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Draft EIS for SUA Optimization to Support Existing Aircraft at Holloman AFB, NM
Appendix G G-1
APPENDIX G
AIR QUALITY SUPPORTING DOCUMENTS
Draft EIS for SUA Optimization to Support Existing Aircraft at Holloman AFB, NM
Appendix G G-2
This page intentionally left blank.
Background AQ Data
Baseline: Alt 1: Alt 2: Alt 3:
Airsapce Sorties Minutes Airsapce Sorties Minutes Airsapce Sorties Minutes Airsapce Sorties MinutesTalon Low 315 12,606 Talon Low 315 12,606
Talon Low A 2,571 102,840 Talon Low A 2,065 82,600 Talon Low B 1,117 44,680 Talon Low B 516 20,640
Smitty Low 2,867 86,005 Smitty Low 1,106 33,180 Lobos Low 716 21,487
Sorties Total Minutes Total HrsGE-100/ PW-220 Sorties Total Minut Total Hrs
GE-100/ PW-220 Sorties Total MinutTotal Hrs
GE-100/ PW-220 Sorties Total MinutesTotal Hrs
GE-100/ PW-220
F-16C 831 33,240 554 305 10,000 400,000 6,667 3,667 10,000 308,310 5,139 2,826 10,000 368,080 6,135 3,374 249 3,000 2,312 2,761
F/A-18C 1,000 60,000 1,000 1,000 60,000 1,000 1,300 78,000 1,300 1,300 78,000 1,3001,554 7,667 6,439 7,435
Percent of time at power setting: Engine model split for F016CMAX 12% Aircraft: 56 55% Block 40 with GE-100 EngineMIL 74% 45 45% Block 42 with PW-220 Engine85% 14%
Below 3kft AGL 3,513 42,280 32,588 38,906 (Minutes/year)Baseline F-16 GE-100 Alt 1 F-16 GE-100 Alt 2 F-16 GE-100 Alt 3 F-16 GE-100
1,948 minutes below 3K 23,442 minutes below 3K 18,069 minutes below 3K 21,572 minutes below 3K228 minutes below 3K in A/B mode 2,748 minutes below 3K in A/B mode 2,118 minutes below 3K in A/B mode 2,529 minutes below 3K in A/B mode
1,720 minutes below 3K in MIL 20,694 minutes below 3K in MIL 15,951 minutes below 3K in MIL 19,043 minutes below 3K in MILF-16 PW-220 F-16 PW-220 F-16 PW-220 F-16 PW-220
1,565 minutes below 3K 18,838 minutes below 3K 14,520 minutes below 3K 17,334 minutes below 3K184 minutes below 3K in A/B mode 2,208 minutes below 3K in A/B mode 1,702 minutes below 3K in A/B mode 2,032 minutes below 3K in A/B mode
1,382 minutes below 3K in MIL 16,629 minutes below 3K in MIL 12,817 minutes below 3K in MIL 15,302 minutes below 3K in MILF-18C (transients) F-18C (transients) F-18C (transients) F-18C (transients)
1,333 minutes below 3K 1,333 minutes below 3K 1,000 minutes below 3K 1,233 minutes below 3K156 minutes below 3K in A/B mode 156 minutes below 3K in A/B mode 117 minutes below 3K in A/B mode 145 minutes below 3K in A/B mode
1,177 minutes below 3K in MIL 1,177 minutes below 3K in MIL 883 minutes below 3K in MIL 1,088 minutes below 3K in MIL
Total Hours 81 727 560 669
Holloman AFB MOA Air Calculations
Table 1. Current Ops and Alternatives 1,2, and 3 - FlaresStudy Area Emission Factor (lb/item)
Type Category # flares VOC CO NOx SO2 PM10 PM2.5 CO2
Flare - baseline CM flare L410 5,000 0.0004 0.0013 0.00013 0.0000079 0.0062 0.0062 0.011 Alternative 1, 2 or 3 CM flare L410 15,360 0.0004 0.0013 0.00013 0.0000079 0.0062 0.0062 0.011
Total Tons AnnuallyVOC CO NOx SO2 PM10 PM2.5 CO2
Flare - baseline 0.001 0.003 0.000 0.000 0.016 0.016 0.028 Alternative 1, 2 or 3 0.003 0.010 0.001 0.000 0.048 0.048 0.084
Net Change 0.002 0.007 0.001 0.000 0.032 0.032 0.057
Table 2. Baseline and Alternatives 1, 2 and 3 Total Emissions with Net Change
Type VOC CO NOx SO2 PM10 PM2.5 CO2
Current Operations 0.43 6.03 13.16 0.61 0.77 0.59 1,554Alternative 1 Operations 4.23 47.22 112.61 5.00 4.77 3.96 12,650Net Change 3.81 41.19 99.45 4.40 4.00 3.37 11,096Alternative 2 Operations 3.26 36.35 86.71 3.85 3.68 3.05 9,740Net Change 2.84 30.32 73.55 3.25 2.91 2.47 8,186Alternative 3 Operations 3.90 43.48 103.64 4.61 4.39 3.65 11,644Net Change 3.47 37.45 90.48 4.00 3.63 3.06 10,090
Table 3. Baseline and Alternatives 1, 2 and 3 Total GHG Emissions with Net ChangeFuel/
enginelb/1000 lb fuel
T/yrType Flight hrs lb/hr CO2 CO2
Current OperationsF100-PW-220
A/B 30 41682 3214.59 2,002MIL 219 9679 3214.59 3,409
F110-GE-100A/B 37 18,088 3214.59 1,064MIL 268 11,358 3214.59 4,900
F404-GE-400A/B 120 15,851 3214.59 6,115
DODEC ID
Emissions T/Yr
MIL 880 7,739 3214.59 21,892Current Operations Totals 1,554 39,381
Alternative 1 OperationsF100-PW-220
A/B 360 41682 3214.59 24,118MIL 2640 9679 3214.59 41,071
F110-GE-100A/B 440 18,088 3214.59 12,793MIL 3227 11,358 3214.59 58,910
F404-GE-400A/B 120 15,851 3214.59 6,115MIL 880 7,739 3214.59 21,892
Alternative 1 Totals 7,667 164,899Net Change 6,113 125,518
Alternative 2 OperationsF100-PW-220
A/B 277 41682 3214.59 18,587MIL 2035 9679 3214.59 31,652
F110-GE-100A/B 339 18,088 3214.59 9,859MIL 2487 11,358 3214.59 45,400
F404-GE-400A/B 156 15,851 3214.59 7,949MIL 1144 7,739 3214.59 28,460
Alternative 2 Totals 6,438 141,907Net Change 4,884 102,525
Alternative 3 OperationsF100-PW-220
A/B 331 41682 3214.59 22,197MIL 2430 9679 3214.59 37,799
F110-GE-100A/B 405 18,088 3214.59 11,771MIL 2969 11,358 3214.59 54,203
F404-GE-400
A/B 156 15,851 3214.59 7,949MIL 1144 7,739 3214.59 28,460
Alternative 3 Totals 7,435 162,379Net Change 5,881 122,997
404 grams of CO2 per mile0.89 lb of CO2 per mile
Table 4. Comparison of GHG Emissions to Additional VehiclesCO2e
Tons/yrAlternative 1 Net Change 125,518 282,041,990 miles
24,525 additional cars driving 11,500 miles per year
Alternative 2 Net Change 102,525 230,377,033 miles20,033 additional cars driving 11,500 miles per year
Alternative 3 Net Change 122,997 276,378,275 miles24,033 additional cars driving 11,500 miles per year
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1. General Information
- Action Location
Base: HOLLOMAN AFB
State: New Mexico
County(s): Otero; Chaves; Eddy
Regulatory Area(s): NOT IN A REGULATORY AREA
- Action Title: Special Use Airspace Optimization at Holloman Air Force Base
- Project Number/s (if applicable):
- Projected Action Start Date: 1 / 2019
- Action Purpose and Need:
The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots
stationed at Holloman Air Force Base. The SUA in this region was created over 30 years ago and does not have
the necessary volume or capabilities to support the training needs for pilots of modern aircraft.
- Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2 with the following differences. The proposed
