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From page 48... ... 3. Select the plot for the specific ADG involved and estimate the risk based only on the runway centerline to taxiway centerline separation (see Figures AA-29 to AA-40) Read the entire page →
From page 49... ... The existing separation between the runway and the parallel taxiway centerlines is 320 ft; however, the standard for A-11 Figure A-12. Typical runway/object scenario for runway veer-off incidents. Read the entire page →
From page 50... ... The risk of collision for ADG III Cat I during the airborne phase of landing is estimated using Figure AA-33. The runway/ taxiway centerline separation for the case is 320 ft, and the A-12 Figure A-13. Read the entire page →
From page 51... ... Collision risk associated with taxiway centerline separation for ADG I ATTACHMENT -- RISK PLOTS This attachment contains several plots that should be used with the methodology described in Appendix A Read the entire page →
From page 52... ... ADG III Standard = 152 ft 1.E-09 1.E-08 1.E-07 1.E-06 1.E-05 R is k of C ol lis io n pe r O pe ra tio n Figure AA-3. Collision risk associated with taxiway centerline separation for ADG III. Read the entire page →
From page 53... ... Collision risk associated with taxiway centerline separation for ADG IV. 226 228 230 232 234 236 Taxiway/Taxiway Centerline to Centerline Separation (ft) Read the entire page →
From page 54... ... Collision risk associated with taxiway centerline separation for ADG VI. 12 14 16 18 20 22 Wingtip Separation (ft) Read the entire page →
From page 55... ... Collision risk associated with taxiway to object separation for ADG I 52 56 60 6454 58 6250 66 Taxiway Centerline to Object Separation (ft) Read the entire page →
From page 56... ... Collision risk associated with taxiway to object separation for ADG III. 98 102 106 110100 104 10896 112 Taxiway Centerline to Object Separation (ft) Read the entire page →
From page 57... ... Collision risk associated with taxiway to object separation for ADG V 142 146 150 156154144 148 152140 158 Taxiway Centerline to Object Separation (ft) Read the entire page →
From page 58... ... Collision risk associated with taxilane to object separation for ADG I 12 16 20 2414 18 2210 2826 Wingtip Separation (ft) Read the entire page →
From page 59... ... ADG III Standard = 140 ft 1.E-09 1.E-08 1.E-07 1.E-06 1.E-05 R is k of C ol lis io n pe r O pe ra tio n Figure AA-17. Collision risk associated with taxilane to object separation for ADG III. Read the entire page →
From page 60... ... Collision risk associated with taxilane to object separation for ADG IV. 224 226223 225222 227 Taxilane/Taxilane Centerline Separation (ft) Read the entire page →
From page 61... ... 1.E-09 1.E-08 1.E-07 1.E-06 1.E-05 R is k of C ol lis io n pe r O pe ra tio n Figure AA-21. Collision risk associated with taxilane wingtip separation distance (any ADG) Read the entire page →
From page 62... ... Collision risk associated with taxilane to object separation for ADG I 48 52 5650 5446 58 Taxilane Centerline to Object Separation (ft) Read the entire page →
From page 63... ... Collision risk associated with taxilane to object separation for ADG III. 95 97 10193 9991 Taxilane Centerline to Object Separation (ft) Read the entire page →
From page 64... ... Collision risk associated with taxilane to object separation for ADG V 137 139 141 143 145 Taxilane Centerline to Object Separation (ft) Read the entire page →
From page 65... ... ADG I Approach Cat C Standard = 300 ft 1.0E-13 1.0E-12 1.0E-11 1.0E-10 R is k of C ol lis io n pe r O pe ra tio n Figure AA-29. Missed approach collision risk for ADG I Cat I Read the entire page →
From page 66... ... Missed approach collision risk for ADG I Cat II. 200 300 400250 350 450150 500 Runway/Taxiway Centerline Separation (ft) Read the entire page →
From page 67... ... ADG III Approach Cat C Standard = 400 ft 1.0E-11 1.0E-10 1.0E-08 1.0E-09 R is k of C ol lis io n pe r O pe ra tio n Figure AA-33. Missed approach collision risk for ADG III Cat I Read the entire page →
From page 68... ... Missed approach collision risk for ADG III Cat II. 600300 700400 550350 450 650 750250 800500 Runway/Taxiway Centerline Separation (ft) Read the entire page →
From page 69... ... Missed approach collision risk for ADG IV Cat II. 600 300 700 400 550 350 450 650 850750 800 500 Runway/Taxiway Centerline Separation (ft) Read the entire page →
From page 70... ... Missed approach collision risk for ADG VI Cat I Read the entire page →
From page 71... ... Figure AA-40. Missed approach collision risk for ADG VI Cat II. Read the entire page →
From page 72... ... ADG III Approach Cat C Standard = 400 ft 1.E-06 1.E-07 1.E-08 1.E-09 R is k of C ro ss in g th e Ta xi w ay Figure AA-43. Landing veer-off collision risk for ADG III. Read the entire page →
