GEN SET PERFORMANCE DATA [HCC PREFIX]

SET PERFORMANCE DATA [HCC PREFIX] Sales Model: 3306 SINA Combustion: SI Aspr: NA Engine Power: 85 W/O F 126 HP Manifold Type: WET Speed: 1,800 RPM Governor Type: PSG After Cooler: After Cooler Temp(F): - - Turbo Quantity: Engine App: GS Turbo Arrangement: Hertz: 60 Application Type: EPG-CONT Engine Rating: GS Strategy: Rating Type: CONTINUOUS Certification: Fuel: PIPELINE Fuel Press (PSI): 1 NOx Level: STD IGN: JW Temp (F): 210 ELEK A/F CONT: Cam Type: Piston: CARB: C/R: 8.0:1 ENGINE POWER BHP ENGINE BMEP PSI General Performance Data FUEL BSFC BTU- BHP/HR FUEL RATE CFH INTAKE MFLD TEMP DEG F INTAKE MFLD P IN-HG INTAKE AIR FLOW CFM EXH MFLD TEMP DEG F EXH STACK TEMP DEG F EXH GAS FLOW CFM 85 100 126 86.73 8,311.82 1,158.32 93.2-4.82 215.42 1,100.84 1,064.84 625.07 76.5 90 113 77.89 8,580.39 1,073.57 93.74-7.49 197.76 1,086.98 1,050.98 572.1 68 80 101 69.18 8,926.72 992.34 94.28-10.16 183.64 1,073.66 1,037.66 522.66 63.8 75 94 64.83 9,124.62 949.97 94.64-11.48 176.57 1,067.18 1,031.18 497.94 59.5 70 88 60.63 9,357.86 911.12 95-12.81 165.98 1,060.52 1,024.52 473.22 51 60 76 52.07 9,916.22 829.9 95.72-14.07 144.79 1,041.8 1,005.8 406.12 REJ TO JW Engine Heat Rejection Data REJ TO ATMOS REJ TO EXHAUST EXH RCOV TO FROM OIL CLR WORK ENERGY LHV ENERGY HHV ENERGY 85 100 6,824.4 853.0 6,369.4 3,184.71 966.8 5,345.8 17,459.1 19,392.6 76.5 90 6,596.9 836.0 5,800.7 2,900.36 909.9 4,777.1 16,207.9 18,027.8 68 80 6,369.4 796.2 5,175.2 2,616.01 853.0 4,265.2 14,956.8 16,606.0 63.8 75 6,312.6 790.5 4,890.8 2,502.27 796.2 3,980.9 14,331.2 15,980.4 59.5 70 6,142.0 779.1 4,606.5 2,331.67 739.3 3,753.4 13,762.5 15,298.0 51 60 5,971.3 762.1 4,037.8 1,990.45 682.4 3,184.7 12,511.4 13,933.1 EXHAUST Sound Data: 4.92 FEET

(A) 85 100 110 109 111 109 101 104 104 102 99 (A) EXHAUST Sound Data: 22.97 FEET 85 100 97 95 98 91 86 89 90 91 87

(A) EXHAUST Sound Data: 49.21 FEET 85 100 90 90 93 87 80 82 83 84 79 (A) MECHANICAL Sound Data: 3.28 FEET 85 100 94 75 85 86 87 89 89 84 80 (A) MECHANICAL Sound Data: 22.97 FEET OBCJ 85 100 82 66 76 74 73 78 76 71 66 (A) MECHANICAL Sound Data: 49.21 FEET 85 100 76 60 70 68 67 72 70 65 60

Certification: EMISSIONS DATA EMISSIONS DATA MEASUREMENT IS CONSISTENT WITH THOSE DESCRIBED IN EPA CFR 40 PART 89 SUBPART D & E AND ISO 8178-1 FOR MEASURING HC, CO, CO2 AND NOX. THESE PROCEDURES ARE VERY SIMILAR TO THE METHODS DESCRIBED IN EPA CFR 40 PART 60 APPENDIX A METHOD 25A FOR HYDROCARBONS, METHOD 10 FOR CO, METHOD 7E FOR NOX. DATA SHOWN IS BASED ON STEADY STATE ENGINE OPERATING CONDITIONS OF 77 DEG F, 28.43 INCHES HG AND FUEL HAVING A LHV OF 911 BTU PER CUBIC FOOT AT 30.00 INCHES HG ABSOLUTE AND 32 DEG F. FUEL RATE IS BASED ON A STANDARD CUBIC FOOT AT 30.00 INCHES HG ABSOLUTE AND 32 DEG F. To properly apply this data you must refer to performance parameter DM1176 for additional information... REFERENCE EXHAUST STACK DIAMETER -- WET EXHAUST MASS 959.0 LB/HR WET EXHAUST FLOW (1,065.20 F STACK TEMP ) 625.42 CFM WET EXHAUST FLOW RATE ( 32 DEG F AND 29.98 IN HG ) 220.00 STD CFM DRY EXHAUST FLOW RATE ( 32 DEG F AND 29.98 IN HG ) -- FUEL FLOW RATE 20 CFM