Talon MOA/ATCAA would be slightly smaller than what is proposed under Alternative 1 and the proposed
Lobos MOA would have a floor of 13,500 feet MSL. SUA no longer needed by the Air Force would be returned
to the National Airspace System including the lower portion of the existing Talon Low MOA (300 to 500 feet
AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine MOA, Bronco 1 MOA, and
Bronco 2 MOA.
- Point of Contact
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
- Activity List:
Activity Type Activity Title
2. Aircraft F-16 (F100-PW-220) aircraft cruising below 3000 feet AGL in airspace
3. Aircraft F-16 (F110-GE-100) aircraft cruising below 3000 feet AGL in airspace
4. Aircraft F-18 (F404-GE-400) aircraft cruising below 3000 feet AGL in airspace
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Emission factors and air emission estimating methods come from the United States Air Force’s Air Emissions Guide
for Air Force Stationary Sources, Air Emissions Guide for Air Force Mobile Sources, and Air Emissions Guide for
Air Force Transitory Sources.
2. Aircraft
2.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Current Operations
- Activity Location
County: Otero; Chaves; Eddy
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: F-16 (F100-PW-220) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Description:
F-16 (F100-PW-220) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2019
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.297317 PM 2.5 0.200233
CO 0.862174 CO2e 5,411
PM 10 0.221754
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.297317 PM 2.5 0.200233
CO 0.862174 CO2e 5,411
PM 10 0.221754
2.2 Aircraft & Engines
2.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F100-PW-220
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Original Aircraft Name:
Original Engine Name:
2.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1084.00 7.94 1.07 4.61 35.30 2.06 1.85 3234
Approach 3837.00 5.12 1.07 12.53 1.92 2.63 2.37 3234
Intermediate 5770.00 2.89 1.07 22.18 0.86 2.06 1.85 3234
Military 9679.00 1.79 1.07 29.32 0.86 1.33 1.20 3234
After Burn 41682.00 1.53 1.07 8.37 11.99 1.15 1.04 3234
2.3 Flight Operations
2.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 138.2
Takeoff [After Burn] (mins): 18.4
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
2.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
2.4 Auxiliary Power Unit (APU)
2.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
2.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
2.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
3. Aircraft
3.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Current Operations
- Activity Location
County: Catron; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: F-16 (F110-GE-100) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Description:
F-16 (F110-GE-100) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2019
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.047539 PM 2.5 0.102311
CO 2.866950 CO2e 5,964
PM 10 0.137725
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.047539 PM 2.5 0.102311
CO 2.866950 CO2e 5,964
PM 10 0.137725
3.2 Aircraft & Engines
3.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F110-GE-100
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
3.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1111.00 0.22 1.07 3.77 24.11 2.60 1.12 3234
Approach 5080.00 0.03 1.07 9.78 5.77 1.37 0.91 3234
Intermediate 7332.00 0.05 1.07 16.92 3.47 0.58 0.41 3234
Military 11358.00 0.04 1.07 29.00 3.38 0.14 0.00 3234
After Burn 18088.00 1.21 1.07 14.26 67.41 3.35 2.98 3234
3.3 Flight Operations
3.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 172
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Takeoff [After Burn] (mins): 22.8
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
3.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
3.4 Auxiliary Power Unit (APU)
3.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
3.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
3.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
2000: Conversion Factor pounds to tons
4. Aircraft
4.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Current Operations
- Activity Location
County: Catron; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: F-18 (F404-GE-400) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Description:
F-18 (F404-GE-400) aircraft cruising below 3000 feet AGL in Talon MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2019
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.079280 PM 2.5 0.267200
CO 2.298090 CO2e 28,007
PM 10 0.392004
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.079280 PM 2.5 0.267200
CO 2.298090 CO2e 28,007
PM 10 0.392004
4.2 Aircraft & Engines
4.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F/A-18C
Engine Model: F404-GE-400
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 2
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
4.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 685.00 3.39 1.07 1.70 110.18 4.47 3.10 3234
Approach 3111.00 0.04 1.07 7.86 2.02 1.46 0.87 3234
Intermediate 6464.00 0.07 1.07 17.03 1.54 1.57 0.90 3234
Military 7739.00 0.02 1.07 25.83 1.48 1.61 0.89 3234
After Burn 15851.00 1.85 1.07 5.43 50.31 3.57 3.21 3234
4.3 Flight Operations
4.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 117.7
Takeoff [After Burn] (mins): 15.6
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
4.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
4.4 Auxiliary Power Unit (APU)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
4.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
4.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
4.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
1. General Information: The Air Force’s Air Conformity Applicability Model (ACAM) was used to perform
an analysis to assess the potential air quality impact/s associated with the action in accordance with the Air Force
Instruction 32-7040, Air Quality Compliance And Resource Management; the Environmental Impact Analysis
Process (EIAP, 32 CFR 989); and the General Conformity Rule (GCR, 40 CFR 93 Subpart B). This report provides
a summary of the ACAM analysis of current operations.
