HomeMy WebLinkAboutDAQ-2024-0050361
DAQC-125-24
Site ID # 16121-B4
MEMORANDUM
TO: STACK TEST FILE – CRUSOE ENERGY SYSTEMS – Duchesne Data Center
Power Station
THROUGH: Harold Burge, Major Source Compliance Section Manager
FROM: Robert Sirrine, Environmental Scientist
DATE: February 6, 2024
SUBJECT: Location: One mile Northeast of Upalco, Duchesne County, UT
Contact: Ken Parker 720-495-3656, Pinyon ES
Kaitlin Meszaros 631-245-0308
Tester: Great Plains Analytical Services (GAS), Macie McClellan 580-225-0403
Source: Two 530 hp Waukesha H24 CEs and one 13,634 kw Titan 130 Turbine
FRS Site ID#: UT0000004901300215
Permit #: AO DAQE-AN161210002-23 Dated February 13, 2023
Action Code: Tr
Subject: Review of stack test report dated January 5, 2024
On January 8, 2024, the DAQ received a stack test report for emissions testing of the Crusoe Energy
Systems – Duchesne Data Center Power Station’s, two 530 hp Waukesha H24 compressor engines and
one 13,634 kw Titan 130 Turbine located 1 mile Northeast of Upalco, Duchesne County, UT. Testing was
performed December 20-21, 2023, to determine compliance with AO Condition II.B.2.a, and NSPS 40
CFR 60, Subpart JJJJ for NOX, CO, and VOC emissions. The DAQ calculated results are:
Source Test Date RM/Pollutant DAQ Result Tester Result Limit
CE H24-1 12/20/23 */NOX 0.12 lb/hr 0.12 lb/hr 0.18 lb/hr
0.12 g/BHP-H 0.12 g/BHP-Hr 0.15 g/BHP-Hr
*/CO 0.02 lb/hr 0.02 lb/hr 0.35 lb/hr
0.02 g/BHP-Hr 0.02 g/BHP-Hr 0.30 g/BHP-Hr
*/VOC 0.01 lb/hr 0.01 lb/hr 0.02 lb/hr
0.01 g/BHP-Hr 0.006 g/BHP-Hr 0.02 g/BHP-Hr
CE H24-2 12/20/23 */NOX 0.01 lb/hr 0.01 lb/hr 0.18 lb/hr
0..01 g/BHP-H 0.01 g/BHP-Hr 0.15 g/BHP-Hr
*/CO 0.02 lb/hr 0.025 lb/hr 0.35 lb/hr
0.03 g/BHP-Hr 0.025 g/BHP-Hr 0.30 g/BHP-Hr
*/VOC 0.004 lb/hr 0.004 lb/hr 0.02 lb/hr
0.004 g/BHP-Hr 0.004 g/BHP-Hr 0.02 g/BHP-Hr
2
Source Test Date RM/Pollutant DAQ Result Tester Result Limit
Turbine 12/21/23 */NOX 2.44 lb/hr 2.42 lb/hr 13.33 lb/hr
0.09 g/BHP-Hr 0.09 g/BHP-Hr 0.33 g/BHP-Hr
*/CO 0.06 lb/hr 0.06 lb/hr 8.11 lb/hr
0.002 g/BHP-Hr 0.002 g/BHP-Hr 0.20 g/BHP-Hr
*/VOC 0.72 lb/hr 0.716 lb/hr 4.65 lb/hr
0.03 g/BHP-Hr 0.028 g/BHP-Hr 0.12 g/BHP-Hr
*ASTM D6348-03
DEVIATIONS: No deviations were noted. The one discrepancy is the Turbine lb/hr value for
NOX, which is an error in entering the correct final value in the test report since
the three values listed in the report yield a final average of 2.44 lb/hr which
matches the DAQ calculated value.
CONCLUSION: All method stipulated QA/QC requirements appear to have been met as
determined by a review of the report and entering the provided data into our
Excel spreadsheets. The emissions test report appears to be acceptable.
RECOMMENDATION: The two 530 hp Waukesha H24 CEs and one 13,634 kw Titan 130 Turbine
should be considered to have been in compliance with the NOx, CO, and VOC
applicable emissions limits at the time of testing.
HPV: No.
ATTACHMENT: Crusoe Energy DDC stack testing report received January 8, 2024.
DAQ generated Excel spreadsheets.
January 5,2024
Harold Burge
Utah Division of Air Quality
PO Box 144820
Salt Lake City, Utah 841144820
Subject Crusoe Energy Systems, lnc. Duchesne Data Center Power Station - Stack Test Reports
On behalf of Crusoe Energy Systems, !nc. (Crusoe Energy) please find attached the three sack test reports for
the engines and turbine tabled below. Below is a able summarizing the tested unis along with their test dates.
Titan 130 turbine 12t7v2023
Waukesha H24 compressor engine 1?/20D023
r Waukesha H24 compressor engine 322 I 509 t2t20t2023
Should you have any questions or comments about these reports, please contact Kaitlin Meszaros by email at
meszaros@pin)ron-env.com or by phone at 631-245-0308.Thank you for your assisance in this matter.
Sincerely,
PINYON ENVIRONMENTAL, INC.,UTAH DEPARTMENT OF
ETWIRONMENTAL OI.iAUTY
{urJ.L-^; $lvfa,f^r.r)
Kaitlin A Meszaros
Air Quality Specialist
Cc: Michael Duplantis, Crusoe Energy Systems, lnc.
JAN B ?024
DIVISION OF AIR QUALITY
Test Started: 08:55 AM Test Completed: 12:37 PM
#As
40 CFR Part 60 Subpart JJJJ
Performance Test Report
Test Type: lnitia!
Test Date: 12fr20n2023
Source:
Waukesha H24
Rich Burn (4 Cycle)
Serial Number:3221509
Engine Hours:3546.8
Location:
Duchesne Data Center Power Station
Duchesne County, Utah
Prepared on Behalf of:
Crusoe Energy Systems, lnc.
UTAH DEPARTMENT OF
ENVIRONMENTAL OUALITY
JAN B ?C24
DIVISION OF AIR QUALITY
303 W.3rd St (s80) 225-0403 Elk City ,OK73644
lndex
1.0 Key Personnel.... ............. 3
2.0 Sampling System..... ....... 3
3.0 Methods Used............ ......................... 3
4.0 Test Summaries.. ............ 5
5.0 Run Summaries.. ............ 6
6.0 Volumetric Flow Rate Data.... ............. 7
7.0 Calculations.............. ...... 8
8.0 Orygen Calibration... ...... 9
9.0 Engine Parameter Data Sheet.. .......... 10
10.0 QA/QC Results........ ........11
11.0 D6348 Annexes...... ........ 12
12.0 Signature Page........ ....... 18
13.0 Appendices.............. ....... 19
14.0 Bottle Certs............ ....".... 20
15.0 Tri Probe Certification via GD-031 ...... 25
16.0 GAS ALT 141_FT|R EPA........ ............26
17.0 Tester Qualifications (resume)... ......... 28
18.0 Raw Data.
Tables
Table 5.1 (Run Summaries)............. ........... 6
Table 6.1 (Volumetric Flow Rate Data)........... ................ 7
Table 6.2 (Stack Gas Measurements)......... .................... 7
Table 8.1 (Oxygen Calibration).. ................. I
Annex Table 1.2.1 (Certified Calibration Bottle Concentrations)......... 12
Annex Table 1.2.2 (Measurement System Capabilities)..................... 12
Annex Table 1.3.1 (Test Specific Talget Analytes)............................. 13
Annex Table 4.1 (Measure System Capabilities) ............ 15
Figures
Figure 6.1 (Location of Traverse Points per Method 1).......................7
Annex Figure 1.4.1 (Sampling Train)..... ..... 13
Annex Figure 1.4.2 (Sampling Points)... ...... 14
Annex Figure 1.4.3 (Sampling Port Locations).... ............ 14
Appendices
Certified Calibration Bottle Certificates............. ...............20
Tri Probe Certification via GD-031 .............. 25
GAS ALT 141_FT|R EPA............. ............... 27
Tester Qualifications (resume)... ................. 28
Raw Data..... ....... 29
29
3
1.0 Key Personnel
GAS
Crusoe Energy Systems, lnc.
Lucas Ennis
Kody Walters
2.0 Sampling System
The sampling system used consisted of a Stainless steel probe, heated Teflon line, gas conditioning
system, and a Gasmet model DX4000 FTIR analyzer. The gas conditioning system used was a Gasmet
Personal Sampling System with a Zirconium Oxide oxygen sensor.
3.0 Methods Used
ASTM D6348.03
This extractive FTIR based field test method is used to quantify gas phase concentrations of multiple target
analytes (CO, NOX, CH2O, & VOC's) from stationary source etfluent. Because an FTIR analyzer is
potentially capable of analyzing hundreds of compounds, this test method is not analyte or source specific.
The analytes, detection levels, and data quality objectives are expected to change for any particular testing
situation. tt is the responsibility of the tester to define the target analytes, the associated detection limits for
those analytes in the particular source effluent, and the required data quality objectives for each specific
test program. Provisions are included in this test method that require the tester to determine critical
sampling system and instrument operational parameters, and for the conduct of QA/QC procedures.
Test'ers lollbwing this test method will generate data that will allow an independent observer to verify the
valid collection, identification, and quantification of the subject target analytes.
EPAMethodl&14
The purpose of the method is to provide guidance for the selection of sampling pods and traverse points at
which sampling for air pollutants will be performed pursuant to regulations set forth in this part.
EPA Method 2 &2C
This method is applicable for the determination of the average velocity and the volumetric flow rate of a gas
stream. The average gas velocity in a stack is determined from the gas density and from measurement of
the average velocity head with a standard pitot tube. Velocity readings are taken from each stack at 16
separate traverse points (Table 6.1) and used to determine the engines mass emissions rate, calculated
utilizing the formulas seen in section 7.0 ol this report.
EPA Method 3A
This is a procedure for measuring oxygen (O2) and carbon dioxide (CO2) in stationary source emissions
using a continuous instrumental analyzer. Quality assurance and quality control requirements are included
to assure that the tester collects data of known quality. Documentation to these specific requirements for
equipment, supplies, sample collection and analysis, calculations, and data analysis will be included.
GAS
4.0 Test Summary
Unit with a serial number of 3221509 which is a Waukesha H24 engine located at Duchesne Data Center
Power Station and operated by Crusoe Energy Sy$tems, lnc. was tested for emissions of: Carbon
Monoxide, Oxides of Nitrogen, and Volatile Organio Compounds. The test was conducted on 1212012023
by Lucas Ennis with Great Plains Analytical Services, lnc. All quality assurance and quality control tests
were within acceptable tolerances.
The engine is a natural gas fired Rich Burn (4 Cycle) engine rated at 530 brake horse power (BHP) at
1800 RPM. The engine was operating at 436 BHP and 1559 RPM which is 82.33o/o of maximum engine
load during the test. The test HP calculation can be found on page 8. The engine was running at the
maximum load available at the test site.
Site Verification Photos
GAS
4.0 Test
Duchesne Dala Center Power Station
Fsd67A atfia Run 1 Run 2 RUne Pesi Permlts
GO 2,000 0.300 o.022 0.021 0.019 0.02'l Pass
co flbs/ht 0.350 0.022 0.020 o.0't7 0.020 Pass
co @15o/o Q2 2.56t 2.576 2.288 2.484
CO @15YoOz 2586.839 2576.367 2288.458 2483.888
co 7.666 7.619 6.839 7.374
GO 9.144 9.104 8.088 8.779
CO (molwt) 28.01
NOx hlhr 1.000 u.'t5u o.132 0.121 0.116 0.123 Pass
NOx (lbsfl U.'IAU 0.133 o.120 0.103 0.118 Pass
NOx @15YoOz 9.3€9.204 8.313 8.955
NOx @15o/o Q2 9347.615 9203.704 8312.872 8954.730
NOx DDmvw)27.700 27.216 24.U1 26.586
NOx (Dpmvd)33.042 32.524 29.381 31.M9
NOx (molwt) 46.01
NMNEHC hp-hr 0.700 0.020 0.007 0.006 0.006 o.006 PASS
NMNEHC (Ibsfl 0.020 0.007 0.006 0.005 0.006 Pass
NMNEHC (oomvd @15o/o QZ 0.512 0.451 0.440 0.468
NMNEHC (ppbvd) @15YoO2 51 1.935 45't.291 439.888 4fjf . to5
NMNEHC ppmvl,l
ippmvd
1.517 1.335 1.315 1.389
NMNEHG 1 .E10 1.595 1.555 1.653
NMNEHC (molw 44.10
GAS
6
5.0 Run Summaries
Table 5.1 Run Summaries
GAS
6.0 Volumetric Flow Rate Data
Table 6.1. Data used for volumetric flow rate (Method 2)
Table 6.2. Stack gas pr€ssure r€a
Aostd = Velocitv head measured bv the' standard pitot tube, (in.) H2O.'
Damore aTrer EacK ruroe.o.50
Within 5% of Last Aostd readino:Yes
Flgure 6.1
16 Traverse Points Were UsedStack Diameter (inches)6.OO
lnches upstream from disturbance 48.00
lnches downstream lrom disturbance 32.00
Pitot readings are taken for Method 2 calculations using measuring points outlined in Method 1
*The exhaust stack dld not present cyclonlc flow condltlons at the sampllng locatlon due to the
absence of cyclones, inertial demlsterc, venturl scrubbers, or tangsntlal lnlets.
'Cyclonlc Flow Chock (Pass/Fai!): PASS
GAS
I
7.0 Calculations
Method 2: Determination of Stack Gas Velocitv and Volumetric Flow Rate
*Note- Use of this method neqates the need for any fuel related numbers for emissions calculations
Ap(avg) - Velocity head of stack gas, mm H2O (in H2O).
3600 = Conversion Factor, sec/hr.
A = Cross-sectional area of stack, m2 (ftz)
Bws = Water vapor in the gas stream (from ASTM D6348)
Cp(std) = Standard pitot tube coefficient; use 0.99
Kp = Velocity equation constant.
Md = Molecular weight ot stack gas, dry basis, g/g-mole (lb./lb.-mole).
Ms = Molecular weight of stack gas, wet basis, g/g-mole (lb./lb. -mole)
Ps = Absolute stack pressure (Pbar+ Pg), mm Hg (in Hg)
Pstd = Standard absolute pressure, 760 mm Hg (29 92 in. Hg).
Qsd = DrJl volumetric stack gas flow rate corrected to
standard conditions, dscm/hr. (dscf/hr.).
Ts(abs) - Absolute stack temperature, "K ("R). = 460 + Ts lor
English units.
Tstd = Standard absolute temperature, 293'K (528 "R).
Vs - Average stack gas velocity, m/sec (ft./sec).
Md = .44(%CO2)+.32(%02)+.28(%N2+%CO)Md = 44( 092)+.s2(0)+ 28( 907+ 001) = 29.475 LB/I-B-MOLE
Ms = Md(1-Bws)+ 18.0(Bws)Ms = 29.475(1 - 16168)+.18 0(.16168) = 27.62 LB/LB-MOLE
vs = Kp.Cp(std;.VApavg'y'(Ts(abs)/(Ps.Ms))vs = 85 49..99',^/ AZ"^/1tSO+.A7424.56',27 62\) = 96.2 FTISEC
Qsd = s600(1 -Bws)Vs.A((Tstd-Ps)/(Ts(abs)-Pstd))Qsd = 3600(1-.162\96.202-.349((528.24.56)/ (1304.67.29.92)) =33672.72 DSCF/HR
Q = Qsd/35.315 Q = 33672.72/35 315 = 953.496 DSCM/HR
Emission Rates (Examples use CO Run 1)
453.6= Conversion lactor lb. to gram HP= Engines rated Horsepower
A = Cross-sectional area of stack, m2 (ftz\. Mfg.= Manufacturer Exhaust flow rate at 100% (ft3/min)
BHP/HR. = Brake work of the engine, horsepower-hour (HP-HR.). 02 = Concentration oi oxygen on a dry basis, percent.
BTU/HP-HR. = Brake Specific Fuel Consumption (HHV) ppm= Pans Per Million (CO)
ER = Emission rate of (CO) in g/HP-hr. ppm@15% 02= PPM corrected lo 15'/"02
F(d )= yelLrr.s of combustion components per unit of heat Qsd = Dry volumetric stack gas flow rate corrected
content, scm/J (scf/million Btu). to standard conditions, dscm/hr. (DSCF/HR.).
Q = Stack gas volumetric flow rate, in standard cubic meters Run Time = Run Time in Minutes
per hour, dry basis Tpy= Tons per year
LB/HR.= Emission rate of (Co) in LB/HR. vs = Average stack gas velocity, m/sec (ft./sec).
Mol wr.= Mol weight of co (28.01)
ppm @ 15% 02 = PPM-((20.9-15o/"O2)l(2o.9-O2l)ppm @ .15% 02 = 9.144'129.9-15)/(20.9-0'/")) = 2.581 PPM @ 15% 02
g/hp-hr = (PPM-(1.1 64-1 0L3)tQ'(Run Time/60))/BHP/HR (9. 1 44.(1 . 1 64.1 0^-3).953.496"(Run Time/60))/455.8 = .022 G/HP-HR
lb/hr = ER-1 /453.6-BHP-HR LB/HR = .022- 1 1453.6- 455 8 = .022 LB/HR
TPY = LB/HR. '4.38 TPY = .022.4.38 = .096 TPY
HP Provided On Site
ppm wet. (1(1-H2O) = ppm dry e 14 = 7.6655-(1(1-.16))
GAS
8.0 Oxygen Calibration 9
8'1 calibration error tost; how do I confirm my analyzer calibration is correct? After the tester has assembled, prepared and calibrated thesampling system and analyzer,.they conduct a 3-point inalyzer calibration error test before the first run and again after any failed system bias test orfailed drift test' They then introduce the low-, mid-, and high-level calibration gases sequentially in direct calibiation mode. At each calibration gas level(low, mid, and high) the calibration error must be within +2.0 percent of the c;libration span.
8'2- lnitial system bias and system calibration enor checks. Before sampling begins, it is determined whether the high- level or mid-levelcalibration gas best approximates the emissions and it is used as the upscale ga!. rn;e upscale gas is introJuced at the probe upstream of all sample-conditioning components in system calibration mode.
(1) Next' zero gas is introduced as described above. The response must be within 0.5 percent ofthe upscale gas concentration.(2) Low-level gas reading is observed until it has reached a final, stable value and the iesults are ,ecoided. rn-e measuremenl system will beoperated at the normal sampling rate during all system bias checks.
(3) 1f the initial system bias specification is not met, corrective action is taken. The applicable calibration error test from Section g.2.3 of EpAMethod 7E is repeated along with the initial system bias _check until acceptable resulis are achieved, after which sampling will begin- The pre-and poslrun system bias must be within t 5.0 percent of the calibration span for the low-level ano upicate calibration gales.
8'3 Post-run system bias check and drift assossment - confirming that each sample colloctsd is valid. Sampling may be performed for multipleruns before performing the poslrun bias or system calibration error chEck provided thistest is passed at the conclusion of the group of runs. A failedfinal test in this case will invalidate all runs subsequent to the last passed test.
