/page 59

5100000 CENTRIFUGAL PUMPS (LUBE OIL AUX, LUBE OIL EMERGENCY, HYDR. OIL AUX) pagina/page 60

5110000 ACOUSTIC ENCLOSURE pagina/page 61

5120000 SEAL GAS FILTER (DESIGN ANSI B16.34) AND N2 FILTERS pagina/page 62

5180000 PRESSURE VESSEL, DIAM>150 MM. AND P>103 KPA pagina/page 63

5182000 OIL ACCUMULATOR pagina/page 64

5200000 AIR COOLER pagina/page 65

5215000 FILTER HOUSE pagina/page 67

5220000 INLET DUCT pagina/page 68

5225000 EXHAUST DUCT pagina/page 69

5230000 VENTILATION DUCTS pagina/page 70

5235000 SUPPORTING STRUCTURE pagina/page 71

5236000 WALKWAY AND PLATFORM pagina/page 72

5240000 VENTILATION FANS pagina/page 73

5245000 ELECTRIC HEATER pagina/page 74

5255000 CONTROL VALVES (ON AUXILIARY SYSTEMS) pagina/page 75

5257000 HOT GAS BY-PASS pagina/page 76

5260000 SAFETY VALVES pagina/page 77

5265000 ANTISURGE VALVE pagina/page 78

5270000 UNIT CONTROL SYSTEM pagina/page 79

5275000 MASTER CONTROLLER PANEL pagina/page 80

5285000 FIRE FIGHTING CO2 SKID pagina/page 81

TAV/SH 8/9

PAG 8/9

Revision No: 1Revision No: 1Revision No: 1Revision No: 1Revision No: 1Revision No: 1Revision No: 1


QCP SOM5086579 /4




5290000 MINERAL OIL VAPOUR SEPARATOR SKIDS pagina/page 82

5310000 FUEL GAS SKID pagina/page 83

5330000 COMMON OIL CONSOLE (INTEGRATED ON GT AUX. BASEPLATE) pagina/page 84

5792000 SEAL GAS PANEL pagina/page 85

6055000 ELECTRIC STARTING MOTOR (M.V./H.V.) pagina/page 86

6075000 BATTERY CHARGER, D.C. PANELS pagina/page 87

6090000 STATIONARY NICKEL CADMIUM BATTERIES pagina/page 88

7010000 ASSEMBLED MACHINES SKID pagina/page 89

7020000 EEX CERTIFICATION pagina/page 90

9005000 COMPLETE STRING TEST pagina/page 91

TAV/SH 9/10

PAG 9/10



QCP SOM5086579 /4




Job Notes

1.THIS DOCUMENT IS VALID FOR THE CONTRACTUAL JOB AS SHOWN ON 1st SHEET OF PRESENT QUALITY CONTROL PLAN. THIS QCP IS INACCORDANCE TO PURCHASE REQUISITION ELM-PUL-MJ-REQ-0053 Rev. 2B. <4>

QCP SUB-SUPPLIER REFERENCE NUMBERS ARE: <4>ELM-195-0001-MR-Q05-0001 FOR LOAD GEAR BOXELM-195-0001-MR-Q06-0001 FOR AIR COOLERELM-195-0001-MR-Q07-0001 FOR ANTI SURGE VALVESELM-195-0001-MR-Q08-0001 FOR FILTER HOUSEELM-195-0001-MR-Q09-0001 FOR FUEL GAS SKIDELM-195-0001-MR-Q10-0001 FOR SEAL GAS PANEL

2. ALL DOCUMENTATIONS SHALL BE IN ENGLISH LANGUAGE. ARH DOSSIERS SHALL BE IN ENGLISH AND FRENCH LANGUAGE. PLEASE REFER TOSOM5459916.

3. THE DOCUMENTATIONS SHALL USE THE UNIT OF MEASUREMENT OF S.I. (INTERNATIONAL SYSTEM).

4. OBSERVED OR WITNESS TESTS SHALL HAVE FOLLOWING ADVANCE NOTIFICATION TIME:

For OBSERVED Tests: 14 CALENDAR DAYS IN ADVANCE (*)

For WITNESSED Tests: 14 CALENDAR DAYS IN ADVANCE (*)

(*) ONLY FOR ITEMS SUBJECT TO ARH, ACCORDING TO SOM5459916: 35 CALENDAR DAYS IN ADVANCE FOR PRELIMINARY NOTICE, 21 DAYS INADVANCE FOR FINAL NOTICE. (1)

5.OIL & GAS NUOVO PIGNONE IS A BUSINESS OF GENERAL ELECTRIC; CONSEQUENTLY INSPECTIONS AND TESTS HELD BY GE ARE VALID ALSO FOROIL & GAS.THE ACTION INDICATED IN COLUMN FOR O&G ACTIVITY, IS EQUIVALENT IF PERFORMED BY PERSONNEL CHARGED BY OIL & GAS QUALITY CONTROLDEPT. OR IF PERFORMED BY QUALITY CONTROL DEPTS OF ANY OTHER GE BRANCH.6. ELECTRICAL COMPONENTS ATEX.

ALL ELECTRICAL COMPONENTS THAT ARE TO BE PLACED ON POTENTIALLY EXPLOSIVE ATMOSPHERES SHALL BE SUMMARIZES ON THE ATEXCERTIFICATE LISTS.EACH ATEX ELECTRICAL COMPONENT IN SCOPE OF SUPPLY SHALL BE PROVIDED WITH THE FOLLOWING DOCUMENTATION ACCORDING TO 94/9/EC (AS APPLICABLE ):

TAV/SH 10/11

PAG 10/11


QCP SOM5086579 /4




-MFR DECLARATION OF CONFORMITY FOR ALL INSTRUMENTS DECLARED AS “SIMPLE APPARATUS” ACCORDING TO EN 60079-11-MFR DECLARATION OF CONFORMITY OR ATEX CERTIFICATE FOR ALL COMPONENTS WITH ELEC. EXEC.”EEX-N”-ATEX CERTIFICATE FOR ALL COMPONENTS WITH ELEC. EXEC.”EEx-ia/EEx-ib/EEx-e/EEx-m”

7. SUPPLIER’S DEDICATED P.I.M. WILL BE CARRIED OUT FOR FOLLOWING ITEMS: (1)LOAD GEARBOX;SEAL GAS PANEL;OIL VAPOUR SEPARATOR;OIL VAPOUR SEPARATOR SKID;FILTERS HOUSE;UNIT CONTROL PANEL;FUEL GAS SCRUBBER SKID;AIR COOLER;VENTILATION FAN;AUXILIARIES SKID;FIRE FIGHTING SKID;

P.I.M. SHALL BE NOTIFIED 14 CALENDAR DAYS IN ADVANCE (1)

8. A LIST OF CORRESPONDANCE BETWEEN NP JOB NUMBER AND TRAINS ITEM TAG NUMBER FOLLOWS: (1)TURBOCOMPRESSOR TRAIN ITEM TAG NO. X01-2701 CORRESPONDS TO NP JOB NO. 1800020 AND 1102487;TURBOCOMPRESSOR TRAIN ITEM TAG NO. X02-2701 CORRESPONDS TO NP JOB NO. 1800021 AND 11024882991491 IS THE NP JOB REFERENCE NUMBER FOR ALL STRING TEST ACTIVITIES. <4>

9. COMPLETENESS INSPECTION IS REQUIRED FOR FOLLOWING ITEMS NOT DETAILED ON THIS QCP:-ANCHOR BOLTS-SPECIAL TOOLS(ALSO FOR THESE ITEMS, AN OFFICIAL INSPECTION NOTIFICATION LETTER WILL BE SEND BY NP TO PETROFAC) <4>

10. BUILT PROGRESS REVIEW (@ 60%, 90% STAGES) IS REQUIRED FOR: <4>- MACHINES SKIDS- GT AUXILIARY SKID

TAV/SH 11/12

PAG 11/12


QCP SOM5086579 /4




- LOAD GEAR BOX- AIR COOLER- ANTI SURGE VALVES- FILTER HOUSE- FUEL GAS SKID- SEAL GAS PANEL

11. ALSO INTERMEDIATE INSPECTION FOR EQUIPMENT ASSEMBLED INTO NP SHOP CAN BE SUBJECT TO CUSTOMER PRESENCE <1>, <4>

TAV/SH 12/13

PAG 12/13


QCP SOM5086579 /4




Abbrevation Notes

DWG = DRAWING

MAT = MATERIAL

EDM = ELECTRO DISCHARGE MACHINING <4>

PWHT = POST WELDING HEAT TREATMENT

PT = PENETRANT TEST

VT = VISUAL TEST

RT = RADIOGRAPHIC TEST

MT = MAGNETIC PARTICLE TEST

UT = ULTRASONIC TEST

MFR = MANUFACTURER

STD = STANDARD

NO STD= NON STANDARD

CS = CARBON STEEL

SS = STAINLESS STEEL

LAS = LOW ALLOY STEEL

MRT = MECHANICAL RUNNING TEST

PRACT = PRACTICE

SPEC = SPECIFICATION

CU (CUSTOMER) = PETROFAC <4>

EU (END USER) = SONATRACH/ANADARCO (ASSOCIATION) -SAA <4>

TP (THIRD PARTY) = ARH AUTHORITY <4>

TAV/SH 13/14

PAG 13/14


QCP SOM5086579 /4

LEGEND:O&G : GE OIL & GAS R : CERTIFICATION REVIEW

CU : CUSTOMER O : OPTIONAL OBSERVED POINT Std/Non-Std: Blank field means "Std.Test". Field marked with Non-Std means

TP : THIRD PARTY W : WITNESS POINT that test is outside GE OIL & GAS Maximum Case

EU : END USER A : APPROVAL

REVISED WHERE SHOWN 6ITEM LANG. ANuovoPignone

FirenzeN. SOM5086579 /4 DESCRIPTION REV. DESCRIPTION REV.


ACTIVITYN. DESCRIPTION REF. DOC. PROCEDURE ACCEPTANCE Cert.Type

O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1005000 INLET PLENUM [GT] 0

1005200 RAW [MATERIAL: CS ASTM A529 Gr 42.50] 1

1005202 LADLE ANALYSIS (FOR MAIN COMPONENT ONLY)ITN02199.01 /

SOK0929020MAT STD MAT STD 3.1 R R Non-Std 1

1005204 MECHANICAL PROPERTIES (FOR MAIN COMPONENT ONLY)ITN02199.01 /


1005400 MACHINED 0

1005404 INSPECTION OF WELDS ITN02199.01 ITN03402.03 LEV.D

ITN03402.03, ASME

VIII DIV1 ART.UW

52, ASME VIII DIV1

APP.12

3.1 O R 5002 0

1005406 FINAL, VISUAL AND DIMENSIONAL CHECK ITN02199.01COMMON

PRACTICEDRAWING 2.1 O R 0

1005408 PAINTING CHECK ITN02199.01 ITN07791 ITN07791 3.1 R R Non-Std 1

1005410 CLEANLINESS CHECK ITN02199.01COMMON

PRACTICEITN02199.01 2.1 R R Non-Std 6

TAV/SH 14/15

PAG 14/15


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1010000 EXHAUST PLENUM [GT: MS5002C] 0

1010200 RAW [MATERIAL: EXTERNAL STRUCTURES: CS (C25), INTERNAL PANELS: FERRITIC CR. SS (ASTM A 666 TP 304)] 3

1010202 LADLE ANALYSIS (FOR MAIN COMPONENT ONLY)ITN02199.02 /


1010204 MECHANICAL PROPERTIES (FOR MAIN COMPONENT ONLY)ITN02199.02 /


1010400 MACHINED 0

1010402 INSPECTION OF WELDS ITN02199.02 ITN03402.03 LEV.D

ITN03402.03, ASME

VIII DIV1 ART.UW

52, ASME VIII DIV1

APP.12

3.1 O R 5002 0

1010406 FINAL, VISUAL AND DIMENSIONAL CHECK DRAWINGCOMMON

PRACTICEDRAWING 3.1 O R Non-Std 1

1010408 PAINTING CHECK ITN02199.02 ITN07791 ITN07791 3.1 R R Non-Std 1

1010410 CLEANLINESS CHECK ITN02199.02COMMON

PRACTICEITN02199.02 2.1 R R Non-Std 6

TAV/SH 15/16

PAG 15/16



QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1035000 INLET CASING [GT: MS5002C] 0

1035200 RAW [MATERIAL: B50A684 (ASTM A395) or ASTM A278 Cl.30] 0

1035202 LADLE ANALYSISB50A684 or A278

Cl.30 / SOK0929020ASTM STD

B50A684 or A278

Cl.303.1 R R Non-Std 5008 1

1035204 MECHANICAL PROPERTIESB50A684 or A278

Cl.30 / SOK0929020ASTM STD

B50A684 or A278

Cl.303.1 R R Non-Std 5009 1

1035206 MAGNETIC PARTICLE TEST P29A-AG355 ASTM E709 P14A-AL-0205 3.1 R R 5007 0

TAV/SH 16/17

PAG 16/17

Revision No: 1Revision No: 1Revision No: 1Revision No: 1Revision No: 1


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1060000 AXIAL COMPRESSOR CASING [GT: MS5002C] 0

1060200 RAW [MATERIAL: B2A1B3 (ASTM A48)] 0

1060202 LADLE ANALYSIS B2A1 / SOK0929020 ASTM STD B2A1B3 3.1 R R Non-Std 5005 1

1060204 MECHANICAL PROPERTIES B2A1 / SOK0929020 ASTM STD B2A1B3 3.1 R R Non-Std 5004 1


TAV/SH 17/18

PAG 17/18

Revision No: 1Revision No: 1


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1080000 AXIAL COMPRESSOR DISCHARGE CASING [GT: MS5002C] 0

1080200 RAW [MATERIAL: B2A8D3 (ASTM A536 Gr.60-40-15)] 0

1080202 LADLE ANALYSIS B2A8 / SOK0929020 ASTM STD B2A8D3 3.1 R R Non-Std 5008 1

1080204 MECANICAL PROPERTIES B2A8 / SOK0929020 ASTM STD B2A8D3 3.1 R R Non-Std 5009 1


TAV/SH 18/19

PAG 18/19


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1120000 TURBINE CASING [GT: MS5002C] 0

1120200 RAW [MATERIAL: B50A684 (ASTM A395)] 0

1120202 LADLE ANALYSISB50A684 /

SOK0929020ASTM STD B50A684 3.1 R R Non-Std 5008 1

1120204 MECHANICAL PROPERTIESB50A684 /



TAV/SH 19/20

PAG 19/20


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1215000 TURBINE EXHAUST CASING (CASTING PART) [GT: MS5002C] 0

1215200 RAW [MATERIAL: B50A684 (ASTM A395)] 0





1215206 MAGNETIC PARTICLE TESTP29A-AG163 /

SOK0929020ASTM E709 P14A-AL-0205 3.1 R R Non-Std 5007 1

1215400 MACHINED 0

1215404 UT ON LIFTING LUGS P29A-AG163 P3C-AL-0054 P29A-AG163 3.1 R R Non-Std 3

1215406 NDE ON CASING SHELL P29A-AG163 P3C-AL-0054 P29A-AG163 3.1 R R Non-Std 4

1215408 DIMENSIONAL CHECK DRAWINGCOMMON

PRACTICEP14A-AL-0205 3.1 R R 0

TAV/SH 20/21

PAG 20/21


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1220000 TURBINE EXHAUST CASING (FABRICATED PART) [GT: MS5002C] 0

1220200 RAW [MATERIAL: ASTM A516 Gr.60] 0

1220202 LADLE ANALYSIS DWG / SOK0929020 ASTM STD ASTM STD 3.1 R R Non-Std 1

1220204 MECHANICAL PROPERTIES DWG / SOK0929020 ASTM STD ASTM STD 3.1 R R Non-Std 1

1220400 MACHINED 0

1220404 MT OR PT ON WELDS DWG P8A-AG1 P8A-AG1 3.1 R R5011,

50160

1220406 DIMENSIONAL CHECK DRAWINGCOMMON

PRACTICEDRAWING 3.1 R R 0

TAV/SH 21/22

PAG 21/22


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1260000 COMBUSTION CHAMBER CASING [GT: MS5002C] 0

1260200 RAW [MATERIAL: ASTM A516 Gr.60] 0

1260202 LADLE ANALYSIS SOK0929020 ASTM STD A516 Gr.60 3.1 R R Non-Std 1

1260204 MECHANICAL PROPERTIES SOK0929020 ASTM STD A516 Gr.60 3.1 R R Non-Std 1

1260400 MACHINED 0

1260402 MAGNETIC PARTICLE TEST ON WELDS DWG ASME V ART.7 P8A-AG1 3.1 R R Non-Std 5011 1

TAV/SH 22/23

PAG 22/23


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1270000 COMBUSTION CHAMBER CAP & LINER [GT: MS5002C] 0