a. Action Location:
Base: HOLLOMAN AFB
State: New Mexico
County(s): Otero; Chaves; Eddy
Regulatory Area(s): NOT IN A REGULATORY AREA
b. Action Title: Special Use Airspace Optimization at Holloman Air Force Base
c. Project Number/s (if applicable):
d. Projected Action Start Date: 1 / 2019
e. Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2 with the following differences. The proposed
Talon MOA/ATCAA would be slightly smaller than what is proposed under Alternative 1 and the proposed
Lobos MOA would have a floor of 13,500 feet MSL. SUA no longer needed by the Air Force would be returned
to the National Airspace System including the lower portion of the existing Talon Low MOA (300 to 500 feet
AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine MOA, Bronco 1 MOA, and
Bronco 2 MOA.
f. Point of Contact:
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
2. Air Impact Analysis: Based on the attainment status at the action location, the requirements of the General
Conformity Rule are:
_____ applicable
__X__ not applicable
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1. General Information
- Action Location
Base: HOLLOMAN AFB
State: New Mexico
County(s): Chaves; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Action Title: Special Use Airspace Optimization at Holloman Air Force Base
- Project Number/s (if applicable):
- Projected Action Start Date: 1 / 2022
- Action Purpose and Need:
The action is the proposed optimization of Special Use Airspace (SUA) to support the training of F-16 pilots
stationed at Holloman Air Force Base. The SUA in this region was created over 30 years ago and does not have
the necessary volume or capabilities to support the training needs for pilots of modern aircraft.
- Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
- Point of Contact
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
- Activity List:
Activity Type Activity Title
2. Aircraft Aircraft cruising below 3000 feet AGL in Talon MOA airspace
3. Aircraft Aircraft cruising below 3000 feet AGL in airspace
4. Aircraft Aircraft cruising below 3000 feet AGL in Talon MOA airspace
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Emission factors and air emission estimating methods come from the United States Air Force’s Air Emissions Guide
for Air Force Stationary Sources, Air Emissions Guide for Air Force Mobile Sources, and Air Emissions Guide for
Air Force Transitory Sources.
2. Aircraft
2.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Chaves; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Description:
F-16 (F100-PW-220) cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 3.576765 PM 2.5 2.407333
CO 10.368002 CO2e *65,189
PM 10 2.666530
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 3.576765 PM 2.5 2.407333
CO 10.368002 CO2e *65,189
PM 10 2.666530
*includes entire flight duration
2.2 Aircraft & Engines
2.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F100-PW-220
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
2.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1084.00 7.94 1.07 4.61 35.30 2.06 1.85 3234
Approach 3837.00 5.12 1.07 12.53 1.92 2.63 2.37 3234
Intermediate 5770.00 2.89 1.07 22.18 0.86 2.06 1.85 3234
Military 9679.00 1.79 1.07 29.32 0.86 1.33 1.20 3234
After Burn 41682.00 1.53 1.07 8.37 11.99 1.15 1.04 3234
2.3 Flight Operations
2.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1662.9
Takeoff [After Burn] (mins): 220.8
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
2.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
2.4 Auxiliary Power Unit (APU)
2.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
1 1 No T-62T-40-8
2.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
T-62T-40-8 272.6 0.493 0.289 1.216 3.759 0.131 0.037 910.8
2.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
3. Aircraft
3.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Chaves; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Description:
F-16 (F110-GE-100) cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.572843 PM 2.5 1.233119
CO 34.542609 CO2e *71,703
PM 10 1.659464
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.572843 PM 2.5 1.233119
CO 34.542609 CO2e *71,703
PM 10 1.659464
*includes entire flight duration
3.2 Aircraft & Engines
3.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F110-GE-100
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
3.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1111.00 0.22 1.07 3.77 24.11 2.60 1.12 3234
Approach 5080.00 0.03 1.07 9.78 5.77 1.37 0.91 3234
Intermediate 7332.00 0.05 1.07 16.92 3.47 0.58 0.41 3234
Military 11358.00 0.04 1.07 29.00 3.38 0.14 0.00 3234
After Burn 18088.00 1.21 1.07 14.26 67.41 3.35 2.98 3234
3.3 Flight Operations
3.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 2069.4
Takeoff [After Burn] (mins): 274.8
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
3.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
3.4 Auxiliary Power Unit (APU)
3.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
3.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
3.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
4. Aircraft
4.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Chaves; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Description:
F-18 (F404-GE-400) cruising below 3000 feet AGL in Talon Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.079280 PM 2.5 0.267200
CO 2.298090 CO2e *28,007
PM 10 0.392004
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.079280 PM 2.5 0.267200
CO 2.298090 CO2e *28,007
PM 10 0.392004
*includes entire flight duration
4.2 Aircraft & Engines
4.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F/A-18C
Engine Model: F404-GE-400
Primary Function: Combat
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Aircraft has After burn: Yes
Number of Engines: 2
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
4.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 685.00 3.39 1.07 1.70 110.18 4.47 3.10 3234
Approach 3111.00 0.04 1.07 7.86 2.02 1.46 0.87 3234
Intermediate 6464.00 0.07 1.07 17.03 1.54 1.57 0.90 3234
Military 7739.00 0.02 1.07 25.83 1.48 1.61 0.89 3234
After Burn 15851.00 1.85 1.07 5.43 50.31 3.57 3.21 3234
4.3 Flight Operations
4.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 117.7
Takeoff [After Burn] (mins): 15.6
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
4.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
4.4 Auxiliary Power Unit (APU)
4.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
4.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
4.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
Total combined direct and indirect emissions associated with the current operations were estimated through ACAM
on a calendar-year basis.
