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

Chapter: Appendix E - Sample of Normal Operations Data

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Page 91
Suggested Citation:"Appendix E - Sample of Normal Operations Data." 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 91

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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) Turbo Commander 680 Rockwell International AC80 46.8 44.5 * Turboprop 2 11,199 * * * 97 Turbo Commander 690 Rockwell International AC90 46.7 44.4 15.0 Turboprop 2 10,251 * * * 97 SAAB 2000 SAAB SB20 81.4 89.6 25.3 Turboprop 2 46,297 4,265.1 4,265.1 110 110 SAAB 340 SAAB SF34 70.2 64.6 23.0 Turboprop 2 28,440 4,265.1 3,608.9 110 115 C-23 Sherpa Short SH33 74.8 58.1 16.4 Turboprop 2 22,597 3,608.9 3,608.9 100 96 SD3-60 Short SH36 74.8 70.9 24.0 Turboprop 2 27,117 4,265.1 3,608.9 110 100 Short SC-7 Skyvan Short SC7 65.0 40.0 15.1 Turboprop 2 13,669 1,968.5 2,296.6 90 90 Fairchild 300 Swearingen SW3 46.3 42.3 16.7 Turboprop 2 12,566 4,265.1 4,265.1 115 120 Socata TBM-700 TBM TBM7 40.0 34.1 13.8 Turboprop 1 6,614 2,132.5 1,640.4 85 80 *Cells that are blank indicate that no data were available in the databases investigated. Table F-1. (Continued).

Next: Appendix F - Aircraft Database Summary »
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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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