1270200 RAW [MATERIAL: B50A436C (HASTELLOY X)] 0


SOK0929020ASTM STD B50A436C 2.1 R R Non-Std 5012 1



1270400 MACHINED 0

1270402 FLUORESCENT DYE PENETRANT TEST ON WELDS DWG P3A-AG4 P8A-AG1 2.1 R R 5016 0

TAV/SH 23/24

PAG 23/24


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1330000 TRANSITION PIECE [GT: MS5002C] 0

1330200 RAW [MATERIAL: B50A436C (HASTELLOY X)] 0





1330600 MACHINED 0

1330602 FLUORESCENT DYE PENETRANT TEST ON WELDS DWG P3A-AG4 P8A-AG1 2.1 R R 5016 0

1330604 FINAL VISUAL AND DIMENSIONAL CHECK DRAWINGCOMMON

PRACTICEDRAWING 3.1 R R Non-Std 0

TAV/SH 24/25

PAG 24/25


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1420000 N.2-3 BEARING SUPPORT [GT: MS5002C] 0

1420200 RAW [MATERIAL: B2M1C] 0

1420202 LADLE ANALYSISB2M1 /

SOK0929020ASTM STD B2M1C 3.1 R R Non-Std 5022 1

1420204 MECHANICAL PROPERTIESB2M1 /



TAV/SH 25/26

PAG 25/26


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1440000 N.4 BEARING SUPPORT [GT: MS5002C] 0

1440200 RAW [MATERIAL: B2M1C] 0

1440202 LADLE ANALYSISB2M1 /


1440204 MECHANICAL PROPERTIESB2M1 /



TAV/SH 26/27

PAG 26/27


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1655000 HIGH PRESSURE ROTOR [GT: MS5002C] 0

1655200 ASSEMBLED 0

1655202 BALANCING CHECK (LOW SPEED)SOM15479,

SOM15647

SOM15479,

SOM15647

SOM15479,

SOM156473.1 O O R Non-Std 5090 1

1655204 TOTAL RUN OUT CHECK DWG DWGITN02183,

SOM266983.1 O O R Non-Std 5132 1

TAV/SH 27/28

PAG 27/28


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1680000 LOW PRESSURE ROTOR [GT: MS5002C] 0

1680200 ASSEMBLED 0

1680202 BALANCING CHECK (LOW SPEED) SOM15648 SOM15648 SOM15648 3.1 O O R Non-Std 5091 1

1680204 TOTAL RUN OUT CHECK DWG DWGITN02183,

SOM266983.1 O O R Non-Std 5132 1

TAV/SH 28/29

PAG 28/29


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

1760000 GAS TURBINE [GT: MS5002C] 0

1760200 ASSEMBLED 0

1760202 NO LOAD MECHANICAL RUNNING TEST (INCLUDING OVERSPEED TEST) JOB SPEC JOB SPEC JOB SPEC 3.1 W W W Non-Std 1

TAV/SH 29/30

PAG 29/30


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2005000 CASING FORGED STEEL: BCL ; NOZZLES FORGED STEEL: BCL [CC] 0

2005200 RAW [MATERIAL: ASTM A350 LF2] 0

2005202 LADLE ANALYSISITN02152.03 /

SOK7352534ASTM STD

ITN02152.03 /

SOK73525343.1 R R Non-Std 5402 4

2005204 MECHANICAL PROPERTIES (INCLUDING IMPACT TEST AT LOW TEMPERATURE AND HARDNESS TEST)ITN02152.03 /

SOK7352534

ASTM STD /

ITN02152.03

ITN02152.03 /

SOK73525343.1 R R Non-Std 5403 4

2005208 MAGNETIC PARTICLE TESTITN02152.03 /

SOK7352534ITN02119

ITN02119 C.2A /

SOK73525343.1 R R Non-Std 4

2005210 ULTRASONIC TESTITN02152.03 /

SOK7352534ITN02151

ITN02151 C.3A /


TAV/SH 30/31

PAG 30/31


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2010000 COVER/S FORGED STEEL (WITHOUT WELDS): BCL [CC] 0

2010200 RAW [MATERIAL: ASTM A350 LF2] 0

2010202 LADLE ANALYSISITN02152.34 / DATA

SHEETASTM STD

ITN02152.34

ITN02152.34 / DATA

SHEET

3.1 R R Non-Std 5473 5

2010204 MECHANICAL PROPERTIES (INCLUDING IMPACT TEST AT LOW TEMPERATURE AND HARDNESS TEST)ITN02152.34 / DATA

SHEET

ASTM STD /

ITN02152.34

ITN02152.34

ITN02152.34 / DATA

SHEET

3.1 R R Non-Std 5474 5

2010208 MAGNETIC PARTICLE TESTITN02152.34 / DATA

SHEETITN02119

ITN02119 C.2A

ITN02152.34 / DATA

SHEET

3.1 O O Non-Std 5

2010210 ULTRASONIC TESTITN02152.34 / DATA

SHEETITN02151

ITN02151 C.3A

ITN02152.34 / DATA

SHEET

3.1 O O Non-Std 5

TAV/SH 31/32

PAG 31/32


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2020000 FABRICATED CASING FOR BCL [CC] 0

2020200 MACHINED / CASING COMPOSITION 0

2020201 PRELIMINARY ARH DOSSIER APPROVALSOM5459916 /

DATA SHEETSOM5459916

SOM5459916 /

DATA SHEET3.2 A A A A Non-Std 5

2020202 HARDNESS CHECK ON WELD JOINTS

ASME VIII / ASME

IX / CUSTOMER

SPEC.

ASME VIII / ASME

IX200 BHN maximum 2.1 R R Non-Std 5

2020203 NOZZLE TO CASING FIT-UP DWG DWG DWG 2.1 O R Non-Std 4

2020204 PWHT TEST RECORDS ASME VIII Div. 1 SOU0113818 ASME VIII Div. 1 3.1 W R Non-Std 4

2020205AFTER PWHT ULTRASONIC TEST ON WELDS:-BOTTOM(IF WELDED)/BODY OF PCL, NOZZLES/BODY OF BCL OR

PCLITN07713.01 ITN07039 ITN07039 3.1 W W Non-Std 5446 4

2020206 AFTER PWHT MAGNETIC PARTICLE TEST ON WELDS ITN07713.01 ITN02119ASME VIII DIV1

APP.63.1 W W Non-Std 4

2020214 DIMENSIONAL CHECK ITN07713.01 STD PROC. MACH. DWG 2.1 W O Non-Std 6

2020216 WPS, PQR, WPQ, AND WELDING MAP ITN07713.01 ASME IX ASME IX 3.1 A R R Non-Std 6

2020400 ASSEMBLED CASING 0

2020401 VISUAL INSPECTION OF COMPLETE FABRICATED CASING MACH. DWG. STD PROC. ARH 2.1 W O Non-Std 1

2020402 HYDRAULIC TEST [60 MINUTES TEST DURATION] SOK7352538ITN07713.01,

ITN07021

API617 (NO

LEAKAGE)3.2 W W W W Non-Std 5

2020403 FINAL ARH DOSSIER SOM5459916 SOM5459916 SOM5459916 3.2 A A A A Non-Std 1

TAV/SH 32/33

PAG 32/33


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2040000 FORGED STEEL COUNTER CASING : BCL [CC] 0

2040200 RAW [MATERIAL: ASTM A 350 LF 2] 0


SHEETMAT STD

ITN02152.06 / DATA

SHEET3.1 R R Non-Std 5466 5

2040204 MECHANICAL PROPERTIES (INCLUDING IMPACT TEST AT LOW TEMPERATURE AND HARDNES TEST)ITN02152.06 / DATA

SHEET

MAT STD /

ITN02152.06

ITN02152.06 / DATA


2040208 ULTRASONIC TESTITN02152.06 / DATA

SHEETITN02151

ITN02151

CLASS.2A / DATA

SHEET

3.1 R R Non-Std 5

TAV/SH 33/34

PAG 33/34


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2100000 DIAPHRAGMS CAST IRON : BCL [CC] 0

2100200 RAW [MATERIAL :ASTM A 278 CL35/CL40C] 0


SHEETASTM STD

ITN02142.01 / DATA

SHEET3.1 R R Non-Std 5

2100204 MECHANICAL PROPERTIES FOR HEAT AND HEAT TREATMENT LOTITN02142.01 / DATA

SHEETASTM STD

ITN02142.01 / DATA


2100208 VISUAL TESTITN02142.01 / DATA

SHEETITN07040

ITN02142.01 / DATA


2100210 MAGNETIC PARTICLE TESTITN02142.01 / DATA

SHEETITN02158

ITN02142.01 / DATA


TAV/SH 34/35

PAG 34/35


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2105000 DIAPHRAGMS FORGED ; BCL [CC] 0

2105200 RAW [MATERIAL : ASTM A350 LF2 , ASTM A 182 F 22] 6


SHEETASTM STD

ITN02152.05 / DATA


2105204 MECHANICAL PROPERTIES FOR HEAT AND H.T.LOTITN02152.05 / DATA

SHEETASTM STD

ITN02152.05 / DATA


2105206 HARDNESS (FOR FORGED)ITN02152.05 / DATA

SHEETBRINNEL STD

ITN02152.05 / DATA


2105208 ULTRASONIC TEST ON 100%ITN02152.05 / DATA

SHEET

ASTM A578-S9 FOR

PLATES; ITN02151

FOR FORGED.

ASTM A578-S9

FOR PLATES;

ITN02151 CL.2A

FOR FORGED. /

DATA SHEET

3.1 R R Non-Std 5

TAV/SH 35/36

PAG 35/36


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2120000 DIAPHRAGMS MACHINED [CC] 0

2120200 MACHINED CAST IRON 0

2120202 VISUAL CHECK ITN07720.01 ITN07040 ITN07040 CL.1 3.1 O R Non-Std 0

2120204 DIMENSIONAL CHECK ITN07720.01COMMON

PRACTICEDWG 3.1 O R Non-Std 3

2120600 MACHINED FORGED 0

2120608 VISUAL CHECK ITN07714COMMON

PRACTICEITN07714 2.1 O R Non-Std 6

2120610 DIMENSIONAL CHECK ITN07714COMMON


TAV/SH 36/37

PAG 36/37


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2185000 IMPELLER/S FORGED STEEL : BCL \ EDM [CC] 0

2185200 RAW [MATERIAL :A 182 F22] 0

2185202 LADLE ANALYSISITN02152.01 /

SOK7352534MAT STD

ITN02152.01 /

SOK73525343.1 R R Non-Std 5418 6

2185208 MECHANICAL PROPERTIESITN02152.01 /

SOK7352534ITN02152.01

ITN02152.01 /


2185210 ULTRASONIC TESTITN02152.01 /

SOK7352534ITN02151

ITN02151 CLASS

1A / SOK73525343.1 R R Non-Std 6

2185400 MACHINED [FOR PMI REQUIREMENT REF. TO SECT. 2-215 OF THIS QCP] 6

2185402 MECHANICAL PROPERTIES (INCLUDING IMPACT TEST AT LOW TEMPERATURE AND HARDNESS TEST)ITN07029 /

SOK7352534SOS9990523

SOS9990517 /

SOK73525343.1 O R Non-Std 6

2185404 DIMENSIONAL AND GEOMETRIC CHECK DWGCOMMON

PRACTICEITN07029 PAR. 12 3.1 O R Non-Std 0

2185408 BALANCING CHECK ITN07029 ITN02177 ITN02177 3.1 W O R Non-Std 1

2185410 OVER SPEED TEST (FOR ALL IMPELLER) ITN07029 ITN07029 ITN07029 3.1 W O O Non-Std 5129 4

2185412 DIMENSIONAL AND GEOMETRIC CHECK DWGCOMMON

PRACTICEITN07029 PAR. 12 3.1 O O R Non-Std 1

2185418 DYE PENETRANT TEST ITN07029 ITN02192 ITN07029 PAR. 12 3.1 W O 5103 0

TAV/SH 37/38

PAG 37/38


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2205000 SHAFT FORGED STEEL CC 0

2205200 RAW [MATERIAL : ASTM A322 TP4340] 0

2205202 LADLE ANALYSIS DATA SHEET ASTM STD

ITN02152.02 /

SOS90233 / DATA

SHEET

3.1 R R Non-Std 5416 5

2205204 MECHANICAL PROPERTIES FOR HEAT AND H.T. LOT DATA SHEET ASTM STD

ITN02152.02 /

SOS90233 / DATA

SHEET

3.1 R R Non-Std 5417 5

2205210 ULTRASONIC TEST DATA SHEET ITN02151

ITN02152.02 /

SOS90233 / DATA

SHEET

3.1 R R Non-Std 5451 5

2205400 MACHINED [FOR PMI REQUIREMENT REF. TO SECT. 2-215 OF THIS QCP] 6

2205412 VISUAL AND DIMENSIONAL CHECK DWGCOMMON


2205417 DIMENSIONAL CHECK OF BEARING JOURNALS AND SEALS DIAMETERS DWG DWG DWG 3.1 O R Non-Std 4

TAV/SH 38/39

PAG 38/39


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2215000 COMPRESSOR ROTOR [CC] 0

2215200 ASSEMBLED 0

2215202 LOW SPEED BALANCING CHECK API 617 ITN02177 API 617 3.1 W O W Non-Std 1

2215204 RUN OUT TEST ITN02183 ITN02183 ITN02183 2.1 W O R Non-Std 5102 1

2215217 POSITIVE MATERIAL IDENTIFICATION SOS2992454 SOS2992454 SOS2992454 3.1 W O Non-Std 5

2215400 ROTOR OVERSPEED TEST 0

2215402 OVERSPEED BALANCING CHECK SOS9990908 SOS9990908 SOS9990908 3.1 W O Non-Std 4

TAV/SH 39/40

PAG 39/40


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2225000 STUD BOLTS (standard configurations ) [CC] 0

2225200 RAW [MATERIAL : SEE ITN 32523] 0

2225202 LADLE ANALYSIS ITN32523 ASTM STD ASTM STD 3.1 R R 0

2225204 MECHANICAL PROPERTIES FOR HEAT AND H.T.LOT ITN32523 ASTM STD ASTM STD 3.1 R R 0

2225208 ULTRASONIC TEST ON STUD BOLTS WITH D>40 MM (on raw bar) ITN31001 ITN02151ITN02151 CLASS

2A2.1 R R 0

2225400 MACHINED 0

2225402 DYE PENETRANT TEST ITN31001 ITN02192 ITN02192 CLASS 0 2.1 R R 5450 0

TAV/SH 40/41

PAG 40/41


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2235000 FORGED STEEL HOUSING FOR TILTING PAD JOURNAL BEARING [CC] 0

2235200 RAW [MATERIAL : 39NICRMO3 EN10083-3] 0

2235202 LADLE ANALYSIS ITN02152.04 MAT STD ITN02152.04 3.1 R R 5419 0

2235400 MACHINED 0

2235402 HARDNESS TEST ITN07711.01 ASTM STD ITN02152.04 3.1 O R Non-Std 5420 0

2235404 DYE PENETRANT TEST ON 100% OF SURFACES ITN07711.01 ITN02192 ITN02192 CLASS 2 3.1 O R Non-Std 0


PRACTICEDWG 3.1 R R Non-Std 0

2235408 CONFORMITY CERTIFICATE ITN07711.01 ITN07711.01 ITN07711.01 2.1 R R 0

TAV/SH 41/42

PAG 41/42


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2240000 PLATE STEEL JOURNAL PAD [CC] 0

2240200 RAW [MATERIAL : C45E EN10083 (CLEAT); C10E EN10083 (SECTOR)] 0

2240202 LADLE ANALYSIS ITN02152.20 MAT STD ITN02152.20 2.1 R R Non-Std 5421 6

2240400 MACHINED 0



TAV/SH 42/43

PAG 42/43


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2245000 BEARING ASSEMBLY (JOURNAL AND/OR THRUST) [CC] 0

2245200 RAW 0

2245202 LADLE ANALYSISASTM STD / DATA

SHEETASTM STD

ASTM STD / DATA


2245204 MECHANICAL PROPERTIESASTM STD / DATA

SHEETASTM STD

ASTM STD / DATA


TAV/SH 43/44

PAG 43/44


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2250000 DRY GAS SEAL [CC] 0

2250200 RAW 0

2250202 LADLE ANALYSISASTM STD /

SOK7352534ASTM STD

ASTM STD /


2250204 MECHANICAL PROPERTIESASTM STD /

SOK7352534ASTM STD

ASTM STD /


2250400 MACHINED 0

2250404 AFTER TEST INTERNALS STRIP DOWN AND VISUAL INSPECTION DGS SPECS DGS SPECS DGS SPECS 2.1 O O O Non-Std 4

2250406 MECHANICAL AND PERFORMANCE TESTS SOS2992251 SOS2992251 SOS2992251 3.1 O O O Non-Std 6

2250410 FINAL, VISUAL AND DIMENSIONAL CHECK DWGCOMMON

PRACTICEDWG 3.1 R R 0

TAV/SH 44/45

PAG 44/45


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2260000 CENTRIFUGAL COMPRESSOR 0