Analysis Summary:
2019 Pollutant Action Emissions (ton/yr)
NOT IN A REGULATORY AREA
VOC 0.424
NOx 13.160
CO 6.027
SOx 0.605
PM 10 0.751
PM 2.5 0.570
Pb 0.000
NH3 0.000
CO2e *39,381
*entire flight duration
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
1. General Information: The Air Force’s Air Conformity Applicability Model (ACAM) was used to perform
an analysis to assess the potential air quality impact/s associated with the action in accordance with the Air Force
Instruction 32-7040, Air Quality Compliance And Resource Management; the Environmental Impact Analysis
Process (EIAP, 32 CFR 989); and the General Conformity Rule (GCR, 40 CFR 93 Subpart B). This report provides
a summary of the ACAM analysis.
a. Action Location:
Base: HOLLOMAN AFB
State: New Mexico
County(s): Chaves; Eddy; Otero
Regulatory Area(s): NOT IN A REGULATORY AREA
b. Action Title: Special Use Airspace Optimization at Holloman Air Force Base
c. Project Number/s (if applicable):
d. Projected Action Start Date: 1 / 2022
e. Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
f. Point of Contact:
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
2. Air Impact Analysis: Based on the attainment status at the action location, the requirements of the General
Conformity Rule are:
_____ applicable
__X__ not applicable
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
Total combined direct and indirect emissions associated with the action were estimated through ACAM on a
calendar-year basis for the “worst-case” and “steady state” (net gain/loss upon action fully implemented) emissions.
“Air Quality Indicators” were used to provide an indication of the significance of potential impacts to air quality.
These air quality indicators are EPA PSD thresholds that are applied out of context to their intended use. Therefore,
these indicators do not trigger a regulatory requirement; however, they provide a warning that the action is
potentially significant. It is important to note that these indicators only provide a clue to the potential impacts to air
quality.
An Air Quality Indicator value of 250 tons/yr is used based on EPA’s PSD threshold. Therefore, the worst-case year
emissions were compared against the Air Quality Indicator and are summarized below.
Analysis Summary:
2022 - (Steady State) Pollutant Action Emissions
(ton/yr)
AIR QUALITY INDICATOR
Threshold (ton/yr) Exceedance (Yes or No)
NOT IN A REGULATORY AREA
VOC 4.229 250 No
NOx 112.605 250 No
CO 47.209 250 No
SOx 5.003 250 No
PM 10 4.718 250 No
PM 2.5 3.908 250 No
CO2e *164,899 NA NA
*entire flight duration
None of estimated emissions associated with this action are above the air quality indicators, indicating no
significant impact to air quality; therefore, no further air assessment is needed.
___________________________________________________ 8/20/19
Lesley Hamilton, Sr Associate DATE
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1. General Information
- Action Location
Base: HOLLOMAN AFB
State: New Mexico and Arizona
County(s): Catron; Hidalgo; Otero; Sierra; Socorro, NM and Graham, AZ
Regulatory Area(s): NOT IN A REGULATORY AREA
- Action Title: Special Use Airspace Optimization at Holloman Air Force Base
- Project Number/s (if applicable):
- Projected Action Start Date: 1 / 2022
- Action Purpose and Need:
The action is the proposed optimization of Special Use Airspace (SUA) to support the training of F-16 pilots
stationed at Holloman Air Force Base. The SUA in this region was created over 30 years ago and does not have
the necessary volume or capabilities to support the training needs for pilots of modern aircraft.
- Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
- Point of Contact
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
- Activity List:
Activity Type Activity Title
2. Aircraft Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA
airspace
3. Aircraft Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA
airspace
4. Aircraft Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA
airspace
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Emission factors and air emission estimating methods come from the United States Air Force’s Air Emissions Guide
for Air Force Stationary Sources, Air Emissions Guide for Air Force Mobile Sources, and Air Emissions Guide for
Air Force Transitory Sources.