From page 73... ... Landing veer-off collision risk for ADG IV. 600 300 700 400 900 1000800 500 Centerline Separation (ft) Read the entire page →
From page 74... ... Landing veer-off collision risk based on wingtip clearance -- any ADG. Read the entire page →
From page 75... ... Section 5.2 -- Takeoff Veer-Off Collision Risk Plots Read the entire page →
From page 76... ... Figure AA-50. Takeoff veer-off collision risk for ADG III. Read the entire page →
From page 77... ... Takeoff veer-off collision risk for ADG V 900400 1000500 600 700 1100800 Centerline Separation (ft) Read the entire page →
From page 78... ... Takeoff veer-off collision risk based on wingtip clearance -- any ADG. Read the entire page →
From page 79... ... B-1 Appendix B of the contractor's final report is not published herein, but is available on the TRB website at http://www.trb.org/Main/Blurbs/165180.aspx. A P P E N D I X B Collision Risk Model Read the entire page →
From page 80... ... C-1 Appendix C of the contractor's final report is not published herein, but is available on the TRB website at http://www.trb.org/Main/Blurbs/165180.aspx. A P P E N D I X C Key Studies on Aircraft Deviation Read the entire page →
From page 81... ... D-1 Appendix D of the contractor's final report is not published herein, but is available on the TRB website at http://www.trb.org/Main/Blurbs/165180.aspx. A P P E N D I X D List of Veer-Off Accidents and Incidents Read the entire page →
From page 82... ... E-1 Appendix E of the contractor's final report is not published herein, but is available on the TRB website at http://www.trb.org/Main/Blurbs/165180.aspx. A P P E N D I X E Sample of Normal Operations Data Read the entire page →
From page 83... ... F-1 A P P E N D I X F Aircraft Database Summary Read the entire page →
From page 84... ... Mohawk 298 Aerospatiale N262 71.9 63.3 20.3 Turboprop 2 23,369 2,296.6 1,312.3 100 110 Aerostar 600 Aerostar AEST 36.7 34.8 12.8 Piston 2 6,305 1,804.5 1,148.3 95 94 A-300 Airbus A30B 147.1 177.5 54.3 Jet 2 378,534 7,349.1 5,026.2 160 135 A-300-600 Airbus A306 147.1 177.5 54.3 Jet 2 378,534 7,349.1 5,026.2 160 135 A-310-200/300 Airbus A310 144.0 153.1 51.8 Jet 2 330,693 7,513.1 4,888.5 160 135 A-318 Airbus A318 111.9 103.2 41.2 Jet 2 130,073 4,593.2 4,265.1 135 138 A-319 Airbus A319 111.9 111.2 38.6 Jet 2 141,096 5,741.5 4,429.1 135 138 A-320 Airbus A320 111.9 123.3 38.6 Jet 2 162,040 7,185.0 4,724.4 145 138 A-321 Airbus A321 111.9 146.0 38.6 Jet 2 182,984 7,250.7 5,249.3 145 138 A-330-200 Airbus A332 197.8 192.9 57.1 Jet 2 507,063 7,545.9 5,905.5 145 140 A-330-300 Airbus A333 197.8 208.7 55.3 Jet 2 507,063 7,545.9 5,905.5 145 130 A-340-200 Airbus A342 197.8 194.8 54.8 Jet 4 606,271 9,071.5 5,790.7 145 150 A-340-300 Airbus A343 197.8 208.7 55.3 Jet 4 606,271 9,071.5 6,003.9 145 150 A-340-500 Airbus A345 208.2 222.8 56.1 Jet 4 811,301 10,498.7 6,299.2 145 150 A-340-600 Airbus A346 208.2 247.0 56.8 Jet 4 811,301 10,301.8 6,561.7 145 150 A-380-800 Airbus A388 261.8 239.5 79.1 Jet 4 1,234,589 9,744.1 6,594.5 150 145 Alenia ATR-42-200/300 ATR AT43 80.7 74.5 24.9 Turboprop 2 36,817 3,608.9 3,280.8 110 104 Alenia ATR-72-200/210 ATR AT72 88.9 89.2 25.3 Turboprop 2 47,399 4,921.3 3,608.9 110 105 Avro 748 Avro A748 98.2 66.9 24.9 Turboprop 2 46,495 3,280.8 2,034.1 110 100 Jetsream 31 Bae Systems JS31 52.0 47.1 17.5 Turboprop 2 15,562 5,905.5 4,265.1 110 125 Jetsream 32 Bae Systems JS32 52.0 47.1 17.7 Turboprop 2 16,226 5,150.9 4,002.6 110 125 Jetsream 41 Bae Systems JS41 60.4 63.4 18.4 Turboprop 2 24,000 4,921.3 4,265.1 110 120 100 King Air Beech BE10 45.9 40.0 15.4 Turboprop 2 11,795 1,476.4 2,132.5 105 111 33 Debonair Beech BE33 33.5 25.6 8.2 Piston 1 3,064 1,148.3 984.3 75 70 Beech 55 Baron Beech BE55 37.7 27.9 9.5 Piston 2 5,071 1,476.4 1,476.4 95 90 Beech 60 Duke Beech BE60 39.4 33.8 12.5 Piston 2 6,768 1,968.5 1,312.3 95 98 Beech 76 Duchess Beech BE76 38.1 29.2 9.5 Piston 2 3,902 2,132.5 1,968.5 85 76 Beech 99 Airliner Beech BE99 45.9 44.6 14.4 Turboprop 2 16,755 3,280.8 2,952.8 115 107 Bonanza V35B Beech BE35 33.4 26.3 7.6 Piston 1 3,400 1,150.0 1,480 * 70 King Air F90 Beech BE9T 45.9 39.8 * Read the entire page →
From page 85... ... Super King Air 300 Beech BE30 54.5 44.0 14.8 Turboprop 2 13,889 1,870.1 1,771.7 115 103 Premier 1A Beechcraft PRM1 44.5 46.0 15.3 Jet 2 12,500 3,792.0 3,170.0 * 121 B707-100 Boeing B701 130.9 144.7 42.3 Jet 4 190,003 8,694.2 6,496.1 * Read the entire page →
From page 86... ... Aircraft Name Manufacturer ICAOCode Wingspan (ft) Length (ft) Read the entire page →
From page 87... ... Aircraft Name Manufacturer ICAO Code Wingspan (ft) Length (ft) Read the entire page →

From page 48...

... 3. Select the plot for the specific ADG involved and estimate the risk based only on the runway centerline to taxiway centerline separation (see Figures AA-29 to AA-40)