1R SCOTE Test Procedure Form 1. Method Version Conducted For. Was This Test Run Under a Valid Calibration? (Y/N)

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Form 1 Method Version Conducted For V = Valid I = Invalid N = Results Can Not Be Interpreted As Representative of Oil Performance (Non-Reference Oil) and Shall Not Be Used For Multiple Test Acceptance Criteria. RO = Reference Oil Test NR = All Other Tests Was This Test Under a Valid Calibration? (Y/N) Lab Is Currently Operating Under An LTMS Precision Alarm * Is Currently Operating Under An LTMS Precision Alarm * * Check box only if YES Test EOT Time Oil Code Formulation/ Alternate Codes SAE Viscosity Grade Test Number Engine EOT Date In my opinion this test been conducted in accordance with the Test Procedure (Research Report) and the appropriate amendments through the information letter system. The remarks included in the report describe the anomalies associated with this test. SUBMITTED BY: Testing Laboratory Signature Typed Name Title

Form 2 Test Report Summary Number Start Date Start Time Total Test Length TMC Oil Lab Internal Oil Engine Serial Number Unadjusted Lab Rating Industry Correction (If Any) Subtotal Lab Severity B Adjustment (If Any) Total CORRECTION EFFECTIVE DATE WD TGC TLC BOTOC g/h EOTOC g/h Oil Con. Delta EOTOC- BOTOC g/h Test Target Mean Test Target Std API A A B Pass Limit EFFECTIVE DATE WD TGC TLC BOTOC g/h EOTOC g/h Oil Con. Delta EOTOC- BOTOC g/h Referee Ratings Referee Lab WD TGC TLC Ring Loss of Side Clearance (mm) Ring End Gap Increase (mm) Is the Ring Stuck? Scuffed Area % Average Wear Step (µm) % Bore Polish Rings Piston Top Inter. 1 Oil Crown Skirt Cylinder Liner Notes: A Reference oil tests or as requested by test sponsor B Non-reference oil tests only

Form 3 Operational Summary Number CONTROLLED PARAMETERS NON-CONTROLLED PARAMETERS Operating Parameter Quality Index Threshold Engine Speed 0.00 r/min 1800 Fuel Flow 0.00 g/min 240 Humidity 0.00 g/kg 17.8 Coolant Flow 0.00 L/min 75 Temperature Coolant Out 0.00 C 105 Oil to Manifold 0.00 C 120 Inlet Air Manifold 0.00 C 60 Fuel into Head 0.00 C 42 Pressures Oil to Manifold 0.00 kpa 415 Inlet Air (Abs.) 0.00 kpa 292 Fuel From Head 0.00 kpa 275 Exhaust (Abs.) 0.00 kpa 252 Operating Parameter Units Intake Air Flow kg/h 360-410 Power kw 65-70 Torque Nm 330-350 Blowby L/min 20-56 Temperature Coolant In C 97-101 Coolant Delta T C 4-8 Oil Cooler In C 120-124 Heating Oil C 165 max. Exhaust C 590-620 Pressures Crankcase kpa 0.09-0.3 Coolant to Jug kpa 64-92 A Total number of data points taken as determined from test length and procedural specified sampling rate. B Number of Bad Quality Data points not used in the calculation of the statistical measures. C Number of points clipped by over/under range limits of the statistical measures. D Gathered from 1Q Matrix Test data. EOT Process Total Data Points Quality Over/Under Index Units Target Average Samples A BQD B Range C Process Total Data Points Typical Over/Under Range D Average Samples A BQD B Range C

Form 4 Assembly Measurements And Part Record Number Assembly Measurements and Parts Record Injector Setting ( GO / NO-GO ) Was Timing Initialized? (YES/NO) Piston/Head Clearance mm Cam Gear Backlash mm Desired Fuel Timing BTC Intake Valve Open ATC Injector Plunger Lift mm @ 72 Intake Valve Lift mm @ 456 Exhaust Valve Lift mm @ 247 Liner Top Ring Intermediate Ring Oil Ring Piston Crown Piston Skirt Fuel Injector ECM EPROM Piston Cooling Jet Part Number Serial Number Date Code Inspection Code A B A C E C E C E D D F G H I J K L A On liner O.D. B On liner O.D. (NNNN) C On box label D On top of piston E On paper envelope containing the ring F Number below E located on piston top G Number below E located on piston top H On bottom surface skirt I On bottom surface under pin bore J On top surface of plunger K On top surface of plunger 6 digits L On ECAT software