2. Aircraft
2.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Hidalgo; Otero; Sierra; Socorro, NM and Graham, AZ
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Description:
F-16 (F100-PW-220) cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 2.757483 PM 2.5 1.855580
CO 7.996226 CO2e *50,239
PM 10 2.055472
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 2.757483 PM 2.5 1.855580
CO 7.996226 CO2e *50,239
PM 10 2.055472
*includes entire flight duration
2.2 Aircraft & Engines
2.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F100-PW-220
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
2.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1084.00 7.94 1.07 4.61 35.30 2.06 1.85 3234
Approach 3837.00 5.12 1.07 12.53 1.92 2.63 2.37 3234
Intermediate 5770.00 2.89 1.07 22.18 0.86 2.06 1.85 3234
Military 9679.00 1.79 1.07 29.32 0.86 1.33 1.20 3234
After Burn 41682.00 1.53 1.07 8.37 11.99 1.15 1.04 3234
2.3 Flight Operations
2.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1281.7
Takeoff [After Burn] (mins): 170.2
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
2.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
2.4 Auxiliary Power Unit (APU)
2.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
1 1 No T-62T-40-8
2.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
T-62T-40-8 272.6 0.493 0.289 1.216 3.759 0.131 0.037 910.8
2.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
3. Aircraft
3.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Hidalgo; Otero; Sierra; Socorro, NM and Graham, AZ
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Description:
F-16 (F110-GE-100) cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.441519 PM 2.5 0.950417
CO 26.623854 CO2e *55,259
PM 10 1.279036
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.441519 PM 2.5 0.950417
CO 26.623854 CO2e *55,259
PM 10 1.279036
*includes entire flight duration
3.2 Aircraft & Engines
3.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F110-GE-100
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
3.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1111.00 0.22 1.07 3.77 24.11 2.60 1.12 3234
Approach 5080.00 0.03 1.07 9.78 5.77 1.37 0.91 3234
Intermediate 7332.00 0.05 1.07 16.92 3.47 0.58 0.41 3234
Military 11358.00 0.04 1.07 29.00 3.38 0.14 0.00 3234
After Burn 18088.00 1.21 1.07 14.26 67.41 3.35 2.98 3234
3.3 Flight Operations
3.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1595.1
Takeoff [After Burn] (mins): 211.8
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
3.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
3.4 Auxiliary Power Unit (APU)
3.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
3.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
3.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
4. Aircraft
4.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Hidalgo; Otero; Sierra; Socorro, NM and Graham, AZ
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Description:
F-18 (F404-GE-400) cruising below 3000 feet AGL in Smitty Low and Lobos Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.059460 PM 2.5 0.200429
CO 1.723615 CO2e *36,409
PM 10 0.294055
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.059460 PM 2.5 0.200429
CO 1.723615 CO2e *36,409
PM 10 0.294055
*includes entire flight duration
4.2 Aircraft & Engines
4.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F/A-18C
Engine Model: F404-GE-400
Primary Function: Combat
Aircraft has After burn: Yes
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Number of Engines: 2
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
4.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 685.00 3.39 1.07 1.70 110.18 4.47 3.10 3234
Approach 3111.00 0.04 1.07 7.86 2.02 1.46 0.87 3234
Intermediate 6464.00 0.07 1.07 17.03 1.54 1.57 0.90 3234
Military 7739.00 0.02 1.07 25.83 1.48 1.61 0.89 3234
After Burn 15851.00 1.85 1.07 5.43 50.31 3.57 3.21 3234
4.3 Flight Operations
4.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 88.3
Takeoff [After Burn] (mins): 11.7
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
4.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
4.4 Auxiliary Power Unit (APU)
4.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
4.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
4.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1. General Information
- Action Location
Base: HOLLOMAN AFB
State: New Mexico and Arizona
County(s): Grant County, NM and Greenlee County, AZ
Regulatory Area(s): Grant Co, NM and Greenlee Co, AZ
- Action Title: Special Use Airspace Optimization at Holloman Air Force Base
- Project Number/s (if applicable):
- Projected Action Start Date: 1 / 2022
- Action Purpose and Need:
The action is the proposed optimization of Special Use Airspace (SUA) to support the training of F-16 pilots
stationed at Holloman Air Force Base. The SUA in this region was created over 30 years ago and does not have
the necessary volume or capabilities to support the training needs for pilots of modern aircraft.
- Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
- Point of Contact
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
- Activity List:
Activity Type Activity Title
2. Aircraft Aircraft cruising below 3000 feet AGL in Lobos Low MOA airspace
3. Aircraft Aircraft cruising below 3000 feet AGL in Lobos Low MOA airspace
4. Aircraft Aircraft cruising below 3000 feet AGL in Lobos Low MOA airspace
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Emission factors and air emission estimating methods come from the United States Air Force’s Air Emissions Guide
for Air Force Stationary Sources, Air Emissions Guide for Air Force Mobile Sources, and Air Emissions Guide for
Air Force Transitory Sources.
2. Aircraft
2.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Grant County, NM and Greenlee County, AZ
Regulatory Area(s): Grant Co, NM and Greenlee Co, AZ
- Activity Title: Aircraft cruising below 3000 feet AGL in Lobos Low MOA airspace
- Activity Description:
F-16 (F100-PW-220) cruising below 3000 feet AGL in Lobos Low MOA
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 2.757483 PM 2.5 1.855580
CO 7.996226 CO2e *50,239
PM 10 2.055472
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 2.757483 PM 2.5 1.855580
CO 7.996226 CO2e *50,239
PM 10 2.055472
*includes entire flight duration
2.2 Aircraft & Engines
2.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F100-PW-220
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
2.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1084.00 7.94 1.07 4.61 35.30 2.06 1.85 3234
Approach 3837.00 5.12 1.07 12.53 1.92 2.63 2.37 3234
Intermediate 5770.00 2.89 1.07 22.18 0.86 2.06 1.85 3234
Military 9679.00 1.79 1.07 29.32 0.86 1.33 1.20 3234
After Burn 41682.00 1.53 1.07 8.37 11.99 1.15 1.04 3234
2.3 Flight Operations
2.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1281.7
Takeoff [After Burn] (mins): 170.2
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