(1) lf the poslrun system bias check is not passed, then the run is invalid. The problem is then diagnosed and fixed, then anothercalibrationerror test and system bias is passed before repeating the run.
(2) After each run' the .low-level and upscale drift is cilculated, using Equation 7E-4 in section .12.5 from EpA Method 7E. lf the poslrun low-and upscale bias checks are passed, but the low-or upscale drift exieecls the specification in section 13.3, the run data are valid, but a 3-pointcalibration error test and a system bias check must be performed and passed prior to additional testing-
Table 8.1 Oxygen Calibration
Method 7E 3.4 To the extent practicable, the measured emissions should be between
20 to 100 percent of the selected calibration span. This may not be practicable in somecases of low concentration measurements or testing for compliance'with an emission
limit when emissions are substantially less than the-limit.
EPA Method 3A CIA Worksheet
ro (,a3 corice-ntraton I Cerflfled Ger Goncentralon I Cerilfled Gac GrLow.Levot (%) | t id-Levet (%) I Xtgtr_t_eu
0.00%l9.O4y"lzo.to,
rncentralon Ittlohl I6-1
I
I Ze e.S: Note: that you may
I risk sampling for muttiple
runs before performing the
post-run bias provided you
pass this test at the
conclusion of the group of
(DIRECT) Anallzer Calibration Error (S 2%)
Check
Certifi6d
Concentration
Value (%)
Direct
Calibration
esponse (%)
Abgolute
Difrerence (7o)
Analyzer
Calibration
Enor (%)
Zero Gas %0-000/o 0.00%0.00%0.00%
Mid-Level cas %
ligh-Level Gas %
9.040h
20.70o/o
9.03%
20.51yo
0.00%
0.19o/o
0.02%
0.90%
(SYSTEM) Calibration Bias Ghecks (S 5%) and Drift Checks (S 3%)Upscale Gas 9.040/o
Zero Offset 0.00%
Bias Prc lnitial Value Bias Post lnital ValuesSpan 20.70
Analfzer
Calibration
Response (%)
Zero Gas O.OOyo
System
Calibrations
Response Pre
(%)
System Bias (7
of Span) Pre
SysEm
Calibration
Response Posl
t%)
iystem Bias (%
of Span) Post
Drifl (% of
Span)
O.O0o/o 0.00o/o 0.000/o 0.00%0.00%
Upscale Gas 9.03o/o 9.02o/o 0.05%9.00%0 14o/o 0.00%
(SYSTEM) Calibratlon Bia3 Checks (S 5%) and Orifl Chech (S 3%)
Avg. Gas Concentration (Run 1)0-Mo/o Effuent Gas (Coas) Run 1 0.040h
Avg. Gas Concentration (Run 2)O.OSVo Effluent Gas (Cgas) Run 2 0.05%
Avg. Gas Concanlration (Run g)0.05o/o Effluent Gas (Cgas) Run 3 0.0s%
EPA Method 3A CIA Worksheet
zero Gas 100% Nitrogen
Mid-Level Gas 9.040/0
High-Level Gas 20.70%
Zero Gas o/o
Mid-Level Gas %
High-Level Gas %
zero Gas % l-;oill Upscale Used
upscate car l-mr%-l s.o4%
Zero Gas % [-;o% lupscare used
Upscate car I ,.o0% I s.o4%
GAS
a
10
9.0 Engine Parameter Data Sheet
Run 1 Run 2 Run 3 Completed
Company reergySystems,lnc.
Facllltv DucheSne L,ata Uenler Fower urarlon
Date '11z2u.t21)23
Site Elevation (ft)5A2t
Unlt lD
Make wauKesna
Model t'124
Serlal Number 3221 509
Technlclan Lucas Ennis
TunStafr-nmes 08:55 AM 110:07 AM 11:20 AM 12i37 PM
Enolne Hours 3543.8 3544.8 3545.8 3546.6
Run 1 Run 2 Run 3 Averaqe
Enqine Speed (RPM)1562.0 1557.0 1ss8.0 1559.0
lntake Manlfold Pressure (Psl)39.2 38.6 35.8 37.9
-[-ntakei/hnlfoldTemp'F 122.O 123.O 122.O 122.3
EnEineLo-afl(BHP)455.E 450.5 402.8 4it6.4
TmEienITemF-F 27.O 34.0 37.O 32.7
Tumldltv%I t.u 59.0 51 .O 62.3
EwFoInt.F 21.O 21.O 21.0 21.O
AFR Manufacturer/Type Waukesha \,Yaukesha Waukesha Waukesha
Suctlon Pressure 75.8 74.3 63.6 71.2
Discharoe Pressure 381 .6 380.7 374.7 379.O
catalvst lYes or N0 Yes
catd-ulvstManuf acturer GE GE GE GE
+o-f
-Catalystlnstalled
2 2 2 2
ilatalvst lnlet Temp oF 1159.0 1153.O 1135.0 1149.0
-atalvst
Outlet Temp'F 1117.O 1 1 16.0 1 103.0 1112.0
eatalist Pressure Drop H2o 8.8 9.O 8.7 8.8
GAS
11
10.0 OA/OC Results
Zero Response Time 45
System Response Time 45 seconds
Nitrogen monoxide NO
Nitrogen dioxide NO2
NOx
voc
Oxygen
Average:0.00
Average:0.00
Average:0.00
Average:0.00
Average:0.55
Average:0.00
CTS Bottle Concentration
CTS Compound Concentration Avg
Tolerance
Difference between measured and expected
Value:100.00
Value:98.56
2.0O/"
1.44o/o
Nitrogen monoxide NO
Nitrogen dioxide N02
NOx
voc
Average:0.00
Average:0.00
Average:0.00
Average:0.00
Average:0.47
Average:0.00
CTS Bottle Concentration
CTS Compound Goncentration Avg
Tolerance
Ditference between measured and expected
Value:100.00
Value:97.7O
5.00%
2.30%
Equilibration Response Time
Spike Reported
Spike Expected
45 seconds
Value:249.61
Value: 251.00
Gas, lnc.
12
1 1.0 D6348 Annexes 1-8
The test q-uality objectives completed for the emissions test are demonstrated throughout Annexes 1,2, g,
4, 5,6,7 & I as layed out per ASTM D6348-03. All reference methods, pre-test and post test procedures
were within acceptable limits. Data generated during the pre-test and post-test procedures ard
summarized below in order of the distinctive Annex.
Three 60 minute test runs were performed. The final analyte concentrations are the average of each test
run. Data was taken at 60 second intervals. Each 60 second measurement was the average of 600 scans.
.lppale is used as the surrogate compound for the Annex 5 Spiking Technique due to Propane being the
VOC that is most commonly found in the combustion process df natural gas. 'Additionally, the molecu-iar
weight of Propane coincides with with molecular weight of VOC's per the EPA.
Annex Table 1.2.1 Certified Calibration Bottle Concentrations
Bottle Expiration N02 Ethylene sF6 02 (Yol
cc517745 7t't3t2026 101.90 9.O4"/o
cG1 1 7503 4t15t2031 100.00
GG76460 7t5t2031 20.7O"/o
Cylinder # CC142828 Expiration: 12-06-2030
Propane co NO sF6
Bottle Value 251.00 5U1 .4U 252.40 9.73
Analyzer System Response 249.61 492.32 247.10 9.60
Percent Difference O.55"/o 1.E1"/o 2.1O"/o 1.29o/"
Annex Table 1.2.2 Measurement System Capabilities
GAS
Annex Table 1.3.1 Test Specific Target Analytes and Data Quality Objectives
Compounds
lnfrared
Analvsls Pcalar
Expected
Concentratlon
Range
Measuremenr
System
Achlevable
Mlnimum
Detectable
Concentratlons
Hequrreq
Measurement
System
Accuracy and
Preclslon lor
fest Appllcatlon
(cm-l)
co 2000-2200 0-1200 ppm 0.16267 ppm 4 ppm
NO 1875-2138 0-1000 oom 0.4007 oom 2 oom
NO2 2700-2950 0-'100 oom 0.4899 oom 2 oom
voc
2600-3200
0-100 ppm 1.8520 ppm Total
VOC'S 1 ppmperVOC910-1 150
2550-2950
CHzO 2550-2850 0-100 oom 0.7878 oom 1 oom
lnterferlng
Compounds
. CO is analyzed in a separate analysis region than CO2 and H2O
coz 926-1 150 0-10h 07"nla
Water VaDor 3200-3401 O-22"/o O.ZOYI nla
'VOCs compiled of Acetaldehyde, Ethylene, Hexane, and Propane.
.4
a2
SENSOR
PROBE
-.,itw-*
Er
ru
ffi
GAS
Figure Annex 1.4.1 Sampling Train
The testing instrumentation is housed in an enclosed vehicle which is located approximately 45 feet from the source. A
heated sample line (sixty feet in length) is attached to the inlet of analyzer system and the source effluent discharges
through the FTIR outlet.
FLOW
MTR.s
$VENT
STACK
GAS
14
Sampling Point Locations
in lnches
16.7"/o 'r.336
50o/o 4.000
433"h 6.664
TRLPROBE SAMPLE POINT L
AS PERCENIAGE OF SIACK
Flgure Annex I Sampllng Polnts
!nterior Stack
lnches
Upstream:
48
lnches
Downstream:
32
SAMPLE
BY
Flgure Annex 1.4.3 Sample Port Locatlon
LOCATION DETERMINEO
FROM USruRBANCE
Taroet Analvte Results (oom)
GO o.162/
NU o.400r
NO2 o.4E9t
Ethvlene o37At
ProDane 0.4351
Hexane o.2237
lvde 0.615'
horm€a o.7a7t
N EA 7T7,
7'7fls
REF 7n
rTns
NEA 717, rMDC*t : 'oorr',s * L'ref Lref
REF'r.:;s Lcert
calabrataon Tlansler standard ExDected Meaaured Path Lenoth valldated
Ethvlene 100 9U.5ti 4.924 Passed
An nex T able 1.2.2 ileasurement System Capabilitles
GAS
Parameter Gas Concentratlon i,leasured % Dlfierence speclflcailon Valldated
Spike Direct
Propane 251.000 250.512 0-'l9o/"+l'2o/o Pass
SF6 9. /3U 9.644 0.88%+l- 2o/o PaSS
CO 501.400 494.777 1.32o/o +l'2o/o PaSS
NO 252.400 247.832 1.81%+l'2o/o Pass
SDIke Run 1 vla the Svstem
Source Output SDike Averaqe Dilution Factor Expected 70 Becovery Specilication
Propane 0.000 22.200 20.180 11O.O1O"/"70-130%
SF6 0.000 o.775 8.036%<1Oo/"
Soike Run 2 via the System
Source OutDut SDike Averaqe Dilutlon Factor ExDected 70 Recovery SDecillcatlon
Propane 0.000 22.351 20.482 109.130%70-130%
SF6 0.000 0.787 8.161y"<10h
sDlKe Hun 3 vta tne svstGm
Source OutDut SDlke Averaoe Dilutlon Factor ExDected o/o Recovery SDecilication
Propane 0.000 22.490 20.708 108.610%70-130%
SF6 0.000 0.796 8.254o/o <1Oo/"
Nolse Equivalent Absorbance (NEA)
RMS High 0.000445
RMS Mid 0.001823
RMS Low 0.001065
Lrne Position
020
u t5
010
005
0 00 '\./
2092 2069 2046 ?fi23 199S X$76 r 953 1930 1907 '1 884 1861 1837 I814.
0.20
0.1 5
010
$CIs
0.OCI
l) 05
Line Position Difference:to Beference I 0.29%0.00% Pass
GAS
Pass
The Gasmet GICCOR (Genzel lnterferometer with Cube Corner Retroreflectors) interferometer is specially
designed for maximum opticalthroughput and maximum signal to noise ratio of 7.72 (cm-1) remaining
stable with any vibration and temperature changes.
lne uasmel ux4uuu rs a low resolulron speqro
setting and the detector linearity was tested with
gas was performed and validated.
158.5898
148.5898
138.5898
128.5898
1185898
108 5898
98 5898
88.5898
78.5898
68 5898695 687 679 672
neter where the aperture is fixed to a maximum angle
an alternate approach. A three point linerarity of the CTS
Linea rity
664 656 648 641 633 625 61 8
158.5898
148 5898
1 38.5898
128.5898
118 5898
- 1CI8.$898
98.5898
88.5898
78.5898
68 5898ntn nn1utu vvl
'15.2439047 Pass
The analytical accuracy of the quantification algorithm is satisfied via the results from Annex 5 per Annex
7.6
POST CTS $rstem Check:
u ls Botfle uoncentratlon:100.00
L; I S Samole L;OncenraIon Averaoe: 98.92
Difference between measured and expectecl:1.O9%
Tolerance:5.OOo/o
Run Data Valldatlon - Automated vs Manual Headlng velEated Commente
HUn r l.OTnIS r & Z On UU/NU/rrOpane All within 2O7o PASSEd Demonstrates no rntenerences observed.
HUn Z HOrntS't & Z On UU/NU/rrOpane All within 2O7o Passecl Demonstrates no Interlerences observed,
HUn 3 l.OTnIS'r & Z On UU/NU/rrOpane All within 2O7o Passed Demonstrates no interferences observed,
GAS
18
12.0 Signature Page
JoUFile Name: Crusoe Energy Systems, lnc.; Duchesne Data Center Power Station; ;JJJJ
We certify thal based on review of test data, knowledge of those individuals directly responsible for
conducting this test, we believe the submitted information to be accurate and complete.
Company: G.A.S. lnc.
Print Name: Lucas Ennis
Title: Emissions Specialist
Dale:1212012023
Company:
Print Name:
Signature:
Title:
Phone Number:
Date:
Company:
Print Name:
Title:
Signature:
G.A.S. lnc.
Chris Oppel
Director of Stack Testing
n/,n/l/.// n(,4 %t-{\
Dale:1212012023
PhoneNumber: 580-225-0403
GAS
Appendices
GAS
Spike (5 Gas)
*iH3S
Part Number:
Cylinder Number:
Laboratory:
PGVP Number:
Gas Code:
Airts Spccislty Gu6
Airgs USA LLC
r2Z2 S. Wetrtmrth Ave.
Chicago, IL 60628
Air8s.@m
CERTIFICATE OF ANALYSIS
Grade of Product: EPA PROTOCOL STANDARI)
E05Nr94E15AC014
cc142828
124 - Chicago (SAP) - lL
812022
CO,CO2,NO,NOX, PPN,BALN
Reference Number: 54402601324-1
Cylinder Volume: 147.O CF
Cylinder Pressure: 2015 PSIG
Valve Ouflet: 660
CertificationDate: DecO6,2022
Dato:
C.rtf€tion pdbrm6d in e@rdane wtih 'EPA Treeability PEto@lbr ABBY.nd CGr{fietd ot Gr$N C.llbEdon St ndrdt (M.y 2012}' d@ment
000/R-l 2y53 l , Eing th. as.y p@.ducs lbtcd. AnaMi@l M.hodology docs not Equlrc @mdoo tor .natylic.l hbrtbGn@. Thl6 cyllndtr ha8 . tot l sn8tytiel
unodeinty as st ild b.low with a ffifid6n6 lovel of 95%. Th€E aB no dgnl€r( impudth6 silich a{tacl th! us ot this elib.atid mixfuE- All ffiGntratiffs aE on a
moL/mola basis unlas othailisa hoied. T}le Esults rrl.t. sry to lhc hcrc t!Ld. Th. r.pd shell nd bG Eprodu6d cxcrpt in full withil appDvel of the laboEtory. Do
Trl.d D.t! Avallabls Upon Rsquest
PERTANENT NOTES:Mixture contalns nominal 1oppm Sulfur l-bxaiuodde as a tracer component. Actual
tested value included within the original Certifi@te of Analysis. Contacl the Airgas laboratory if a reprint is
requircd
NOTES:Mixture contains nominal 10ppm Sulfur Hexafluoride as a tracer component. Actual tested value
included within the original Certificate of Analysis. Contact the Argas laboratory if a reprint is required.
SF6 Results:
JMR137-9.73[PPME n n rl
lln
Approved for Release P.g. I of I
ANALYTICAL RESII,'LTS
Gomponent Requested Actual Protocol TotalRel.ilv.Assay
Date3ConcenEaton Concentratlon Uothod Uncartllntv
NOX 250.0 PPM 253.0 PPM Gl +/- 1.2% NIST TE€ble 11128DO22,12/0612O22
NITRIC OXIDE 250.0 PPM 252.4 PPM Gl +^ 1.0% NIST TE€able 1112812022, 1AOO|2022
PROPANE 250.0 PPM 251.0 PPM G1 +/- 0.7% NIST TE€ble 11I3ODO22
CARBON MONOXIDE 500.0 PPM 501.4 PPM G1 +/- 0.6% NIST TEeable 1112912022
CARBON DIOXIDE 5.000 % 5.025 % G1 +/- 1.4% NIST TE@able 1112U2022
NITROGEN Balene
CAI,IBRATTON STANDARDS
TyDe Lot lD Cvllnder No Concantratldr Unceitalnw ErDlBtlon Datg
NTRM 200603-31
PRM 12386
GMIS 401423838104
NTRM 200502-13
NTRM 13010109
NTRM 13060423
E80113125 250,3 PPM NITRIC OXIDE/NITROGEN
D685025 9,91 PPM NITROGEN DIOXIDE/AIR
CC5O559O 4,373 PPM NITROGEN DIOXIDE/NITROGEN
6162697Y 243.3 PPM PROPANE.IAIR
KALOO3925 495.4 PPM CARBON MONOXIDE/NITROGEN
co113685 7.489 % CARBON D|OXIDE/N|TROGEN
+l-0.8%
+l-2.O%
+l-2.0%
+l-0.5%
+t- 0.60k
+l-O.6%
Oct 29, 2026
Feb20,2020
F€b 18, 2023
Mat 17,2027
Jul 03, 2024
May 14,2025
ANALYTICAL EQI,IIPMENT
lnstrumenuluako/Modol Analytcal Pdnclpls Le3t llultpolnt C.llbratlon
Ni@l€t iS50 AUP2010242
CO-1 SIEMENS ULTMMAT 6E N1J57OO
Ni@let lS50 AUP2010242
Ni@let iS50 AUP2010242
Ni@let iS50 AUP2110277
NoY 07,2022
Nov 28,2022
Oec05,2022
Dec 05,2022
Nov 07, 2022
FTIR
NDIR
FTIR
FTIR
FTIR
GAS
Airgas
ah A[ Lqude company
9o/o O2|NO2
AlrgrsSFdsftyGaG
Airgs USAUa
525 North Industial I&p Rosd
T@le, UT84074
Airgu.om
CERTIFICATE OF ANIALYSIS
Grade of Product: EPA PROTOCOL STANDARD
Part Number:
Cylinder Number
Laboratory:
PGVP Number:
Gas Code:
E03Nt90E15W0003
cc517745
124 - Tooele (SAP) - UT
872023
NO2,02.BALN
Date:
C.rlilletkh pcrbm.d in .@rd.ne wih 'EPA TE6.bill9 PDb@l br
Tdad Data Avallablo Upon Roque3l
Approved for Relea3e
Reference Number: 153402786436-1
Cylinder Volume: '145.0 CF
Cylinder Pressure: 2015 PSIG
Valve Outlet: 660
Certification Date: Jul 13,2023
C.lbEdon St$dad8 (M.y 2012)' d@m.nt
600/R.12531, Elng thG a$.y prclduEs listod. AMMi€l M.thodology d6s rct EquiG q.d6 tEr .Mlydel inbrf.En@. Thb crlhdd h.s . tot.l .n.Miel
unorblnty .s sbbd bdil wlth e dfidcE lcvel of g5%. Thc6 .E m signflldht lhpu.itl& whlcfi aft c't tha ue ol thl! dllbrdid mlxtiE. All 6ehbaliil6 aE m a
molG/moL b.8i6 unh$ othwis. not d. Tho Euh6 rclgte dly to lh. lbm6 i.rtcd. Th. ruport Gh.ll not bc Epoduod .xc.pt ln tull wihoul .ppDv.l ol t!. leboEbry. Do
Pr!. I ol I
ANALYTICALRESULTS
Roqu.stsd Actual Protocol Total Relatvg
ConcentEflon Concontra0on ileihod Uncertalntv
Componont A.3ay
Datsg
NITROGENDIOXIDE '100.0PPM 101.9PPM Gt +12.0%NISTTE€eble 0710612023,0711312023
OXYGEN 9.000 % 9.037 o/o Gl +/- 1.0% NIST TE@sbl€ 071612023
NITROGEN Bdan€
CALIBRATIONSTANDARDS
Type Lot lD Cyllndsr No Concentraton Uncertalnty ExplEtlon O.i.