2260200 ASSEMBLED [FOR REMOVAL DEMOSTRATION REFER TO ITEM 7 010 OF THIS QCP] 6

2260202 CLEARANCE CHECK

CLEARANCE

TABLE / DATA

SHEET

COMMON

PRACTICE

CLEARANCE

TABLE / DATA

SHEET

3.1 W W Non-Std 5

2260400MECHANICAL RUNNING TESTS [DRY GAS SEAL STRIP INSPECTION WILL BE DONE AT SUB SUPPLIER SHOP. REFERTO ITEM 2 250 OF THIS QCP]

5

2260402 MECHANICAL RUNNING TEST UNDER VACUUM WITH JOB COUPLING SOS0400090 SOS0400090 SOS0400090 3.1 W W W Non-Std 5

2260403 SHOP VERIFICATION TEST / UNBALANCE RESPONSE VERIFICATION TEST API 617 SOS0400090 SOS0400090 3.1 W W W Non-Std 5

2260800 POST MECHANICAL RUNNING TESTS 5

2260802GAS LEAKAGE TEST WITH NITROGEN, AFTER MECHANICAL RUNNING TEST [The gas leakage test shall be

conducted at the DGS design pressure]API 617 API 617 API 617 3.1 W W W Non-Std 1

TAV/SH 45/46

PAG 45/46


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

2260000/1 CENTRIFUGAL COMPRESSOR 0

2260800 POST MECHANICAL RUNNING TESTS 5

2260806 PERFORMANCE TEST ( ACCORDING TO ASME PTC10 TYPE 2 ) SOS0400090ASME PTC 10 (Type

2)SOS0400090 3.1 W W W Non-Std 6

2260808 BEARINGS INSPECTION AND DGS EXTERNAL INSPECTION (DGS WILL NOT BE DISASSEMBLED) SOS0400090 SOS0400090 SOS0400090 2.1 W W W Non-Std 5

2260813 AFTER TEST DRY GAS SEALS VISUAL INSPECTION AND PACKING [MATERIAL SHIPPED LOOSE TO SITE]SOS9990593 /

SOS9990610

COMMON

PRACTICE

SOS9990593 /

SOS99906102.1 O O Non-Std 6

TAV/SH 46/47

PAG 46/47


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5005000 LOAD COUPLINGS (INCLUDING TORQUEMETER) [GT, CC] 1

5005200 COUPLING, RAW 1

5005202 LADLE ANALYSIS ON MAIN COMPONENTSMAT STD / DATA

SHEETMAT STD

MAT STD / DATA


5005204 MECHANICAL PROPERTIES ON MAIN COMPONENTSMAT STD / DATA

SHEETMAT STD

MAT STD / DATA


5005400 COUPLING, MACHINED 1

5005402 BALANCING CHECK DWG API 671 API 671 3.1 O R R Non-Std 4


PRACTICEDWG 3.1 O O R Non-Std 4

5005500 TORQUEMETER, ASSEMBLED 1

5005501 CALIBRATION STD MFR STD MFR STD MFR 3.1 O O R Non-Std 4

TAV/SH 47/48

PAG 47/48


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5010000 AUXILIARY COUPLING [GT] 0

5010200 RAW 0

5010202 LADLE ANALYSIS ON MAIN COMPONENTSMAT STD / DATA

SHEETMAT STD MAT STD 2.1 R R Non-Std 3

5010204 MECHANICAL PROPERTIES ON MAIN COMPONENTSMAT STD / DATA


5010400 MACHINED 0

5010402 BALANCING CHECK DWG API 671 API 671 3.1 R R 0

TAV/SH 48/49

PAG 48/49


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5020000 LOAD GEAR 0

5020200 RAW [MATERIALS: MFR STD] 0

5020202 LADLE ANALYSIS (FOR MAIN COMPONENT ONLY)MAT STD / DATA

SHEETMAT STD

MAT STD / DATA


5020204 MECHANICAL PROPERTIES (FOR MAIN COMPONENT ONLY)MAT STD / DATA

SHEETMAT STD

MAT STD / DATA


5020400 MACHINED WHEEL AND PINION 0

5020402 HARDNESS TEST ON TOOTHJOB SPEC / DATA

SHEETMFR STD

JOB SPEC./ DATA


5020404 BALANCING CHECK (PINION AND BULL GEAR)API 613 / DATA

SHEETMFR STD

API 613 / DATA

SHEET3.1 R R R Non-Std 5

5020800 ASSEMBLED 0

5020802 TAPE LIFT CONTACT CHECK DWG MFR STD DWG 3.1 R R 0

5020808 MECHANICAL RUNNING TEST (WITH JOB PROBES) API 613 JOB SPEC API 613 3.1 W W W Non-Std 1

5020814 TOOTH MESH CONTACT CHECK [AFTER MRT] API 613COMMON

PRACTICEDWG 3.1 W W W Non-Std 1

5020816 BRG INSPECTION [AFTER MRT] API 613COMMON

PRACTICE

COMMON

PRACTICE2.1 W W W Non-Std 1

5020900 FINAL 1

5020902 PAINTING CHECK DWG / SOM5459890COMMON

PRACTICEDWG 2.1 O O O Non-Std 1

TAV/SH 49/50

PAG 49/50


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5020000/1 LOAD GEAR 0

5020900 FINAL 1

5020903 DIMENSIONAL CHECK DWG / SOM6700012COMMON


5020904 FINAL AND VISUAL CHECK DWG / SOM6700012COMMON


TAV/SH 50/51

PAG 50/51


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5025000 GT AUXILIARY GEAR [GT] 1

5025200 RAW [MATERIALS: MFR STD] 0

5025202 LADLE ANALYSIS (FOR MAIN COMPONENT ONLY)MAT STD / DATA


5025204 MECHANICAL PROPERTIES (FOR MAIN COMPONENT ONLY)MAT STD / DATA


5025400 MACHINED 0

5025402 HARDNESS TEST ON TOOTH MAT STD MAT STD SUP. SPEC. 3.1 R R 0

5025600 ASSEMBLED 0

5025602 MECHANICAL RUNNING TEST MFR STD JOB SPEC MFR STD 3.1 W W Non-Std 4

5025604 TOOTH MESH CONTACT CHECK [AFTER MRT] MFR STDCOMMON

PRACTICEMFR STD 3.1 W W Non-Std 4

5025608 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECKDWG / SUPPL.

CHECK LIST

COMMON

PRACTICEDWG 2.1 O R 0

TAV/SH 51/52

PAG 51/52


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5040000 GT AUXILIARY BASEPLATES (INCLUDING OIL TANK) 1

5040200 RAW [MATERIAL: CARBON STEEL S275JR] 4

5040202 LADLE ANALYSIS ITN07759 MAT STD MAT STD 3.1 R R Non-Std 1

5040204 MECHANICAL PROPERTIES ITN07759 MAT STD MAT STD 2.1 R R 0

5040400 FABRICATED 5

5040402 WELD NDT [INCLUDING MPI ON LIFTING POINTS] ITN07759 ITN03402.03 LIV.D ITN03402.03 3.1 O R Non-Std 5021 5

5040404 LEAK TEST ON THE FABRICATED BASE TANK ITN07759 ITN07036 NO LEAKAGE 3.1 O R 0

5040406 PAINTING CHECK SOM5459890 ITN07791 SOM5459890 3.1 O R Non-Std 1

5040408 FINAL, VISUAL AND DIMENSIONAL CHECK DWG / SCL a27COMMON

PRACTICEDWG 3.1 O O Non-Std 4

TAV/SH 52/53

PAG 52/53


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5045000 GT MAIN BASEPLATES AND COMPRESSOR BASEPLATES 1

5045200 RAW [MATERIAL: CARBON STEEL S275JR] 4

5045202 LADLE ANALYSIS ITN07759 MAT STD MAT STD 3.1 R R Non-Std 1

5045204 MECHANICAL PROPERTIES ITN07759 MAT STD MAT STD 2.1 R R 0

5045400 FBRICATED 5

5045402 WELD NDT [INCLUDING MPI ON LIFTING POINTS] ITN07759 ITN03402.03 LIV.D ITN03402.03 3.1 O R Non-Std 5021 5

5045404 PAINTING CHECK SOM5459890 ITN07791 SOM5459890 3.1 O R Non-Std 1

5045406 FINAL, VISUAL AND DIMENSIONAL CHECK DWG / SCL a27COMMON


TAV/SH 53/54

PAG 53/54


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5050000 CRITICAL PIPING SERVICE: HYDRAULIC OIL, SEAL GAS (1st AND 2nd CLASSES OF SPEC. FOR LINES) 1

5050200 RAW [MATERIAL: CARBON/STAINLESS/LOW TEMPERATURE STEELS] 0

5050202 LADLE ANALYSIS SOK2308544 MAT STD MAT STD 3.1 R R Non-Std 3

5050204 MECHANICAL PROPERTIES SOK2308544 MAT STD MAT STD 3.1 R R Non-Std 3

5050400 MACHINED 0

5050402 WPS, PQR, WPQ, AND WELDING MAP ASME IX ASME IX ASME IX 3.1 A R Non-Std 6

5050404 NDT ON WELDING [(CS, LOW TEMP. CS OR SS)]

ITN03401.01(CS),

ITN03401.02(LOW

TEMP CS),

ITN03401.03(SS)

ASME V; ART.7(CS

OR LOW TEMP

CS) ART.6(SS);

ART.2-22;5;6

ITN03401.01(CS),

ITN 03401.02(LOW

TEMP CS),

ITN03401.03(SS)

3.1 O R

5059,

5960,

5961

0

5050408 HYDRAULIC TEST SOK2308544 ITN07021 NO LEAKAGE 3.1 O O Non-Std 4

5050410 POSITIVE MATERIAL IDENTIFICATION ITN07070.01 ITN07070.01 ITN07070.01 3.1 O O Non-Std 2

5050412 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK DWG; SOM5459890COMMON


TAV/SH 54/55

PAG 54/55


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5055000NON CRITICAL PIPING SERVICE: SEAL/FUEL GAS, LUBE OIL, AIR, WATER, ATM. DRAINS&VENTS (3rd AND 4th CLASSES

OF SPEC FOR LINES)1

5055200 RAW [MATERIAL: CARBON/STAINLESS/LOW TEMPERATURE STEELS] 0

5055202 LADLE ANALYSIS SOK2308544 MAT STD MAT STD 2.1 R R Non-Std 3

5055204 MECHANICAL PROPERTIES SOK2308544 MAT STD MAT STD 2.1 R R Non-Std 3

5055206 NDT ON WELDING [(CS, LOW TEMP. CS OR SS)]

ITN03401.01(CS),

ITN03401.02(LOW

TEMP CS),

ITN03401.03(SS)

ASME V; ART.7(CS

OR LOW TEMP

CS) ART.6(SS);

ART.2-22;5;6

ITN03401.01(CS),

ITN 03401.02(LOW

TEMP CS),

ITN03401.03(SS)

3.1 O R 0

5055207 HYDROTEST (IF APPLICABLE) SOK2308544 SOK2308544 SOK2308544 3.1 R R Non-Std 3

TAV/SH 55/56

PAG 55/56


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5070000 LV ELECTRIC MOTORS A.C. 0

5070200 ASSEMBLED 0

5070201 HIGH POTENTIAL CHECK IEC 60034-1 IEC 60034-1 IEC 60034-1 3.1 R R Non-Std 4

5070204

ROUTINE TEST [THIS INCLUDE: ROTATION CHECK, MEASUREMENT OF NO LOAD RUNNING CURRENT,

MEASUREMENT OF LOCKED ROTOR CURRENT AND TORQUE, WINFING RESISTANCE MEASUREMENT,

VIBRATION CHECK, PERFORMANCE CHECK, AFTER TEST BEARING CHECK]

ITN62110.12 IEC IEC 3.1 O O Non-Std 5062 4

TAV/SH 56/57

PAG 56/57


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5075000 LV ELECTRIC MOTORS A.C. dedicated to VENTILATION FANS 0

5075200 ASSEMBLED 0

5075201 MOTOR CONFORMITY CERTIFICAATE MAT STD MAT STD MAT STD 2.1 R R Non-Std 5

5075202 HIGH POTENTIAL CHECK IEC 60034-1 IEC 60034-1 IEC 60034-1 3.1 R R Non-Std 5

5075204

ROUTINE TEST [THIS INCLUDE: ROTATION CHECK, MEASUREMENT OF NO LOAD RUNNING CURRENT,

MEASUREMENT OF LOCKED ROTOR CURRENT AND TORQUE, WINFING RESISTANCE MEASUREMENT,

VIBRATION CHECK, PERFORMANCE CHECK, AFTER TEST BEARING CHECK]

ITN62110.12 IEC IEC 3.1 O R Non-Std 5062 4

TAV/SH 57/58

PAG 57/58


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5080000 LV ELECTRIC MOTOR D.C. 0

5080200 ASSEMBLED 0

5080202 ROUTINE TEST IEC IEC IEC 3.1 O O Non-Std 5111 4

TAV/SH 58/59

PAG 58/59


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5090000 VOLUMETRIC PUMPS (HYDR. OIL MAIN, RATCHET OIL, LUBE OIL MAIN) 3

5090200 RAW 0

5090202 LADLE ANALYSIS ON MAIN COMPONENTS MAT STD MAT STD MAT STD 2.1 R R 0

5090204 MECHANICAL PROPERTIES ON MAIN COMPONENTS MAT STD MAT STD MAT STD 2.1 R R 0

5090400 MACHINED 0

5090402 HYDRAULIC TEST ON PUMP BODY API 676 MFR STD NO LEAKAGE 3.1 R R 0

5090404 FUNCTIONAL / PERFORMANCE TESTS

API676 / SOM19466

/ RP_05593 /

RP_43660

MFR STD MFR STD 3.1 R R R Non-Std 4

5090406 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK DWG, PAINT SPEC.COMMON

PRACTICEDWG, PAINT SPEC. 3.1 R R 0

TAV/SH 59/60

PAG 59/60


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5100000 CENTRIFUGAL PUMPS (LUBE OIL AUX, LUBE OIL EMERGENCY, HYDR. OIL AUX) 3

5100200 RAW 0

5100202 LADLE ANALYSIS ON MAIN COMPONENTS MAT STD MAT STD MAT STD 2.1 R R 0

5100204 MECHANICAL PROPERTIES ON MAIN COMPONENTS MAT STD MAT STD MAT STD 2.1 R R 0

5100400 MACHINED 0

5100402 HYDRAULIC TEST ON PUMP BODY ISO9906 gr2 MFR STD NO LEAKAGE 3.1 R R 0

5100404 FUNCTIONAL AND PERFORMANCE TESTISO9906 gr2 /

ITN62102MFR STD MFR STD 3.1 R R Non-Std 4

5100406 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK DWG, PAINT SPEC.COMMON

PRACTICEDWG, PAINT SPEC. 3.1 R R 0

TAV/SH 60/61

PAG 60/61


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5110000 ACOUSTIC ENCLOSURE 0

5110200 RAW 0

5110202 LADLE ANALYSIS (FOR MAIN COMPONENT ONLY) MAT STD MAT STD MAT STD 2.1 R R 0

5110204 MECHANICAL PROPERTIES (FOR MAIN COMPONENT ONLY) MAT STD MAT STD MAT STD 2.1 R R 0

5110400 MACHINED ON BASE 0

5110402 STRUCTURE WELDING NDT CONSTR. DWG ITN03402.03 ITN03402.03 LEV-D 2.1 R R 0

5110404 FINAL, VISUAL AND DIMENSIONAL CHECK CONSTR. DWGCOMMON

PRACTICECONSTR. DWG 3.1 W O Non-Std 4

5110406 WPS, PQR, AND WELDING MAP ASME IX ASME IX ASME IX 2.1 A R 0

5110408 PAINTING / GALVANIZING COMPONENTS CHECK CONSTR. DWGITN07791/

SOM5459890

ITN07791/

SOM54598902.1 R R Non-Std 1

TAV/SH 61/62

PAG 61/62


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5120000 SEAL GAS FILTER (DESIGN ANSI B16.34) AND N2 FILTERS 0