2.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
2.4 Auxiliary Power Unit (APU)
2.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
2.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
2.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
3. Aircraft
3.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Grant County, NM and Greenlee County, AZ
Regulatory Area(s): Grant Co, NM and Greenlee Co, AZ
- Activity Title: Aircraft cruising below 3000 feet AGL in airspace
- Activity Description:
F-16 (F110-GE-100) cruising below 3000 feet AGL in Lobos Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.441519 PM 2.5 0.950417
CO 26.623854 CO2e *55,259
PM 10 1.279036
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.441519 PM 2.5 0.950417
CO 26.623854 CO2e *55,259
PM 10 1.279036
*includes entire flight duration
3.2 Aircraft & Engines
3.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F110-GE-100
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
3.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1111.00 0.22 1.07 3.77 24.11 2.60 1.12 3234
Approach 5080.00 0.03 1.07 9.78 5.77 1.37 0.91 3234
Intermediate 7332.00 0.05 1.07 16.92 3.47 0.58 0.41 3234
Military 11358.00 0.04 1.07 29.00 3.38 0.14 0.00 3234
After Burn 18088.00 1.21 1.07 14.26 67.41 3.35 2.98 3234
3.3 Flight Operations
3.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1595.1
Takeoff [After Burn] (mins): 211.8
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
3.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
3.4 Auxiliary Power Unit (APU)
3.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
3.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
3.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
4. Aircraft
4.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Grant County, NM and Greenlee County, AZ
Regulatory Area(s): Grant Co, NM and Greenlee Co, AZ
- Activity Title: Aircraft cruising below 3000 feet AGL in Lobos Low MOA airspace
- Activity Description:
F-18 (F404-GE-400) cruising below 3000 feet AGL in Lobos Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.059460 PM 2.5 0.200429
CO 1.723615 CO2e *36,409
PM 10 0.294055
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.059460 PM 2.5 0.200429
CO 1.723615 CO2e *36,409
PM 10 0.294055
*includes entire flight duration
4.2 Aircraft & Engines
4.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F/A-18C
Engine Model: F404-GE-400
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 2
- Aircraft & Engine Surrogate
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
4.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 685.00 3.39 1.07 1.70 110.18 4.47 3.10 3234
Approach 3111.00 0.04 1.07 7.86 2.02 1.46 0.87 3234
Intermediate 6464.00 0.07 1.07 17.03 1.54 1.57 0.90 3234
Military 7739.00 0.02 1.07 25.83 1.48 1.61 0.89 3234
After Burn 15851.00 1.85 1.07 5.43 50.31 3.57 3.21 3234
4.3 Flight Operations
4.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 88.3
Takeoff [After Burn] (mins): 11.7
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
4.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
4.4 Auxiliary Power Unit (APU)
4.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
4.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
4.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF CONFORMITY ANALYSIS (ROCA)
1. General Information: The Air Force’s Air Conformity Applicability Model (ACAM) was used to perform
an analysis to assess the potential air quality impact/s associated with the action in accordance with the Air Force
Instruction 32-7040, Air Quality Compliance And Resource Management; the Environmental Impact Analysis
Process (EIAP, 32 CFR 989); and the General Conformity Rule (GCR, 40 CFR 93 Subpart B). This report provides
a summary of the ACAM analysis.
a. Action Location:
Base: HOLLOMAN AFB
State: New Mexico, Arizona
County(s): Grant, NM and Greenlee, AZ
Regulatory Area(s): Grant Co, NM and Greenlee Co, AZ
b. Action Title: Special Use Airspace Optimization at Holloman Air Force Base
c. Project Number/s (if applicable):
d. Projected Action Start Date: 1 / 2022
e. Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
f. Point of Contact:
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
2. Analysis: Total combined direct and indirect emissions associated with the action were estimated through
ACAM on a calendar-year basis for the “worst-case” and “steady state” (net gain/loss upon action fully
implemented) emissions. General Conformity under the Clean Air Act, Section 1.76 has been evaluated for the
action described above according to the requirements of 40 CFR 93, Subpart B.
Based on the analysis, the requirements of this rule are: _____ applicable
__X__ not applicable
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF CONFORMITY ANALYSIS (ROCA)
Conformity Analysis Summary:
2022 - (Steady State)
Pollutant
Action
Emissions
(ton/yr)
GENERAL CONFORMITY Air Quality Indicator
Threshold
(ton/yr)
Exceedance
(Yes or No)
Threshold
(ton/yr)
Exceedance
(Yes or No)
Grant Co, NM and Greenlee, AZ
VOC 3.258 250 No
NOx 86.711 250 No
CO 36.344 250 No
SOx 3.852 100 No NA NA
PM 10 3.629 250 No
PM 2.5 3.006 250 No
CO2e *141,907 NA NA
*entire flight duration
None of estimated emissions associated with this action are above the conformity threshold values established
at 40 CFR 93.153 (b); Therefore, the requirements of the General Conformity Rule are not applicable.
___________________________________________________________ 8/19/19
Lesley Hamilton, Sr Associate DATE
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
1. General Information
- Action Location
Base: HOLLOMAN AFB
State: New Mexico
County(s): Catron; Chaves; Eddy; Otero; Sierra; Socorro
Regulatory Area(s): NOT IN A REGULATORY AREA
- Action Title: Special Use Airspace Optimization at Holloman Air Force Base
- Project Number/s (if applicable):
- Projected Action Start Date: 1 / 2022
- Action Purpose and Need:
The action is the proposed optimization of Special Use Airspace (SUA) to support the training of F-16 pilots
stationed at Holloman Air Force Base. The SUA in this region was created over 30 years ago and does not have
the necessary volume or capabilities to support the training needs for pilots of modern aircraft.
- Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
- Point of Contact
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
- Activity List:
Activity Type Activity Title
2. Aircraft Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA
airspace
3. Aircraft Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA
airspace
4. Aircraft Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA
airspace
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Emission factors and air emission estimating methods come from the United States Air Force’s Air Emissions Guide
for Air Force Stationary Sources, Air Emissions Guide for Air Force Mobile Sources, and Air Emissions Guide for
Air Force Transitory Sources.