GMIS 153/,022022601 CC517858 10r.r PPM NTTROGEN DTOXTDENTTROGEN 1.1%
PRM 12420 D887373 98.9 PPM NITROGEN DIOXIDE/I,IITROGEN 1.O%
NTRM 98051010 SG9161286BAL 12.05% OXYGEN/N|TROGEN 0.7%
ft. SRM- ffiRM. Pil. d R& mH ebE l. mtu in tud b he GMIS ud ln he Bsv end not Efr dhe an*d.-
Nov 09, 2025
Fob23,2023
Ds 14,2023
ANALYIICAL EQI,IIPMENT
Anlly[c.l Prlnclplelnstrum€nutak rtodcl L.st 1{ultlpolnt Clllbrstlon
MKS FTIR NO2 018143349
Horiba MPA610 W603MM58 02
FTIR
02 Psmmaon€tic (DIXON)
Jun 29,2023
Jun29.2023
GAS
Airgas.
& Alr Lhuide cmparry
Cusbmer
Part Number
Cy{indar Number
Laboratory:
Analy3b Date:
Lot Numbor
kimary Standad Gas
Component ReqfGonc
ETHYLENE
NITROGEN
ilot |:GREAT PLAINS ANAL CERTIFIED BY FTIR
AppDr,.dfurR.L...
etutuSpcddVCrs
AirtuUSAUa
12722 g. Watmrth AE.
Chiogo, IL6o628
lttof!.@
OFAIIIALYSIS
STATTIDARI)
ReErcnce Number 54.{i02811378-1
Cy,llndervoluma: '144.0 CF
Clllndor Pro$ule: 2015 PSIGVahrsoutot 350
, yseights and/a N.I.S.T. G6 Mbture rcftrcnce materials.
RESI.'LTS
Gonccntretlon Anaffical
Uncoftalnty
+l- 1c*
P.go I otl
Explradon Dft:
Airgas.
3n Ar Lqude lmp€rry
BIP
AiryuMtd Southrcgion
Airgs USA LLC
9741 E. S6th SL North
l\lsa, OK74u7
AirgE.@m
CERTIFICAIE OF BATCH ANALYSIS
Grade of Product: BIp-BUfLT IN PURIFIER
Part Number:
Cylinder Analfzed:
Laboratory:
Analysis Date:
Component
Nt BtP300
TWo$867349
106 - Tulse Fast Fi[ (SAp) - OK
Feb 10,2016
Reference Number: 29-400672389-1
Cylinder Volume: 304.0 CF
Cylinder Pressure: 2O4O pSlG
Roquosbd Gertlfled
WATER
TOTAL HYDROCARBONS
CARBON DIOXIDE
CARBON MONOXIDE
1 PPM
1 PPM
0.1 PPM
0.5 PPM
0.5 PPM
0.94 PPM
0.058 PPM
0.1 PPM
0.235 PPM
0.235 PPM
Permanent Not'3:This cart includes val,
Salos Repres€ntative for this infomatbn.
C-tfllnders ln B.tch:
4263617Y, TW04671107, TWO+831574, TW0S865966, TWO$867349, TW0$867538, TWO5-867578, TW0S81687, TWOS-881820,TW0S920689, TW0S92o76o, TW05848694, TW05867441,TW058g7265, TW05897512, TW05920678, TW05920686, TW05920695,TW0592078 1, TW05920874
tmpurities vedrred against anaryticar stanaa@
Approved for Release Prg. t ol I
GAS
*itg"*,$'
21o/o 02
Air88 SIEcisltY GaG
Air86 USALrc
525 North Indstrisl IeP Road
To@le, tIT 84074
Ar18a.@m
CERTIFICATE OF AIYALYSIS
Grade of Product: EPAPROTOCOL STAI{DARI)
Part Number:
Cylinder Number:
Laboratory:
PGVP Number:
Gas Code:
E02N179E15A00B1
cc76460
124 -Tooele (SAP) - UT
872023
02.BALN
Reference Number: 153402783621'1
Cylinder Volume: 146.0 CF
Cylinder Pressure: 2015 PSIG
Valve Outlet: 590
Certification Date: Jul 05,2023
ileto p.rlo-.a in e@rd.ne wi$ 'EPA Tra66bility Asray end ot GeooB CalibEton (Msy 2012)'d@mdt EPA
,";il;V;;ilird tto* witr i qttdcne lcwlotgs%' Th@rro
,,i15#ilvo"1,1""f#*1t1,H"""ffi#flIlJ*i?"rJ*t,ff;I,ih'J'EEl;ffi;;#ii"jilil;-"i".ptlnr,rr*n'o,t"pp*arotth'.bo6bry' oo
Trlad Daia Av.llable UPon Roquest
sllnatum on flle
-
Approved tor Roleaso Prg. I ot I
ANALYIICALRESTJLTS
Componont Requosted
Concrnttatlon
Aciual
concentratlon
Proiocol Total Rolrtvo
ilcttrod Unc.rtalnty
t-*"Utt 0710512023OrC/cEN 21.o1.h 20.7O'h
CALIBRAMON STAIYDARDS
Tvm LotlD CyllnderNo Concenlailon Uncsrttlnty ExPlratlon Dato
-
ANALYTIOAL EQI,IIPMENT
lnstrumonUilake/ilodel Analyucal Pdnclple La3t MultlPolnt Callbratlon
GAS
SAS
Part Number:
Laboratory:
Analysis Date:
LOT Number:
SN:
CERTIF'ICATE OF ANALYSIS
Grade of Product: CERTIFIED STAI\DARD-PROBE
Measut€d Flow Measured Flow Measurcd Flow Meu Probe
Port A (Vml Port B lvm) Port C (Uml Port Srmpled
lDelta oll lDelta o2l lDeha o3l Flow (I.,/m)
Great Plalns Analytlcal Servlces
303 w 3d st
Elk City, OK 73544
(5801225-0403 Fax: (5801?25-2612
Tri Probe Certification
8L
GAS INC.
3t3t2022
A
22A8L
Reference 22
Number:
Stack Diameter: 8'
Target Flow 3Umin
Rate:
Numberof 3
Points:
Product performance verified by direct comparison to calibration standards traceable to N.I.S.T.
*The probe listed on this form meets the multipoint traverse requirement of EPA Method 7e,
section 8.4 as shown in the accompanying data. Method 7e, section 8.4 states that the multipoint
traverse requirement can be satisfied by sampling via "a multi-hole probe desigred to sample at
the prescribed points with a flow +/- l0 percent of mean flow rate".
ANALYTICAL RESULTS
Total Flow
(Uml
Rul
Rm2
2 LPM
4 LPM
0.720
(r.00a)
t.4t
(7.09A)
0.660
(-r.004)
1.30
(-t.21L)
0.520
(-?.00a)
t.24
(_5.82A)
*Calibration conducM in accordmce with Emission M€asurement Cenrcr Grideline Dommt - EMC GD-031
31312022
DateApproved for Release
Probe size: 8L
"ja... rrUa ',
,, |\f!f .:'
.i-
"',r .-. rt.
UNITED $TATHS ENVIRONMENTAL PROTECTION AGTNTY
[t[$fiAtlf,H tHlAh\rGl-E PARK l.lC ?771 ]
March 15,2021
Mr. Jordan Williamson
CEO
GAS Inc.
303 W. 3ra Street
Elk City, OK73644
Dear Mr- Williamson:
We are writing in response to your letter received on September 17, 2020,in which you request the approval
of alternative testing procedures. The EPA's Office of Air Quality Planning and Standards (OAQPS) is the
delegated authority for consideration of major alternatives to test methods and procedures as set forth in 40
CFR parts 60 and 63 under which your request must be addressed, GAS Inc. is requesting a change to one of
the test methods, ASTM D6348-03, used for conducting performance tests to determine compliance under
40 CFR part 60, Subpart JJJJ - Standards of Performance for Stationary Spark Ignition Internal Combustion
Engines (Subpart JJJJ) and 40 CFR part 63, Subpart ZZZZ - National Emissions Standards for Hazardous
Air Pollutants for Perfornance for Stationary Reciprocating Internal Combustion Engines (Subpart ZZZZ).
The change being requested will be used to check detector linearity of the Fourier Transform Infrared (FTIR)
inskumentation used to conduct this method. Specifically, you are requesting that the procedures of section
8.3.3 of Method 320 (40 CFR part 60, Appendix A), another FTIR-based method allowed under Subparts
JJJJ and ZZZZ, be used in lieu of section A6.4.1of ASTM D6348-03 when conducting testing using ASTM
D6348-03 under 40 CFR part 60, Subpart JJJJ and 40 CFR part 63, Subpart ZZZZ.
In your request, you state that this alternative linearity check procedure will produce consistent results when
utilizing either Method 320 or ASTM D6348-03. Additionally, some FTIR instrumentation does not allow
for reducing the size of the aperture in the instrument and, thus, it would not be feasible to properly conduct
the entirety of the ASTM D6348-03 method in its current form using such an instrument.
Based on our understanding of FTIR instrument principles and recognition that the requested alternative
determination of detector linearity is both technically sound and contained within Method 320,we are
approving the requested change. We believe that this alternative is acceptable for use for use in testing all
engines subj ect to 40 CFR part 60 Subpart JJJJ and 40 CFR part 63 , Subpart ZZZZ. Also, we will post this
letter as ALT-141 on EPA's website (atwww.epa.gov/emc/broadly-applicable-approved-alternative-
testmethods) to announce that our approval of this alternative test method is broadly applicable to engines for
the purposes of meeting Subparts JJJJ and ZZZZ-
If you should have any questions or require further information regarding this approval, please contact David
Nash of my staff at 919-541-9425 or email at nash.dave@epa.gov.
Sincerely,
Digitally signed by
STEFFAN JOHNSON
cc:
STEFFAN
roHNsoN rffrHil,'
Steffan M. Johnson, Group Leader
Measurement Technology Group
Sara Ayers, EPA/OECA/OCA{AMPD, (ayres. sara@epa. gov)
Melanie King, EPA/OAR/OAQPS/SPPD, (king.melanie@epa.gov)
James Leather, EPA Region 6, (leatherjames@epa.gov)
David Nash, EPA/OAR/OAQPS/AQAD, (nash.dave@epa.gov)
Lucas Ennis
GAS
580-225-0403
info@gasinc.us
Type of Sources Tested:
Stationary lnternal Combustion Engines. 4 Stroke Rich Burn Engines. 2 Stroke & 4 Stroke Lean Burn Engines
Stationary Natural Gas Fired Generators
Stationary Propane Fired Generators
Gas Fired Boilers
Types of Analyzers:. Gasmel DX4000 FTIR. Gasmet Portable Sampling Unit with Zirconium Oxide 02 Sensory. Testo 350. Flame lonization Detector
Qualilications:
Trained, studied, and fully demonstrates compliance for emissions testing via data collection outlined in the
following Reference Methods:. EPA Method 1 & 1A - Sampling & Traverse Points. EPA Method 2 &2C - Velocity & Volumetric Flow Rate of a Gas Stream. EPA Method 3A - Oxygen. EPA Method 7E - NOX. EPA Method 10 - Carbon Monoxide. EPA Method 25A- Volatile Organic Compounds. ASTM D6348 - Extractive Fourier Transform lnfrared Spectroscopy
Conducts emissions testing on a weekly basis including, but not limited to, the following test types: lnitial
Compliance, Biennial Compliance, SemiannualCompliance & Quarterly Compliance. Alltests performed
are in accordance to any and all Federal & State requirements as applicable (i.e. JJJJ, ZZZZ, 106.512, 117,
PEA, etc.). Performed testing in Colorado, Utah, Wyoming, North Dakota, Montana, Kansas, New Mexico,
Oklahoma, Texas, Louisiana (land and off-shore), Arkansas, Ohio, Pennsylvania, West Virginia, New York,
Kentucky, & Mississippi.
. Quarterly Performance Reviews covering ongoing changes with Federal Regulations, State
Compliance guidelines, & site-specific safety certifications.
GAS
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40 CFR Part 60 Subpail JJJJ
Performance Test Report
Test Type: lnitial
Test Date: 1U2M2O23
Source:
Waukesha H24
Rich Burn (4 Cycle)
Serial Number:1663358
Engine Hours:3600.2
Location:
Duchesne Data Genter Power Station
Duchesne County, Utah
Prepared on Behalf of:
Grusoe Energy Systems, !nc.
#As
ureH oTPIRTIUENT oF
uvt noru ut= ttIAL-aUAL!ry
303 W. 3rd St (580) 22s-0403 Elk City , OK73644
lndex
1.0 Key Personnel.... ............. 3
2.0 Sampling System..... ....... 3
3.0 Methods Used............ ......................... 3
4.0 Test Summaries.. ............ 5
5.0 Run Summaries.. .......,,,,, 6
6.0 Volumetric Flow Rate Data.... ............. 7
7.0 Calculations.............. ...... I
8.0 Orygen Calibration... ...... I
9.0 Engine Parameter Data Sheet.. .......... 10
10.0 QA/QC Results........ ........ 11
11.0 D6348 Annexes...... ."...... 12
12.0 Signature Page........ ....... 18
13.0 Appendices.............. ....... 19
14.0 Bottle Certs............ ......... 20
1s.0 GAS ALT 141_FTrR EPA......... ...........25
16.0 Tester Qualifications (resume)... ......... 27
17 0 Raw Data .
i;i;;
.......... 28
Table 5.1 (Run Summaries)............. ........... 6
Table 6.1 (Volumetric Flow Rate Data)............ ............... 7
Table 6.2 (Stack Gas Measurements)......... ....................7
Table 8.1 (Oxygen Calibration).. ................. I
Annex Table 1.2.1 (Certified Calibration Bottle Concentrations)......... 12
Annex Table 1.2.2 (Measurement System Capabilities)..................... 12
Annex Table 1 .3. 1 (Test Specific Target Analytes)............................. 1 3
Annex Table 4.1 (Measure System Capabilities) ............ 15
Figures
Figure 6.1 (Location of Traverse Points per Method 1)....................... 7
Annex Figure 1.4.1 (Sampling Train)..... ..... 13
Annex Figure 1.4.2 (Sampling Points)... ...... 14
Annex Figure 1.4.3 (Sampling Port Locations).... ............ 14
Appendices
Certified Calibration Boftle Certificates............. ...............20
GAS ALT 141_FT|R EPA............. ............... 27
Tester Qualifications (resume)... ................. 27
Raw Data.... ........ 28
1.0 Key Personnel
GAS, !nc.
Crusoe Energy Systems, lnc.
Lucas Ennis
Kody Walters
2.0 Sampling System
The sampling system used consisted of a Stainless steel probe, heated Teflon line, gas conditioning
system, and a Gasmet model DX4000 FTIR analyzer. The gas conditioning system used was a Gasmet
Personal Sampling System with a Zirconium Oxide oxygen sensor.
3.0 Methods Used
ASTM D6348-03
This extractive FTIR based field test method is used to quantity gas phase concentrations of multiple target
analytes (CO, NOX, CH2O, & VOC's)from stationary source etfluent. Because an FTIR analyzer is
potentially capable of analyzing hundreds of compounds, this test method is not analyte or source specific.
The analytes, detection levels, and data quality objectives are expected to change for any particular testing
situation. lt is the responsibility of the tester to define the target analytes, the associated detection limits for
those analytes in the particular source effluent, and the required data quality objectives for each specific
test program. Provisions are included in this test method that require the tester to determine critical
sampling system and instrument operational parameters, and for the conduct of QA/QC procedures.
Testers following this test method will generate data that will allow an independent observer to verify the
valid collection, identification, and quantification of the subject target analytes.
EPA Method 1 & 1A
The purpose of the method is to provide guidance for the selection of sampling ports and traverse points at
which sampling for air pollutants will be performed pursuant to regulations set forth in this part.
EPA Method2 &2C
This method is applicable for the determination of the average velocity and the volumetric flow rate of a gas
stream. The average gas velocity in a stack is determined from the gas density and from measurement of
the average velocity head with a standard pitot tube. Velocity readings are taken from each stack at 16
separate traverse points (Table 6.1) and used to determine the engines mass emissions rate, calculated
utilizing the formulas seen in section 7.0 of this report.
EPA Method 3A
This is a procedure for measuring oxygen (O2) and carbon dioxide (CO2) in stationary source emissions
using a continuous instrumental analyzer. Quality assurance and quality control requirements are included
to assure that the tester collects data of known quality. Documentation to these specific requirements for
equipment, supplies, sample collection and analysis, calculations, and data analysis will be included.
Gas, lnc.
4.0 Test Summary
Unit with a serial number of 1663358 which is a Waukesha H24 engine located at Duchesne Data Center
Power Station and operated by Crusoe Energy Systems, lnc. was tested for emissions of: Carbon
Monoxide, Oxides of Nitrogen, and Volatile Organic Compounds. The test was conducted on 1212012023
by Lucas Ennis with Great Plains Analytical Services, lnc. All quality assurance and quality control tests
were within acceptable tolerances.
The engine is a natural gas fired Rich Burn (4 Cycle)engine rated at 530 brake horse power (BHP)at
1800 RPM. The engine was operating at 440 BHP and 1552 RPM which is 83.00% of maximum engine
load during the test. The test HP calculation can be found on page 8. The engine was running at the
maximum load available at the test site.
This test will satisfy the testing requirements for 40 CFR Part 60 Subpart JJJJ.
Site Verification Photos
Gas, lnc.
4.0 Test
Gas, lnc.
6
5.0 Run Summaries
Table 5.1 Run Summaries
Gas, lnc.