Form 5 Piston Rating Summary Lab EOT Date End Time Method Test Fuel Fuel Batch Date Rated Rater Initial Verified By Last Reference Information Date Completed TMC Oil Code WD TGC TLC BOTOC g/h Last Reference on this Industry Average Industry ard Deviation Total Piston Ratings Summary Grooves Lands Groove Lands No. 1 No. 2 No. 1 No. 2 No. 3 No. 3 No. 4 Deposit Factor A,% Demerit A,% Demerit A,% Demerit A,% Demerit C a r b o n Total V a r n i s h HC - 1.0 MC - 0.5 LC -.25 Oil Cooling EOTOC g/h Under Crown Deposit Factor A,% Demerit A,% Demerit A,% Demerit A,% Demeit A,% Demerit 8 9 7-7.9 6-6.9 7.5 5-5.9 4-4.9 3-3.9 4.5 2-2.9 1-1.9 >0-0.9 1.5 Clean 0 0 0 0 Clean 0 0 0 0 0 Total Rating Location Factor 2 3 1 3 20 20 60 0.5 1 Industry Rating WD: TLHC %: TGF %: IGF %: TLFC %: Unweighted: TLC: TGC: IGC: Under Crown Carbon:

Form 5A Number Refer to Appendix A14 for an example of Piston Rating Worksheet.

Form 6 Supplemental Piston Deposits (Groove Sides and Rings) Number Carbon Varnish Deposit Type HC MC LC 8-9 7-7.9 6-6.9 5-5.9 4-4.9 3-3.9 2-2.9 1-1.9 >0 - CLEAN Groove Top and Bottom Top Bottom and Back of Rings 1 2 3 1 2 3 T B T B T B T B BK T B BK T B BK Additional Deposit & Condition Ratings Piston Crown Piston Skirt Rings Liner

Form 6A Referee Rating Test Identification Referee Rating Information Company Rating Number Date Rated Rater Total Piston Ratings Summary Grooves Lands Groove Lands No. 1 No. 2 No. 1 No. 2 No. 3 No. 3 No. 4 Deposit Factor A,% DEM. A,% DEM. A,% DEM. A,% DEM. C A HC - 1.0 R MC - 0.5 B LC -.25 O N TOTAL V A R N I S H Oil Cooling Under Crown Deposit Factor A,% DEM. A,% DEM. A,% DEM. A,% DEM. A,% DEM. 8-9 7-7.9 6-6.9 7.5 5-5.9 4-4.9 3-3.9 4.5 2-2.9 1-1.9 >0-0.9 1.5 Clean 0 0 0 0 Clean 0 0 0 0 0 Total Rating Location Factor 2 3 1 3 20 20 60 0.5 1 Industry Rating WD: TLHC %: TGF %: IGF %: TLFC %: Unweighted: TLC: TGC: IGC: Undercrown Carbon:

Form 7 Oil Analysis Data Test Identification Test Fuel Fuel Batch Oil Analysis New VISC @ 100 C VISC @ 40 C TBN D4739 TAN D664 TGA Soot % Fe Al Si Cu Cr Pb Fuel Dilution IR O 2 Blowby(L/min) Oil Consumption g/h for hrs ending Oil Consumption r 2 Fuel Position (mm) Wear Metals (ppm) Other Results Note: (1) Total oil in system 5800 ± 50 g (2) Refill oil scale cart to full level every 36 h. Take oil samples at hours shown before adding oil.

Form 8 Downtime Summary Number Number of Downtime Occurrences Test Hours Date Downtime Reasons Total Downtime (125 HR. MAX) Comments Number of Comment Lines

Form 8A Downtime Summary Number Number of Downtime Occurrences Test Hours Date Downtime Reasons Total Downtime (125 HR. MAX) Comments Number of Comment Lines

Form 8B Downtime Summary Number Number of Downtime Occurrences Test Hours Date Downtime Reasons Total Downtime (125 HR. MAX) Comments Number of Comment Lines

Form 9 Ring Measurements All Ring Measurements Are Made Using Metric Feeler Gages Ring Gaps Specifications (mm) 1Y4014 Top 0.350 0.550 1Y4013 Intermediate 0.754 0.906 1Y4012 Oil 0.400 0.750 Pre-Test Post-Test Increase Ring Side Clearance* A B C D Average Minimum Specification Pre-Test Top Post-Test 0.090 mm 0.127 mm LSC Pre-Test Int. Post-Test 0.060 mm 0.110 mm LSC Pre-Test Oil Post-Test 0.030 mm 0.080 mm LSC * Notes: 1. Write STUCK in place of dimension when applicable. 2. Write <0.03 mm for clearance when applicable. 3. Write > before calculated decrease or average decrease values that incorporate a <0.03 mm in calculation. 4. LSC = Loss of side clearance 5. MIN: Oil Ring minimum side clearance is measured 360 around piston.