2. Aircraft
2.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Chaves; Eddy; Otero; Sierra; Socorro
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Description:
F-16 (F100-PW-220) cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 3.291640 PM 2.5 2.215314
CO 9.542961 CO2e *59,995
PM 10 2.453871
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 3.291640 PM 2.5 2.215314
CO 9.542961 CO2e *59,995
PM 10 2.453871
*includes entire flight duration
2.2 Aircraft & Engines
2.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F100-PW-220
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
2.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1084.00 7.94 1.07 4.61 35.30 2.06 1.85 3234
Approach 3837.00 5.12 1.07 12.53 1.92 2.63 2.37 3234
Intermediate 5770.00 2.89 1.07 22.18 0.86 2.06 1.85 3234
Military 9679.00 1.79 1.07 29.32 0.86 1.33 1.20 3234
After Burn 41682.00 1.53 1.07 8.37 11.99 1.15 1.04 3234
2.3 Flight Operations
2.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1530.2
Takeoff [After Burn] (mins): 203.2
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
2.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
2.4 Auxiliary Power Unit (APU)
2.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
1 1 No T-62T-40-8
2.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
T-62T-40-8 272.6 0.493 0.289 1.216 3.759 0.131 0.037 910.8
2.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
3. Aircraft
3.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Chaves; Eddy; Otero; Sierra; Socorro
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Description:
F-16 (F110-GE-100) cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.527185 PM 2.5 1.134846
CO 31.789182 CO2e *65,974
PM 10 1.527191
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.527185 PM 2.5 1.134846
CO 31.789182 CO2e *65,974
PM 10 1.527191
*includes entire flight duration
3.2 Aircraft & Engines
3.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F-16C
Engine Model: F110-GE-100
Primary Function: Combat
Aircraft has After burn: Yes
Number of Engines: 1
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
3.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 1111.00 0.22 1.07 3.77 24.11 2.60 1.12 3234
Approach 5080.00 0.03 1.07 9.78 5.77 1.37 0.91 3234
Intermediate 7332.00 0.05 1.07 16.92 3.47 0.58 0.41 3234
Military 11358.00 0.04 1.07 29.00 3.38 0.14 0.00 3234
After Burn 18088.00 1.21 1.07 14.26 67.41 3.35 2.98 3234
3.3 Flight Operations
3.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 1904.3
Takeoff [After Burn] (mins): 252.9
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
3.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
3.4 Auxiliary Power Unit (APU)
3.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
3.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
3.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
4. Aircraft
4.1 General Information & Timeline Assumptions
- Add or Remove Activity from Baseline? Add
- Activity Location
County: Catron; Chaves; Eddy; Otero; Sierra; Socorro
Regulatory Area(s): NOT IN A REGULATORY AREA
- Activity Title: Aircraft cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Description:
F-18 (F404-GE-400) cruising below 3000 feet AGL in Talon Low and Smitty Low MOA airspace
- Activity Start Date
Start Month: 1
Start Year: 2022
- Activity End Date
Indefinite: Yes
End Month: N/A
End Year: N/A
- Activity Emissions:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.073674 PM 2.5 0.247670
CO 2.134898 CO2e *36,409
PM 10 0.363113
- Activity Emissions [Flight Operations (includes Trim Test & APU) part]:
Pollutant Emissions Per Year (TONs) Pollutant Emissions Per Year (TONs)
VOC 0.073674 PM 2.5 0.247670
CO 2.134898 CO2e *36,409
PM 10 0.363113
*includes entire flight duration
4.2 Aircraft & Engines
4.2.1 Aircraft & Engines Assumptions
- Aircraft & Engine
Aircraft Designation: F/A-18C
Engine Model: F404-GE-400
Primary Function: Combat
Aircraft has After burn: Yes
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
Number of Engines: 2
- Aircraft & Engine Surrogate
Is Aircraft & Engine a Surrogate? No
Original Aircraft Name:
Original Engine Name:
4.2.2 Aircraft & Engines Emission Factor(s)
- Aircraft & Engine Emissions Factors (lb/1000lb fuel)
Fuel Flow VOC SOx NOx CO PM 10 PM 2.5 CO2e
Idle 685.00 3.39 1.07 1.70 110.18 4.47 3.10 3234
Approach 3111.00 0.04 1.07 7.86 2.02 1.46 0.87 3234
Intermediate 6464.00 0.07 1.07 17.03 1.54 1.57 0.90 3234
Military 7739.00 0.02 1.07 25.83 1.48 1.61 0.89 3234
After Burn 15851.00 1.85 1.07 5.43 50.31 3.57 3.21 3234
4.3 Flight Operations
4.3.1 Flight Operations Assumptions
- Flight Operations
Number of Aircraft: 1
Number of Annual LTOs (Landing and Take-off) cycles for all Aircraft: 10
Number of Annual TGOs (Touch-and-Go) cycles for all Aircraft: 0
Number of Annual Trim Test(s) per Aircraft: 0
- Default Settings Used: No
- Flight Operations TIMs (Time In Mode)
Taxi/Idle Out [Idle] (mins): 0
Takeoff [Military] (mins): 108.8
Takeoff [After Burn] (mins): 14.5
Climb Out [Intermediate] (mins): 0
Approach [Approach] (mins): 0
Taxi/Idle In [Idle] (mins): 0
- Trim Test
Idle (mins): 0
Approach (mins): 0
Intermediate (mins): 0
Military (mins): 0
AfterBurn (mins): 0
4.3.2 Flight Operations Formula(s)
- Aircraft Emissions per Mode for LTOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * LTO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
LTO: Number of Landing and Take-off Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for LTOs per Year
AELTO = AEMIDLE_IN + AEMIDLE_OUT + AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AELTO: Aircraft Emissions (TONs)
AEMIDLE_IN: Aircraft Emissions for Idle-In Mode (TONs)
AEMIDLE_OUT: Aircraft Emissions for Idle-Out Mode (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for TGOs per Year
AEMPOL = (TIM / 60) * (FC / 1000) * EF * NE * TGO / 2000
AEMPOL: Aircraft Emissions per Pollutant & Mode (TONs)
TIM: Time in Mode (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
TGO: Number of Touch-and-Go Cycles (for all aircraft)
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for TGOs per Year
AETGO = AEMAPPROACH + AEMCLIMBOUT + AEMTAKEOFF
AETGO: Aircraft Emissions (TONs)
AEMAPPROACH: Aircraft Emissions for Approach Mode (TONs)
AEMCLIMBOUT: Aircraft Emissions for Climb-Out Mode (TONs)
AEMTAKEOFF: Aircraft Emissions for Take-Off Mode (TONs)
- Aircraft Emissions per Mode for Trim per Year
AEPSPOL = (TD / 60) * (FC / 1000) * EF * NE * NA * NTT / 2000
AEPSPOL: Aircraft Emissions per Pollutant & Power Setting (TONs)
TD: Test Duration (min)
60: Conversion Factor minutes to hours
FC: Fuel Flow Rate (lb/hr)
1000: Conversion Factor pounds to 1000pounds
EF: Emission Factor (lb/1000lb fuel)
NE: Number of Engines
NA: Number of Aircraft
NTT: Number of Trim Test
2000: Conversion Factor pounds to TONs
- Aircraft Emissions for Trim per Year
AETRIM = AEPSIDLE + AEPSAPPROACH + AEPSINTERMEDIATE + AEPSMILITARY + AEPSAFTERBURN
AETRIM: Aircraft Emissions (TONs)
AEPSIDLE: Aircraft Emissions for Idle Power Setting (TONs)
DETAIL AIR CONFORMITY APPLICABILITY MODEL REPORT
AEPSAPPROACH: Aircraft Emissions for Approach Power Setting (TONs)
AEPSINTERMEDIATE: Aircraft Emissions for Intermediate Power Setting (TONs)
AEPSMILITARY: Aircraft Emissions for Military Power Setting (TONs)
AEPSAFTERBURN: Aircraft Emissions for After Burner Power Setting (TONs)
4.4 Auxiliary Power Unit (APU)
4.4.1 Auxiliary Power Unit (APU) Assumptions
- Default Settings Used: No
- Auxiliary Power Unit (APU)
Number of APU
per Aircraft
Operation
Hours for Each
LTO
Exempt
Source?