RATED SPEED "Potential site variation" ENGINE POWER BHP TOTAL NOX (AS NO2) LB/HR TOTAL CO LB/HR TOTAL HC LB/HR NON- METH HC LB/HR OXY IN LAMBDA EXHAUST 85 100 126 3.8800.2100.5400 0.08 1.0100 1.08 63.8 75 113 3.1700.1700.4500 0.07.8200 1.07 42.5 50 101 2.1000.1100.3200 0.05.8300 0.92

Ambient Operating Temp. A l t i t u d e 0 F 984.25 F 1,640.42 F 3,280.84 F 4,921.26 F 6,561.68 F 8,202.1 F Altitude Capability Data(Corrected Power Altitude Capability) 50 F 68 F 86 F 104 F 122 F NORMAL 122.03 115.33 107.28 101.92 124.71 118.01 111.3 104.6 123.37 120.69 113.99 107.28 100.58 119.35 116.67 109.96 103.26 116.67 113.99 107.28 100.58 124.71 122.03 116.67 109.96 97.89 93.87 104.6 97.89 95.21 91.19 88.51 99.24 9,842.52 F 95.21 92.53 88.51 85.83 83.14 95.21 10,498.69 F 92.53 89.85 87.17 84.48 81.8 92.53 The powers listed above and all the Powers displayed are Corrected Powers Identification Reference and Notes Engine Arrangement: 9Y7892 Lube Oil Press @ Rated Spd(PSI): 65.3 Effective Serial No: Piston Speed @ Rated Eng SPD(FT/Min): 1,773.6 Primary Engine Test Spec: Max Operating Altitude(FT): 492.1 Performance Parm Ref: TM0001 PEEC Elect Control Module Ref Performance Data Ref: TM9737 PEEC Personality Cont Mod Ref Aux Coolant Pump Perf Ref: Cooling System Perf Ref: Turbocharger Model Certification Ref: Fuel Injector Certification Year: Timing-Static (DEG): 35.00 Compression Ratio: 8.0 Timing-Static Advance (DEG): -- Combustion System: SI Timing-Static (MM): -- Aftercooler Temperature (F): -- Unit Injector Timing (MM): -- Crankcase Blowby Rate(CFH): -- Torque Rise (percent) -- Fuel Rate (Rated RPM) No Load(Gal/HR): -- Peak Torque Speed RPM -- Lube Oil Press @ Low Idle Spd(PSI): 50.8 Peak Torque (LB.FT): --

Reference Number: TM9737 CHANGE 01: UPDATED USING IMPROVED SPECIFIC HEAT CALCULATION Parameters Reference: TM0001 GAS ENGINE PERFORMANCE TOLERANCES: AMBIENT AIR CONDITIONS AND FUEL USED WILL AFFECT THESE VALUES. EACH OF THE VALUES MAY VARY IN ACCORDANCE WITH THE FOLLOWING TOLERANCES: POWER +/- 3% EXHAUST STACK TEMPERATURE +/- 8% INLET AIR FLOW +/- 5% INTAKE MANIFOLD ABSOLUTE PRESSURE - NA +/- 5% INTAKE MANIFOLD ABSOLUTE PRESSURE - TA +/- 5% INTAKE MANIFOLD TEMPERATURE +/- 5 DEG C EXHAUST GAS FLOW +/- 6% SPECIFIC FUEL CONSUMPTION +/- 5% FUEL RATE +/- 5% CONDITIONS: POWER FOR GAS ENGINES IS BASED ON FUEL HAVING A LHV OF 33.74 KJ/L (905 BTU/CU FT) AT 101 KPA (29.91 IN HG) AND 15 DEG C (59 DEG F). FUEL RATE IS BASED ON A CUBIC METER AT 100 KPA (29.61 IN HG) AND 15.6 DEG C (60.1 DEG F). AIR FLOW IS BASED ON A CUBIC FOOT AT 100 KPA (29.61 IN HG) AND 25 DEG C (77 DEG F). EXHAUST FLOW IS BASED ON A CUBIC FOOT AT 100 KPA (29.61 IN HG) AND STACK TEMPERATURE. ENGINE PERFORMANCE IS OBTAINED IN ACCORDANCE WITH SAE J1995, ISO 3046/1, BS5514/1 AND DIN 6271/1 STANDARDS. TRANSIENT RESPONSE DATA IS ACQUIRED FROM AN ENGINE/ERATOR COMBINATION AT NORMAL OPERATING TEMPERATURE AND IN ACCORDANCE WITH ISO 3046/1 STANDARD AMBIENT CONDITIONS. ALSO IN ACCORDANCE WITH SAE J1995, BS5514/1 AND DIN 6271/1 STANDARD REFERENCE CONDITIONS. ENGINES ARE EQUIPPED WITH STANDARD ACCESSORIES; LUBE OIL PUMP,