6.0 Volumetric Flow Rate Data
Table 6.1. Data used for volumetric flow rate (Method 2)
7
Pltot Tube Coefllclent CD(stdl= .99
sracx otamerer = b nches or:.5 Ieet. or:.2 Square Feel
H20 o/od 16.24 16.39 16.31 16.31
co2 o/od 9.25 9.34 9.3U 9.30
02 o/od 0.53 0.45 o.37 0.45
GO ppmd 18.05 14.27 '17.54 16.62
Molecular Weiqht Stack Gas dry basis I mole 29.50 29.51 29.50 29.5't
Molecular Weiqht Stack Gas wet basis (Ms q/o mole 27.63 27.63 27.63 27.63
Stack Static Pressure 'H20 0.62 0.52 o.47 0.54
Stack Static Pressure "Hq 0.05 0.04 0.03 0.04
Atmospheric Pressure at Location (Pbar MBAR 828.63 828.03 828.72 828.46
Atmospheric Pressure at Location (Pbar "Ho 24.47 24.46 24.48 24.47
Absolute Stack Pressure (Ps ,Hq 24.52 24.s0 24.s'.l,24.5'.1
Stack Temperature Deq G 441.11 442.78 438.89 440.93
Stack Temperature Deq F 826.00 829.00 822.00 825.67
Stack Temoerature Deo R 1285.67 1288.67 1281.67 1285.34
Stack Gas Velocity rusec 91.57 84.57 79.82 85.45
Stack Flow Rate Q cfs 17.98 't6.61 15.67 16.78
Stack Gas Wet Volmetric Flow Rate scf/hr 21783.37 20053.34 19042.81 20325.68
Stack Gas Dry Volumetric Flow Rate scf/hr 18245.21 16766.20 15937.50 17009.78
Emissions Samolino Points lnches
Sinole Point Samolino Used 6 inches and Under 3
uamDle afler EacK ruroe.o.46
Within 5% of Last Aostd readinq:YES
measured with a standard tube use for Volumetric Flow Rate
Flgure 6.1
16 Traverse Points Were Used
Table 6.2. Stack gas pressure rea
Aostd = Velocitv head measured bv the' standard pitot tube, (in.) H2O.'
stack L,rameter (tnchesl 6.OO
lnches upstream lrom disturbance 48.00
lnches downstream from disturbance 32.00
Pitot readings are taken for Method 2 calculations using measuring points outlined in Method
'The exhaust stack dld not prEsent cyclonlc flow condltlons at the sampllng locauon due to the
absence of cyclones, lnertla! deml3te,!, venturl scrubbei!, or tangentlal lnlets.
'Cyclonlc Flow Check (Pass/Fall): PASS
Gas, lnc.
7.0
Method 2: Determination of Stack Gas Velocitv and Volumetric Flow Rate
*Note- Use of this method neqates the need for any fuel related numbers for emissions calculations
Ap(avg) = Velocity head ol stack gas, mm H2O (in. H2O).
3600 = Conversion Factor, sec/hr.
A = Cross-sectional area of stack, n2 (ll2).
Bws = Water vapor in the gas stream (from ASTM D6348)
Cp(std) = Standard pitot tube coefiicient; use 0.99
Kp = Velocity equation constant.
Md = Molecular weight ol stack gas, dry basis, g/g-mole (lb./lb.-rnole).
Ms = Molecular weight of stack gas, wet basis, g/g-mole (lb.flb. -mole).
Ps = Absolute stack pressure (Pbar+ Pg), mm Hg (in Hg)
Pstd = Standard absolute pressure, 760 mm Hg (29.92 in. Hg).
Qsd = DU volumetric stack gas flow rate corrected to
standard conditions, dscm/hr. (dscf/hr.).
Ts(abs) - Absolute stack temperature, oK ("R). = 460 + Ts for
English units.
Tstd = Standard absolute temperature, 293"K (528'R).
Vs = Average stack gas velocity, m/sec (ft./sec).
Md = ./t4(.093)+.32(.006)+.28(.899+.002) = 29.5O2 LB/I-B-MOLE
lyls = Md(1-Bws)+18.o(Bws)Ms = 29.502(1 -.16243)+.18.0(.16243) = 27.634 LB/LB-MOLE
vs = 85.+9'.99-y'62'{(zgs.6zt(24.s2'2z.694ll = 91 .57 FTlsEc
Qsd = 3600(1 -Bws)Vs'A(frstd'Ps)/fis(abs)'Pstd))Osd = 3600(1-.162)91.s6s'.196(s28'24.s211 1128s.67'29.921) = 1824s.21 DSCF/HR
Q = Qsd135.315 Q = 18245.2OG135.315 = 516.il2 DSCM/HR
Emission Rates (Examoles use CO Run 1
453.6= Conversion factor lb. to gram HP= fnglngs rated Horsepower
A = Cross-sectional area of stack, m2 (ftz). Mfg.= Manufacturer Exhaust flow rate at 100% (ft3/min)
BHP/HR. = Brake work ol the engine, horsepower-hour (HP-HR.). 02 = Concentration ol orygen on a dry basis, percent.
BTU/HP-HR. = Brake Specilic Fuel Consumption (HHV) ppm- Parts Per Million (CO)
ER = Emission rate ol (CO) in g/HP-hr. ppm@15% 02= PPM corrected lo 15%02
F(d )= Volumes ol combustion components per unit of heat Qsd = Dry volumetric stack gas flow rate corrected
content, scm/J (scf/million Btu). to standard conditions, dscm/hr. (DSCF/HR.).
Q = Stack gas volumetric flow rate, in standard cubic meters Run Time = Run Time in Minutes
per hour, dry basis Tpy= Tons peryear
LB/HR.= Emission rate of (co) in LB/HR. vs = Average stack gas velocity, m/sec (ft./sec).
Molwt.= MolWeight ol CO (28.01)
ppm @ 15% 02 = PPM'((20.9-15VoO2)t(20.9-O2l)ppm @ 15% 02 = 21 .549'(20.9-15)(20.9-,6%)) = 6.209 PPM @ 1 5% 02
g/hphr = (PPM'(1 . 1 64'1 043)'Q.(Run Time/60))rBHP/H R (21.549'(1.164-10^-3f51 6.il2-(Run Time/60))t429.3 =.03 c/HP-HR
LB/HR = .03'1/453.6'429.3 = .029 LB/HRlb/hr = ER'1 /453.6'BHP-HR
TPY = .029'4.38 = .127 TPY
ppm wet - (1(1-H2O) = ppm dry 21.55 = 18.049'(1(1-.16))
Gas, lnc.
8.0 Oxygen Calibration 9
8.1 Calibration error test; how do I confirm my analyzor calibration is corroc{? After the tester has assembled, prepared and calibrated the
sampling system and analyzet, they conduct a 3-point analyzer calibration error test before the first run and again after any failed system bias test or
failed drift test. They then introduce the low-, mid-, and high-level calibration gases sequentially in direct calibration mode. At each calibration gas level
(low, mid, and high) the calibration error must be within + 2.0 percent of the calibration span.
8.2 lnitial systom bias and systsm calibration orror chocks. Before sampling begins, it is determined whether the high- level or mid-level
calibration gas best approximates the emissions and it is used as the upscale gas. The upscale gas is introduced at the probe upstream of all sample-
condltioning components in system calibration mode.
(1) Next, zero gas is introduced as described above. The response must be within 0.5 percent ofthe upscale gas concentration.
(2) LowJevel gas reading is observed until it has reached a final, stable value and the results are recorded. The measurement system will be
operated at the normal sampling rate during all system bias checks.
(3) lf the initial system bias specification is not met, corrective action is taken. The applicable calibration enor test from Section 8.2.3 of EPA
Method 7E is repeated along with the initial system bias check until acceptable results are achieved, after which sampling will begin. The pre-
and post-run system bias must be within t 5.0 percent of the calibration span for the low-level and upscale calibration gases.
8.3 Post-run system bias chsck and drift asssssment - confirming that each sample collected is valid. Sampling may be performed for multiple
runs before performing the post-run bias or system calibration error check provided this test is passed at the conclusion of the group of runs. A failed
final test in this case will invalidate all runs subsequent to the last passed test.
(1) lf the post-run system bias check is not passed, then the run is invalid. The problem is then diagnosed and fixed, then another calibration
enor test and system bias is passed before repeating the run.
(2) After each run, the low-level and upscale drift is calculated, using Equation 7E-4 in Section 12.5 from EPA Method 7E. lf the post-run low-
and upscale bias checks are passed, but the low-or upscale drift exceeds the specification in Section 13.3, the run data are valid, but a 3-point
calibration error test and a system bias check must be performed and passed prior to additional testing.
Table 8.1 Oxygen Calibration
Method 7E 3.4 To the extent practicable, the measured emissions should be between
20 to 100 percent of the selected calibration span. This may not be practicable in some
cases of low concentration measurements or testing for compliance with an emission
limit when emissions are substantially less than the limit.
EPA Method 3A CliA Worksheet
Certlfied Gac Concentr.lon I Ceilmod Ger Concentrelon I Cortlfbd Ga. Co
Low.Level (%) I ltlld.Level (%) | Hlgh.Levo
flOO'/
(DIRECT) Analy.er Callbrallon Error (3 2olo)
Llnoaritv Check
ncentralon
7E 8.5: Note: that you may
risk sampling for multiple
runs before performing the
poslrun bias provided you
pass this test at the
conclusion of the group of
runs
Certfied
Concentralion
Value (%)
Dircct
Calibration
Response (%)
Absolute
Difrerence (o/o)
Analfzer
Calibration
Enor(%)
Zero Gas %0.00% 0.00%0.00% 0.00%
Mid-Level Gas %
High-Level Gas %
9.04o/o
20.700h
9.03%
20.510/"
0.00%
0.190/o
o.o2%
0.90%
(SYSTEM) Calibration Bias Checks (S 5%) and Drift Ghecks (S 3%)Upscale Gas 9.Mo/o
Zero Offset 0.00%
Bias Pre lnitlal Value Bias Post lnilal ValuesSpan 20.70
Analyzer
Calibration
RespoNe (%)
Zero Gas 0.00%
Systcm
Calibralions
Rasponse Pre
(%l
iystom Bias (9(
of Span) Pre
Syst6m
Calibration
Response Pcst
(ohl
Systam Elias (%
of Span) Post
Dffi(%of
Span)
0.00%0.000/"0.000/.0.00% 0.00%
Upscale Gas 9.03o/o 9.02Yo 0.0s%9.02o/o 0.06%0.00%
(SYSTEM) Calibration Bias Checks (S 5%) and Driff Check (S 3%)
Avg. Gas Concentration (Run 1)0.84% Effluent Gas (Coas) Run 1 0.il%
Avg. Gas Concentration (Run 2)0.il6h Effluent Gas (Cgas) Run 2 o.*%
Avg. Gas Concentsation (Run 3)0.45o/o Efflueni Gas (Cga8) Run 3 o.450/"
EPA Method 3A Cl,A Worksheet
Zero Gas 100o/o Nikogen
Mid-Level Gas 9.04o/o
High-Level Gas 20.7004
Zero Gas o/o
Mid-Level Gas %
High-Level Gas %
zero Gas % ]-o%-l upscare used
upscate Cat I g.ozy" | 9.04o/o
zero Gas y" f];iill upscar€ us€d
Upscate Cal I g.oz* | 9.O4yo
Gas, lnc.
10
9.0 Engine Parameter Data Sheet
Run 1 Run 2 Run 3 Completed
Company Grusoe Enerqy Systems, lnc.
Faclllty lJuche8ne Data Center Power Station
Date 12t20t2023
SIte Elevatlon (ft)5844
Unlt lD
Make Waukesha
Model t124
Serial Number 16633s8
Technlclan Lucas Ennis
Run Start Tlmes 01:31 PM 02:46 PM 03:58 PM 05:28 PM
Enolne Hours 3591.2 3598.2 3599.2 sejuu.z
Englne Parameter Data
Run 1 Hun 2 RUN 3 Averaqe
EnElne Spe6d (RPM)r 552.O 1550.O 1554.O 1552.0
htake Manllold Pressure (Dsl)37.9 36.6 3E.E 38.4
lntal(e Manllold TemO "F 12.7 t:z.J.1 tzz.z 86.O
ENEINE LOAd (EHP}429.3 44C.2 +45.2 439.9
Amblent Temp "F 40.0 41 .O 40.o 40.3
Humldlw%46.0 44.O 47.O 45.7
DEW POINT "F 21.O 21.O 21.O 21.O
AFR Manufacturer/Type Waukesha Waukesha waul(esha waul(esha
sucilon Pressure 73.2 75.3 14.9 t4.5
Dlscharqe Pressure 3U'l 379.2 379.1 380.0
catalvst (Yes or N0 Yes
cataNst Manulacturer GE GE GE GE
# oI Catary$ hstalled 2 2 2 2
Catalyst lnlet Temp'F 1126.0 1125.0 1125.0 1125.3
Catalyst Outlet Temp oF 1078.0 1080.0 1078.0 1078.7
Catalyst Pressure Drop H2O 6.0 6.1 6.1 6.1
Gas, lnc.
11
10.0 OA/OC Results
Time
Spike Reported
Spike Expected
Value:249.61
Value: 251.00
System Zero Response Time
System Response Time 45 seconds
Nitrogen monoxide NO
Nitrogen dioxide N02
NOx
voc
Average:0.00
Average:0.00
Average:0.00
Average:0.55
Average:0.00
CTS Compound Concentration Avg
Tolerance
Ditference between measured and expected
Value:100.00
Value:98.56
2.O00/o
1.44o/o
Nitrogen monoxide NO
Nitrogen dioxide N02
NOx
voc
Oxygen
Average:0.00
Average:0.00
Average:0.00
Average:0.00
Average:0.47
Average:0.00
CTS Bottle Concentration
CTS Compound Concentration Avg
Tolerance
Ditference between measured and expected
Value:100.00
Value:97.7O
5.00%
2.30o/o
Gas, lnc.
11.0 D6348 Annexes 1-8
The test quality objectives completed for the emissir
4, 5, 6, 7 & I as layed out per ASTM D6348-03. All
were within acceptable limits. Data generated durin
summarized below in order of the distinctive Annex.
s test are demonstrated throughout Annexes 1,2,3,
rference methods, pre-test and post test procedures
the pre-test and post-test procedures are
analyte concentrations are the average of each test
second measurement was the average of 600 scans.
rex 5 Spiking Technique due to Propane being the
rcess of natural gas. Additionally, the molecular
of VOC's per the EPA.
Three 60 minute test runs were performed. The fi
run. Data was taken at 60 second intervals. Each
Propane is used as the surrogate compound for the
VOC that is most commonly f-ound in the combustior
weight of Propane coincides with with molecular we
Annex Table 1.2.1 Certlfied Bottle Concentrations
Annex fable 1.2.2 System Capabllltles
I
I
I
9"'
I
t
I
, lnc.
13
1.
Annex Table 1.3.1 Test Specific Target Analytes and Data Quality Objectives
Compounds
Infrared
Analysls Reglon
(cm-l)
Erpected
Concentratlon
Range
Measuremenr
System
Achlevable
Mlnlmum
Detectable
Concentratlons
Hequrreq
Measurement
System
Accuracy and
Preclslon for
fest Annllcatlon
CO 2000-2200 0-1200 oDm 0.16267 Dom 4 oDm
NO 1875-2138 0-'1000 oom 0.4007 oDm 2 DDm
N02 2700-2950 0-100 oom 0.4899 oom 2 oom
voc
2600-3200
0-100 ppm 1.8520 ppm Total
VOC'S 1 ppmperVOC910-1 150
2550-2950
cH20 2550-2850 0-100 DDm 0./6/6 DDm 1 DDm
lnterferlng
Compounds
* CO is analyzed in a separate analysis region than CO2 and H2O
co2 926-1 150 O-1Oo/o o,/o nla
Water Vapor 3200-3401 O'22o/o O.zOYo nla
* VOCs compiled of Acetaldehyde, Ethylene, Hexane, and Propane.
.4
{-HtF_
Figure Annex 1.4.1 Sampling Train
The testing instrumentation is housed in an enclosed vehicle which is located approximately 45 feet from the source. A
heated sample line (sixty feet in length) is attached to the inlet of analyzer system and the source effluent discharges
through the FTIR outlet.
1
ffi
GAS
STACK
Gas, lnc.
14
Central Sampling Point
Location in lnches
TRI.PROBE SAMPLE POINT L
AS PERCENTAGE OF STACK
SAMPLE
BY DISI
Flgurc Annex 1.4.3 Sample Port Locatlon
Sampllng Points
LOCATION DETERMINED
FROM USruRBANCE
Flgure Annex
lnterior Stack
lnches
Upstream:
48
lnches
Downstream:
32
NEA#,' *
nerfi.s:
MDC#1 : *'n&" * cr?-rLrar
RE F rr' L""tt
7'717,5
calDrafl on Tranaler Standard ExDected ueasuled Path Lenqth Yaladated
tsthvlene r(x)98.56 4.924 Passed
Annex Table 1.2.2 Measurement System Capabllltles
Gas, lnc.
Parameter Gas Concentratlon ifeasur6d 70 Dffierenee specatrcatIon vdtdated
Spike Direct
Propane 25't.000 ztu.51z o.19"h +l- 2"h HASS
SF6 9.730 Y.b44 O.EE%+l- 2"h Pass
co 501.400 4Y4.t 1.32"/o +l- 2o/o PaSs
NO 252.400 z4t.E32 1.81"/o +l- zYo PaSs
SDike Run 1 vla tho Svstem
Source Output splke AveraEe Dilution Factor Expectecl 70 ReCOvery specification
Propane 0.025 z1 19.977 109.010%7O'13O"/o
SF6 0.000 o.767 7.953"/o 11Oo/o
Splle Run 2 vla the System
Source Output spil(e Average Dilution Factor Expected 70 ReCOvery Specilication
Propane o.o00 22.564 f 20.055 112.51O4/o 70-130%
SF6 0.000 v.t t1 7.995Vo 11U"/o
sDlKe Hun 3 vla the svstem
Source Output spil(e Average Dillrtlon Factor Expected 70 ReCOvery specllicailon
Propane 0.000 z1 tY4 19.578 1.32OYo 70-130y"
SF6 0.000 u. /55 7.8O8"/o 11Oo/o
Noise Equivalent Absorbance (NEA)
RMS High 0.000445
RMS Mid 0.00',1823
RMS Low 0.001065
Line Position
20$2 2069 :046 2023 1999',]976 1953 1930'X807 18S4 1861 1837 181{
pass
Gas, lnc.
n 1(
010
nntr
005
n 1n
c00
005
@ o.oo% Pass
The Gasmet GICCOR (Genzel lnterferometer with Cube Corner Retroreflectors) interferometer is specially
designed for maximum optical throughput and maximum signal to noise ratio of 7.72 (cm-1) remaining
stable with any vibration and temperature changes.
a low resolution spectrometer where the aperture is fixed to a maximum angle
setting and the detector linearity was tested with an alternate approach. A three point linerarity of the CTS
gas was performed and validated.
