National Academies Press: OpenBook

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

Chapter: Appendix D - List of Veer-Off Accidents and Incidents

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Page 90
Suggested Citation:"Appendix D - List of Veer-Off Accidents and Incidents." 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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Page 90

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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) Astra Pilatus PC7 34.1 32.2 10.5 Turboprop 1 6,393 984.3 1,312.3 90 90 Eagle Pilatus PC12 53.1 47.2 14.1 Turboprop 1 9,921 1,968.5 1,804.5 110 85 Apache Piper PA23 37.0 27.1 10.3 Piston 2 4,799 * * * * Arrow 4 Piper P28T 35.4 27.2 8.2 Piston 1 2,910 1,148.3 656.2 70 70 Aztec Piper PA27 37.4 31.2 10.2 Piston 2 5,203 984.3 1,640.4 75 70 Cherokee Lance Piper P32R 36.1 28.2 8.5 Piston 1 3,616 1,640.4 1,804.5 75 75 Cherokee Six Piper PA32 36.1 26.9 8.2 Piston 1 3,616 1,640.4 1,804.5 75 75 Cheyenne 2 Piper PAY2 42.7 36.4 12.8 Turboprop 2 8,995 2,132.5 2,460.6 100 100 Cheyenne 3 Piper PAY3 47.6 43.3 14.8 Turboprop 2 11,244 2,296.6 2,132.5 105 105 Cheyenne 400 Piper PAY4 47.6 43.3 17.1 Turboprop 2 12,059 2,296.6 2,132.5 125 110 Comanche Piper PA24 36.0 24.1 7.5 Piston 1 2,551 * * * * Malibu Meridian Piper P46T 43.0 29.5 11.5 Turboprop 1 4,740 1,476.4 1,476.4 80 75 Malibu Mirage Piper PA46 43.0 28.5 11.5 Piston 1 4,299 1,476.4 1,476.4 80 75 Navajo Chieftain Piper PA31 40.7 32.5 13.1 Piston 2 6,504 1,312.3 1,968.5 90 100 PA-28-140 Cherokee Piper P28A 35.1 24.0 7.2 Piston 1 2,425 984.3 984.3 65 65 PA-28R Cherokee Arrow Piper P28R 29.9 24.3 7.9 Piston 1 2,491 984.3 984.3 70 70 Seminole Piper PA44 38.7 27.6 8.5 Piston 2 3,792 984.3 1,312.3 75 80 Seneca Piper PA34 39.0 28.5 9.8 Piston 2 4,762 984.3 1,312.3 80 80 Tomahawk Piper PA38 35.1 23.0 9.2 Piston 1 1,676 820.2 656.2 60 65 Twin Comanche Piper PA30 36.0 25.0 8.3 Piston 2 3,600 * * * * 400 Beechjet Raytheon BE40 43.6 48.6 13.8 Jet 2 16,094 3,937.0 3,608.9 130 111 90 King Air Raytheon BE9L 50.2 35.4 14.1 Turboprop 2 10,099 2,296.6 1,246.7 100 100 Bae 125-1000 Raytheon H25C 51.5 53.8 17.1 Jet 2 30,997 6,233.6 2,916.7 125 132 Bae 125-700/800 Raytheon H25B 54.5 51.2 18.0 Jet 2 27,403 5,577.4 2,952.8 125 125 Beech 1900 Raytheon B190 58.1 57.7 15.4 Turboprop 2 16,954 3,773.0 2,706.7 110 113 Beech 36 Bonanza Raytheon BE36 27.6 26.6 8.5 Piston 1 3,638 1,148.3 1,476.4 75 75 Beech 58 Baron Raytheon BE58 37.7 29.9 9.7 Piston 2 5,512 2,296.6 1,968.5 100 96 Super King Air 200 Raytheon BE20 54.5 44.0 14.8 Turboprop 2 12,500 1,870.1 1,771.7 115 103 Super King Air 350 Raytheon B350 58.1 46.6 14.4 Turboprop 2 14,991 3,280.8 2,690.3 120 110 Aero Commander 500 Rockwell International AC50 48.9 36.7 15.1 Piston 2 6,746 1,312.3 1,312.3 80 97 Sabreliner 60 Rockwell International SBR1 44.5 48.3 * Jet 2 20,000 * * * 120 Table F-1. (Continued).

Next: Appendix E - Sample of Normal Operations Data »
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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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