National Academies Press: OpenBook

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

Chapter: Appendix C - Key Studies on Aircraft Deviation

« Previous: Appendix B - Collision Risk Model
Page 89
Suggested Citation:"Appendix C - Key Studies on Aircraft Deviation." 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.
×
Page 89

Below is the uncorrected machine-read text of this chapter, intended to provide our own search engines and external engines with highly rich, chapter-representative searchable text of each book. Because it is UNCORRECTED material, please consider the following text as a useful but insufficient proxy for the authoritative book pages.

Aircraft Name Manufacturer ICAO Code Wingspan (ft) Length (ft) Height (ft) Engine Type Engines (#) MTOW (lb) Takeoff Distance (ft) Landing Distance (ft) V2 (kts) Approach Speed (kts) 1125 Astra Israel Aerospace Industries ASTR 52.8 55.4 18.0 Jet 2 24,648 5,249.3 2,952.8 130 126 1126 Galaxy Israel Aerospace Industries GALX 58.1 62.3 21.3 Jet 2 34,851 5,905.5 3,444.9 125 130 Learjet 24 Learjet LJ24 35.1 43.0 Jet 2 13,001 128 Learjet 25 Learjet LJ25 35.4 47.6 12.1 Jet 2 14,991 3,937.0 2,952.8 130 137 Learjet 31 Learjet LJ31 43.6 48.6 12.5 Jet 2 15,498 3,608.9 2,952.8 130 120 Learjet 35 Learjet LJ35 39.4 48.6 12.1 Jet 2 18,298 4,265.1 2,952.8 140 125 Learjet 35 Learjet LJ35 39.4 48.6 12.1 Jet 2 18,298 4,265.1 2,952.8 140 125 Learjet 45 Learjet LJ45 47.9 58.1 14.1 Jet 2 19,511 4,265.1 2,952.8 140 140 Learjet 55 Learjet LJ55 43.6 55.1 14.8 Jet 2 21,010 4,593.2 3,280.8 140 140 Learjet 60 Learjet LJ60 44.0 58.7 14.8 Jet 2 23,104 5,249.3 3,608.9 140 140 AC-130 Spectre Lockheed C130 132.5 97.8 38.7 Turboprop 4 155,007 3,608.9 2,624.7 120 130 Electra Lockheed L188 99.1 104.3 32.8 Turboprop 4 112,987 4,265.1 2,952.8 120 130 L-1011 TriStar Lockheed L101 155.5 178.1 55.4 Jet 3 429,990 7,874.0 5,905.5 150 138 P-3 Orion Lockheed P3 99.7 116.8 0.0 Turboprop 4 135,000 * * * ** * * 134 DC-10 McDonnell Douglas DC10 165.4 180.4 58.1 Jet 3 572,009 9,842.5 5,905.5 150 136 MD-11 McDonnell Douglas MD11 169.9 200.8 57.7 Jet 3 630,500 10,170.6 6,889.8 160 155 MD-80 McDonnell Douglas MD80 107.8 147.7 30.2 Jet 3 149,500 6,732.3 5,200.1 140 150 MD-81 McDonnell Douglas MD81 107.8 147.7 30.2 Jet 3 149,500 6,732.3 5,200.1 140 150 MD-82 McDonnell Douglas MD82 107.8 147.7 30.2 Jet 3 149,500 6,732.3 5,200.1 140 150 MD-83 McDonnell Douglas MD83 107.8 147.7 30.2 Jet 3 160,001 6,732.3 5,200.1 140 150 MD-88 McDonnell Douglas MD88 107.8 147.7 30.2 Jet 3 149,500 6,732.3 5,200.1 140 150 LR-1 Marquise Mitsubishi MU2 39.0 33.1 12.8 Turboprop 2 10,053 2,132.5 1,968.5 120 88 Aerostar 200 Mooney M20P 35.1 23.3 8.2 Piston 1 2,579 1,476.4 820.2 70 70 Observer Partenavia P68 39.4 30.8 11.2 Piston 2 4,586 1,312.3 1,968.5 75 73 P-180 Avanti Piaggio P180 45.9 47.2 12.8 Turboprop 2 11,552 2,952.8 2,952.8 120 120 Table F-1. (Continued). (continued on next page)

Next: Appendix D - List of Veer-Off Accidents and Incidents »
Risk Assessment Method to Support Modification of Airfield Separation Standards Get This Book
×
 Risk Assessment Method to Support Modification of Airfield Separation Standards
MyNAP members save 10% online.
Login or Register to save!

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.

READ FREE ONLINE

  1. ×

    Welcome to OpenBook!

    You're looking at OpenBook, NAP.edu's online reading room since 1999. Based on feedback from you, our users, we've made some improvements that make it easier than ever to read thousands of publications on our website.

    Do you want to take a quick tour of the OpenBook's features?

    No Thanks Take a Tour »
  2. ×

    Show this book's table of contents, where you can jump to any chapter by name.

    « Back Next »
  3. ×

    ...or use these buttons to go back to the previous chapter or skip to the next one.

    « Back Next »
  4. ×

    Jump up to the previous page or down to the next one. Also, you can type in a page number and press Enter to go directly to that page in the book.

    « Back Next »
  5. ×

    To search the entire text of this book, type in your search term here and press Enter.

    « Back Next »
  6. ×

    Share a link to this book page on your preferred social network or via email.

    « Back Next »
  7. ×

    View our suggested citation for this chapter.

    « Back Next »
  8. ×

    Ready to take your reading offline? Click here to buy this book in print or download it as a free PDF, if available.

    « Back Next »
Stay Connected!