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Risk Assessment Method to Support Modification of Airfield Separation Standards (2011)

Chapter: Appendix B - Collision Risk Model

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Suggested Citation:"Appendix B - Collision Risk Model." National Academies of Sciences, Engineering, and Medicine. 2011. Risk Assessment Method to Support Modification of Airfield Separation Standards. Washington, DC: The National Academies Press. doi: 10.17226/14501.
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Aircraft Name Manufacturer ICAOCode Wingspan (ft) Length (ft) Height (ft) Engine Type Engines (#) MTOW (lb) Takeoff Distance (ft) Landing Distance (ft) V2 (kts) Approach Speed (kts) EMB-110 Bandeirante Embraer E110 50.2 46.6 16.1 Turboprop 2 13,007 3,937.0 4,265.1 90 92 EMB-120 Brasilia Embraer E120 65.0 65.6 21.0 Turboprop 2 26,455 4,593.2 4,593.2 120 120 EMB-145 Embraer E145 65.7 98.0 22.2 Jet 2 46,734 6,561.7 4,429.1 130 135 EMB-145XR Embraer E45X 68.9 98.0 22.2 Jet 2 46,734 6,561.7 4,429.1 130 135 Embraer 140 Embraer E140 65.7 93.3 22.1 Jet 2 46,518 6,069.6 4,527.6 130 135 Embraer 175 Embraer E175 85.3 103.9 31.9 Jet 2 82,673 7,362.2 4,137.1 140 145 Embraer 195 Embraer E195 94.2 126.8 34.6 Jet 2 107,564 7,149.0 4,206.0 140 145 ERJ-135 Embraer E135 65.7 86.4 22.2 Jet 2 44,070 5,774.3 4,461.9 125 130 ERJ-170 Embraer E170 85.3 98.1 32.3 Jet 2 79,344 5,393.7 4,176.5 140 145 ERJ-190 Embraer E190 94.2 118.9 34.7 Jet 2 105,359 6,745.4 4,340.6 140 145 328 Jet Envoy 3 Fairchild- Dornier J328 68.8 69.9 23.6 Jet 2 33,510 4,265.1 3,937.0 135 120 Fairchild-Dornier 328 Fairchild- Dornier D328 68.8 69.3 23.9 Turboprop 2 30,843 3,280.8 3,937.0 110 110 F-27 Friendship Fokker F27 95.1 75.8 27.9 Turboprop 2 44,996 2,296.6 1,968.5 100 120 F-28 Fellowship Fokker F28 88.8 89.9 27.9 Jet 2 72,995 5,577.4 3,280.8 135 125 Fokker 100 Fokker F100 92.2 116.5 27.9 Jet 2 95,659 5,577.4 4,593.2 135 130 Fokker 50 Fokker F50 95.1 82.7 27.2 Turboprop 2 43,982 3,608.9 3,608.9 120 120 Fokker 70 Fokker F70 95.5 101.4 27.9 Turboprop 2 71,981 4,265.1 3,937.0 125 120 Greyhound C2 Grumman C2 80.7 57.7 18.4 Turboprop 2 54,426 2,608.3 1,476.4 105 105 695 JetProp Commander 980/1000 Gulfstream Aerospace AC95 52.2 43.0 15.1 Turboprop 2 11,199 1,640.4 1,640.4 100 500 G-1159 Gulfstream 2 Gulfstream Aerospace GLF2 68.1 79.1 * Jet 2 65,301 * * * 141 G-1159A Gulfstream 3 Gulfstream Aerospace GLF3 77.8 83.0 24.6 Jet 2 69,710 5,905.5 3,280.8 145 136 G-1159C Gulfstream 4 Gulfstream Aerospace GLF4 77.8 88.3 24.3 Jet 2 73,193 5,249.3 3,280.8 145 128 G-1159D Gulfstream 5 Gulfstream Aerospace GLF5 93.5 96.5 25.9 Jet 2 90,689 5,150.9 2,900.3 145 145 Ilyushin IL-62 Ilyushin IL62 141.7 174.2 40.7 Jet 4 363,763 10,826.8 7,545.9 150 152 Ilyushin IL-96 Ilyushin IL96 197.2 181.4 57.4 Jet 4 595,248 9,186.4 6,561.7 150 150 1124 Westwind Israel Aerospace Industries WW24 44.9 52.2 15.7 Jet 2 22,928 4,839.2 2,460.6 125 129 Table F-1. (Continued).

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TRB’s Airport Cooperative Research Program (ACRP) Report 51: Risk Assessment Method to Support Modification of Airfield Separation Standards is intended to be used to support requests for modification of standards in those circumstances where the design criteria for separations between taxiways/taxilanes and other taxiways/taxilanes and fixed or movable objects as well as separations between taxiways and runways cannot be met.

The following appendices, included in the pdf and print version of the report, will be helpful in understanding the methodology.

  • Appendix A: Risk Assessment Methodology presents a methodology for five different types of circumstances: taxiway/taxilane to taxiway, taxiway to object, taxilane to taxilane, taxilane to an object, and runway to taxiway/taxilane or object;
  • Appendix F: Aircraft Database Summary presents a summary of aircraft characteristics by model; and
  • Appendix H: Analysis of MOS Cases summarizes information collected in the modification of standards survey and presents results of application of the methodology described in Appendix A to each modification of standards case.

Other report appendices, which are available online only, provide detail and information on the development of the methodology.

In addition, the project developed a

PowerPoint presentation

that may be useful for introducing and explaining the methodology to stakeholders.

In July 2021, an errata was posted for this publication: In Table 7 on page 25, the LDVO coefficient was changed from -3.088 to -13.088. The online version of the report has been corrected.

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