Designation Manufacturer
4.4.2 Auxiliary Power Unit (APU) Emission Factor(s)
- Auxiliary Power Unit (APU) Emission Factor (lb/hr)
Designation Fuel
Flow
VOC SOx NOx CO PM 10 PM 2.5 CO2e
4.4.3 Auxiliary Power Unit (APU) Formula(s)
- Auxiliary Power Unit (APU) Emissions per Year
APUPOL = APU * OH * LTO * EFPOL / 2000
APUPOL: Auxiliary Power Unit (APU) Emissions per Pollutant (TONs)
APU: Number of Auxiliary Power Units
OH: Operation Hours for Each LTO (hour)
LTO: Number of LTOs
EFPOL: Emission Factor for Pollutant (lb/hr)
2000: Conversion Factor pounds to tons
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
1. General Information: The Air Force’s Air Conformity Applicability Model (ACAM) was used to perform
an analysis to assess the potential air quality impact/s associated with the action in accordance with the Air Force
Instruction 32-7040, Air Quality Compliance And Resource Management; the Environmental Impact Analysis
Process (EIAP, 32 CFR 989); and the General Conformity Rule (GCR, 40 CFR 93 Subpart B). This report provides
a summary of the ACAM analysis.
a. Action Location:
Base: HOLLOMAN AFB
State: New Mexico
County(s): Catron; Chaves; Eddy; Otero; Sierra; Socorro
Regulatory Area(s): NOT IN A REGULATORY AREA
b. Action Title: Special Use Airspace Optimization at Holloman Air Force Base
c. Project Number/s (if applicable):
d. Projected Action Start Date: 1 / 2022
e. Action Description:
Under the Proposed Action, the Air Force would modify the dimensions and altitudes of training airspace in the
vicinity of Holloman AFB. The proposed airspace modifications would result in appropriately sized and
configured training airspace needed to conduct IQT activities. The modified airspace would improve airspace
availability and scheduling flexibility for training activities.
Under Alternative 1, the Talon MOA would be reconfigured and expanded. Training operations, to include the
use of defensive countermeasures, would occur throughout the proposed airspace.
Under Alternative 2, the Cato and Smitty MOAs would be reconfigured and expanded, and Lobos MOA would
be established. Training operations, to include the use of defensive countermeasures, would occur throughout
the proposed airspace.
Alternative 3 would be a combination of Alternatives 1 and 2, the proposed Talon MOA/ATCAA would be
slightly smaller than what is proposed under Alternative 1 and the proposed Lobos MOA would have a floor of
13,500 feet MSL as opposed to the 500 feet AGL proposed under Alternative 2. SUA no longer needed by the
Air Force would be returned to the National Airspace System including the lower portion of the existing Talon
Low MOA (300 to 500 feet AGL), the northern portion of the existing Cato and Smitty MOAs, Valentine
MOA, Bronco 1 MOA, and Bronco 2 MOA.
f. Point of Contact:
Name: Lesley Hamilton
Title: Sr Associate
Organization: Cardno
Email:
Phone Number:
2. Air Impact Analysis: Based on the attainment status at the action location, the requirements of the General
Conformity Rule are:
_____ applicable
__X__ not applicable
AIR CONFORMITY APPLICABILITY MODEL REPORT
RECORD OF AIR ANALYSIS (ROAA)
Total combined direct and indirect emissions associated with the action were estimated through ACAM on a
calendar-year basis for the “worst-case” and “steady state” (net gain/loss upon action fully implemented) emissions.
“Air Quality Indicators” were used to provide an indication of the significance of potential impacts to air quality.
These air quality indicators are EPA PSD thresholds that are applied out of context to their intended use. Therefore,
these indicators do not trigger a regulatory requirement; however, they provide a warning that the action is
potentially significant. It is important to note that these indicators only provide a clue to the potential impacts to air
quality.
An Air Quality Indicator value of 250 tons/yr is used based on EPA’s PSD threshold. Therefore, the worst-case year
emissions were compared against the Air Quality Indicator and are summarized below.
Analysis Summary:
2022 - (Steady State) Pollutant Action Emissions
(ton/yr)
AIR QUALITY INDICATOR
Threshold (ton/yr) Exceedance (Yes or No)
NOT IN A REGULATORY AREA
VOC 3.892 250 No
NOx 103.640 250 No
CO 43.467 250 No
SOx 4.605 250 No
PM 10 4.344 250 No
PM 2.5 3.598 250 No
CO2e *162,379 NA NA
*entire flight duration
None of estimated emissions associated with this action are above the air quality indicators, indicating no
significant impact to air quality; therefore, no further air assessment is needed.
___________________________________________________________ 8/21/19
Lesley Hamilton, Sr Associate DATE