Linearity
1 58 5898
148 5898
1 38 5898
128 5898
1 18 5898
108 5898
oa <Qoa
88.5898
78.5898
68 5898695 687
158.5898
148.5898
138 5898
128 5898
1 18.5898
108 5898
98 5898
88.5898
78 5898
68 5898610 602679 672 664 656 648 64.1 633 625 618
1s.2439047
The analytical accuracy of the quantification algorithm is satisfied via the results from Annex 5 per Annex
7.6
POST GTS Ststem Ghecl(:
u I ti E oTlte uoncenlraton.100.oo
u ru lramDre uoncemralton Averaqe:99.O1
umerence between measured and exoected:.UU-/o
I Oterance:5.OO7o
BUn Uata Yalloaflon - Automated v3 tanual Roadlno valldated Gomrnonts
Run 1 Points 1 & 2 on CO/NO/Prooane Allwithin 20%Passed uemonstrates no rntenerences oDserved,
Run 2 Points 1 & 2 on CONO/Prooane All wlthln 2O7o Passed L'emonstrates no rntenerences observed
Run 3 Points 1 & 2 on CO/NO/ProDane Allwithin 20%Passed Demonstrates no interferences observed,
Gas, lnc.
18
12.0 Slgnature Page
Job/Flle Name: Crusoe Energy Systems, lnc.;
-#e,ffi+$ &v :.8E
*
We certify that based on review of test data, kno
conducting this test, we believe the submitted inl
psne Data Center Power Station; ;JJJJ
\ {^-'qk;h
ra nf lhnea inr{ivir{rralc diraatlv racnnncihla fnr
rdilon to be accurate and comilete.
Company: G.A.S. lnc.
Print Name: Chris Oppel
Title: Director of Stack Testing
Signature:
uq^<
PhoneNumber: 580-22$'0403
Dale:12120f2O23
Company: G.A.S. lnc.
Print Name: Lucas Ennis
Title: Emissions Specialist
Dale:1212012023
Gompany:
Print Name:
Signature:
Tifle:
Phone Number:
Date:
lnc.
Appendices
Gas, lnc.
Spike (5 Gas)
Airgas.
AirtaSpeddtycuB
Airgs USA LI-C
1222 S, Wentworth Ave.
Chic{8o, IL 60628
AirgB.@m
Part Number:
Cylinder Number:
Laboratory:
PGVP Number:
Gas Code:
CERTIFICATE OF ANALYSIS
Grade of Product: EPA PROTOCOL STANDARI)
805N194E15AC014 Reference Number: *402601324-1
CC142828 Cylinder Volume'. 147 .O CF
124 - Chicr.go (SAP) - lL Cylinder Pressure: 2015 PSIG812022 Valve Outlet: 660
CO,CO2,NO,NOX,PPN,BALN Certification Date: Oec06,2022
Date:
Cdlifi@tir pstorhcd in .@rdane with 'EPA TEeability Preb@l turAssy .nd Clrlifatio of GasM CslibrafM Slend.rds (Msy 2012) d@ment EPA
600/R-12/531, 6ing th. .$.y peeduEs listld. Anelytiel M.hodology dG mt EquiE ffiir hr amtytiel inbrbB@. Thb cylinda has e total ssMhd
une.taint s steH bebw wih a ffifidanB lewl of 95%- ThcE eE no sigdfer( impurilie6 $!ki 6f*'t thc u* of lhb calibdion mituE. Al 66batids eE oh a
molcJmole ba5b unle$ othwise noted. The Gults Elat6 ory io the itere Ectcd. Thr ropon shalt nd bc EpEdu@d erept hr full wi0ujt 6pplMl of the laboEtory. Oo
Trlad Data Avallable Upon Request
PERMAT{ENT NOTES:Mixture contains nominal 10ppm Sulfur tlexafiuoride as a tracer component Aciual
tested value included within the original Certificate of Analysis. Contact the Airgas laboratory if a reprint is
required
NOTES:Mixture contains nominal 10ppm Sulfur Hexafluoride as a tracer component. Aciual tested value
included within the original Certificate of Analysis. Contacl the Argas laboratory if a reprint is required.
SF6 Results:
JMR137-9.73[PPMn r r n n rl n I
FN
Approved for Releare Pr!. I ot I
Compononl
ANALYNCALRESII'LTS
Requestod Ac'tual Protocol Total Relatlve
Concentra0on Conc.ntrrtlon Method Uncert lnty
A$.y
Dates
NOX 250.0PPM 253.0PPM Gl +/-1.2%NISTTE€able 1112U20?2,121O81202.
N|TRIC OXIDE 250.0 PPM 252.4PPM Gl +/- 1.0% N|ST TEffible 11t2812022,1?i06t2022
PROPANE 250.0 PPM 251.0 PPM G1 +^ 0.7% NIST TEeabb 1'113U2022
CARBON MONOXIDE 500.0 PPM 501.4 PPM Gl +/- 0.6% NIST TBffibte 11129/2022
CARBON DIOXIDE 5.m0 % 5.025% c'l +/- 1.4% NIST TEeable 11t2U2022
NITROGEN Bdane
CALIBRAIIONSTANDARDSType Lot lD Cyllndor No Concentratldr Unc€i.lnty ErDlratlon Dato
EB0113125 250.3 PPM NtIRtC OXTDE/NtTROct
D685025 9,9lPPMNITROGENDIOXIDE/AIR
+/- 0.8%
+l- 2.oor'"
+l-2.0%
+/- 0.5%
+/- 0.6%
+/- 0.6%
tu 29, 2026
Feb20,2020
Feb 18,2023
Mar 17,2027
Jlt03,2024
May 14,2025
NTRM 200503-31
PRM 12386
GMIS 401423838104 CC505590 4.373 ppM NTTROGEN O|OX|DSNITROGEN
NTRM 200602-13
NTRM 13010109
NTRM 13060423
6162697Y 243.3 PPM PROPANE/AIR
KALOO3925 495.4 PPM CARBON MONOXIDE/NITROGEN
cot't3685 7.489 % CARmN DIOX|DE/N|TROGEN
The SRM. NrRM. PRM. d RGM notsd ebove 16 onlv in r6f6r6n6 to lh. GMIS md ln the s$v.nd hot Bd dh
ANALYTICALEQUIPMENTlnstrumonutake,Uodol Analytbrl PdnclDlo Lr3t ilultDolnt Callbr.tlon
Ni@let lS50 AUP2010242
CO-1 SIEMENS ULTFAMAT6E N1J57OO
Ni@lei iS50 AUP2010242
Ni@let iS50 AUP2010242
Ni@let iS50 AUP2110277
NN07,2022
NoY 28,2022
Dec.05,2022
D@05,20?2.
NN O7 2022
FTIR
NDIR
FTIR
FTIR
FTIR
Gas, lnc.
Airuas.
d Ar Lqurd€ cmpany
9% O2INO2
AirtuSpccidtyGu6
Ail8a USA Ua
525 North Induskial Inp Road
T@le, UT84074
Ahza.@m
CERTIFICATE OF ANALYSTS
Grade of Product: EPA PROTOCOL STANDARI)
Part Number:
Cy,linder Number:
Laboratory:
PGVP Number:
Gas Code:
E03N|90E15W0003
cc517745
124 - Tooele (SAP) - UT
872023
NO2,02,BALN
Reference Numb€r: 153.402786436-1
Cylinder Volume: 145.0 CF
Cylinder Pressure: 2015 PSIG
Valve Outlet 660
CertificationDate: Jul13,2023
trEL./molc b.dr mLs odlwiec mtad. Tha cuh6 roleta illy io tha lbm Hcd. Th. Epod 3hall
Td.d Drt Avrll.ble Upon Roque3t
Approved for Rslearo
h tull withdit +plwl of th. l.boEtory. Do
Prg! I ol I
Cst'fi€tdr pdturrud an .@rdan@ wilh 'EPA TE€.bility PDb@l br Assy.nd C€rtifetid of G.ffi C.lioctih Sf.nd{d8 (M.y 2012)' d@mnt EPA
6{XrlR-12/531. Eing the .sy pl@duE8 listld. Amlyth.l M.hodology dG not Equh! mdon tu eBlyli:.|inbrftGr. Thb cylindd has a tdc .nstfi6l
un€ti.inty s. st bd b.k , wlth . ffilldcne l.wl of 95%. Th.E .E rc Bilrnifont impuitior wfiiirr alt c{ tho us of thb cdib..lhn mixtuE. Al m@ffiida .E m a
Not t 8. Thb 1(x)i.c. 0.7
ANALYTICAL REST,'LTS
Raquested Acfual Protocol Totrl Rola0ve
Conc.nt.flon Concontreflon U.thod Uncortdnw
Comporenl Arsay
Datos
NITROGENDIOXIDE 100.0PPM 10'|.9PPM Gl +/-2.0%NlSTTEeable O7l06,lm23,O7l1WO23
OXYGEN 9.000 % 9.037 oh Gl +/- 1.0% NIST TB€able 07106112023
NITROGEN Balane
CALIBRATIONSTANDARDS
Typc Lot lD Cyllndcr No Concont luon Uncort lnty Erplratlon Dat
D887373
SG9,I61286BAL 12.05%OXYGENNITROGEN
TIESRU.NTRM.PRM.dRGMmtd.bosl.onlvlnr.tffi6blh€GMISuodlnlh6*vanddMdolth.
Nov 09, 2025
Frb 23, 2023
Occ 14,2023
GM|S 153/,02022601 CC517858
PRM 12420
NTRM 98051010
10,I.1 PPM NITROGEN DIOXIDE/NITROGEN
98.9 PPM NITROGEN DIOXIDE/NITROGEN
1.1%
1.0%
o.7%
lnatrumonutak modd
ANALYIICAL EQTIIPMENT
Analttc.l PrlnclDls L!3t tultlpolnt Callbrltlon
FTIR
02 PaEmaqnctic (DXON)
Jun23,2023
Jun29,m23
MKS FT|R NO2 018143349
Horibs MPA€10 W603MM58 02
Gas, lnc.
Airgas.
eArtj(iido drprry
CERfIFICA OFAIYALYSIS
Grade of PRIMARYSTAIVDARI)
etrIlrrepcalvOrrcl
AiTfUUSAIL
rrra g.WattmfthAE.
Ctiafo, lL5o6a8
fftsgtm
Rafarcnce Number WO281137U1
Cllindervolume: 14/..0 CF
CyllnderPr€ssurs: 2015PS|GVahooude* 350
+l-1L
P.go t ort
Cu3bmor
Part Numbel:
Cy,linder Numbel:
Laborabry:
Anailols Date:
Lot Numbel:
ETHITENE
NITROGEN
GREAT PI.AINS AMLYTICAL
x02Nr99P1sACVH8
ccfi7503
12a - Chlcago (SAP) - lL
tug 15,2023
5/-40,2811378.',|
E:elradon Dtr:
100.0 PPM
Balenca
15,2081
Primary Standard @s Minres are traceaHe b . wdghts and/fr i{.LS.T. G6 Mbtur€ r€ftren@ maElrials,
ANAL RESI[[IS
Component Req Gonc Goncentratlon Analytca!
Unccrtalnty
ilort3GREAT PI-AINS AIIIALYTICAL, CERTIFIEO BY FflR
alff.luriltl.
Appronrd ior Roloao
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CERTIFICATts OT AATCH
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Gas, lnc.
Airgas
an Ar LqurcE compsy
21% 02
Airt8SFcidtycrE
Airgs USA Lrc
525 North Indushial I@p Road
Tmle, UT 84074
Arrte,@h
CERTIFICATE OF AIVALYSIS
Grade of Product: EPA PROTOCOL STANDARI)
Part Number:
Cylinder Number:
Laboratory:
PGVP Number:
Gas Code:
E02Nl79E15A00Bl
cc76460
124 -loo,ele (SAP) - UT
872023
02,BALN
Reference Number 153402783621-1
CylinderVolume: 146.0CF
Cylinder Pressure: 2015 PSIG
Valve Outlet: 590
Certification Date: Jul 05,2023
Date:
Cdlifietkh pstomed in a@dane wilh 'EPA TEeabillty Prcto@l tor Assy.hd Ccitifetiil of G.ss CalibEiim SEnd*ds (Mey 2012)' d@hili EPA
600/R-1 2,/53l , 6ing thc .say pmeduE6 listed. AnaMi€l Mcihodology dcs not EquiE omcliril 6. anatytiel interlbE@. This cylinda has a toial .n.Micel
un@rtainty a8 statad bahw wih s diid.n@ lcwl of 95%. ThcE src no sigrlfent impuriti$ wtil5 affed thc u$ ol thb calibdiril mb&c- All 66htids aE d a
rElc/mole baab unl.s oth.Nia€ nobd. The Gults Elate mly to thc item tcted. Th. rcport shall nd b€ EpEduccd crept in tullwi0tdjt.ppowl of ihe leboEtory. Do
Trlad Data Avallsble Upon Regu.st
SldnrftrE nn f,|.
Approved for Release Prg. I ot I
Component Requested
ConcantEtlon
ANALYIICAI, RT,SI'LTS
Ac-tual Prctocol
Concentratlon fofiod
Tot l Rolatlvo
Uncort lnty
Assay
Dates
oxYGEN 21.OO% 20.70%
NITROGEN Balane
Gl +/- 1.4% NIST Traeable O7|OSD023
CALTBRATION STAIYDARDSType Lot lD Cyllndor No Concsntatlon Uncortrlnty Expratlon Dato
NTRi' 09061434 CC282492 22.53 % OXYGENNTTROGEN 0.4%Mav 13.2025
lnatrumonuuako/todel
ANALYTICAL EQI,'IPMENT
An.lytcll Pdnclple L.3t tultlpolnt Callbrrtlon
Honbs MPA-510 W603MM58 02 02 Psramaon€dc (DIXON)Jun29.2023
Gas, lnc.
UNITED STATES ENVIRONMENTAL PHOTTCTION AGENCY
'JESEARCH
TRIANGLE PARK, NC 87717
March 15,2021
Mr. Jordan Williamson
CEO
GAS Inc.
303 W. 3'a Street
Elk City, OK73644
Dear Mr. Williamson:
We are writing in response to your leffer received on September 17, 2020, in which you request the approval
of alternative testing procedures. The EPA's Office of Air Quality Planning and Standards (OAQPS) is the
delegated authority for consideration of major alternatives to test methods and procedures as set forth in 40
CFR parts 60 and 63 under which your request must be addressed. GAS Inc. is requesting a change to one of
the test methods, ASTM D6348-03, used for conducting performance tests to determine compliance under
40 CFR part 60, Subpart JJJJ - Standards of Performance for Stationary Spark Ignition Internal Combustion
Engines (Subpart JJJJ) and 40 CFR part63, Subpart ZZZZ-National Emissions Standards for Hazardous
Air Pollutants for Perfornance for Stationary Reciprocating Internal Combustion Engines (Subpart ZZZZ).
The change being requested will be used to check detector linearity of the Fourier Transform Infrared (FTIR)
instrumentation used to conduct this method. Specifically, you are requesting that the procedures of section
8.3.3 of Method 320 (40 CFR part 60, Appendix A), another FTIR-based method allowed under Subparts
JJJJ and ZZZZ, be used in lieu of section A6.4.1of ASTM D6348-03 when conducting testing using ASTM
D6348-03 under 40 CFR part 60, Subpart JJJJ and 40 CFR part 63, Subpart ZZZZ.
In your request, you state that this alternative linearity check procedure will produce consistent results when
utilizing either Method 320 or ASTM D6348-03. Additionally, some FTIR instrumentation does not allow
for reducing the size of the aperture in the instrument and, thus, it would not be feasible to properly conduct
the entirety of the ASTM D6348-03 method in its current form using such an instrument.
Based on our understanding of FTIR instrument principles and recognition that the requested alternative
determination of detector linearity is both technically sound and contained within Method 320,we are
approving the requested change. We believe that this alternative is acceptable for use for use in testing all
engines subject to 40 CFR part 60 Subpart JJJJ and 40 CFR part 63, Subpart ZZZZ. Also, we will post this
letter as ALT-141 on EPA's website (atwww.epa.gov/emc/broadly-applicable-approved-alternative-
testmethods) to announce that our approval of this alternative test method is broadly applicable to engines for
the purposes of meeting Subparts JJJJ and ZZZZ.
lf you should have any questions or require further
Nash of my staffat 919-541-9425 or ernail at
regarding this approval, please contact David
STEFFAN
12*850 {}[',00
Group Leader
Technology Group
Sara Ayers, EPA/OECA/OCA{AMPD,
Melanie King, EPA/OAR/OAQPS/SPPD,melanie@epa.gov)
James Leather, EPA Region 6, (leatherj )
David Nash, EPA/OAR/OAQPS/AQAD, (
JOHN
Dlgltally slgned by
SIEFFAH JOHNSOi'|
202t o3.t5
cc:
Lucas Ennis
GAS, lnc.
580-225-0403
info@gasinc.us
Type of Sources Tested:
Stationary lnternal Combustion Engines. 4 Stroke Rich Burn Engines. 2 Stroke & 4 Stroke Lean Burn Engines
Stationary Natural Gas Fired Generators
Stationary Propane Fired Generators
Gas Fired Boilers
Types of Analyzers:. Gasmet DX4000 FTIR. Gasmet Portable Sampling Unit with Zirconium Oxide 02 Sensory. Testo 350. Flame lonization Detector
Qualifications:
Trained, studied, and fully demonstrates compliance for emissions testing via data collection outlined in the
following Reference Methods:. EPA Method 1 & 1A - Sampling & Traverse Points. EPA Method 2 &2C - Velocity & Volumetric Flow Rate of a Gas Stream. EPA Method 3A - Oxygen. EPA Method 7E - NOX. EPA Method 10 - Carbon Monoxide. EPA Method 25A- Volatile Organic Compounds. ASTM D6348 - Extractive Fourier Transform lnfrared Spectroscopy
Conducts emissions testing on a weekly basis including, but not limited to, the following test types: lnitial
Compliance, Biennial Compliance, Semiannual Compliance & Quarterly Compliance. Alltests performed
are in accordance to any and all Federal & State requirements as applicable (i.e. JJJJ, ZZZZ, 106.512, 1 17,
PEA, etc.). Performed testing in Colorado, Utah, Wyoming, North Dakota, Montana, Kansas, New Mexico,
Oklahoma, Texas, Louisiana (land and off-shore), Arkansas, Ohio, Pennsylvania, West Virginia, New York,
Kentucky, & Mississippi.
. Quafterly Performance Reviews covering ongoing changes with Federal Regulations, State
Compliance guidelines, & site-specific safety certifications.
Gas, lnc.
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1
EI
Test Started: 08:51 AM Test Completed: 01:20 PM
#As
State Gompliance Test
Performance Test Report
Test Type: lnitia!
Test Date: 1?fi21n023
Source:
Titan 130
Lean Burn (4 Cycle)
Serial Number: KGl4856
Engine Hours:3538
Location:
Duchesne Data Center Power Station
Duchesne County, Utah
Prepared on Behalf of:
Crusoe Energy Systems, lnc.
- ^r,l'llt o r pn n iturE rtTbF-
E_NyiEq N I,IEIIAIS uA!= irv
JAN - I 2A24
DIVISION OF AIR QUALIry
303 W. 3rd St (s80) 225-0403 Elk City ,OK73644
1.0
2.0
3.0
4.0
5.0
6.0
7.0
8.0
9.0
10.0
11.0
12.0
13.0
14.0
15.0
16.0
17.0
18.0 Raw Data....
Table 6.2 (Stack Gas
Raw Data...
Key Personne|.........................
Sampling System........
Methods Used...............-......
Test Summaries...................
Run Summaries.......................
Volumetic Flow Rate Data......