5120200 RAW [MATERIAL: STAINLESS STEEL ASTM A 182 F316/316L] 4

5120201 PRELIMINARY ARH DOSSIER APPROVAL SOM5459916 SOM5459916 SOM5459916 3.2 A A A A Non-Std 1

5120202 LADLE ANALYSIS MAT STD MAT STD MAT STD 3.1 R R 0

5120204 MECHANICAL PROPERTIES MAT STD MAT STD MAT STD 3.1 R R 0

5120400 MACHINED 0

5120402 WPS, PQR,WM SPEC/DWG ASME IX ASME IX 3.1 A R Non-Std 6

5120404 PMI ITN07070.01 ITN07070.01 ITN07070.01 3.1 R R Non-Std 3

5120406 HYDRAULIC TEST [60 MINUTES TEST DURATION] SPEC/DWG ASME VIII NO LEAKAGE 3.2 W W W W Non-Std 5

5120407 ULTRASONIC AND MAGNETIC PARTICLE TEST ON WELDS, BUTT JOINT AFTER HYDRAULIC TEST ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 2.1 R R Non-Std 5


PRACTICEDWG 3.1 R R 0


TAV/SH 62/63

PAG 62/63


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5180000 PRESSURE VESSEL, DIAM>150 MM. AND P>103 KPA 1

5180200 RAW [MATERIAL: MATERIAL AISI 316L] 4

5180202 LADLE ANALYSIS MAT STD MAT STD MAT STD 3.1 R R 0

5180204 MECHANICAL PROPERTIES MAT STD MAT STD MAT STD 3.1 R R 0

5180400 MACHINED 0

5180402 RADIOGRAPHIC EXAMINATION ON WELDS ASME VIII DIV1 ASME VIII DIV1ASME VIII DIV 1

ART UW-51, UW-523.1 O R Non-Std 4

5180404 ULTRASONIC TEST ON WELDS [(WHEN RT IS IMPOSSIBLE)] ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 3.1 O R 0

5180406 MAGNETIC PARTICLE TEST ON WELDS BEFORE HYDRAULIC TEST (WHERE APPLICABLE) ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 3.1 O R Non-Std 4

5180408 VISUAL CHECK ON WELDS ASME VIII DIV1COMMON

PRACTICEASME VIII DIV1 2.1 O R Non-Std 0

5180412 PNEUMATIC TEST ON REINFORCED PAD ONLY ASME VIII DIV1COMMON

PRACTICEASME VIII DIV1 3.1 O R 0

5180414 POSITIVE MATERIAL IDENTIFICATION ITN07070.01 ITN07070.01 ITN07070.01 3.1 O O Non-Std 2

5180418 FINAL, VISUAL AND DIMENSIONAL CHECK ASME / DWGCOMMON

PRACTICEASME / DWG 2.1 O R 0

5180420 HYDRAULIC TEST [60 MINUTES TEST DURATION] ASME VIII or DWG ASME VIII or DWG NO LEAKAGE 3.1 O O Non-Std 5


5180422 WPS, PQR, WPQ, AND WELDING MAP ASME IX ASME IX ASME IX 3.1 A R Non-Std 5

TAV/SH 63/64

PAG 63/64


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5182000 OIL ACCUMULATOR 3

5182200 RAW [MATERIAL: SEE DWG COMPONENT] 0

5182201 PRELIMINARY ARH DOSSIER APPROVAL SOM5459916 SOM5459916 SOM5459916 3.2 A R A A Non-Std 1

5182202 LADLE ANALYSIS MAT STD MAT STD MAT STD 3.1 R R Non-Std 0

5182204 MECHANICAL PROPERTIES MAT STD MAT STD MAT STD 3.1 R R Non-Std 0

5182400 MACHINED 0

5182402 RADIOGRAPHIC EXAMINATION ON WELDS ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 3.1 O R Non-Std 0

5182404 ULTRASONIC TEST ON WELDS [(WHEN RT IS IMPOSSIBLE)] ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 3.1 O R Non-Std 0

5182406 MAGNETIC PARTICLE TEST ON WELDS BEFORE HYDRAULIC TEST (WHERE APPLICABLE) ASME VIII DIV1 ASME VIII DIV1 ASME VIII DIV1 3.1 O R Non-Std 4

5182412 PNEUMATIC TEST ON REINFORCED PAD ONLY ASME VIII DIV1COMMON

PRACTICEASME VIII DIV1 3.1 O R Non-Std 0

5182418 FINAL, VISUAL AND DIMENSIONAL CHECKASME / DWG /

SOM6700018

COMMON

PRACTICEASME / DWG 2.1 O R Non-Std 1

5182420 HYDRAULIC TEST [60 MINUTES TEST DURATION] ASME VIII or DWG ASME VIII or DWG NO LEAKAGE 3.2 W W W W Non-Std 5


5182422 WPS, PQR, WPQ, AND WELDING MAP ASME IX ASME IX ASME IX 3.1 A A Non-Std 5


TAV/SH 64/65

PAG 64/65


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5200000 AIR COOLER [IN COMPLIANCE WITH ASME SECT. VIII, DIV. 1] 0

5200200 RAW, MACHINED [MATERIAL: REF. TO FABRICATION DWG] 0

5200202 PRELIMINARY ARH DOSSIER APPROVAL SOM5459916 SOM5459916 SOM5459916 3.2 A A A A Non-Std 1

5200203 LADLE ANALYSIS SPEC/DWG ASME VIII ASTM / DWG 3.1 R R Non-Std 0

5200204 MECHANICAL PROPERTIES SPEC/DWG ASTM ASTM / DWG 3.1 R R 0

5200206 TRANSFER OF MARKING (VT) [INCLUDING PRODUCTION TEST PLATES (IF REQ.D)] SPEC/DWG ASME VIIICOMMON

PRACTICE3.1 R R 0

5200208 CHECK WPS, PQR, WPQ SPEC/DWG ASME IX ASME IX 3.1 A R Non-Std 6

5200212 RT OR UT TEST OF BUTT WELDS SPEC/DWG ASME V ASME VIII 3.1 R R 0

5200214 PT OF FILLET WELDS SPEC/DWG ASME V ASME VIII 3.1 R R 0

5200220 AIR-SOAP TEST OF REINF. PAD SPEC/DWG DWG NO LEAKAGE 3.1 R R 0

5200222 HYDROSTATIC TEST [60 MINUTES TEST DURATION] SPEC/DWG ASME VIII NO LEAKAGE 3.2 W W W W Non-Std 5

5200223 HELIUM LEAK TEST SOG7203337 SOG7203337 NO LEAKAGE 3.1 O R Non-Std 5

5200400 ASSEMBLED 0

5200401 FLUSHING CHECK API614 JOB SPEC JOB SPEC 3.1 O O Non-Std 1

5200402 VISUAL AND DIMENSIONAL SOM6700019/DWGCOMMON

PRACTICEITN02039 3.1 W R Non-Std 1

5200404 PAINTING SOM5459890/DWG SOM5459890 SOM5459890 3.1 R R Non-Std 1

5200406 COMPLETENESS OF MFR. DOSSIER SPEC/DWG ITN04001 ITN04001 2.1 R R Non-Std 5

5200408 PMI ITN07070.01 SOS2992454 SOS2992454 3.1 O O Non-Std 5

TAV/SH 65/66

PAG 65/66


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5200000/1 AIR COOLER [IN COMPLIANCE WITH ASME SECT. VIII, DIV. 1] 0

5200400 ASSEMBLED 0


TAV/SH 66/67

PAG 66/67


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5215000 FILTER HOUSE 0

5215200 RAW 0

5215202 LADLE ANALYSIS (FOR MAIN COMPONENTS ONLY) MAT STD MAT STD MAT STD 2.1 R R 0

5215204 MECHANICAL PROPERTIES (FOR MAIN COMPONENTS ONLY) MAT STD MAT STD MAT STD 2.1 R R 0

5215400 MACHINED [HORIZONTAL FLOW PULSE JET F. H.] 0

5215402 WPS, PQR AND WELDING MAP ASME IX ASME IX ASME IX 3.1 A R Non-Std 5

5215404 NDT ON WELDS SMO9969860 ITN03402.03 ITN03402.03 3.1 R R 0

5215420 PAINTING CHECKSMO9969860 & SCL

015_2SMO9969860 ITN07791 3.1 W R 0

5215422 VISUAL, DIMENSIONAL & CLEANESS CHECKSOM6700016 /

SMO9969860SMO9969860 SMO9969860 3.1 W O Non-Std 3

TAV/SH 67/68

PAG 67/68


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5220000 INLET DUCT 0

5220200 RAW 0



5220600 MACHINED 0




012SMO9970497 ITN07791 3.1 R R 0

5220612 VISUAL, DIMENSIONAL & CLEANESS CHECKSMO9970497 & SCL

012SMO9970497 SMO9970497 3.1 W R 0

TAV/SH 68/69

PAG 68/69


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5225000 EXHAUST DUCT 0

5225200 RAW 0



5225600 MACHINED 0




013SMO9971102 ITN07791 3.1 R R 0

5225612 VISUAL AND DIMENSIONAL CHECKSMO9971102 & SCL

013SMO9971102 SMO9971102 3.1 R R 0

TAV/SH 69/70

PAG 69/70


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5230000 VENTILATION DUCTS 0

5230200 RAW 0

5230202 LADLE ANALYSIS (FOR MAIN COMPONENTS ONLY) ITN02199.03 MAT STD ITN02199.03 2.1 R R 0

5230204 MECHANICAL PROPERTIES (FOR MAIN COMPONENTS ONLY) ITN02199.03 MAT STD ITN02199.03 2.1 R R 0

5230400 MACHINED [PAINTED] 0


5230404 NDT ON WELDS ITN02199.03 ITN03402.03 ITN03402.03 3.1 R R 0

5230410 PAINTING CHECK ITN02199.03 ITN07791 ITN07791 3.1 R R 0

5230412 VISUAL, DIMENSIONAL & CLEANESS CHECK ITN02199.03 ITN02199.03 ITN02199.03 3.1 W R 0

TAV/SH 70/71

PAG 70/71


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5235000 SUPPORTING STRUCTURE 0

5235200 RAW [MAATERIAL: CARBON STEEL S235JR] 4



5235400 MACHINED [FILTER HOUSE] 0


5235408 PAINTING / GALVANIZING COMPONENTS CHECKSMO9969860/ASTM

A123

ITN07791/ASTM

A123

ITN07791/ASTM

A1233.1 R R 0

5235410 VISUAL AND DIMENSIONAL CHECK SMO9969860 SMO9969860 SMO9969860 3.1 O O Non-Std 3

5235800 MACHINED [VENTILATION SYSTEM] 3



5235808 PAINTING / GALVANIZING COMPONENTS CHECKSMO9970453/ASTM

A123

ITN07791/ASTM

A123

ITN07791/ASTM

A1233.1 O O Non-Std 4

5235810 VISUAL AND DIMENSIONAL CHECK SMO9970453 SMO9970453 SMO9970453 3.1 O O Non-Std 3

TAV/SH 71/72

PAG 71/72


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5236000 WALKWAY AND PLATFORM 1

5236100 FINAL TEST 1

5236101SHOP FIT UP [MOST CRITICAL COMPONENTS (bracing to beams and columns) -NOTE: ONLY FOR MACHINE

SUBJECT TO STRING TEST]DWG

COMMON


5236102 PAINTING CHECK DWGCOMMON

PRACTICESOM5459890 3.1 O O Non-Std 3

5236103 FINAL INSPECTION DWGCOMMON


TAV/SH 72/73

PAG 72/73


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5240000 VENTILATION FANS 0

5240200 MACHINED (FAN) 0

5240202 LADLE ANALISYS MFR STD MFR STD MFR STD 2.1 R R 0

5240210 WPS/PQR/WM ASME IX ASME IX ASME IX 3.1 A R Non-Std 5

5240400 ASSEMBLED (FAN + EL.MOTOR) 0

5240402 MECHANICAL RUNNING TEST JOB SPEC MFR STD MFR STD 3.1 O O Non-Std 1

5240410 PAINTING CHECKJOB SPEC & SCL

a17ITN07791 ITN07791 3.1 W O Non-Std 1

5240412 FINAL, VISUAL AND DIMENSIONAL CHECK DWG / SOM6700020COMMON

PRACTICEDWG 3.1 W O Non-Std 1

TAV/SH 73/74

PAG 73/74


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5245000 ELECTRIC HEATER 0

5245200 MACHINED 0

5245202 FUNCTIONAL TEST MFR STD MFR STD MFR STD 3.1 R R 0

5245204 ELECTRICAL CHECKS (insulation, ins. resistance, sealing) MFR STD MFR STD MFR STD 3.1 R R 0

5245206 FINAL, VISUAL AND DIMENSIONAL CHECK MFR STD MFR STD MFR STD 2.1 R R 0

TAV/SH 74/75

PAG 74/75


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5255000 CONTROL VALVES (ON AUXILIARY SYSTEMS) 0

5255200 RAW 0

5255202 LADLE ANALYSIS ITN04204.36 MAT STD MAT STD 3.1 R R 0

5255204MECHANICAL PROPERTIES [THIS INSCLUDES HARDESS CHECK ON CONNECTION FLANGES – WHERE

APPLICABLE]ITN04204.36 MAT STD MAT STD 3.1 R R Non-Std 5

5255205 NON DESTRUCTIVE TESTS JOB SPEC. ASTM STD. MAT. STD. 3.1 R R Non-Std 5

5255400 ASSEMBLED 0

5255402 PNEUMATIC TEST OF SEAT-PLUG SEAL ITN04204.36 ANSI B16.104 ANSI B16.104 3.1 R R 5463 0

5255404 PNEUMATIC TEST OF ACTUATOR SHELL AND DIAPHRAGMS SEAL ITN04204.36 MFR STD NO LEAKAGE 3.1 R R 0

5255406 HYDRAULIC TEST (ON BODY VALVE) [ACC. TO API 598 OR B16.34] ITN04204.36 API STD 6D NO LEAKAGE 3.1 R R Non-Std 4

5255407 PMI ON BODY VALVE JOB SPEC JOB SPEC JOB SPEC 3.1 O O Non-Std 5

5255408OPERATIONAL TEST [THIS INCLUDE: TRAVEL, START UP POINT, HYSTERESIS, OPENING/CLOSING TIME, CHECK

OF LIMIT SWITCHES]ITN04204.36 MFR STD SPEC. VALUES 3.1 R R Non-Std 4

TAV/SH 75/76

PAG 75/76


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5257000 HOT GAS BY-PASS 0

5257200 RAW 0


5257202 LADLE ANALYSIS ITN04204.36 MAT STD MAT STD 3.1 R R Non-Std 0




5257400 MACHINED 0

5257402 PNEUMATIC TEST OF SEAT-PLUG SEAL ITN04204.36 ANSI B16.104 ANSI B16.104 3.1 R R Non-Std 5463 0

5257404 PNEUMATIC TEST OF ACTUATOR SHELL AND DIAPHRAGMS SEAL ITN04204.36 MFR STD NO LEAKAGE 3.1 R R Non-Std 0

5257406 HYDRAULIC TEST (ON BODY VALVE) [ACC. TO API 598 OR B16.34] ITN04204.36 API STD 6D NO LEAKAGE 3.2 W W W W Non-Std 4

5257407 PMI ON BODY VALVE SOS2992454 SOS2992454 SOS2992454 3.1 O O Non-Std 5

5257408OPERATIONAL TEST [THIS INCLUDE: TRAVEL, START UP POINT, HYSTERESIS, OPENING/CLOSING TIME, CHECK

OF LIMIT SWITCHES]ITN04204.36 MFR STD SPEC. VALUES 3.1 O O Non-Std 4

5257410 FINAL ARH DOSSIER SOM5459916 SOM5459916 SOM5459916 3.2 A R A A Non-Std 1

TAV/SH 76/77

PAG 76/77


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5260000 SAFETY VALVES 0

5260200 RAW 0


5260202 LADLE ANALYSIS ITN04204.37 MAT STD MAT STD 3.1 R R 0


APPLICABLE]ITN04204.37 MAT STD MAT STD 3.1 R R 0


5260400 1

5260406 4

5260408 4

5260410 5

5260412 1

TAV/SH 77/78

PAG 77/78


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5265000 ANTISURGE VALVE 0

5265200 ASSEMBLED 0


5265202 LADLE ANALYSIS ITN04204.36 MAT STD MAT STD 3.1 R R Non-Std 5



5265206 NON DESTRUCTIVE TESTS JOB SPEC MAT STD JOB SPEC 3.1 R R Non-Std 5

5265208 PMI ON BODY VALVE SOS2992454 SOS2992454 SOS2992454 3.1 R R Non-Std 5

5265210 HYDRAULIC TEST [ON BODY VALVES ACC. TO API 598 OR B16.34] ITN04204.36COMMON

PRACTICENO LEAKAGE 3.2 W W W W Non-Std 4

5265211 MINIMUM CLOSING SEAT LEAKAGE VERIFICATION ANSI CLASS V ANSI CLASS V ANSI CLASS V 3.1 O O Non-Std 4

5265212 DYNAMIC TEST [verification of valve dynamic responses]ITN04204.36 / job

dwg

COMMON

PRACTICEJOB SPEC/DOC 3.1 O O O Non-Std 4

5265214 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECKDWG / Suppl. Check

List

COMMON


5265216 FINAL ARH DOSSIER SOM5459916 SOM5459916 SOM5459916 3.2 A R A A Non-Std 1

TAV/SH 78/79

PAG 78/79


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5270000 UNIT CONTROL SYSTEM 0

5270200 ASSEMBLED 0

5270202 ELECTRIC INSPECTION AND 100% I/O LOOP CHECK [point to point check, load check, switch on/off, power supply, etc] ITN04240 JOB SPEC/DWG JOB SPEC/DWG 3.1 W O O Non-Std 6

5270204 FUNCTIONAL TEST (ON JOB FUNCTIONS ONLY) [I/O check (100%), main start/stop/aux. Sequences]ITN04240 /

SOM6700017SOM6702546 SOM6702546 3.1 W O W Non-Std 6

5270206 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK [INCLUDING TERMINAL BOARD CHECK]ITN04240 /

SOM6700017

COMMON

PRACTICESOM6700017/DWG 2.1 W O Non-Std 6

5270207REDUNDANT MODBUS AND OPC COMMUNICATION LINK TESTING WITH ICSS TEST KIT [TO BE DONE DURING

UCS FAT]JOB SPEC/DOC JOB SPEC/DOC JOB SPEC/DOC 2.1 W W W Non-Std 4

5270208UCS SUBSYSTEMS TEST [To be done during UCS FAT. Check of communication between UCS subsystems (e.g.

