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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

APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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Page 1: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

Draft EIS for SUA Optimization to Support Existing Aircraft at Holloman AFB, NM

Appendix G G-1

APPENDIX G

AIR QUALITY SUPPORTING DOCUMENTS

Page 2: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

Draft EIS for SUA Optimization to Support Existing Aircraft at Holloman AFB, NM

Appendix G G-2

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Page 3: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 4: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 5: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 6: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 7: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 8: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 9: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 10: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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)

Page 11: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

Page 12: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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

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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)

Page 14: APPENDIX G AIR QUALITY SUPPORTING DOCUMENTS€¦ · The action is the proposed optimization of special use Airspace (SUA) to support the training of F-16 pilots stationed at Holloman

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)

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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:

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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

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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)

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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

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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

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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

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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

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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

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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)

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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

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- 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

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- 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)

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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

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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

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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)

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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)

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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

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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

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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

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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

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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

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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

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- 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

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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)

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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

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- 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

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- 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

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- 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

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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

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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

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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)

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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

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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

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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

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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)

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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)

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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

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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)

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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

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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)

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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

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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

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- 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)

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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

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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

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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

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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

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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

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- 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

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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)

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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

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- 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

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- 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

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- 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

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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

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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

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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)

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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

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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

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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