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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
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4.5.2 Phraseoloav. The second state
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number of causes of accidents durin
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1 ACC X 8 WCB's x 102 Itat risk" WC
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5.3.2 Technical Observer Assessment
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BIBLIOGRAPHY Bilicki, H. W., TGF an
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GLOSSARY Aimort Surveillance Radar
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- 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
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- 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 and 102: PILOT BREAK-OUT QUESTIONNAIRE DIA S
- Page 103 and 104: 2.0 GENERAL COMMENTS I 2.1 Please p
- Page 105: APPENDIX H CONTROLLER REPORT
- Page 109: APPENDIX I TECHNICAL OBSERVER REPOR
- Page 112 and 113: The Technical Observers believe tha
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- Page 119: APPENDIX K OPERATIONAL ASSESSMENT
- Page 122 and 123: RECOMMENDATIONS The Multiple Parall
- Page 125 and 126: RISK ANALYSIS OF BLUNDERS 1.0 INTRO
- Page 127 and 128: 2.3 BASIC RISK EQUATION A TCV will
- Page 129 and 130: involving a ground crew member duri
- Page 131 and 132: P(A') = P(11)P(2')P(3') . . . P(10'
- Page 133 and 134: through the blundering aircraft. Th
- Page 135 and 136: angle is assumed to be 30°, then t
- Page 137 and 138: lunder rate may be computed. The sp