BentlyNevada, CCC)]ITN04240 JOB SPEC/DOC JOB SPEC/DOC 2.1 W W W Non-Std 6

5270214 INTEGRATION TEST OF UCS AT ICSS SHOPCUSTOMER/DCS

VENDOR SPEC

CUSTOMER/DCS

VENDOR SPEC

CUSTOMER/DCS

VENDOR SPEC3.1 W W W Non-Std 6

5270220 HEAT SOAK TEST JOB SPEC/DOC JOB SPEC/DOC JOB SPEC/DOC 2.1 R R Non-Std 3

5270243

INTEGRATION TEST BETWEEN CCC and MASTER CONTROLLER [INTEGRATION TEST BETWEEN ACP2 SECTION

OF UCS (CCC RACS), MASTER CONTROLLER PANEL AND REMOTE TRAINVIEW. This include complete Functional

and Communication tests between the CCC Controllers, Remote TrainWiew Server and Client PC Workstations]

JOB SPEC/DOC JOB SPEC/DOC JOB SPEC/DOC 3.1 W W W Non-Std 6

TAV/SH 79/80

PAG 79/80


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

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5275000 MASTER CONTROLLER PANEL 2

5275200 ASSEMBLED 0

5275202 ELECTRIC INSPECTION AND I/O LOOP CHECK [100% point to point check, load check, switch on/off, power supply, etc] ITN04240 JOB SPEC/DWG JOB SPEC/DWG 3.1 O O O Non-Std 4

5275204 FUNCTIONAL TEST (ON JOB FUNCTIONS ONLY) [I/O check (100%), main start/stop/aux. Sequences] ITN04240 JOB SPEC/DOC JOB SPEC/DOC 3.1 O O O Non-Std 4

5275206 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK [INCLUDING TERMINAL BOARD CHECK]ITN04240 / Suppl.

Check List

COMMON

PRACTICEJOB SPEC/DWG 2.1 O O 0

TAV/SH 80/81

PAG 80/81


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5285000 FIRE FIGHTING CO2 SKID 0

5285200 RAW 0

5285203 LADLE ANALYSIS (FOR MAIN COMPONENTS ONLY) ITM65300 MFR STD MFR STD 3.1 R R Non-Std 0

5285204 MECHANICAL PROPERTIES (FOR MAIN COMPONENTS ONLY) ITM65300 MFR STD MFR STD 3.1 R R 0

5285400 ASSEMBLED 0

5285402 WPS, PQR, WM ASME IX ASME IX ASME IX A R Non-Std 1

5285404 HYDRAULIC PIPING TEST ITM65300COMMON

PRACTICENO LEAKAGE 3.2 W W W W Non-Std 1

5285408 FUNCTIONAL TEST [WITHOUT CO2 RELEASE] ITM65300 MFR STD JOB SPEC 3.1 W O 0

5285410 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK

OUTLINE DWG,

PAINTING SPEC.,

SOM6700022

COMMON

PRACTICE

OUTLINE DWG,

PAINTING SPEC.2.1 O O Non-Std 1

TAV/SH 81/82

PAG 81/82


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5290000 MINERAL OIL VAPOUR SEPARATOR SKIDS 1

5290200 RAW 0



5290400 ASSEMBLED 0

5290404 FUNCTIONAL TEST: VIBRATION/NOISE TEST ON MOTOR-FAN GROUPITN40950.00 (min.) ;

ITN40951.00 (synt.)MFR STD

ITN40950.00 (min.) ;

ITN40951.00 (synt.)3.1 O R 0

5290406 PAINTING CHECK DWGCOMMON

PRACTICEDWG 3.1 O R 0

5290408 FINAL, VISUAL AND DIMENSIONAL CHECK DWG / SOM6700015COMMON


TAV/SH 82/83

PAG 82/83


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5310000 FUEL GAS SKID 0

5310200 RAW 3

5310202 LADLE ANALYSIS (FOR MAIN COMPONENTS ONLY) MAT STD MAT STD MAT STD 2.1 R R Non-Std 3

5310204 MECHANICAL PROPERTIES (FOR MAIN COMPONENTS ONLY) MAT STD MAT STD MAT STD 2.1 R R Non-Std 3

5310400 ASSEMBLED 3


PRACTICEDWG 2.1 W R Non-Std 3

TAV/SH 83/84

PAG 83/84


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5330000 COMMON OIL CONSOLE (INTEGRATED ON GT AUX. BASEPLATE) 1

5330200 ASSEMBLED 0

5330204 FUNCTIONAL TEST JOB SPEC. JOB SPEC. JOB SPEC. 3.1 O R 0

5330206 FINAL, VISUAL, PAINTING AND DIMENSIONAL CHECK DWG/SOM6700021 SOM5085321 SOM5085321 3.1 O R Non-Std 5040 1

TAV/SH 84/85

PAG 84/85


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

5792000 SEAL GAS PANEL 0

5792100 RAW 0

5792101 LADLE ANALYSIS MAT STD MAT STD MAT STD 3.1 R R Non-Std 0

5792102 MECHANICAL PROPERTIES MAT STD MAT STD MAT STD 3.1 R R Non-Std 0

5792200 ASSEMBLED 0

5792201 PRESSURE TEST MFR STD MFR STD MFR STD 3.1 R R Non-Std 0

5792202 FINAL VISUAL AND DIMENSIONAL CHECK SOS9973553 SOS9973553 SOS9973553 2.1 R R Non-Std 6

5792204 FUNCTIONAL TEST (DURING STRING TEST) JOB SPEC. JOB SPEC. JOB.SPEC. 2.1 O O Non-Std 1

5792205 CLEANLINESS CHECK API 614COMMON

PRACTICEAPI 614 2.1 O R Non-Std 4

TAV/SH 85/86

PAG 85/86


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

6055000 ELECTRIC STARTING MOTOR (M.V./H.V.) 0

6055400 ASSEMBLED 0

6055401 PRELIMINARY ARH DOSSIER APPROVAL SOM5459916 SOM5459916 SOM5459916 3.2 A R A R Non-Std 1

6055406

ROUTINE TESTS [VISUAL AND DIMENSIONAL CHECK PAINTING CHECK WINDING RESISTANCE AT COLD NO

LOAD CURRENT NO LOAD LOSSES VIBRATION TEST LOCKED ROTOR CURRENT LOCKED ROTOR TORQUE

INSULATION RESISTANCE ON MOTOR WINDINGS BEFORE HEAT RUN (IF ANY) AND DIELECTRIC TEST

DIELECTRIC TEST ON MOTOR WINDINGS AND AUXILIARIES AFTER HEAT RUN (IF ANY) AND DIELECTRIC

TEST POLARIZATION INDEX DIRECTION OF ROTATION AND PHASE MARKING OVERSPEED TEST CHECK OF

AUXILIARIES FINAL CHECK OF JOB DOCUMENTATION]

ITN61511,

SOM6702737 & SCL

025

IEC STD IEC STD 3.1 W W W Non-Std 4

6055600 EXECUTION TYPE 0

6055602 Ex-d EXECUTION CERTIFICATE ITN61511, JOB DOC IEC STD IEC STD 3.1 O R 0


TAV/SH 86/87

PAG 86/87


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

6075000 BATTERY CHARGER, D.C. PANELS 0

6075200 ASSEMBLED 0

6075202

ROUTINE TEST [COMPLIANCE WITH SPECIFICATIONS AND PURCHASE ORDER CHECK PAINTING CHECK

DIMENSIONAL CHECK AND VISUAL INSPECTION FRAME STRUCTURES AND PAINTING CHECK CHECKING OF

EQUIPMENT LIST CHECKING OF THE DEGREE OF PROTECTION NAMEPLATE CHECK STATIC PERFORMANCE

TESTS DYNAMIC PERFORMANCE TESTS RIPPLE MEASUREMENT MECHANICAL OPERATION TEST ELECTRICAL

OPERATION TEST WIRING AND SEQUENCE TEST DIELECTRIC TEST FOR MAIN AND AUX CIRCUITS EXCLUDING

THOSE UTILIZING ELECTRONIC DEVICES INSULATION RESISTANCE MEASUREMENT EXCLUDING THOSE

UTILIZING ELECTRONIC DEVICES CHECK OF CERTIFICATES AND FINAL DOCUMENTATION, INSULATION

RESISTANCE TEST IN ACCORDANCE WITH IEC60146]

ITN62000IEC STD+DWG

WIRING

IEC STD+DWG

WIRING3.1 O R Non-Std 4

6075206 SPECIAL TEST: BURN-IN TEST AT FULL LOAD [On complete system for 48 hours or as agreed in test plan]ITN62000+JOB

SPEC.IEC STD IEC STD 3.1 O R Non-Std 1

TAV/SH 87/88

PAG 87/88


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

6090000 STATIONARY NICKEL CADMIUM BATTERIES 0

6090200 ASSEMBLED 0

6090202FACTORY TEST [VISUAL INSPECTION CAPACITY TEST CHECK OF CERTIFICATES AND FINAL DOCUMENTATION

+ QUANTITATIVE CHCK, DISCHARGE TEST (ONLY ON Nr 1 OR 2 CELLS FILLED)]ITN61506 IEC STD IEC STD 3.1 R R Non-Std 1

TAV/SH 88/89

PAG 88/89


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

7010000 ASSEMBLED MACHINES SKID [CC, GT] 0

7010200 FABRICATED (C/O NP) 0

7010201 DEMOSTRATION OF BUNDLE REMOVAL BEFORE STRING TEST [ON ONE TRAIN ONLY] SOS78180 SOS78180 SOS78180 2.1 W W Non-Std 6

7010202 FINAL, VISUAL AND DIMENSIONAL CHECK DWG SOM5085321 SOM5085321 2.1 W O Non-Std 5040 5

7010204 PAINTING CHECKITN07791/

SOM5459890ITN07791

ITN07791/

SOM54598903.1 W R Non-Std 5

7010208 PREPARATION FOR SHIPMENT ITN54750 ITN54750 ITN54750 2.1 W O Non-Std 5

TAV/SH 89/90

PAG 89/90


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

7020000 EEX CERTIFICATION 0

7020200 ASSEMBLED 0

7020202 EEX CERTIFICATION/ATEX CERTIFICATE LIST JOB SPEC. MFR STD JOB SPEC. 2.1 R R 0

TAV/SH 90/91

PAG 90/91


QCP SOM5086579 /4









O&G CU TP EU

Std/Non-Std

TestEXT. REV.

9005000 COMPLETE STRING TEST 0

9005200 ASSEMBLED 0

9005203 PERFORMENCE TEST PTC10 TYPE 1 [ON 1st TRAIN 1102487] DATA SHEET SOS0400090DATA SHEET/

SOS04000903.1 W W Non-Std 6

9005204 STRING TEST ( FULL SPEED FULL LOAD ) DATA SHEET SOS0400104DATA SHEET /

SOS04001043.1 W W W Non-Std 5

9005206 NOISE TEST [SPL AT 1M DISTANCE FROM SKID EDGE AND 1.5 M ELEVATION ON 1st TRAIN 1102487 - 1800020] DATA SHEET SOS0400104DATA SHEET /

SOS04001043.1 W W W Non-Std 6

9005223 AFTER TEST DRY GAS SEALS VISUAL INSPECTION AND PACKING [MATERIAL SHIPPED LOOSE TO SITE] SOS9990753COMMON

PRACTICESOS9990753 2.1 O O Non-Std 6

TAV/SH 91/92

PAG 91/92


QCP SOM5086579 /4




ITN Details5002 -- TESTS ON CARBON STEEL WELDS ACCORDING TO ITN 03402.03VISUAL EXAMINATION -VISUAL EXAMINATION WILL BE CARRIED OUT ACCORDING TO ASME CODE SECTION V ART.9. -EVALUATION SHALL BE MADEOF THE REGULARITY OF THE SHAPE AND THE SURFACE ASPECT OF THE WELDS AND OF ANY EMERGING DEFECTS (POROSITY-CRACKS) ANDZONES WHOSE APPEARANCE INDICATES THAT INTERNAL DEFECTS MAY BE PRESENT, REQUIRING VERIFICATION THROUGH OTHER TEST METHODS.THE WELDS SHALL BE WELL FILLETED WITH THE ADJACENT BASE MATERIAL. -EACH RUN SHALL PRESENT A SURFACE FREE FROM EMERGINGDEFECTS AND SHALL BE SUFFICIENTLY WELL FILLETED AT THE MARGINS OF THE BEVEL TO ALLOW DEPOSITING OF THE NEXT RUNS WITHOUTTHE DANGER OF LATERAL SLAG. IF THE SURFACE OF A RUN SHOULD BE IRREGULAR AND NOT WELL FILLETED, THE IRREGULARITY SHALL BEREMOVED BY GRINDING. -THE SURFACE OF THE FILLET WELDS SHALL BE EITHER SLIGHTLY CONVEX, FLAT OR SLIGHTLY CONCAVE. CONVEXITYSHALL NOT EXCEED THE VALUE OF 0.1 X 1 OR 0.75 MM, WHERE 1 IS THE DIMENSION OF THE SIDE OF THE BEAD. CONCAVITY SHALL BE SUCH ASNOT TO REDUCE THE DEPTH OF THE GROOVE REQUIRED BY THE DESIGN. -THE MACHINING ALLOWANCE ON BUTT WELDS SHALL NOT EXCEED,ALSO FROM THE BACK WHEN IT CAN BE EXAMINED: -2.5 MM FOR THICKNESSES MAX. 12 MM -3.5 MM FOR THICKNESSES RANGING BETWEEN 12AND 25 MM -4.5 MM FOR THICKNESSES MIN. 25 MM -UNDERSIZING IN THE SIDES OF THE WELDS IS PERMISSIBLE UP TO 1.5 MM FOR A LENGTH LESSTHAN 10% OF THE TOTAL LENGTH OF THE WELD. -THE WELDS SHALL NOT PRESENT OVERLAP ON THE MARGINS. -MARGIN INCISIONS SHALL BEOF LOCAL NATURE, WITH LENGTH NOT EXCEEDING TWICE THE THICKNESS OF THE WELD AND DEPTH NOT EXCEEDING 0.7 MM. IF NECESSARY,THEY SHALL BE FILLETED BY GRINDING. -IF VISUAL EXAMINATION REVEALS THE PRESENCE OF CRACKS, THE ENTIRE LENGTH OF THE WELD SHALLBE SUBJECTED TO MAGNETIC PARTICLE OR LIQUID PENETRANT DYE EXAMINATION AND THE CRACKS SHALL BE REPAIRED. -WHEN EMERGINGDEFECTS (UNACCEPTABLE INCISIONS, POROSITY, WORMHOLES,ETC.) ARE DETECTED, THEY SHALL BE ELIMINATED DOWN TO THE ROOT, ANDTHE EXCAVATION SHALL BE EXAMINED BY LIQUID PENETRANT DYE TEST. THE NECESSARY REPAIR SHALL THEN BE EFFECTED ACCORDING TO ITN03402.03 POINT 11. -DRIPPING AND IRREGULARITY IN WELD LINKS CAN BE ELIMINATED BY GRINDING. RADIOGRAPHIC EXAMINATION -ACCEPTABILITYOF ANY DEFECTS DETECTED WILL BE DECIDED ON THE BASIS OF ASME CODE SECTION VIII DIVISION 1 ARTICLE UW 52. IN CASE ONE OR MOREX-RAYED JOINTS ARE NOT ACCEPTABLE, WE SHALL PROCEED AS FOLLOWS: -REPAIR OF THE SAME JOINT -CHECK EXTENSION ON A DOUBLEQUANTITY OF JOINTS OF THE SAME TYPOLOGY AND WELDER. -IF EVEN ONE OF THESE JOINTS IS CONSIDERED UNACCEPTABLE, THE CHECK IS TOBE EXTENDED TO ALL JOINTS OF THE SAME TYPOLOGY AND WELDER. -THE CHECK RESULTS SHALL BE CERTIFIED SO AS TO INDICATE WELDERSAND JOINTS (IF ANY) TO BE REPAIRED OR DEFECTS JUDGED WITHIN THE LIMITS, IN ADDITION TO THE FINAL RESULT OF THE TEST. ULTRASONICINSPECTION -THE CRITERIA ARE THOSE SPECIFIED BY ASME CODE SECT.VIII DIV.1 APP.12 (CONTAINED IN ITN 07039) -THE TEST REPORTS WILLCONTAIN A JUDGEMENT FOR EACH LENGTH OF WELDING EXAMINED. IN THE CASE OF NON-ACCEPTABILITY, THE DEFECT (OR DEFECTS) TO BEREPAIRED, THEIR NATURE AND ESTIMATED POSITION WITHIN THE WELD SHALL BE CLEARLY SPECIFIED. MAGNETIC PARTICLE EXAMINATION-THE CRITERIA ARE THOSE SPECIFIED BY ASME CODE SECT.VIII DIV.1 APP.6 (CONTAINED IN ITN 02119). -THE TEST REPORTS WILL EXPRESS AJUDGEMENT FOR EACH LENGTH OF WELDING EXAMINED. IN THE CASE OF NON-ACCEPTABILITY, THE DEFECT (OR DEFECTS) TO BE REPAIRED,THEIR NATURE AND ESTIMATED POSITION WITHIN THE WELD SHALL BE CLEARLY SPECIFIED. LIQUID PENETRANT DYE TEST -THE CRITERIA ARETHOSE SPECIFIED BY ASME CODE SECTION VIII DIV.1 APP.8 (CONTAINED IN ITN 02192) -THE TEST REPORTS WILL EXPRESS A JUDGEMENT FOR