Calculations
Orygen Calibration...
Engine Parameter Data Sheet.
QA/OC Results........
D6348 Annexes......
Signature Page............
Appendices.
Botile Certs.
Tri Probe Certification via
GAS ALT 14l-FTIR EPA........
Tester Qualifications
Table 5.1 (Run Summaries).............
Table 6.1 (Volumetric Flor Rate
Table 8.1 (Oxygen Calibration).....
Annex Table 1.2.1 (Ceriified Bottle Concentrations).........
Annex Table 1.2.2 (Measurement Capabilities)
Annex Table 1.3.1 (Test Specilic T Analytes).....
Annex Table 4.1 (Measure System
Figure 6.1 (Location of Traverse per Method 1 ).......................
Annex Figure 1.4.1 (Sampling
Annex Figure 1.4.2 (Sampling
Annex Figure 1.4.3 (Sampling Port
Certified Calibration Bottle
Tri Prcbe Certification via GD-031...
GAS ALT 141 FTIR EPA...............
Tester Qualifications (resume).........
2
1.0 Key Personnel
GAS
Crusoe Energy Systems, lnc.
Lucas Ennis
Kody Walters
2,0 Sampling System
The sampling system used consisted of a Stainless steel probe, heated Teflon line, gas conditioning
system, and a Gasmet model DX4000 FTIR analyzer. The gas conditioning system used was a Gasmet
Persona! Sampling System with a Zirconium Oxide orygen sensor.
3.0 Methods Used
ASTM D6348-03
This extractive FTIR based field test method is used to quantify gas phase concentrations of multiple target
analytes (CO, NOX, CH2O, & VOC's)from stationary source etfluent. Because an FTIR analyzer is
potentially capable of analyzing hundreds of compounds, this test method is not analyte or source specific.
The analytes, detection levels, and data quality objectives are expected to change for any particular testing
situation. lt is the responsibility of the tester to define the target analytes, the associated detection limits for
those analytes in the particular source etfluent, and the required data quality objectives for each specific
test program. Provisions are included in this test method that require the tester to determine critical
sampling system and instrument operational parameters, and for the conduct of QA/QC procedures.
Testers following this test method will generate data that will allow an independent observer to verify the
valid collection, identilication, and quantification of the subject target analytes.
EPAMethodl&1A
The purpose of the method is to provide guidance for the selection of sampling ports and traverse points at
which sampling for air pollutants will be performed pursuant to regulations set forth in this part.
EPA Method 2 &2C
This method is applicable for the determination of the average velocity and the volumetric flow rate of a gas
stream. The average gas velocity in a stack is determined from the gas density and from measurement of
the average velocity head with a standard pitot tube. Velocity readings are taken from each stack at 16
separate traverse points (Table 6.1) and used to determine the engines mass emissions rate, calculated
utilizing the formulas seen in section 7.0 ol this report.
EPA Method 3A
This is a procedure for measuring oxygen (O2) and carbon dioxide (CO2) in stationary source emissions
using a continuous instrumental analyzer. Quality assurance and quality control requirements are included
to assure that the tester collects data of known quality. Documentation to these specific requirements for
equipment, supplies, sample collection and analysis, calculations, and data analysis will be included.
GAS
4.0 Test Summary
Unit with a serial number of KG14856 which is a Titan 130 engine located at Duchesne Data Center
Power Station and operated by Crusoe Energy Systems, lnc. was tested for emissions of: Carbon
Monoxide, Oxides of Nitrogen, and Volatile Organic Compounds. The test was conducted on 1212112023
by Lucas Ennis with Great Plains Analytical Services, lnc. All quality assurance and quality control tests
were within acceptable tolerances.
The engine is a natura! gas fired Lean Burn (4 Cycle) engine rated at 13,364 Kilowatts (KW) at N/A
RPM. The engine was operating at 11,816.59 BHP and RPM which is 86.67% of maximum engine
load during the test. The test HP calculation can be found on Table 7.0. The engine was running
at the maximum load available at the test site.
Site Verification Photos
3
GAS
4.0 Test
GAS
5
5.0 Run Summaries
Table 5.1 Run Summaries
GAS
Pltot Tube Coefilclent Cp(std)= .99
srecx olameret = bu ncheS 0r:leet. or:19.63 square Feel
H20 o/od 5.64 5.52 5.s3 5.56
co?"/od 2.93 2.84 2.84 2.87
02 o/od 14.39 14.53 14.55 't4.49
GO ppmd 0.03 0.47 0.00 o.17
Molecular Weioht Stack Gas dry basis (Md)q/q mole 29.O4 29.04 29.O4 29.04
Molecular Weiqht Stack Gas wet basis (Ms)o/o mole 28.42 28.43 28.43 28.42
Stack Static Pressure (Po)"H20 4.O4 3.89 2.93 3.62
Stack Static Pressure (Po),HO 0.30 o.29 o.22 o.27
AtmosDheric Pressure at Location (Pbar)MBAR 834.77 835.00 834.05 834.61
Atmosoheric Pressure at Location (Pbar)'Ho 24.66 24.66 24.63 24.65
Absolute Stack Pressure (Ps)"Ho 24.95 24.95 24.85 24.92
Stack Temperature Deq G 496.67 497.22 495.56 496.48
Stack Temperature Deq F 926.00 927.OO 924.OO 925.67
Stack Temperature Deq R 1385.67 1386.67 1383.67 1385.34
Stack Gas Velocitv fusec 237.g'.233.49 202.89 225.32
Stack Flow Rate Q cls 4671.43 4584.49 3983.66 u24.O9
Stack Gas Wet Volmetric Flow Rate sc?hr 5344280.7 s240139.3 4545227.O1 5055284.77
Stack Gas Dry Volumetric Flow Rate scflhr 5043050.4 4950883.6 4293739.60 4774050.86
tmlsstons samDltno Potnls - 3 Dolnl lono ltne samDltno DroD€lnches
First Samolino Point aken @ 16.7o/o ol Stack Diameter 10.02
Second SamDlino Point Taken @ SOyo ot Stac Diameter 30
Third SamDlino Point Taken @ 8{1.3% of Stacl Diameter 49.98
6.0 Volumetric Flow Rate
6.1. Data used for volumetrac flow rate (Method 2)
Table 6.2. Stack gas pressure measured with a standard tube use for Volumetrlc Flow Rate
Aostd = Velocitv head measured bv the' standard pitot tube, (in.) H2o.'
Flgure 6.1
16 Traverse Points Were UsedStack Diameter (inches)60.00
lnches upstream lrom disturbance 12.OO
lnches downstream lrom disturbance 35.00
Pitot readings are taken for Method 2 calculations using measuring points outlined in Method 1
rThe exhaust stack dld not present cyclonlc flow condltlons at the sampllng locatlon duo to the
absence of cyclones, Inertlal demlstetr, yenturl scrubberu, or tangentlal lnlets.
6Data
Table
GAS
7.0 Calculations
Method 2: Determination of Stack Gas Velocitv and Volumetric Flow Rate
*Note- Use of this method neoates the need for anv fuel related numbers for emissions calculations
Ap(avg) = Velocity head of stack gas, mm H2O (in. H2O).
3600 = Conversion Factor, sec/hr.
A = Cross-sectional area of stack, m2 (ft2).
Bws = Water vapor in the gas stream (from ASTM D6348)
Cp(std) = Standard pitot tube coetficient; use 0.99
Kp = Velocity equation constant.
Md = Molecular weight of stack gas, dry basis, g/g-mole (lb./b.-mole).
Ms = Molecular weight ol stack gas, wet basis, g/g-mole (lb./lb. -mole).
Ps = Absolute stack pressure (Pbar+ Pg), mm Hg (in Hg)
Pstd = Standard absolute pressure,760 mm Hg (29.92 in. Hg).
Q5d = Dry volumetric stack gas flow rate conected to
standard conditions, dscm/hr. (dsct/hr.).
Ts(abs) - Absolute stack temperature, oK ('R). = 460 + Ts for
English units.
Tstd = Standard absolute temperature, 293'K (528 "R).
Vs = Average stack gas velocity, m/sec (ft./sec).
Md = .44(.029)+.32(.153)+.28(.81 8+0) = 29.044 LB/LB-MOLEMd = .M(/"CO2I+.32(/"O2)+.28(%N2+%CO)
Ms - Md(l-Bws)+1 8.0(Bws)Ms = 29.044(1 -.056it7)+. 1 8.0( .O5637) = 28.421 LB/LB-MOLE
vs = 8s.+9'.99-y'+.04-y'(1 gas.67(24.9s-zl.4z1ll = 237.91 FTlsEc
Qsd = 3600(1 -Bws)Vs-A(fistd'Ps)(Ts(abs)'Pstd))
Q = 5043050.403/35.31 5 = 142801 .937 DSCM/HR
Emission Rates (Examples use CO Run I
453.6= Conversion lactor lb. to gram HP= Engines rated Horsepower
A = Cross-sectional area of stack, m2 (ll2l. Mfg.= Manufacturer Exhaust flow rate at 100% (ft3/min)
BHP/HR. = Brake work of the engine, horsepower-hour (HP-HR.). 02 = Concentration of oxygen on a dry basis, percent.
BTU/HP-HR. = Brake Specilic Fuel Consumption (HHV) ppm= Parts Per Million (CO)
ER = Emission rate ol (CO) in g/HP-hr. ppm@15% 02= PPM corrected lo 15o/oO2
F(d )= Velurnss ol combustion components per unit of heat Qsd = DU volumetric stack gas llow rate corrected
content, scm/J (scf/million Btu). to standard conditions, dscm/hr. (DSCF/HR.).
Q = Stack gas volumetric flow rate, in standard cubic meters Run Time = Run Time in Minutes
per hour, dry basis Tpy= Tons peryear
LB/HR.= Emission rate ol (Co) in LB/HR. vs = Average stack gas velocity, m/sec (ft./sec).
Molwt.= MolWeight ol CO (28.01)
ppm @ 15% 02 = PPM'((20 .9-151oO2)l(2O.9-O2)l ppm @ 15% 02 =.03'(20.9-'t5)l(20.9-15.3yo)) = .032 PPM @ 15% 02
g/hphr = (PPM'(1.1 64'1oa3)-Q',(Run Time/60))rBHP/HR (.03'(1 . 1 64.1 0^-3)-1 42801 .937t(Run Time/60))/1 1 81 6.59 = 0 G/HP-HR
LB/HR = 0'1/453.6'1 1816.59 = .011 LB/HR
TPY = .01 1'4.38 = .048 TPY
ppm wet'(1(1-H2O) = ppm dry .03 = .0285.(1(1-.06))
GAS
E.0 oxygen calibration 8
8.1 Calibration error test; how do I confirm my analyzsr calibration is correc{? After the tester has assembled, prepared and calibrated the
sampling system and analyzet, they conduct a 3-point analyzet calibration error test before the first run and again afier any failed system bias test or
failed drift test. They then introduce the low-, mid-, and high-level calibration gases sequentially in direct calibration mode. At each calibration gas level
(low, mid, and high) the calibration error must be within I 2.0 percent of the calibration span.
8.2 lnitial system bias and systsm calibration orror chocks. Before sampling begins, it is determined whether the high- level or mid-level
calibration gas best approximates the emissions and it is used as the upscale gas. The upscale gas is introduced at the probe upstream of all sample-
conditioning components in system calibration mode.
(1) Next, zero gas is introduced as described above, The response must be within 0.5 percent ofthe upscale gas concentration.
(2) Low-level gas reading is observed until it has reached a final, stable value and the results are recorded. The measurement system will be
operated at the normal sampling rate during all system bias checks.
(3) lf the initial system bias specification is not met, conective action is taken. The applicable calibration error test from Section 8.2.3 of EPA
Method 7E is repeated along with the initial system bias check until acceptable results are achieved, after which sampling will begin. The pre-
and postrun system bias must be within I 5.0 percent of the calibration span for the low-level and upscale calibration gases.
8.3 Post-run systsm bias check and drift asssssment - confirming that each sample collected is valid. Sampling may be performed for multiple
runs before performing the poslrun bias or system calibration error check provided this test is passed at the conclusion of the group of runs. A failed
final test in this case will invalidate all runs subsequent to the last passed test.
(1) lf the postrun system bias check is not passed, then the run is invalid. The problem is then diagnosed and fixed, then another calibration
error test and system bias is passed before repeating the run.
(2) After each run, the low-level and upscale drift is calculated, using Equation 7E-4 in Section '12.5 from EPA Method 7E. lf the post-run low-
and upscale bias checks are passed, but the low-or upscale drift exceeds the speciflcation in Section '13.3, the run data are valid, but a 3-point
calibration error test and a system bias check must be performed and passed prior to additional testing.
Table 8.1 Oxygen Calibration
Method 7E3.4To the extent practicable, the measured emissions should be between
20 to 100 percent of the selected calibration span. This may not be practicable in some
cases of low concentration measurements or testing for compliance with an emission
limit when emissions are substantially less than the limit.
EPA Method 3A CIA Worksheet
Certified Gas Concantralon I Ceriifiod Gas Concordralon I Cortmed Ga! Co
Low-Level (%) | mld-Loyel (%) | High-Levo
oro./
(DIRECT) Anallzer Callbratlon Error (S 2olo)
Chock
ncont.aion
7E 8.5: Note: that you may
risk sampling for multiple
runs before performing the
post-run bias provided you
pass this test at the
conclusion of the group of
runs
Certified
Concenlration
Value (%)
Direct
Calibration
R$ponse (%)
Absolute
Difference (
Analyzer
Calibration
Enor (o/o)
Zero Gas o/o 0.00% 0.00% 0.00% 0.00%
Mid-Level Gas %
High-Level Gas %
9.04%
20.70o/o
9.02o/o
20.680/0
0.01o/o
O.O2o/o
0.07%
0.08%
(SYSTEM) Galibration Bias Checks (S 5%) and Driff Checks (S 3%)Upscale Gas 9.04o/o
Zero Offset 0.00%
Bias Pre lnilial Value Bias Post lnital Values
Span 20.70
Analyzer
Calibration
Response (%)
Zero Gas 0.00%
Svstem
Calibrations
R€sponse Pre
(olrl
lFtem Biss (91
of Span) Pre
System
Calibralion
Response Posl
(1/.',
iystem Bias (%
of Span) Post
Drift (% of
Span)
0.000/o 0.00%O.O0!o 0.00o/o 0.00%
Upscale Gas 9.02o/o 9.01%0.080/"9.00%0.11o/o 0.00%
(SYSTEill) Calibration Bias Checks (S 5%) and Drifi Checks (S 3%)
Avs. Gas Concentration (Run I 15.25% Effiuent Gas (Coas) Run 1 15.31o/o
Avg. Gas Concentration (Run 2)15.38%Effiuent Gas (Cgas) Run 2 15.44o/o
Avg. Gas Concentration (Run 3)15.40o/o Efiluent Gas (C,gas) Run 3 15.460/o
EPA Method 3A CIA Worksheet
Zero Gas 100% Nitrogen
Mid-Level Gas 9.O40
High-Level Gas 20.7OYo
Zero Gas o/o
Mid-Level Gas %
High-Level Gas %
zero cas 7" [G;fl upscate used
upscale cat t ,!o% I s.o4%
GAS
9
9.0 Engine Parameter Data Sheet
AS
,4nalylicul $erra'ces. Inc
Run 1 Run 2 Run 3 Completed
Company Grusoe Enerov Svstems. lnc.
Faclllty lJucheBne Data conter Power station
Date 1'4Z1|ZUZ$
SIte Elevatlon (ft)5474
Unlt lD
Make Tltan
Model 130
Serlal Number KG14E56
Technlclan Lucas Ennis
Run Start Tlmes 06:51 AM IO:44 AM 11:5E AM 01 :20 PM
Enqlne Hours 3535 3536 3537 3538
GAS
10
10.0 OA/QC Results
Equilibration Response Time
Spike Reported
Spike Expected
Value:248.78
Value: 251.00
system zero Hesponse !rme
System Response Time
45 SeCOnOS
45 seconds
Nitrogen monoxide NO
Nitrogen dioxide NO2
NOx
voc
Orygen
Average:0.00
Average:0.00
Average:0.00
Average:0.01
Average:0.00
alue:100.00
CTS Compound Concentration Avg
Tolerance
Ditference between measured and expected
Value:99.32
2.OO/"
0.68%
Nitrogen monoxide NO
Nitrogen dioxide NO2
NOx
voc
Orygen
Average:0.00
Average:0.00
Average:0.00
Average:0.00
Average:0.13
Average:0.00
Mechanical Response Time
CTS Bottle Concentration
CTS Compound Concentration Avg
Tolerance
Ditference between measured and expected
Value:100.00
Value:97.4O
5.00%
2.60o/"
Gas, lnc.
11
11.0 D6348 Annexes 1-8
The test quality objectives completed for the emissiqns test are demonstrated throughout Annexes 1,2,3,
4, 5, 6, 7 & 8 as layed out per ASTM D6348-03. Allfeference methods, pre-test and post test procedures
were within acceptable limits. Data generated durin! the pre-test and post-test procedures ard
summarized below in order of the distinctive Annex.'
Three 60 minute test runs were performed. The finaf analyte concentrations are the average of each test
run. Data was taken at 60 second intervals. Each 6Q second measurement was the average of 600 scans.
Pppale is used as the surrogate compound for the lAnnex 5 Spiking Technique due to Propane being the
VOC that is most commonly found in the combustiorf process of natural gas. Additionally, the molecu-iar
weight of Propane coincide's with with molecular welBht of VOC's per the-EPA.
i
Annex Table 1.2.1 Cefilfled Bottle Concentratlons
Annex Table 1.2.2 System Capabilities
GAS
Annex Table 1.3.1 Test Specilic Target Analytes and Data Quality Objectives
Compounds
lntrared
Analysls Reglon
(cm-l)
Expected
Concentratlon
Range
luleasuremenr
System
Achlevable
Mlnlmum
Detectable
Concentratlons
l.lequrreq
Measurement
System
Accuracy and
Preclslon lor
fest Appllcatlon
CO 2000-2200 0-1200 ppm 0.16267 ppm 4 ppm
NO 1 875-21 38 0-1000 ppm 0.4007 ppm 2 ppm
NO2 2700-2950 0-'100 ppm 0.4899 ppm zppm
voc
2600-3200
0-100 ppm 1.8520 ppm Tota
VOC'S I ppmperVOC910-1 150
2550-2950
CH20 2550-2850 0-1OO ppm 0.7878 ppm 1 ppm
lnterferlng
Compounds
* CO is analyzed in a separate analysis region than CO2 and H2O
coz 926-1 150 O-1O"/o o"h nla
Water Vapor 3200-3401 O-22"/o O.2O"/o nla
* VOCs compiled of Acetaldehyde, Ethylene, Hexane, and Propane.
T1
FLOW
MTR.
VENT
Figure Annex 1.4.1 Sampling Train
The testing instrumentation is housed in an enclosed vehicle which is located approximately 45 feet from the source. A
heated sample line (sixty feet in length) is attached to the inlet of analfzer system and the source effluent discharges
through the FTIR outlet.
l
ffi
GAS
STACK
13
Sampling Point Locations
ln lnches
16.7o/o 10.
50o/o 30.
83.3% 49.