JACKET WATER PUMP, SEPARATE CIRCUIT AFTERCOOLER WATER PUMP AND MAGNETO (EXCEPT EIS). POWER REQUIRED TO DRIVE AUXILIARIES MUST BE DEDUCTED FROM THE GROSS OUTPUT TO ARRIVE AT THE NET POWER AVAILABLE FOR THE EXTERNAL (FLYWHEEL OR ERATOR). TYPICAL AUXILIARIES INCLUDE COOLING FANS, AIR COMPRESSORS AND CHARGING ALTERNATORS. RATINGS MUST BE REDUCED TO COMPENSATE FOR ALTITUDE AND/OR AMBIENT TEMPERATURE CONDITIONS ACCORDING TO THE APPLICABLE DATA SHOWN ON THE PERFORMANCE DATA SET. DEFINITIONS: INDUSTRIAL CONTINUOUS - THE POWER AND SPEED CAPABILITY OF THE ENGINE WHICH CAN BE USED WITHOUT INTERRUPTION OR CYCLING. ERATOR SET CONTINUOUS - OUTPUT WHICH MAY BE UTILIZED CONTINUOUSLY WITHOUT CYCLING. ALTITUDE: ALTITUDE CAPABILITY - THE RECOMMENDED POWER VALUES FOR SUSTAINED ENGINE OPERATION AT SPECIFIC LEVELS AND AMBIENT TEMPERATURES. COLUMN "N" DATA - THE FLYWHEEL POWER OUTPUT AT NORMAL AMBIENT TEMPERATURE. AMBIENT TEMPERATURE - TO BE MEASURED AT THE AIR CLEANER AIR INLET DURING NORMAL ENGINE OPERATION. NORMAL TEMPERATURE - THE NORMAL TEMPERATURE AT VARIOUS SPECIFIC ALTITUDE LEVELS FOUND ON TM2001.

HEAT REJECTION TOLERANCES: +/- 5% LHV OR HHV ENERGY WORK ENERGY +/- 3% REJECTION TO COOLANT +/- 10% REJECTION TO EXHAUST +/- 10% EXHAUST RECOVERY +/- 10% FROM OIL COOLER +/- 20% FROM AFTERCOOLER +/- 5% REJECTION TO ATMOSPHERE +/- 50% THE FOLLOWING FORMULAS APPLY WHEN DOING AN ENERGY BALANCE: STANDARD TEMPERATURE SYSTEM HHV ENERGY = REJ TO COOLANT + REJ TO ATMOS + REJ TO EXH + FROM AFTCLR + WORK ENERGY COERATION (HIGH TEMPERATURE) SYSTEM AND G3600 HHV ENERGY = REJ TO COOLANT = REJ TO ATMOS + REJ TO EXH + FROM OIL CLR + FROM AFTCLR + WORK ENERGY DEFINITIONS: REJ TO COOLANT (JACKET WATER) - TOTAL AMOUNT OF HEAT PICKED UP BY THE ENGINE COOLING SYSTEM. FOR STANDARD TEMPERATURE SYSTEMS THE OIL COOLER HEAT REJECTION IS INCLUDED. FOR COERATION SYSTEM AND G3600 THE OIL COOLER IS SEPARATE FROM THE JACKET WATER. THEREFORE, THE OIL COOLER HEAT REJECTION IS NOT INCLUDED IN THE REJ TO COOLANT. REJECTION TO EXHAUST - IS BASED ON COOLING EXHAUST STACK FLOW TO 25 DEG C (77 DEG F) AND IS USED IN THE ENERGY BALANCE. EXHAUST RECOVERY - IS THE ENERGY AVAILABLE IF THE EXHAUST STACK FLOW IS COOLED TO 177 DEG C (350.6 DEG F). DEFINITIONS: Sound Power : DM8702 Sound Pressure : TM7080 Date Released : 10/04/11