TAV/SH 92/93

PAG 92/93


QCP SOM5086579 /4




EACH LENGTH OF WELDING EXAMINED. IN THE CASE OF NON-ACCEPTABILITY,. THE DEFECT (OR DEFECTS) TO BE REPAIRED, THEIR NATURE ANDESTIMATED POSITION WITHIN THE WELD SHALL BE CLEARLY SPECIFIED.

TAV/SH 93/94

PAG 93/94


QCP SOM5086579 /4




ITN Details5004 -- MECHANICAL PROPERTIES ACCORDING TO B2A1B3-TENSILE STRENGTH, MIN.= 30000 PSI (206 MPA) AFTER STRESS RELIEF ANNEAL -BRINELL HARDNESS, MAX.= 225 ON SPECIMENS OF A FLATSURFACE OF THE CASTING WHEN SPECIFICALLY AGREED UPON BY THE CUSTOMER.

TAV/SH 94/95

PAG 94/95


QCP SOM5086579 /4




ITN Details5005 -- LADLE ANALYSIS ACCORDING TO B2A1B3MATERIAL B2A1B3 ACCORDING TO ASTM A48

TAV/SH 95/96

PAG 95/96


QCP SOM5086579 /4




ITN Details5007 -- MAGNETIC PARTICLE TEST ACCORDING TO P14A-AL-0205-WHEN MP/LP INSPECTION IS REQUIRED BY THE DRAWING, PART SPECIFICATION OR PURCHASE ORDER, EACH CASTING SHALL BE SO INSPECTEDIN THE AREAS DESIGNATED AND BY THE PROCEDURE(S) STIPULATED. -LIFTING LUGS AND INTEGRAL STRUT AND FLANGE FILLETS OF ALL SANDCASTING AS WELL AS ANY ADDITIONAL AREAS DESIGNATED ON APPLICABLE PART SPECIFICATIONS SHALL BE MAGNETIC PARTICLE INSPECTEDIN ACCORDANCE WITH ASTM E709 (MAGNETIC MATERIALS) OR LIQUID PENETRANT INSPECTED AS PER ASTM E165 (NON-MAGNETIC MATERIALS).-WHEN DUE TO THE GEOMETRY OF A PARTICULAR AREA, IT IS IMPOSSIBLE TO OBTAIN A MEANINGFUL M.P. TEST, LIQUID PENETRANT INSPECTIONMAY BE SUBSTITUTED WITH PRIOR APPROVAL BY THE PURCHASER BY VRMD (REF. PAR.6.9). A SMOOTH SURFACE IS REQUIRED FOR SUCH ASUBSTITUTION. -UNLESS OTHERWISE NOTED ON THE INDIVIDUAL PART SPECIFICATION, LINEAR MP OR LP INDICATIONS ARE NOT PERMISSIBLE.NON-LINEAR INDICATIONS SHOULD BE EVALUATED TO THE VISUAL EXAMINATION STANDARDS IN 6.4.4 OR 6.4.5.

TAV/SH 96/97

PAG 96/97


QCP SOM5086579 /4




ITN Details5008 -- LADLE ANALYSIS ACCORDING TO B2A8D3MATERIAL B2A8D3 ACCORDING TO ASTM A536

TAV/SH 97/98

PAG 97/98


QCP SOM5086579 /4




ITN Details5009 -- MECHANICAL PROPERTIES ACCORDING TO B2A8D3-TENSILE STRENGTH, MIN.= 60000 PSI (412 MPA) -YIELD POINT, MIN.= 40000 PSI (277 MPA) -ELONGATION, MIN. PERCENTAGE AT 0,2% ON 50 MM.,MIN.=15%

TAV/SH 98/99

PAG 98/99


QCP SOM5086579 /4




ITN Details5011 -- MAGNETIC PARTICLE TEST ON WELDS ACCORDING TO P8A-AG1ALL WELDS SHALL BE SUBJECTED TO MAGNETIC PARTICLE TEST. ACCEPTANCE CRITERIA ARE THE FOLLOWING: A-LINEAR DEFECTS UP TO 0,5 T(WHERE T IS THE THICKNESS OF THE WELD) BUT NOT EXCEEDING 6,35 MM. ARE ACCEPTABLE AS LONG AS THEY ARE NOT VISIBLE CRACKS B-THETOTAL LENGTH OF THE DEFECTS MUST NOT EXCEED THE VALUE OF T FOR EACH LENGTH OF WELDING EQUAL TO 12 T

TAV/SH 99/100

PAG 99/100


QCP SOM5086579 /4




ITN Details5012 -- LADLE ANALYSIS ACCORDING TO B50A436C (HASTELLOY X)C = 0,05-0,10 % S = 0,03 MAX % W = 0.20-1,00 % MN= 1,00 MAX % CR= 20,50-23,00 % FE= 17,00-20,00 % SI= 1,00 MAX % CO= 0,50-2,50 % B = 0,008 MAX %P = 0,04 MAX % MO= 8,00-10,00 % NI= REMAINDER

TAV/SH 100/101

PAG 100/101


QCP SOM5086579 /4




ITN Details5013 -- MECHANICAL PROPERTIES ACCORDING TO B50A436C (HASTELLOY X)- TENSILE STRENGTH, MIN. = 105000 PSI (721 MPA) - YIELD POINT AT 0,2 %,MIN. = 45000 PSI (309 MPA) - ELONGATION ON A LENGTH OF 50 MM OR 4DIAMETERS, MIN. = 35 %

TAV/SH 101/102

PAG 101/102


QCP SOM5086579 /4




ITN Details5016 -- DYE PENETRANT TEST ON WELDS (AS PER P8A-AG1 AND SOM 15127)ALL WELDS SHALL BE SUBJECTED TO LIQUID PENETRANT TEST. ACCEPTANCE CRITERIA ARE THE FOLLOWING: A - CRACKS ARE NOT ACCEPTABLE.B - ISOLATED DEFECTS WITH MAX. DIAMETER LESS THAN 0.76 MM (NOT INTERPRETABLE AS CRACKS) ARE ACCEPTABLE. C - GROUPS OF 3 OR MOREDEFECTS (WITH MAX. LENGTH OF INDIVIDUAL DEFECTS LESS THAN 0.76 MM) ARE NOT ACCEPTABLE IF THE DISTANCE BETWEEN THE INDIVIDUALDEFECTS IS LESS THAN THE MAX. LENGTH OF THE LONGEST OF THEM. GROUPS OF DEFECTS WITH MAX. LENGTH OF INDIVIDUAL DEFECTS LESSTHAN 0.51 MM, NOT INTERPRETABLE AS CRACKS, ARE ACCEPTABLE. D - THE TOTAL LENGTH OF THE DEFECTS CALCULATED ON EACH SECTION OFWELD EQUAL TO 12 TIMES THE THICKNESS SHALL NOT EXCEED THE THICKNESS ITSELF.

TAV/SH 102/103

PAG 102/103


QCP SOM5086579 /4




ITN Details5021 -- NON DESTRUCTIVE TEST ON WELDS (AS ITN 03402.03)1.VISUAL EXAMINATION WILL BE CARRIED OUT ACCORDING TO ASME CODE SEC.V ART.9.2.EVALUTION SHALL BE MADE OF THE REGULARITY OFTHE SHAPE AND THE SURFACE ASPECT OF THE WELDS AND OF ANY EMERGING DEFECTS (POROSITY-CRACKS) AND ZONES WHOSE APPEARANCEINDICATES THAT INTERNAL DEFECTS MAY BE PRESENT, REQUIRING VERIFICATION THROUGH OTHER TEST METHODS. THE WELDS SHALL BEWELL FILLETED WITH THE ADJACENT BASE MATERIAL.3.EACH RUN SHALL PRESENT A SURFACE FREE FROM EMERGING DEFECTS AND SHALL BESUFFICIENTLY WELL FILLETED AT THE MARGINS OF THE BEVEL TO ALLOW DEPOSITING OF THE NEXT RUNS WITHOUT THE DANGER OF LATERALSLAG. IF THE SURFACE OF A RUN SHOULD BE IRREGULAR AND NOT WELL FILLETED, THE IRREGULARITY SHALL BE REMOVED BY GRINDING.4.THESURFACE OF THE FILLET WELDS SHALL BE EITHER SLIGHTLY CONVEX, FLAT OR SLIGHTLY CONCAVE.5.CONVEXITY SHALL NOT EXCEED THEVALUE OF 0.1 X "L" OR 0.75 MM, WHERE "L" IS THE DIMENSION OF THE SIDE OF THE BEAD. CONCAVITY SHALL BE SUCH AS NOT TO REDUCE THEDEPTH OF THE GROOVE REQUIRED BY THE DESIGN.6.THE MACHINING ALLOWANCE ON BUTT WELDS SHALL NOT EXCEED, ALSO FROM THEBACK WHEN IT CAN BE EXAMINED: -2.5 MM FOR THICKNESSES MAX.12 MM -3.5 MM FOR THICKNESSES RANGING BETWEEN 12 AND 25 MM -4.5MM FOR THICKNESSES MIN.25 MM7.UNDERSIZING IN THE SIDES OF THE WELDS IS PERMISSIBLE UP TO 1.5 MM FOR A LENGTH LESS 10% OFTHE TOTAL LENGTH OF THE WELD.8.THE WELDS SHALL NOT PRESENT OVERLAP ON THE MARGINS.9.MARGINS INCISIONS SHALL BE OF LOCALNATURE , WITH LENGTH NOT EXCEEDING TWICE THE THICKNESS OF THE WELD AND DEPTH NOT EXCEEDING 0.7 MM. IF NECESSARY, THEYSHALL BE FILLETED BY GRINDING.10.IF VISUAL EXAMINATION REVEALS THE PRESENCE OF CRACKS, THE ENTIRE LENGTH OF THE WELD SHALLBE SUBJECTED TO MAGNETIC PARTICLE OR LIQUID PENETRANT DYE EXAMINATION AND THE CRACKS SHALL BE REPAIRED.11-WHEN EMERGINGDEFECTS (UNACCEPTABLE INCISIONS, POROSITY, WORMHOLES, ETC.) ARE DETECTED, THEY SHALL BE ELIMINATED DOWN TO THE ROOT, ANDTHE EXCAVATION SHALL BE EXAMINED BY LIQUID PENETRANT DYE TEST.12.DRIPPING AND IRREGULARITY IN WELD LINKS CAN BE ELIMINATEDBY GRINDING.MAGNETIC PARTICLE EXAMINATION1.THE CRITERIA ARE THOSE SPECIFIED BY ASME CODE SECT.VIII DIV.1 APP.6 (CONTAINED IN ITN02119)

TAV/SH 103/104

PAG 103/104


QCP SOM5086579 /4




ITN Details5022 -- LADLE ANALYSIS ACCORDING TO B2M1CC = 0,3 MAX % SI= 0,6 MAX % MN= 0,7 MAX % CU= 0,3 MAX % P = 0,04 MAX % FE= REMAINDER S = 0,04 MAX %

TAV/SH 104/105

PAG 104/105


QCP SOM5086579 /4




ITN Details5023 -- MECHANICAL PROPERTIES ACCORDING TO B2M1C- R MIN.= 65000 PSI (446 MPA) - RS MIN.(1) = 3500 PSI (240 MPA) - A MIN. (50 MM) = 24 % - Z MIN. = 35 % (1) WHERE A DEFINITE YIELD POINT SHALL NOTBE EXHIBITED, THE YIELD STRENGTH CORRESPONDING TO AN OFFSET OF 0,2 % SHALL BE USED INSTEAD

TAV/SH 105/106

PAG 105/106


QCP SOM5086579 /4




ITN Details5040 -- FINAL TEST (AS SOM5085321)

MECHANICAL PARTS 1.1-ALL PIPING COMPLETED DURING THE ASSEMBLY SHOULD BE TESTED IN ACCORDANCE WITH THE JOB LINESPECIFICATIONS. 1.2-BRACKETS AND SUPPORTS SHALL BE SEAM-AND-SEAL-WELDED. CHECK THE INTERNAL CLEANNESS OF TANKS. ?THEINSULATING MATERIAL SHOULD BE PLACED BETWEEN S/STEEL COMPONENTS AND CARBON STEEL COMPONENTS. -CHECK THAT ARE ENOUGHSUPPORTS ADEQUATELY POSITIONED FOR A CORRECT BRACKETING OF PIPING IN ORDER TO GUARANTEE VIBRATION DAMPING, AS PERAPPLICABLE JOB DOCUMENTS. -THE INTERNAL PAINTING OF CARBON STEEL TANKS SHALL BE INSPECTED AND, IF NECESSARY, RESTORED ASPED ITN07737. 1.3- THE RIGHT ROUTE PIPING SHOULD BE VERIFIED THROUGH THE ASSEMBLY DRAWINGS AND JOB LAYOUTS. 1.4- THE CORRECTPOSITION, DIAMETER AND FREEDOM FROM INTERFERENCES OF THE FOUNDATION HOLES SHOULD BE CHECKED. CONNECTIONS ON THE LIMITSOF THE SUPPLY SHALL COMPLY WITH THE INDICATIONS OF THE RELEVANT JOB TABLE. THE POSITION OF SAID CONNECTIONS IN RESPECT TO THEREFERENCE AXES SHALL NOT DEVIATE ± 30mm FROM THE VALUE REPORTED ON THE ASSEMBLY DRAWING (WITH THE EXCEPTION OF SPECIFICREQUESTS BY THE CUSTOMER, WHICH SHALL BE REPORTED ON THE PRA/JOB DRAWINGS) 1.5-VISUAL INSPECTION SHOULD BE CARRIED OUT ONWELDING JOINT, STRUCTURES AND PANEL OF THE ENCLOSURE. ?CHECK ECLOSURE AND PROTECTION OF THE DOORS, THE CORRECT EXECUTIONOF PLUGGING AND CROSSINGS AND CHECK THE ENCLOSURE INTERNAL CLEANNESS. 1.6-ALL PIPING AND/OR COMPONENTS PRODUCTS ORASSEMBLED BEYOND THE BASE OUTER EDGE SHALL BE DISASSEMBLED TO FACILITATE PACKING, IF REQUIRED, TRANSPORT AND RELEVANTPOSITIONING ON THE UTILIZED SYSTEM. 1.7-PAINTED SURFACES SHOULD BE CHECKED ACCORDING TO ITN 07793 PAR.7.2. INSTRUMENT ANDELECTRICAL PARTS 2.1-INSTRUMENTS AND EQUIPMENT SHALL BE INSTALLED FOLLOWING THE INDICATIONS REPORTED ON THE JOB DRAWING ANDITN04202 2.2-CHECK THE CORRECT RUN AND EXECUTION OF PRIMARY AND SECONDARY CONNECTIONS AND ALL ELECTRICAL CONNETIONS, WHICHSHOULD COMPLY WITH THIS SPECIFICATION AND THE JOB DOCUMENTS.(PRIMARY & PNEUMATIC HOOK-UP AND ELECTRIC HOOK-UP) 2.3-SPOTCHECK FOR THE RIGHT WIRING OF INSTRUMENT AND EQUIPMENT TERMINAL BOXES. 2.4-CHECK THE ?CONDUIT? AND CABLE TRAYS CORRECTEXECUTION ALL STAINLESS STEEL TUBING SHALL BE ISOLATED FROM CARBON STEEL SUPPORTS IN ORDER TO AVOID GALVANIC CORROSION. ALLCONDUIT PIPES AND CABLE TRAYS SHALL BE FREE FROM BURRS, CHIPS FLAKES, SPALLING AND ANYTHING THAT MAY HINDER THE PASSAGE OFELECTRIC CABLES. 2.5-CARRY OUT CONTINUITY AND INSULATION TESTS ON ALL ELECTRIC CONNECTIONS AND CARRY OUT A PNEUMATIC TESTON LINES IN TUBING. 2.6-CHECK THAT ALL INSTRUMENTATION AND OTHER EQUIPMENT CARRY AN ID PLATE ACCORDING TO THE P&Id AND THEJOB INSTRUMENTS LIST. FIXING METHOD AND PLATE MATERIAL SHALL COMPLY WITH THE JOB SPECIFICATIONS. 2.7- THE CORRECT EXECUTIONOF GROUND AND ELECTRIC SYSTEMS SHOULD BE CHECKED ACCORDING TO JOB SPECIFICATIONS AND ITN04202 FINAL DOCUMENTATION 3.1 THEFINAL DOCUMENTATION WILL BE SUPPLIED TO THE END OF THE INSPECTION AS PER OPERATIVE INSTRUCTION ATTACHED TO REF. DOCUMENT.FOR PAINTING CONFORMITY CERTIFICATE REF. TO ITN07771 IF APPLICABLE. PUNCH LIST (IF ANY) SHOULD BE PROVIDED IN ACCORDANCE WITH THEJOB REQUIREMENTS.