Inches
Upstream:
12
lnches
Downstream:
35
TRI.PROBE SAMPLE POINT
AS PERCENTAGE OF $IACK D
Flgure Annex 1.4.3 Sample Port Locatlon
Flgure Annex 1 Sampllng Polnts
SAMPLE LOCATION DETERMINEO
BY OIST FROM USruRBANCE
Taroet Analvte Results (oom)
GO o.162r
NO o.400t
NO2 o.4E9t
Ethvlene o3742
Prooane o.rtit51
Hexane o.223i
Acetaldehvde o.8l5i
Formaldehvde o.7a7t
NEA fit
rtrls
REF TN :rTn s
M DCt*t : *'n'#" * crqrLrcr
REF r';s Lceu
Galibreton Transtbl standald ExDected MeaSured Path Lenqth va!ldated
Ethvlena 100 99.32 4.906 Pas{ied
Annex Table 1,2.2 lieasurement System Capabilltles
GAS
Parameter Ges Gonoentratbn Ueasured 70 Dlflerence SDeclllcatlon valldated
Spike Direct
Propane 251 .000 251.609 O.24o/"+l- 2o/"Pass
SI-6 9.t$U 9.726 O.O4"/"+l- 2o/"Pass
co 501 .400 492.662 - 14"/o +l- 2o/"Pass
NO 252.400 249.Uztj 1.34o/o +l- 20/.Pass
Splke Run 1 vla the System
Source Output Splke Averaqe Dllr,.rtlon Factor Expected 70 Recoverv Speciflcation
Propane 0.000 20.183 20.156 100.140/.7O-13O/"
SF6 0.000 0.781 8.030%11O"/o
DplKe l{Un Z Vra Ino uyalem
source output Spike Averaqe Dllutlon Factor ExDected 70 Recoverv Speciflcatlon
Propane o.ooo 19.510 20.632 94.560%7O'13Q"/o
SF6 0.000 0.799 8.215o/o <10/"
liprrg Hun 5 vra me uyalem
Source Output Splke Averaoe Dllutlon Factor Erpected I o/o Recovery speclflcatlon
Propane U.UUU 18.991 19.603 96.880%7O-13Oo/o
SF6 0.000 0.760 7.8'14/"<10"h
Noise Equivalent Absorbance (NEA)
RMS High 0.000486
RMS Mid 0.000283
RMS Low 0.000316
Line Position
015
0.10
0.05
,,:_.:.. ,l-_.
6 66 ;l -:::',.:-_l'.--- -:\ _f \\,/
0.20
015
0.10
005
000
-0 05 -0.05
2092 2069 2046 2023 19S9 1976 1953 1930 1907 1884 1861 1837 1814
@ o.oo% pass pass
GAS
The Gasmet GICCOR (Genzel lnterferometer with Cube Corner Retroreflectors) interferometer is specially
designed for maximum optical throughput and maximum signal to noise ratio of 7.72 (cm-1) remaining
stable with any vibration and temperature changes.
The Gasmet DX4000 is a low resolution spectrometer where the aperture is fixe,
setting and the detector linearity was tested with an alternate approach. A three point linerarity of thie CTS
a
gas was performed and validated.
Linearity
164 7422
154 7422
t44 t 4tl
134.7422
124 7422
114 7422
104 7422
94 7422
84.7422
74 7422
695 687 679 672 664 656 648 641 633 625 6'18 610
164 7422
154.7422
144^7422
lJ+ /+tz
124 7422
114 7422
104 7422
94 7422
84 7422
74 7422
but
15.4326919 Pass
The analytical accuracy of the quantification algorithm is satisfied via the results from Annex 5 per Annex
7.6
POST CTS W3tsm Checr:
u ls Eonle uoncentraton:100.oo
u I s samote uoncenralron Averaoe:100.69
Difference between measured and expected:0.68%
toterance:5.OO%
Fun Drta Valldrflon - Automctod vr Manual Rsadlno Yaldatod commentt
HUn I HOtnIS 1 & Z On UU/NU/HrOOane All wlthln 2O7o Passed Demonstrates no interterences observed.
HUn Z HOtnIS I & Z On UU/NU/HrODane All within 2O7o Passed Demonstrates no lnterterences observed.
F{Un 5 rOlnIS r & Z On UU/NU/rrOpane All within 2oolo Passed Demonstrates no interlerences observed.
GAS
17
12.0 Signature Page
Job/File Name: Crusoe Energy Systems, lnc.; Duchesne Data Center Power Station; ; State Compliance Test
II
We certify that based on review of test data, knowledge of those individuals directly responsible for
conducting this test, we believe the submitted information to be accurate and complete-
Company: G.A.S. lnc.
Print Name: Lucas Ennis
Title: Emissions Specialist
Dale:1212112023
Company: G.A.S. lnc.
Print Name: Chris Oppel
Title: Director of Stack Testing
Signature: /,[ C 0?fl"///\
PhoneNumber: 580-225-0403
Dale:1212112023
Company:
Print Name:
Signature:
Title:
Phone Number:
Date:
GAS
Appendices
GAS
Spike (5 Gas)
Airgas.
an Arr Lqude company
AittaSpcddtyGsH
Airgs USA LI-C
12722 S. Wstwortb Are.
Chiago, IL 60628
Aillu.@m
CERIIFICATE OF ANALYSIS
Grade of Product: EPA PROTOCOL STANDARI)
Part Number
Cylinder Number
Laboratory:
PGVP Number
Gas Code:
E05Nt94E15AC014
ccl42828
124 - Chicago (SAP) - lL
812022
CO,CO2,NO,NOX,PPN,BALN
Referencs Number il4O26O1324-1
Cylinder Volume:. 147.O CF
CylinderPressure: 2015PS|G
Valve Ouflet: 660
CertificationDate: Dec06,2022
mola/ftolG basb Mbs othwi6. notld. Thr 6ut6 rcletc dly to th. it m3 t-rt.d. Th. Epo.t dr.ll nd bc Eproduc.d o@.pt ih tul wilhdjt EpplMl ol fir l.boEbry. D,o
Tdad Data Avallable Upon Requeit
PERIANENT NOTES:Mixture contains nominal 1oppm Sulfur Hexaf,uodde as a tracer componenL Aciual
tested value included within the original Certifcate of Analysis. oontacl the Airgas laboratory if a reprint is
requiI€d
NOTES:Mixture contains nominal loppm Sulfur Hexafluoride as a tracer component. Actual testsd value
includ€d within the original Certificab of Analysis. Contact the Atgas laboratory if a repdnt is Equired.
SF6 Resulb:
JMR137-9.73PPMi E E r-t n n Il r
nn
SldhrluE 6n il.
Approved for Releele Plg.1oll
Cdt'fietbnp..bm.din.6rdsh6wiih'EPATBe.bilityPrcto@llo.A6sysndCcrtfelidofc.$ffiC5llbr.lirSbdgds(Msy2012) ddmstEPA
600/R-12531, Ging thc asy proc€duEs listcd. AneMlel MGthodology doG not cqJlE @.dd br .Blylical inb.lbEM. Thb crlindd has a totel eaMiEl
un6rtahty aa atatad bclo, with a dIHGE Lwl of g5%. ThaB aro no 6igrient impuddcs rfildr .llLsl lhc u$ ol thb elib.etio mlxtrc. All dqMiils aE m a
Nd lJ6. Thl.tm i. O7
ANALYIICAL RESIT'LTS
Componelrt Requerted Actual Protocol TotalRslatlve Assay
Dats3Concentretlon Concentratlon Ueftod Uncort lnty
NOX 250.0 PPM 253.0 PPM G1 +/- 1.2% NIST TE@bh 1'lli28l2l22, 1AOG|202.
NITRIC OXIDE 250.0 PPM 252.4 PPM Gl +/- 'l .0% NIST TE€abl€ 1112812022, 1A0612022.
PROPANE 250.0 PPM 251.0 PPM Gl +/- 0.7% NIST TBeeble 1113il2022
CARBON MONOXIDE 500.0PPM sol.4PPM G1 +/-0.6%NISTTE@ble 11Ds12022
CARBON DIOXIDE 5.000 % 5.025% cl +/- 1.4% NIST Ttuabl€ 1112812022
NITROGEN Bdane
CALTBRATIONSTANDARDS
TyDo Lot lD Cyllnder No Concontratlolr Uncert lnty ExDlratlon D.to
EB0113125 250.3 PPM NtlRtC OXTDE/NTIROGEN
D685025 9,9,I PPM NITROGEN DIOXIDSAIR
GMIS 401423838104 CC505590 4.373 PPM NTTROGEN DTOX|DE/NTTROGEN
NTRM 2fl)60331
PRM 12386
+/- 0.8%
+l- 2.0o/"
+l- 2.Oo/"
+l- O.sP/o
+/- 0.6%
+/- 0.6%
OcrZi,2,.26
Feb20,2O2O
Feb 18,2023
Msr 17,2027
Jul 03,2024
May 14,2025
NTRtil 2m602-13
NTRII 13010109
NTRM 13060423
6162697Y 243.3 PPM PROPANE/AIR
KALOO3925 49s.4PPMCARBONMONOXIDE/NITROGEN
cc4'13685 7.489 % CARBON DTOXTOE/NTTROGEN
tlE SRM. NTRM. PRM. d RGM ffid.bow lr dlv lh r.t hnd io fr . GMls ld h h. sv and d En dtu.r
ANALYTICALEQUIPMENTlnstrumenutrk.ruodel An.lyflC.l Prlnclds L.3t tultpolnt Callbrruon
Nl@bt lS50 AUP2010242
CO.1 SIEMENS ULTMMAT 6E N1J57OO
Ni@let iS50 AUP2010242
Nl@let lS50 AUP2010242
Ni@bt iS50 4UP2110277
Nw07,2022
Nw28,2022
])€c,05,2022
D€c05,2022
Nw07,2O2.
FTIR
NDIR
FTIR
FTIR
FTIR
GAS
Airgas.
il Ar Uquid€ cmpary
9o/o O2|NO2
Alrgl!spcdrltyctg
Airg8 USALrc
525 North Indusuial Iep Rqd
T@le,UT84074
Airtu@m
CERTIFICAIE OF ANALYSIS
Grade of Product: EPA PROTOCOL STA\IDARI)
Part Number:
Cylindor Numbsr:
Laboratory:
PGVP Number:
Gas Code:
E03Nt90E15W0003
cc517745
124 -'roD,eb (SAP) - UT
872023
NO2.02.BALN
Refer€nce Number: 153.402786436-1
Cylinder Volume: 145.0 CF
Cylinder Pressure: 2015 PSIG
Valve Outlel 660
Certification Date: Jul 13,2023
Cdn€ton pdiomld in .@d.n6 with 'EPA TE6.t llty Prc(o@l lbr Asy.nd Ccrdidtd of G.-@ C.lb..iff Stsdrd. (M.y m12I d@'Mt EPA
000/R-12631,uCigth..s.ypl@du6lh.d.An bdelM.,lhodologydGndEqdE@m(doilb..mlyd€lkrbdbEE.Thbcrfindth.!.totcil.lyti4lun6d.hy...t ird bdil rilh . @ffrn6 lrvll of 95%. Th.E .E m.lgnlllent lmpurit . wfihar.lt d th. us dlhb cCb..toi mbdrE. All dqtciona.E on .
ildc6rybt
tld um Thh b.ld,
bG 6p.odE d .rc.pt
0.7
.pplMl of th! leDffiuy.
ANALYTICALRESTJLTS
Req@.ted Actu.l Protocol Tot l Reldvo
Conc.ntr.Uon Conccntnuon U.ffrod Uncert lnty
A3s.yD.biCompon€nt
NITROGENDIOXIDE 100.0PPM 101.9PPM G1 +^2.0%NISTTEHtI€ o7106,fm23,071132023
OXYGEN 9.000 % 9.037 % Gi +/- 1.0% NlSTTffible O7I06,DO23
NITROGEN Bebne
CALIBRATIONSTANDARDS
TyDa LotlD CyllndcrNo ConcenElton Uncortrlnty ExDlrrtlon D.!a
Nry 09, 2025
F6b23,2023
D*14,2023
GMIS
PRM
NTRM
1sw202@1
12120
98051010
CC5l7858,IO1.1PPMNITROGENDIOXIDE/NITROGEN
D887373 98.9 PPM NITROGEN DIOXIDFJNITROGEN
SG9161286BAL 12.05%OXYGEIVNTTROGEN
1.1%
1.0%
o.704
ln3trumenut.kdtodcl
ANALYTICAL EQT,IIPMENT
Anrhrtdl PilnclDl.Lert llultloolni Cellbreilon
FTIR
02 PaEmenolb aDXON)
Jun 29,2023
Jun29.2023
MKS FT|R NO2 0't8143349
Horlbe MPA-5iO W8O3MM58 02
Tdad Dlt Avllhble Upon Requs3t
Approvod for Releare P.g. I ot I
GAS
Alruas.
e AF tiqulo wDdry
elrluSpcdrlryOea
AtugUUSAIIC
unz S.Watwo[ttAc
Cbt6ge, IL60618
At!!r.@
OFAIYALYSE
PRIMARY STAI{DARI)
RefaronceNumbd: 54-4(,?81137'}1Crlndervolur€: 141-OG
Cyllnder Prcosum: 2015 PSlc
Vahro Outlo* 350
Pror I ol I
Crrsbmec
Part Nwnb€r:
Cyllnder Number
Laboratory:
Anaurb Dab:
Lot Number
Grade of
GRE{T PLNNS ANALYTIO{I
x02Nr99P1sACVH8
ccfi7503
12a - Chioago (SAP) - lL
AtS 15,2023
w:t281137&.1
Epln0on Deta:t5,203t
Prlmary Sbndad G.6 MbGrcs arctEoeable b f. uteighE and/r N.IS.T, G6 llbltrc rcftrenoe maE lals.
RESI,'LIS
Componcnt Rcq Gonc Gonccntrdon Analy{cal
Unccttalfi16)
ETHYLENE 100.0 PPM
BaLnc.
+l- 1Vt
iloil[:GREAT PLAINS A]IALYTICAL. CERf,IFIED BY mR
.lr.trmdil.
AppotrdiorRobu
AI\IAI
Ailgas.
e Ar Liquid€ Mparry
BIP
rtufu MtdSouthEliotr
AirgsUSALLC
974r E.55th St- North
ftbs, Ox74rr7
Airta.@a
CERTIFICATE OF BATCH AIYALYSIS
Part Number:
Cylinder Analyzed:
Laboratory:
Analysis Date:
Grade
Nt BtP300
TWo$867349
106 - Tulsa Fast Fill (SAP) - OK
F€b 10,2016
of Product: BIP-BUILT IN PT RIFIER
Referenca Number: 29.400672389-1
Cylindor Volume: 304.0 CF
Cy'inder Pressure: 2O40 PSIG
Valve Ou0et 580
Compononl
ANALYTICAL RESI.'LTS
Requelt d
Purlty
Certlflod
Concentratlon
NITROGEN
OXYGEN
WATER
TOTAL HYDROCARBONS
CARBON DIOXIDE
CARBON MONOXIDE
99.999 %
1 PPM
1 PPM
0.1 PPM
0.5 PPM
0.5 PPM
99.999 %
0.94 PPM
0.058 PPM
0.1 PPM
0.235 PPM
0.235 PPM
Pa]meneirt llotaa:This cort lndud€s \€lues from the nfrll' sH€ and is not ropres€ntative of the 'us€' side pudty. Contacrt an Airgas
Sales Representative br thls infomatbn.
C}lndorr In B.tch:
42861ry, TW04671107, TW0$831574, TW0$865966, TW0$867349, TW0+867538, TW05-867578, Tw0il8r687, TW05-881820,
TW0$920689, TW0$920760, TW05848694, TW0586744't, TW05897265, TW05897512, TW05920678, TW05920686, TUm5920695,
TW05920781, TW05920874
lmpuritiss v6rifi6d against anaMical stBndards tracoeble to NIST by weight and/or analysis.
Approvcd for Rclearo P.g. 'l ot I
GAS
Airgas.
aArLiquir:k cmpsy
21% 02
AiryuSpcsidtycrg
AirysUSALrc
525 North Indutrisl fmp Rod
T@le, uT84074
Airt8.@m
CERTIFICAIE OF AI\IALYSIS
Grade of Product: EPA PROTOCOL STANDARD
Parl Number
Cylinder Number
Laboratory:
PGVP Number:
Gas Code:
E02Nr79E15A00B1
cc76460
124 -Tooele (SAP) - UT
872023
02,BALN
Refer€nce Number: 1534027 8362'l -'l
Cylinder Volume: 146.0 CF
Cylinder Pressure: 2015 PSIG
Valve Outlet 590
Certification Date: Jul 05,2023
Date:2031
Cqffetbo p{tomrd in .@rd.ne wlth 'EPA TE@eblllty PDio@l br Alsy.nd C..tlletio of G..rs C.lbi.tim Slndrdr (M.y 2012)' d@mdn
6m/R-1 Z53l , Blng thG r$y prEduG. lisi.d. AnaMi€l M.lhodology l@3 not EqulE mrioi ftr .mtyt6l lnbdbE6. Thb crhdd h.s e tot l s.ldal
unori.inty.. tt t d b.lo, wlth e ffilldc@ lGwl.of 95%. ThoE.rc no sigrtf€nt impu,id.. rtrkfi eli.oi th. u! ol thh cCb..tbo mlr(irE. Al o6t tioo. .E d s
rEb/md6 b.ds unhs o(h.illaa rctad. Tha cult6 Elgte sly b lhc hrm3 taatrd. Th. Epod $.! d b. EFoduc.d cxc.pl h full wlthdrt .ppEEl ot lh. l.hoEbry. Oo
Td.d Date Avallable Upon Roquo3l
Sldh.hrn ah fl.
Approved lor Relea:e Prg. I ot I
Component Requolled
ConcantEtlon
ANALYUCALRESULTS
Ac.tual Protocol
ConmnlBdon t.lhod Totll Rolatlvo
Uncarlrlnty
Assay
Datsr
oxYGEN 21.00% 20.70%
NITROGEN Balam
G1 +/- 1.4% NIST Tr66aHe O1lOSnO23
CAIIBRAIION STAIYDARDS
Typo LotlD Cyllndorilo Concontadon Uncertllnty Explrltlon Dlt
NTRM 09061434 C,c282492 22.s3%OXYGENNTIROGEN O.4%M8v 13,2025
lnstrumenutaks/todsl
ANNLYTICAL EQT,IIPMENT
An.hrdc.l PrlnclDl.La3t ilultlDolnt C.llbnllon
Horiba MPA-510 W603MM58 02 02 PaBmaondc (DIXON)Jln?9,2023
GAS
@es
Great Plains Analytical Services
so3 w 3d st
Elk City, OK73644
(580) 2 2 5-0403 Fax (580)225 -26L2
CERTIFICATE OF ANALYSIS
Grade of Product: CERTIFIED STAI\DARD-PROBE
Part Number: 60L Reference P1
Number:
Laboratory: GAS INC. Stack Diameter: 60'
Analysis Date: 312712023 Target Flow 3Umin
Raie:
LOT Number: A
Number of 3SN: P1A 60L Points:
Product performance verified by direct comparison to calibration standards traceable to N.I.S.T.
