Published Report (DOT/FAA/CT-94-36)

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FLIGHTCREW OPINION SURVEY DIA Simulation DATE : SITE: AVIA BOEING DELTA/B737 DELTA/MD88 <strong>FAA</strong>TC NASA TWA PILOT LETTER: TOTAL NUMBER YEARS FLIGHT EXPERIENCE: Answer each question to the best of your ability using the scoring scheme shown. You are invited to provide- additional comments on any item in the space provided at the end of the survey form. Please reference the item number. 1.0 SURVEY ITEMS 1 - strongly agree 2 - agree 3 - neutral 4 - disagree 5 - strongly disagree 1.1 Current parallel runway procedures require 1000 ft of vertical separation at the localizer turn-on for separation. In the event that one (or both) aircraft overshoot the localizer, 1000 ft of vertical separation would provide an acceptable safety margin provided aircraft maintain their assigned altitude until established on the localizer course. 1 2 3 4 5 1.2 1.3 To emphasize the importance of a quick response from the threatened aircraft, special phraseology should be used for the break-out maneuver. 1 2 3 4 5 Given the premise that the resolution of a conflict situation is primarily dependent on monitor controller to pilot communications, please respond to the following statements. An alternate communication frequency 1 2 3 4 5 would be useful. Breakout instructions should be broadcast simultaneously on the ILS frequency. 1 2 3 4 5 (voice on the localizer) G-2
2.0 GENERAL COMMENTS I 2.1 Please provide any suggestions on types of training to be required, types of certification (etc.) that you think would enable the operation of multiple simultaneous parallel ILS approaches to be a safe and effective procedure. 2.2 Please provide any suggestions on types of special terminology/phraseology/instructions for an evasive maneuver (e.g. , llImmediately, IIEscape, call sign emphasis by repeating callsign 2 times, altitude instruction before heading instruction, published escape maneuver). THANK YOU FOR YOUR PARTICIPATION AND ALL COMMENTS GIVEN. G-3
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1 DOT/FAA/CT-94/3 6 FAA Technical C
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1. Title and Subtitle Technical Rep
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TABLE OF CONTENTS Page EXECUTIVE SU
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Figure 1 2 3 4 5 6 LIST OF ILLUSTRA
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An evaluation of NBO's and NTZ entr
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One specific effect of high density
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Technical Center. Indicated air spe
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-: zg cui r - I -----1 s: i I - OM
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sometimes instructed to disregard c
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ILS Localizer Cen tex line A Note:
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The Simulation Pilot Subsystem cons
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provided by ARTS displays, FMA's pr
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Controllers also submitted a report
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a. NTZ transgression frequency: b.
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3.3.1.1 No-Controller Intervention
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analyses and the TWG operational as
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I [OOOO l'OS66) [OOS6'0SP6) [0006'0
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[OOSS' OSPS) [OOOS'OS6P) [OOSP' OSP
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TABLE 8. TCV DATA, TWA621/AAL204 Bl
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directed not to respond), the 17R c
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4.2.6 Blunder Resolution Performanc
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[LSI [ssl [ESI L 35
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4.4.2 Post-Simulation Controller Ou
Page 51 and 52: 4.5.2 Phraseoloav. The second state
Page 53 and 54: number of causes of accidents durin
Page 55 and 56: 1 ACC X 8 WCB's x 102 Itat risk" WC
Page 57 and 58: 5.3.2 Technical Observer Assessment
Page 59 and 60: BIBLIOGRAPHY Bilicki, H. W., TGF an
Page 61 and 62: GLOSSARY Aimort Surveillance Radar
Page 63 and 64: Outer Marker (OM) - A marker beacon
Page 65: APPENDIX A MULTIPLE PARALLEL APPROA
Page 69: APPENDIX B SIMULATION USING THE FDA
Page 72 and 73: Thus, the controller,s ability to d
Page 75: TECHNICAL OBSERVERS REPORT DIA SIMU
Page 79 and 80: FDADS SIMULATION AT DENVER A demons
Page 81: isk blunders, but only 2 TCV's. The
Page 85 and 86: ILS 10L DENVER INTERNATlONAL AIRPOR
Page 87: ILS 17L 1 DENVER TOWER 1205 1 DENVE
Page 91 and 92: POST-RUN CONTROLLER QUESTIONNAIRE D
Page 93 and 94: POST-SIMULATION CONTROLLER QUESTION
Page 95 and 96: CONTROLLER TEST CRITERION VIOLATION
Page 97: 111. STATEMENT: 1. From your knowle
Page 101: PILOT BREAK-OUT QUESTIONNAIRE DIA S
Page 105: APPENDIX H CONTROLLER REPORT
Page 109: APPENDIX I TECHNICAL OBSERVER REPOR
Page 112 and 113: The Technical Observers believe tha
Page 115 and 116: .. v) CI t E" E 8 - a c .- 0 CI 5 2
Page 117: c X > 0 4 L 5-3
Page 121 and 122: MULTIPLE PARALLEL APPROACH PROGRAM
Page 123: APPENDIX L RISK ANALYSIS OF BLUNDER
Page 126 and 127: 2.0 BASIC RISK COMPUTATION 2.1 DEFI
Page 128 and 129: a fatal accident during an approach
Page 130 and 131: 3.4 ESTIMATING COLLISION RISK The f
Page 132 and 133: 4.0 DETERMINATION OF ALIGNMENT WIND
Page 134 and 135: The roots of the quadratic equation
Page 136 and 137: e estimated as the ratio of the num
Page 138: This is a very high rate, which wou
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Published Report (DOT/FAA/CT-94-36)

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