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ITN Details5059 -- RT OR UT/PT/MT ON WELDING OF CARB. STEEL PIPES ACCORDING TO ITN 03401.011.RADIOGRAPHIC EXAMINATION1.1.THIS EXAMINATION MUST BE PERFORMED IN COMPLIANCE WITH THE SPECIFICATION ITN 02196 TO THEPERCENTAGE DEFINED IN THE FOLLOWING CLASSIFICATION, INDI- CATED ON THE CONSTRUCTION DRAWINGS. IF THE CORNER PIPING AS WELLAS THE CONFIGURATION AND THE DIMENSIONS OF BUTT JOINTS DON'T ALLOW THE EXECUTION OF THE RADIOGRAPHIC EXAMINATION, ANOTHEREXAMINATION IS ALLOWED AS SPECIFIED UNDER POINT 2.1.2.DEFINITION OF THE CHECK CATEGORIES CATEGORY % CHECK FIELD APPLICATIONI 100 AT LEAST FOR ALL THE PIPING WHOSE OPERATING PRESSURE IS HIGHER THAN 151 BARS II 50 AT LEAST FOR ALL THE PIPING WHOSEOPERATING PRESSURE IS INCLUDED BETWEEN 71 AND 150 BARS III 20 PIPING WITH A DIAMETER MIN.8'' AND PRESSURE BETWEEN 13 AND 70BARS 10 PIPING WITH A DIAMETER UP TO 6'' AND PRESSURE BETWEEN 13 AND 70 BARS 5 PIPING WITH DIAMETER MIN.3/4'' AND PRESSURE MAX.12BARS IV ZERO1.3.FOR THE APPLICATION OF THE CATEGORIES II AND III (SPOT CHECK) THE SUPPLIER SHALL ISSUE A CHECK LIST CONSIDERINGTHE PERCENTAGE PROVIDED, THE WELDERS CONCERNED AND THE DIFFERENT JOINT TYPES.1.4.IN CASE OF DETECTION OF DEFECTS WHICHARE NOT ACCEPTABLE THE EXAMINATION EXTENSION SHALL BE CARRIED OUT AS SPECIFIED HERE BELOW ALWAYS IN REGARD TO THEWELDERS AND JOINT TYPES: A)X-RAY INCLUDING ALL THE JOINTS TO BE CHECKED. IT MUST BE PERFORMED IN ZONES NEAR THE DEFECTIVEONE (BEFORE AND AFTER) FOR AN EXTENSION EQUAL TO THREE TIMES THE X-RAYED LENGTH. IF THERE ARE NOT ACCEPTABLE DEFECTS THEPRESENT EXAMINATION MUST BE EXTENDED TO ALL THE WELDING2.ALTERNATIVE CHECKS TO THE RADIOGRAPHIC EXAMINATIONTHEY MUSTBE CARRIED OUT FOR THE CONDITIONS STATED UNDER 1.1. AS A FUNCTIONOF THE JOINT THICKNESS [MM] AS SPECIFIED HERE BELOW:MIN.35ULTRASONIC CHECK IN COMPLIANCE WITH ITN 07039, ACCEPTANCE FOLLOWING ASME SEC. VIII DIV.1BETWEEN 10 AND 15 ULTRASONIC CHECK INCOMPLIANCE WITH ITN 07041, ACCEPTANCE FOLLOWING ASME/ANSI B.31.3MAX.10 DYE PENETRANT EXAMINATION IN COMPLIANCE WITH ITN 02192,ACCEPTANCE FOLLOWING ASME SEC.VIII DIV.1 OR ,ACCORDING TO THE SUPPLIER'S CHOICE: MAGNETIC PARTICLE CHECK IN COMPLIANCE WITHITN 02119, ACCEPTANCE FOLLOWING ASME SEC. VIII DIV.1THE ACCEPTANCE CRITERIA ARE INDICATED IN THE RELEVANT ITN.FOR THE CHECKSDESCRIBED IN THE CATEGORIES II AND III (SPOT CHECK) THE PERCEN-TAGE TO BE APPLIED IS A FUNCTION OF THE JOINT LENGTH FOLLOWINGTHE PROCEDURESDEFINED FOR THE RADIOGRAPHIC EXAMINATIONTHE ACTION TO BE UNDERTAKEN IN CASE OF DETECTION OF NOT ACCEPTABLEDEFECTSSHALL BE THOSE STATED UNDER 1.4.

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ITN Details5062 -- ROUTINE TESTS ON A.C. ELECTRIC MOTOR ACCORDING TO ITN 61502THE FOLLOWING TESTS SHALL BE CARRIED OUT : - COLD WINDING RESISTANCE MEASUREMENT - NO LOAD AND LOCKED ROTOR TEST - INSULATIONRESISTANCE MEASUREMENT OF WINDINGS AND AUXILIARIES - DIELECTRIC TEST ON THE WINDINGS AND AUXILIARIES - VIBRATION TEST - BEARINGINSPECTION

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ITN Details5090 -- BALANCING CHECK ACCORDING TO SOM 15479/15647ACCORDING TO DRAWINGS OF PARTS AND SUBASSEMBLIES OF THE ROTOR AND TO SPECIFICATIONS SOM 15479/S AND SOM 15647/S. BALANCINGIS PERFORMED ON THE INDIVIDUAL COMPONENTS AND/OR SUBASSEMBLIES IN SUCCESSIVE STAGES, WITH A FINAL CHECK OF BALANCING ON THECOMPLETELY ASSEMBLED ROTOR. THE FINAL CHECK OF BALANCING IS THE FOLLOWING: 1. CHECKING DYNAMIC BALANCING ON COMPLETE HIGHPRESSURE ROTOR. AFTER ASSEMBLY OF THE TURBINE BUCKETS AND THE SEAL PLATES, PERFORMED ON THE BASIS OF AN ASSEMBLY CHARTDESIGNED TO MINIMIZE UNBLANCE INDUCED BY THESE COMPONENTS ON THE ROTOR, DYNAMIC BALANCING IS CHECKED ON TWO PLANES. THERESIDUAL UNBALANCE ON EACH PLANE (N.1 AND N.3) SHALL NOT EXCEED 2540 GR.MM. MAXIMUM CORRECTION BALANCE SHALL NOT EXCEED12700 GR.MM. ON PLANE N.1 AND 25400 ON PLANE N.3. 2. NOTE: PRECISION AND REPEATABILITY OF THE BALANCING MACHINE - THE PRECISIONOF THE BALANCING MACHINE CAN BE SUCH THAT A MAXIMUM TOTAL RESIDUAL UNBALANCE OF 2,845 GR.MM. FOR COMPRESSOR ROTOR, ANDCOMPRESSOR ROTOR PLUS COMPRESSOR SHAFT END, AND A MAXIMUM 4,089 GR.MM. FOR THE COMPLETE ROTOR IS NOT MEASURABLE (0.0005MM. BALANCING MACHINE). - AFTER FINAL BALANCING OF THE ROTOR HAS BEEN PERFORMED, THE SUBSEQUENT CHECKS OF BALANCING ON THEBALANCING MACHINE VARYING THE POSITIONING OF THE ROTOR CAN DEVIATE FROM THE INITIAL VALUE BY A TOTAL OF 7,620 GR.MM. WITHOUTREQUIRING CORRECTION. THIS DOES NOT APPLY TO ROTORS THAT HAVE BEEN REMACHINED OR MODIFIED AFTER BALANCING.

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ITN Details5091 -- BALANCING CHECK ACCORDING TO SOM 15648ACCORDING TO DRAWINGS OF PARTS AND TO SPECIFICATION SOM 15648/S. BALANCING IS PERFORMED ON THE INDIVIDUAL COMPONENTS AND/ORSUBASSEMBLIES IN SUCCESSIVE STAGES DURING ASSEMBLY, WITH A FINAL CHECK OF BALANCING ON THE COMPLETELY ASSEMBLED ROTOR. THEFINAL CHECK OF BALANCING IS THE FOLLOWING: 1. CHECKING DYNAMIC BALANCING OF COMPLETE LOW PRESSURE ROTOR. AFTER ASSEMBLY OFTHE TURBINE BUCKETS AND THE LOWER PLATES, PERFORMED ON THE BASIS OF AN ASSEMBLY CHART DESIGNED TO MINIMIZE THE UNBLANCEINDUCED ON THE ROTOR BY THESE COMPONENTS, DYNAMIC BALANCING IS CHECKED ON TWO PLANES. THE RESIDUAL UNBALANCE ON EACHPLANE (N.1 AND N.2) SHALL NOT EXCEED 1016 GR.MM. MAXIMUM CORRECTION BALANCE SHALL NOT EXCEED 12700 GR.MM. ON PLANE N.1 AND25400 ON PLANE N.3. 2. NOTE: PRECISION AND REPEATABILITY OF THE BALANCING MACHINE. - THE PRECISION OF THE BALANCING MACHINECAN BE SUCH THAT A MAXIMUM TOTAL RESIDUAL UNBALANCE OF 1,651 GR.MM. (FOR THE COMPLETE ROTOR) IS NOT MEASURABLE (0.0005 MM.BALANCING MACHINE). - AFTER FINAL BALANCING OF THE ROTOR HAS BEEN PERFORMED, THE SUBSEQUENT CHECKS OF BALANCING ON THEBALANCING MACHINE VARYING THE POSITIONING OF THE ROTOR CAN DEVIATE FROM THE INITIAL VALUE BY A TOTAL OF 7,620 GR.MM. WITHOUTREQUIRING CORRECTION. THIS DOES NOT APPLY TO ROTORS THAT HAVE BEEN REMACHINED OR MODIFIED AFTER BALANCING.

TAV/SH 110/111

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ITN Details5099 -- HARDNESS (AS ITN 02152.05)MATERIAL: HARDNESS HB X12CR13 UNI 6901 MAX 200 ASTM A182 F22 MAX 207 ASTM A350 LF2 MOD. MAX 197 FE 410B UNI 7746 130-180 ASTM A350LF3 MAX 197 ASTM A350 LF5 CL.2 MOD. MAX 197

TAV/SH 111/112

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ITN Details5102 -- RUN OUT TEST FOR COMPRESSOR AND STEAM TURBINE (AS ITN 02183)LIMITS OF ACCEPTABILITY: A)RESIDUAL MAGNETISM: 2 GAUSS B)MECHANICAL RUN-OUT: 5 MICRONS (TOTAL READING ON COMPARATOR) C)TOTALRUN-OUT (ELECTRIC + MAGNETIC + MECHANICAL): 6.35 FOR SQUARE ROOT OF 12000/RPM (MICRONS) WHERE RPM= MAX CONTINUOUS SPEED OR 6MICRONS, WHICHEVER OF THE TWO VALUES IS THE GREATER (SEE SOS 13013/4)

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ITN Details5103 -- DYE PENETRANT TEST (AS ITN 07029)ONLY ROUNDED DEFECTS, EITHER ISOLATED (I.) OR IN GROUPS (R.) CONSISTING OF POROSITY OR INCLUSION WITHIN THE LIMITS OF THECLASSIFICATION IN TABLE ARE ACCEPTABLE. LINEAR DEFECTS (DEFECTS WITH LENGTH MORE THAN 3 TIMES THEIR WIDTH) ARE NOT ACCEPTABLE.TABLE -MAX DIAM. ISOLATED DEFECT (I) MM 3 -MAX N. OF I. IN WORTS LINEAR DM 5 -MIN DISTANCE BETWEEN I. AND I. BETWEEN I, AND R., BETWEENR AND R MM 15 -MAX DIAM. OF CIRCLE ENCLOSING GROUPS OF DEFECTS (R.) MM 6 -MAX DIAM. OF DEFECTS FORMING PART OF GROUP MM 1.5 -MAXN. OF GROUPS IN A PART 4

TAV/SH 113/114

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ITN Details5111 -- ROUTINE TEST (AS SOM 26844)ROUTINE TEST ON D.C. ELECTRIC MOTOR ACCORDING TO SOM 26844. THE FOLLOWING TESTS SHALL BE CARRIED OUT: - COLD WINDINGRESISTANCE MEASUREMENT - OVERLAP TEST - NO LOAD TEST - DIELECTRIC TEST - WINDING INSULATION MEASUREMENT TEST - VIBRATION TEST -OVERSPEED TEST - LOAD TEST - EXCITATION CHARACTERISTIC TEST

TAV/SH 114/115

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ITN Details5129 -- OVERSPEED (AS ITN 07029)SEE FIGURE IN PAR. 12.5. ITN 07029 DIAMETER | DEFORMATION DIAMETER | DEFORMATION D1 (MM) | MAX (MM) D2 D3 D4 D5 (MM) | MAX (MM) MAX.450 | 0,04 MAX 450 | 0,02 MIN. 450 | 0,06 MIN. 450 | 0,03

TAV/SH 115/116

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ITN Details5132 -- TOTAL RUN OUT (AS SOM 26698)ELECTRICAL RUNOUTS AS RECORDED BY THE ROTOR DISPLACEMENT PROBES SHALL BE AS FOLLOW: -RADIAL PROBE LOCATIONS 0.013MM -AXIALPROBE LOCATIONS 0.025MM -KEY PHASOR PROBE LOCATIONS 0.038MM EXCLUDING THE SLOT

TAV/SH 116/117

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ITN Details5402 -- LADLE ANALYSIS (AS ITN 02152.03)FORGINGS FOR CASING, INTAKE AND DELIVERY FLANGES WITH WELDED JOINTS FOR CE/CO MATERIAL : C% P S -1- MAX 0.25 MAX 0.025 MAX 0.025-2- MAX 0.25 MAX 0.020 MAX 0.015 -3- MAX 0.015 MAX 0.010 -4- MAX 0.25 MAX 0.015 MAX 0.010 MATERIAL: -1- ASTM A266 CL.2 MOD. -2- ASTM A350 LF 2MOD. -3- ASTM A350 LF 3 MOD. -4- ASTM A350 LF 5 MOD.