Form 10 Liner Measurements Liner Surface Finish (µm) Distance From Top Transverse Longitudinal Average 130 mm 50 mm 25 mm Total Average (Spec: 0.4 0.8 µm) % Liner Bore Polish Grid (Add T/AT Values From Grid) Thrust Anti-Thrust Total Liner Bore Measurement (137.154 mm minimum) Before Test - Diameter (Dial Bore Gage) Bore Height Longitudinal Transverse 250 mm 210 mm 170 mm 130 mm 50 mm 25 mm 15 mm Taper (0.050 mm max.) Wear Step @ 13 mm Out of Round (0.038 mm max) After Test (Surface Profile) Longitudinal µm Transverse µm Front Rear T AT

Form 11 Characteristics of the Data Acquisition System 11 Sensing Device (2) Calibration Frequency (3) Record Device (4) Observation Frequency (5) Record Frequency (6) Log Frequency (7) Parameter (1) Operation Conditions Engine Speed (r/min) Engine Power (kw) Fuel Flow (g/min) Humidity (g/kg) Temperatures ( C) Coolant Out Coolant In Oil to Manifold Oil Cooler In Inlet Air Exhaust Fuel To Head Pressures (kpa) Oil to Manifold Inlet Air Exhaust Fuel from Head Crankcase Flows (L/min) Blowby Coolant Flow Legend: (1) OPERATING PARAMETER (5) DATA OBSERVED BUT ONLY RECORDED IF OFF SPEC. (2) THE TYPE OF DEVICE USED TO MEASURE TEMPERATURE, PRESSURE, OR FLOW (6) DATA ARE RECORDED BUT ARE NOT RETAINED AT EOT (3) THE FREQUENCY AT WHICH THE MEASUREMENT IS CALIBRATED (7) DATA ARE LOGGED AS PERMANENT RECORD, NOTE SPECIFY: (4) THE TYPE OF DEVICE WHERE DATA IS RECORDED SS SNAPSHOT TAKEN AT SPECIFIED FREQUENCY LG HANDLOG SHEET AG/X AVERAGE OF X DATA POINTS AT SPECIFIED FREQUENCY DL AUTOMATIC DATA LOGGER (8) TIME FOR THE OUTPUT TO REACH 63.2% OF FINAL VALUE FOR STEP CHANGE AT INPUT SC STRIP CART RECORDER C/N COMPUTER, USING MANUAL ENTRY C/D COMPUTER, USING DIRECT I/O ENTRY System Response (8)

Form 12 Engine Operational Data Plots

Form 13 Torque and Exhaust Temperature History Data From Last 10 Tests Test Number Average Exhaust Temp. Average Engine Torque 1 2 3 4 5 6 7 8 9 10

Form 14 Oil Consumption : Oil Consumption g/h Initial (0 252) End of Test (468-504) Oil Con Delta (EOTOC BOTOC) 30 28 26 24 22 20 18 16 14 12 10 8 6 4 2 0 0 36 72 108 144 180 216 252 288 324 360 396 432 468 504 HOURS

Form 15 Piston, Ring and Liner Photographs Refer to Appendix A14 for an example of Photo

Form 16 Severity Adjustment History : Usage Dates WD TGF TLC BTOC ETOC Start Time Zi S.A. Zi S.A. Zi S.A. Zi S.A. Zi S.A.

Form 17 Fuel Batch Analysis Refer to Appendix A14 for examples of appropriate Fuel Batch Analysis

Form 18 TMC Control Chart Analysis (Reference Oil Tests Only) Refer to Appendix A14 for examples of Control Chart Analysis page.

Form 19 American Chemistry Council Code of Practice Test Laboratory Conformance Statement Test Laboratory Test Sponsor Formulation / Code Test Number Start Date Start Time Time Zone No. 1 All requirements of the ACC Code of Practice for which the test laboratory is responsible were met in the conduct of this test. Yes No * No. 2 The laboratory ran this test for the full duration following all procedural requirements; and all operational validity requirements of the latest version of the applicable test procedure (ASTM or other), including all updates issued by the organization responsible for the test, were met. Yes No * If the response to this Declaration is No, does the test engineer consider the deviations from operational validity requirements that occurred to be beyond the control of the laboratory? Yes * No No 3. A deviation occurred for one of the test parameters identified by the organization responsible for the test as being a special case. Yes * No (This currently applies only to specific deviations identified in the ASTM Information Letter System) Operational review of this test indicates that the results should be included in the Multiple Test Acceptance Criteria calculations. *Operational review of this test indicates that the results should not be included in the Multiple Test Acceptance Criteria calculations. Note: Supporting comments are required for all responses identified with an asterisk. Comments Signature Typed Name Date Title