*The probe listed on this form meets the multipoint traverse requirement of EPA Method 7e,
section 8.4 as shown in the accompanying data. Method 7e, section 8.4 states that the multipoint
traverse requirement can be safisfied by samplingvia"amulti-hole probe designed to sample at
the prescribed points with a flow +/- l0 percent of mean flow rate".
ANALYTICAL RESULTS
Run fr Total Flow Measured Flow Measured Flow Measured Flow Mean Probe
(Uml Port A (t/ml Port B (Uml Port C (Um) Port Sampled
(Delta qll (Delta q2l (Delta q3l Flow (L/m)
Run I 2LPM
Run2 4LPM
0.690 0.550 0.580 0.640
(7.814) (1.564) (-e.384)
1.39 t.3l 1.23 1.31(6.ll^) (0.004) (-6.lra)
*Calibration conducted in accordance with Emission Measurement Center Guideline Document - EMC GD-031
Notes:
312712023
Approved for Release Date
in /..j a"',
tNZJ, -\*'4t t ntr'tt "
UilITED STATES ENVIRONMENTAL PROTHCTION AGENCY
RESEARCH TRIANGLI PAHK. NC T7711
March 15,2021
' ; ; i i ,i
r,;i. ;, ;,1, i' r ;)i ,il,ilJll,ir ,
,rral .,!t {r1l
Mr. Jordan Williamson
CEO
GAS Inc.
303 W. 3'a Street
Elk City, OK73644
Dear Mr. Williamson:
We are writing in response to your leffer received on September 17, 2020,in which you request the approval
of alternative testing procedures. The EPA's Office of Air Quality Planning and Standards (OAQPS) is the
delegated authority for consideration of major alternatives to test methods and procedures as set forth in 40
CFR parts 60 and 63 under which your request must be addressed. GAS Inc. is requesting a change to one of
the test methods, ASTM D6348-03, used for conducting performance tests to determine compliance under
40 CFR part 60, Subpart JJJJ - Standards of Performance for Stationary Spark Ignition Internal Combustion
Engines (Subpart JJJJ) and 40 CFR part63, Subpart ZZZZ - National Emissions Standards for Hazardous
Air Pollutants for Performance for Stationary Reciprocating Internal Combustion Engines (Subpart ZZZZ).
The change being requested will be used to check detector linearity of the Fourier Transform Infrared (FTIR)
instrumentation used to conduct this method. Specifically, you are requesting that the procedures of section
8.3.3 of Method 320 (40 CFR part 60, Appendix A), another FTIR-based method allowed under Subparts
JJJJ and ZZZZ, be used in lieu of section A6.4.1of ASTM D6348-03 when conducting testing using ASTM
D6348-03 under 40 CFR part 60, Subpart JJJJ and 40 CFR part 63, Subpart ZZZZ.
In your request, you state that this alternative linearity check procedure will produce consistent results when
utilizing either Method 320 or ASTM D6348-03. Additionally, some FTIR instrumentation does not allow
for reducing the size of the aperture in the instrument and, thus, it would not be feasible to properly conduct
the entirety of the ASTM D6348-03 method in its current form using such an instrument.
Based on our understanding of FTIR instrument principles and recognition that the requested alternative
determination of detector linearity is both technically sound and contained within Method 320, we are
approving the requested change. We believe that this alternative is acceptable for use for use in testing all
engines subject to 40 CFR part 60 Subpart JJJJ and 40 CFR part63, Subpart ZZZZ. Also, we will post this
letter as ALT-l4l on EPA's website (atwww.epa.gov/emc/broadly-applicable-approved-alternative-
testmethods) to announce that our approval of this alternative test method is broadly applicable to engines for
the purposes of meeting Subparts JJJJ and ZZZZ.
If you should have any questions or require firther information regarding this approval, please contact David
Nash ofmy staffat 919-541-9425 or email atnash.dave@epa.gov.
STEFFAN Dlgltelfi rlgned by
AN JOHHSOf{
202t.03.15JOHNS
cc:
t2f$50 -{t4'0s
SteffanM. Johnson, Group Leader
Measurement Technolory Group
Sara Ayers, EPA/OECA/OC/I\dAMPD, (ayres.sara@epa.gov)
Melanie King, EPA/OAR/OAQPS/SPPD, fting.melanie@epa.gov)
James Leather, EPA Region 6, (leatherjames@epa.gov)
David Nash, EPA/OAR/OAQPS/AQAD, (nash.dave@epa.gov)
Sincerely,
Lucas Ennis
GAS
580-225-0403
info@gasinc.us
Type of Sources Tested:
Stationary Internal Combustion Engines. 4 Stroke Rich Burn Engines. 2 Stroke & 4 Stroke Lean Burn Engines
Stationary Natural Gas Fired Generators
Stationary Propane Fired Generators
Gas Fired Boilers
Types ol Analyzers:. Gasmet DX4000 FTIR. Gasmet Portable Sampling Unit with Zirconium Oxide 02 Sensory. Testo 350. Flame lonization Detector
Qualifications:
Trained, studied, and fully demonstrates compliance for emissions testing via data collection outlined in the
following Reference Methods:. EPA Method 1 & 1A - Sampling & Traverse Points. EPA Method 2 &2C - Velocity & Volumetric Flow Rate of a Gas Stream. EPA Method 3A - Oxygen. EPA Method 7E - NOX. EPA Method 10 - Carbon Monoxide. EPA Method 254- Volatile Organic Compounds. ASTM D6348 - Extractive Fourier Transform lnfrared Spectroscopy
Conducts emissions testing on a weekly basis including, but not limited to, the following test types: lnitial
Compliance, BiennialCompliance, SemiannualCompliance & Quarterly Compliance. Alltest-s performed
are in accordance to any and all Federal & State requirements as applicable (i.e. JJJJ,ZZZZ, 106.512, 117,
PEA, etc.). Performed testing in Colorado, Utah, Wyoming, North Dakota, Montana, Kansas, New Mexico,
Oklahoma, Texas, I ouisiana (land and off-shore), Alkansas, Ohio, Pennsylvania, West Virginia, New York,
Kentucky, & Mississippi.
. Quarterly Performance Reviews covering ongoing changes with Federal Regulations, State
Compliance guidelines, & site-specific safety certifications.
GAS
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Run NOx ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 33.042 0.04 9.35 0.30 0.00000 0.13291 0.13221
2 32.524 0.05 9.20 0.31 0.00000 0.12012 0.12081
3 29.381 0.05 8.31 0.28 0.00000 0.10313 0.11608
AVG 31.649 0.05 8.95 0.30 0.00000 0.11872 0.12303
Run CO ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 9.144 0.04 2.59 #DIV/0! 0.00000 0.02239 0.02227
2 9.104 0.05 2.58 #DIV/0! 0.00000 0.02047 0.02059
3 8.088 0.05 2.29 #DIV/0! 0.00000 0.01728 0.01945
AVG 8.779 0.05 2.48 #DIV/0! 0.00000 0.0200 0.02077
Run VOC ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 1.81 0.04 0.51 #DIV/0! 0.00000 0.00698 0.00694
2 1.60 0.05 0.45 #DIV/0! 0.00000 0.00565 0.00568
3 1.56 0.05 0.44 #DIV/0! 0.00000 0.00523 0.00589
AVG 1.65 0.05 0.47 #DIV/0! 0.00000 0.0060 0.00617
Run HCOH ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 0.00 #DIV/0! 0.00000 0.0000 0.00000
2 0.00 #DIV/0! 0.00000 0.0000 0.00000
3 0.00 #DIV/0! 0.00000 0.0000 0.00000
AVG #DIV/0! #DIV/0! 0.0000 #DIV/0! 0.00000 0.0000 0.00000
Operating Parameter R1 R2 R3 AVG.
Engine Load %86.00 85.00 76.00 82.33
Fuel Feed Rate (SCF/hr):#DIV/0!
F-Factor;#DIV/0!
Engine HP 456.00 451.00 403.00 436.67
BSFC (BTU/BHP-hr):#DIV/0!
Q Stack dscf/hr 33672.72 30915.70 29384.03 31324.15
HHV #DIV/0!
Ambient Temperature (F):#DIV/0!
Crusoe Energy - Duchesne Data Center; H24 Compressor Engine-1 Stack Test Date 12/20/23, Reviewed by Robert Sirrine on 02/03/24
Test Results NOx
Test Parameters Generator #1
Test Results VOC
Test Results HCOH
Test Results CO
Analyte High Recovery +- 10% Gas Value Pre Direct Response % Recovery Pre System Response % Recovery Post System Reponse % Recovery
NOx 354.30 0.00 0.00 0.00
NO2 101.9 0.00 0.00 0.00
NO 252.40 247.83 98.19 247.10 97.90 246.65 97.72
CO 501.40 494.78 98.68 492.32 98.19 494.06 98.54
Ethylene (CTS) 100.00 98.56 98.56 97.70 97.70 98.92 98.92
Oxygen 9.04 9.03 99.89 9.02 99.78 9.00 99.56
SF6 9.73 9.64 99.12 9.60 98.71 9.62 98.89
Propane 251.00 250.51 99.81 249.61 99.45 250.29 99.72
Baseline Baseline R1 Baseline R2 Baseline R3
NOx 0.0000 0.0000 0.000
NO2 0.0000 0.0000 0.000
NO 0.0000 0.0000 0.000
CO 0.0000 0.0000 0.000
VOC 0.3500 0.6100 0.610
Oxygen 0.0000 0.0000 0.000
Analyte Cal Gas Value Stack gas measured Stack + Spike measured Spike % Recovery Dilution Factor +=10% Spike Value
SF6 run 1 9.73 0.0000 0.78 99.12 0.080 0.78
SF6 run 2 9.73 0.0000 0.79 99.11 0.082 0.79
SF6 run 3 9.73 0.0000 0.80 99.11 0.083 0.80
Propane spike run 1 251.00 0.0000 22.20 110.06 0.080 20.17
Propane spike run 2 251.00 0.0000 22.35 109.11 0.082 20.48
Propane spike run 3 251.00 0.0000 22.49 108.56 0.083 20.72
Analyte CO NO NO2 Form CO2 VOC
MDC 0.1627 0.4007 0.4899 0.7878 0.0000 1.8520
Calibration Transfer Standard (CTS)
Analyte/Spike %Recovery, Error & Drift
System Zero Background Check Pretest
Spiked amout should be < 10% of the Certified gas concentration. The DF should be < 0.100
Spiked amout should be +-50% of the Stack analyte gas concentration
Sample Spike Recovery (70%-130%)
Sample Spike MDC ppmdv
Run NOx ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 4.555 0.64 1.33 0.06 0.00000 0.00993 0.01050
2 4.735 0.54 1.37 0.06 0.00000 0.00948 0.00967
3 3.733 0.45 1.08 0.05 0.00000 0.00711 0.00724
AVG 4.341 0.54 1.26 0.06 0.00000 0.00884 0.00914
Run CO ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 21.549 0.64 6.28 #DIV/0! 0.00000 0.02859 0.03023
2 17.065 0.54 4.95 #DIV/0! 0.00000 0.02081 0.02121
3 20.962 0.45 6.05 #DIV/0! 0.00000 0.02430 0.02477
AVG 19.859 0.54 5.76 #DIV/0! 0.00000 0.0246 0.02540
Run VOC ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 2.25 0.64 0.65 #DIV/0! 0.00000 0.00469 0.00496
2 1.96 0.54 0.57 #DIV/0! 0.00000 0.00377 0.00384
3 1.58 0.45 0.46 #DIV/0! 0.00000 0.00288 0.00294
AVG 1.93 0.54 0.56 #DIV/0! 0.00000 0.0038 0.00391
Run HCOH ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 0.00 #DIV/0! 0.00000 0.0000 0.00000
2 0.00 #DIV/0! 0.00000 0.0000 0.00000
3 0.00 #DIV/0! 0.00000 0.0000 0.00000
AVG #DIV/0! #DIV/0! 0.0000 #DIV/0! 0.00000 0.0000 0.00000
Operating Parameter R1 R2 R3 AVG.
Engine Load %81.00 84.00 84.00 83.00
Fuel Feed Rate (SCF/hr):#DIV/0!
F-Factor;#DIV/0!
Engine HP 429.00 445.00 445.00 439.67
BSFC (BTU/BHP-hr):#DIV/0!
Q Stack dscf/hr 18245.21 16766.20 15937.50 16982.97
HHV #DIV/0!
Ambient Temperature (F):#DIV/0!
Crusoe Energy - Duchesne Data Center; H24 Compressor Engine-2 Stack Test Date 12/20/23, Reviewed by Robert Sirrine on 02/05/24
Test Results NOx
Test Parameters Generator #1
Test Results VOC
Test Results HCOH
Test Results CO
Analyte High Recovery +- 10% Gas Value Pre Direct Response % Recovery Pre System Response % Recovery Post System Reponse % Recovery
NOx 354.30 0.00 0.00 0.00
NO2 101.9 0.00 0.00 0.00
NO 252.40 247.83 98.19 247.10 97.90 246.63 97.71
CO 501.40 494.78 98.68 492.32 98.19 495.03 98.73
Ethylene (CTS) 100.00 98.56 98.56 97.70 97.70 99.01 99.01
Oxygen 9.04 9.03 99.89 9.02 99.78 9.02 99.78
SF6 9.73 9.64 99.12 9.60 98.71 9.61 98.77
Propane 251.00 250.51 99.81 249.61 99.45 249.97 99.59
Baseline Baseline R1 Baseline R2 Baseline R3
NOx 0.0000 0.0000 0.000
NO2 0.0000 0.0000 0.000
NO 0.0000 0.0000 0.000
CO 0.0000 0.0000 0.000
VOC 0.3500 0.5400 0.430
Oxygen 0.0000 0.0000 0.000
Analyte Cal Gas Value Stack gas measured Stack + Spike measured Spike % Recovery Dilution Factor +=10% Spike Value
SF6 run 1 9.73 0.0000 0.77 99.12 0.080 0.77
SF6 run 2 9.73 0.0000 0.77 99.11 0.080 0.78
SF6 run 3 9.73 0.0000 0.75 99.12 0.078 0.76
Propane spike run 1 251.00 0.0250 21.78 108.96 0.080 19.96
Propane spike run 2 251.00 0.0000 22.56 112.44 0.080 20.07
Propane spike run 3 251.00 0.0000 21.79 111.20 0.078 19.60
Analyte CO NO NO2 Form CO2 VOC
MDC 0.1627 0.4007 0.4899 0.7878 0.0000 1.8520
Calibration Transfer Standard (CTS)
Analyte/Spike %Recovery, Error & Drift
System Zero Background Check Pretest
Spiked amout should be < 10% of the Certified gas concentration. The DF should be < 0.100
Spiked amout should be +-50% of the Stack analyte gas concentration
Sample Spike Recovery (70%-130%)
Sample Spike MDC ppmdv
Run NOx ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 5.149 15.31 5.43 0.01 0.00000 3.10198 0.11907
2 4.264 15.44 4.61 0.01 0.00000 2.52187 0.09680
3 3.337 15.46 3.62 0.01 0.00000 1.71165 0.06570
AVG 4.250 15.40 4.55 0.01 0.00000 2.44516 0.09386
Run CO ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 0.030 15.31 0.03 #DIV/0! 0.00000 0.01100 0.00042
2 0.495 15.44 0.53 #DIV/0! 0.00000 0.17823 0.00684
3 0.000 15.46 0.00 #DIV/0! 0.00000 0.00000 0.00000
AVG 0.175 15.40 0.19 #DIV/0! 0.00000 0.0631 0.00242
Run VOC ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 1.12 15.31 1.18 #DIV/0! 0.00000 0.64615 0.02480
2 1.72 15.44 1.86 #DIV/0! 0.00000 0.97447 0.03741
3 1.11 15.46 1.20 #DIV/0! 0.00000 0.54375 0.02087
AVG 1.31 15.40 1.41 #DIV/0! 0.00000 0.7215 0.02769
Run HCOH ppm %O2 PPM @ 15% O2 PPM @ ISO lb/MMBtu lb/hr g/hp-hr
1 0.00 #DIV/0! 0.00000 0.0000 0.00000
2 0.00 #DIV/0! 0.00000 0.0000 0.00000
3 0.00 #DIV/0! 0.00000 0.0000 0.00000
AVG #DIV/0! #DIV/0! 0.0000 #DIV/0! 0.00000 0.0000 0.00000
Operating Parameter R1 R2 R3 AVG.
Engine Load %87.00 87.00 87.00 87.00
Fuel Feed Rate (SCF/hr):#DIV/0!
F-Factor;#DIV/0!
Engine HP 11816.60 11816.60 11816.60 11816.60
BSFC (BTU/BHP-hr):#DIV/0!
Q Stack dscf/hr 5043050.40 4950883.64 4293739.60 4762557.88
HHV #DIV/0!
Ambient Temperature (F):#DIV/0!
Crusoe Energy - Duchesne Data Center; Titan 130 Turbine Stack Test Date 12/21/23, Reviewed by Robert Sirrine on 02/08/24
Test Results NOx
Test Parameters Generator #1
Test Results VOC
Test Results HCOH
Test Results CO
Analyte High Recovery +- 10% Gas Value System Response % Recovery Pre Direct Response % Recovery Post System Reponse % Recovery
NOx 354.30 0.00 0.00 0.00
NO2 101.9 0.00 0.00 0.00
NO 252.40 249.03 98.66 246.72 97.75 249.56 98.87
CO 501.40 492.66 98.26 487.31 97.19 491.49 98.02
Ethylene (CTS) 100.00 99.32 99.32 97.40 97.40 100.69 100.69
Oxygen 9.04 9.02 99.78 9.01 99.67 9.00 99.56
SF6 9.73 9.73 99.96 9.62 98.82 9.72 99.89
Propane 251.00 251.61 100.24 248.78 99.12 251.24 100.10
Baseline Baseline R1 Baseline R2 Baseline R3
NOx 0.0200 0.0000 0.000
NO2 0.0200 0.0000 0.000
NO 0.0000 0.0000 0.000
CO 0.0000 0.0000 0.000
VOC 0.2200 1.0800 0.790
Oxygen 0.0000 0.0000 0.000
Analyte Cal Gas Value Stack gas measured Stack + Spike measured Spike % Recovery Dilution Factor +=10% Spike Value
SF6 run 1 9.73 0.0000 0.78 99.96 0.080 0.78
SF6 run 2 9.73 0.0000 0.80 99.96 0.082 0.80
SF6 run 3 9.73 0.0000 0.76 99.96 0.078 0.76
Propane spike run 1 251.00 0.0000 20.18 100.14 0.080 20.16
Propane spike run 2 251.00 0.0000 19.51 94.62 0.082 20.62
Propane spike run 3 251.00 0.0000 18.99 96.83 0.078 19.61
Analyte CO NO NO2 Form CO2 VOC
MDC 0.1627 0.4007 0.4899 0.7878 0.0000 1.8520
Calibration Transfer Standard (CTS)
Analyte/Spike %Recovery, Error & Drift
System Zero Background Check Pretest
Spiked amout should be < 10% of the Certified gas concentration. The DF should be < 0.100
Spiked amout should be +-50% of the Stack analyte gas concentration
Sample Spike Recovery (70%-130%)
Sample Spike MDC ppmdv