TAV/SH 117/118

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ITN Details5403 -- MECHANICAL PROPERTIES (AS ITN 02152.03)FORGINGS FOR CASING, INTAKE AND DELIVERY FLANGES WITH WELDED JOINTS FOR CE/CO. ASTM A266 CL.2 MOD.= NORMALIZING OR HARDENINGAND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)= MIN.250 - A% MIN.20 Z% MIN.33 IMPACT STRENGTH(J)= NOT REQUIRED ASTM A350 LF2 MOD.=NORMALIZING OR HARDENING AND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)= MIN.250 - A% MIN.22 Z% MIN.30 IMPACT STRENGTH(J)= (1=MIN.27 - 2= MIN.20 - TEMP.= -46 C.) ASTM A350 LF3 MOD.= NORMALIZING OR HARDENING AND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)=MIN.259 - A% MIN.22 Z% MIN.35 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= -101 C.) ASTM A350 LF5 MOD.= NORMALIZING OR HARDENINGAND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)= MIN.259 - A% MIN.22 Z% MIN.35 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= -60 C.)(1)= AVERAGE VALUE OBTAINED FROM 3 IMPACT TESTS CONDUCTED AT INDICATED TEMPERATURE (2)= MINIMUM SINGLE VALUE

TAV/SH 118/119

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ITN Details5409 -- LADLE ANALYSIS (AS ITN 02152.05)MATERIAL: C%MAX MN%MAX SI%MAX CR%MAX NI%MAX MO%MAX P%MAX S%MAX N%MAX -1- 0.09-0.15 1.00 1.0 11.5-14 1.0 -- 0.040 0.030 -- -2- 0.150.3-0.6 0.5 2.0-2.5 -- 0.87-1.13 0.040 0.040 -- -3- 0.25 1.35 0.15-0.3 -- -- -- 0.035 0.040 -- -4- 0.23 0.35-0.7 0.35 -- -- -- 0.045 0.045 0.010 -5- 0.25 -- -- -- -- -- 0.0550.055 -- -6- 0.25 0.80 0.15-0.40 -- 2.1-2.5 -- 0.035 0.040 -- -7- 0.23 0.80 0.15-0.40 -- 3.25-3.75 -- 0.035 0.040 -- -8- 0.25 0.85-1.2 0.15-0.40 -- -- -- 0.035 0.040 -- -9-0.20 1.9 0.2-0.35 -- 3.25-3.75 -- 0.035 0.040 -- -10- 0.25 1.35 0.20-0.35 -- 1.0-2.0 -- 0.035 0.040 -- -1- X12CR13 UNI 6901 -2- ASTM A 182 F 22 -3- ASTM A 350 LF2MOD. -4- FE 410B UNI 7746 -5- FE 430B UNI 7070 -6- ASTM A 203 GR B -7- ASTM A 203 GR E -8- ASTM A 516 GR.70 MOD. -9- ASTM A350 LF3 -10- ASTMA350LF5 MOD.

TAV/SH 119/120

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ITN Details5411 -- MECHANICAL PROPERTIES (AS ITN 02142.01)MATERIAL : HEAT TREATMENT R(N/MM2) RP(0.2)(N/MM2) A% ASTM A 278 CL.40 ANNEALING (550-600 C) 276 --- -- ASTM A 278 CL.35 ANNEALING (500-550C) 241 --- -- ASTM A 536 GR 60-40-18 TO OBTAIN A FERRITIC 414 276 18 MATRIX WITHOUT CARBIDE

TAV/SH 120/121

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ITN Details5412 -- MAGNETIC PARTICLE TEST (AS ITN 02142.01)1) CONTACT SURFACE : CLASS 1 2) GAS FLOW SURFACE : CLASS 0 3) OTHER SURFACES : CLASS 2 -ONLY FOR ASTM A 536 GR.60-40-18CASTS,LINEAR DEFECTS ARE ALSO ACCEPTABLE IF THEY ARE ATTRIBUTABLE TO INCLUSIONS OF VARIOUS OXIDES WHICH INVOLVE ONLY ANDESCLUSIVELY THE SURFACE LAYER OF THE CASTING FOR A MAXIMUM DEPTH OF NO MORE THAN 20% OF THE NOMINAL THICKNESS. THE DEPTH OFTHE DEFECT WILL BE EVALUATED UTILIZING A SAMPLE ZONE,SELECTED IN THE AREA OF MAXIMUM CONCENTRATION, MECHANICALLY REMOVINGTHE DEFECT AND MEASURING THE DEPTH OF THE CAVITY PRODUCED.

TAV/SH 121/122

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ITN Details5414 -- MECHANICAL PROPERTIES (AS ITN 02152.05)MATERIAL: R(N/MM2) RP(0.2)(N/MM2) A%MIN IMPACT TEST KV(J) (1) (2) TEMPERATURE -1- MIN.588 MIN.392 18 20 -- AMBIENT -2- MIN.517 MIN.310 20-- -- --- -3- 485-655 MIN.250 20 20 16 -46 C -4- 410-490 MIN.235 23 35(KCU) -- AMBIENT -5- 430-560 MIN.255 23 27 21 AMBIENT -6- 485-620 MIN.275 21 2016 -60 C -7- 485-620 MIN.275 21 27 -- -101 C -8- 485-620 MIN.260 21 18 14 -46 C -9- 485-655 MIN.260 22 20 16 -101 C -10- 485-655 MIN.260 22 20 16 -60 C-1- X12CR13 UNI 6901 NORMALIZING-TEMPERING -2- ASTM A 182 F 22 NORMALIZING-TEMPERING -3- ASTM A 350 LF 2 NORMALIZING -4- FE 410 B UNI7746 NORMALIZING-TEMPERING -5- FE 430 B UNI 7070 ANNEALING -6- ASTM A 203 GR.B NORMALIZING -7- ASTM A 203 GR.E NORMALIZING -8- ASTMA516 GR.70S5 MOD. NORMALIZING -9- ASTM A350 LF3 NORMALIZING -10-ASTM A350 LF5 MOD. NORMALIZING (1)CHARPY V NOTCH IMPACT VALUEREQUIRED FOR ACCEPTANCE(AVERAGE OF 3 SPECIMENS) (2)CHARPY V NOTCH IMPACT VALUE WITHOUT REQUIRING RETEST (ONE SPECIMEN ONLYOF A SET)

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ITN Details5416 -- LADLE ANALYSIS (AS ITN 02152.02)MATERIAL: C% MN% SI% CR% NI% MO% P% S% -1- 0.37-0.44 0.5-0.80 0.15-0.40 0.6-0.9 1.60-1.9 0.2-0.35

TAV/SH 123/124

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ITN Details5417 -- MECHANICAL PROPERTIES (AS ITN 02152.02)MATERIAL : SPECIMEN R(N/MM2) RP(0.2)(N/MM2) A% Z% IMPACT KV(J) 40NICRMO7 TF LONGITUDINAL 931 735 14 NOT 27* MOD. UNI7874 TRANSVERSE882 686 12 PRESCRIBED 17* ASTM A 320 LONGITUDINAL 862 725 16 50 27** L43 TRANSVERSE 813 676 12 40 17** 39NICRMO3 TF LONGITUDINAL 880685 12 NOT 27* MOD. UNI 7874 TRANSVERSE 832 639 10 PRESCRIBED 17* 414 SIAS LONGITUDINAL 784 637 15 50 25* TRANSVERSE 735 588 12 40 15* *MINIMUM AVERAGE OBTAINED FROM 3 IMPACT TESTS CONDUCTED AT AMBIENT TEMPER. ** MINIMUM AVERAGE OBTAINED FROM 3 IMPACT TESTSCONDUCTED AT -101 CENTIGRADE

TAV/SH 124/125

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ITN Details5418 -- LADLE ANALYSIS (AS ITN 02152.01)MATERIAL : C% SI% MN% P% S% CR% NI% MO% CU% OTHERS% SD 22/3 0.13- 0.3- 0.4-

TAV/SH 125/126

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ITN Details5419 -- LADLE ANALYSIS (AS ITN 02152.04)MATERIAL : C% MN% SI% CR% NI% MO% 39NICRMO3 0.36-0.43 0.5-0.8 0.15-0.40 0.6-0.9 0.7-1 0.15-0.30 UNI 7874

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ITN Details5420 -- HARDNESS (AS ITN 02152.04 & ITN 07711.01)MATERIAL : HEAT TREATMENT HARDNESS (HB) 39NICRMO3 UNI 7874 HARDENING & TEMPERING 290-310

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ITN Details5421 -- LADLE ANALYSIS (AS ITN 02152.20)MATERIAL : PARTICLE C% MN% SI% P%MAX S%MAX C 45 UNI 7845 CLEAT 0.42-0.50 0.5-0.8 0.15-0.40 0.035 0.035 C 10 UNI 7846 SECTOR 0.70-0.130.3-0.6 0.15-0.35 0.035 0.035 NOTE : BABBIT MATERIAL MUST BE OF A PINK METAL LINING + WHITE METAL LINING HOYT 11 R WHOSE CHEMICALCOMPOSITION MUST BE ACCORDING TO THE FOLLOWING VALUES: SB(8.5-10) CU%(3.0-5.0) SN% (OTHER)

TAV/SH 128/129

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ITN Details5446 -- ULTRASONIC TEST ON WELDS (AS ITN 07039)1-ANY INDICATIONS PRODUCING A REFLECTED SIGNAL WHOSE MAGNITUDE IS GREATER THAN 20% OF THE REFERENCE LEVEL SHALL BEEXAMINED IN ORDER TO DETERMINE THEIR FORM, LOCATION AND NATURE, AND SHALL BE EVALUATED FOR ACCEPTANCE AS SPECIFIED IN ITEM2. 2-DISCONTINUITIES INTERPRETED AS CRACKS, LACK OF FUSION OR INCOMPLETE PENETRATION ARE UNACCEPTABLE, REGARDLESS OF THEIRSIZE OR SIGNAL AMPLITUDE. INDICATIONS OF SLAG, POROSITY ARE ACCEPTABLE IF THE ECHO IS HIGHER THAN THAT OF THE REFERENCE LEVELAND IF: A-THE MAXIMUM DIMENSION IS MAX= 6 MM FOR WELDS WITH THICKNESS MAX= 19 MM. B-THE MAXIMUM DIMENSION IS MAX= 1/3 T. WHENTHE WALL THICKNESS T IS INCLUDED BETWEEN 19 MM AND 57 MM C-THE MAXIMUM DIMENSION IS MAX= 19 MM FOR WELDS WITH THICKNESS 57 MM.WHERE "T" IS THE THICKNESS OF THE JOINT UNDER EXAMINATION. IF EDGES OF DIFFERENT THICKNESSES ARE JOINED IN THE WELD, "T" IS THELESSER OF THE THICKNESSES UNDER EXAMINATION. ALL DISCONTINUITIES CONSIDERED UNACCEPTABLE SHALL BE REMOVED FROM THE WELD,AND THE WELD SHALL BE REPAIRED BY THE APPROPRIATE PROCEDURES. THE REPAIRED AREAS OF THE WELD AND THEIR ADJACENT AREASSHALL BE RE-EXAMINED BY ULTRASONIC TEST AS DESCRIBED IN THIS PROCEDURE.

TAV/SH 129/130

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ITN Details5450 -- DYE PENETRANT TEST (AS ITN 31001)THE PERCENTAGE OF DYE PENETRANT TEST MUST BE : *Q= {SQUARE ROOT}OF N *Q= QUANTITY CONTROLLED N= NUMBER OF PIECES IN A LOTACCEPTANCE : CLASS 0

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ITN Details5451 -- ULTRASONIC TEST (AS ITN 02152.02)ULTRASONIC EXAMINATION AS PER ITN 02151, ACCEPTABILITY CLASS: 1A IN AXIAL EXAMINATION 3A IN RADIAL EXAMINATION

TAV/SH 131/132

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ITN Details5463 -- PNEUMATIC TEST (ITN 04204.36)LEAKAGE VALUES ARE RELATIVE TO THE TYPE OF VALVE INDICATED IN THE SPECIFICATION

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ITN Details5466 -- LADLE ANALYSIS (AS ITN 02152.06)MATERIAL : C% MN% SI% CR% NI% MO% P% MAX S% MAX X12CR13 0.09-0.15 MAX 1.0 MAX 1.0 11.5-14 MAX 1.0 -- 0.040 0.30 UNI 6901 ASTM A 182 MAX0.15 0.3- 0.6 MAX 0.5 2.0-2.5 -- 0.87-1.13 0.040 0.40 F 22 MOD. ASTM A 350 MAX 0.25 MAX 1.35 0.15-0.30 -- -- -- 0.035 0.40 LF 2 MOD. ASTM A 266 MAX 0.250.4-1.05 0.15-0.35 -- -- -- 0.040 0.40 CL.2 MOD. ASTM A350 MAX 0.25 MAX 1.35 0.20-0.35 -- 1.0-2.0 -- 0.035 0.40 LF 5 MOD. ASTM A 350 MAX 0.20 MAX 0.900.20-0.35 -- 3.25-3.75 -- 0.035 0.40 LF 3

TAV/SH 133/134

PAG 133/134


QCP SOM5086579 /4




ITN Details5467 -- MECHANICAL PROPERTIES (AS ITN 02152.06)MATERIAL: R(N/MM2) RP(0.2)(N/MM2) A% Z% IMPACT KV(J) TEMPERAT.(CENTIG.) -1- MIN 638 539-621

TAV/SH 134/135

PAG 134/135


QCP SOM5086579 /4




ITN Details5473 -- LADLE ANALYSIS (AS FOR ITN 02152.34)FORGINGS FOR CASING, END FLANGES WITHOUT WELDED JOINTS FOR CE/CO WITH P.P. MAX.354 KG/CM2. ASTM A266 CL2 MOD. - C%= MAX 0.25- MN%= 0.40-1.05 - SI%= 0.15-0.35 P%= MAX 0.015 - S%= MAX 0.010 ASTM A182 F22 MOD. - C%= MAX 0.15 - MN%= 0.30-0.60 - SI%= MAX 0.50 CR%=2.00-2.50 - MO%= 0.87-1.13 - P%= MAX 0.015 S%= MAX 0.010 ASTM A350 LF2 MOD. - C%= MAX 0.25 - MN%= MAX 1.35 - SI%= 0.15-0.30 P%= MAX 0.015 -S%= MAX 0.010 ASTM A350 LF3 MOD. - C%= MAX 0.20 - MN%= MAX 0.90 - SI%= 0.20-0.35 NI%= 3.25-3.75 - P%= MAX 0.015 - S%= MAX 0.010 ASTM A350LF5 MOD. - C%= MAX 0.25 - MN%= MAX 1.35 - SI%= 0.20-0.35 NI%= 1.0-2.0 - P%= MAX 0.015 - S%= MAX 0.010 X12CR13 UNI 6901 - C%= 0.09-0.15 - MN%=MAX 1.00 - SI%= MAX 1.00 CR%= 11.5-14.0 - NI%= MAX 1.00 - P%= MAX 0.040 S%= MAX 0.030

TAV/SH 135/136

PAG 135/136


QCP SOM5086579 /4




ITN Details5474 -- MECHANICAL PROPERTIES (AS FOR ITN 02152.34)ASTM A266 CL2 MOD. - NORMALIZING OR HARDENING AND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)= MIN.250 - A%= MIN.20 Z%= MIN.33IMPACT STRENGTH(J)= NOT PRESCRIBED ASTM A182 F22 MOD. - HARDENING AND TEMPERING - R(N/MM2)= MIN.705 RP(0.2)(N/MM2)= 539-617 -A%= MIN.18 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= AMB.) ASTM A350 LF2 MOD. - NORMALIZING OR HARDENING AND TEMPERINGR(N/MM2)= 485-655 - RP(0.2)(N/MM2)= MIN.250 A%= MIN.22 - Z%= MIN.30 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= -46 C) ASTM A350 LF3MOD. - NORMALIZING OR HARDENING AND TEMPERING R(N/MM2)= 485-655 - RP(0.2)= MIN.259 - A%= MIN.22 Z%= MIN.35 IMPACT STRENGTH(J)= (1=MIN.27 - 2= MIN.20 - TEMP.= -101 C) ASTM A350 LF5 MOD. - NORMALIZING OR HARDENING AND TEMPERING R(N/MM2)= 485-655 - RP(0.2)(N/MM2)=MIN.259 - A%= MIN.22 Z%= MIN.35 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= -60 C) X12CR13 UNI 6901 MOD. - NORMALIZING ORTEMPERING - R(N/MM2)= MIN.588 RP(0.2)(N/MM2)= MIN.392 - A%= MIN.18 IMPACT STRENGTH(J)= (1= MIN.27 - 2= MIN.20 - TEMP.= AMB.) (1)= AVERAGEVALUE OBTAINED FROM 3 IMPACT TESTS CONDUCTED AT INDICATED TEMPERATURE (2)= MINIMUM SINGLE VALUE

TAV/SH 136/136

PAG 136/136

Date post:	01-Nov-2014
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ELM-1950001-MR-Q03-1001-R6

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