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

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TABLE OF CONTENTS (Continued) APPENDIXES A - Multiple Parallel Approach Program (MPAP) Summary B - Simulation Using the FDADS, Controller Report C - Simulation Using the FDADS, Technical Observers Report D - Simulation Using the FDADS, Risk Assessment E - Approach Plates F - Controller Questionnaires G - Pilot Questionnaires H - Controller Report I - Technical Observer Report J - Observer Logs K - Operational Assessment L - Risk Analysis of Blunders vi
Figure 1 2 3 4 5 6 LIST OF ILLUSTRATIONS Airport Configuration Curved Asymptotic Approach and Aircraft Deviations Target Generation Facility Configuration Full Range of CPA's, Flight Simulator Evaders Distribution of CPA's for 30-Degree, No Response Blunders into Flight Simulators Frequency of Nuisance Breakouts Page 6 10 13 24 26 35 Table 1 2 3 4 5 6 7 8 9 10 11 12 LIST OF TABLES True Airspeed vs. Indicated Airspeed DIA ILS Runway Turn-On Altitudes Required Sample Size Blunders that Resulted in a Conflict Evading Flight Simulator Data Evading Flight Simulator CPA Data CPA Lower Distribution Data TCV Data, TWA621/AAL204 Dialogue for TCV, TWA621/AAL204 TCV Data, AWE234/NWA893 Dialogue for TCV, AWE234/NWA893 Nuisance Breakout Data vii Page 2 7 21 23 23 25 28 29 30 31 32 36
Page 1 and 2: 1 DOT/FAA/CT-94/3 6 FAA Technical C
Page 3: 1. Title and Subtitle Technical Rep
Page 7: TABLE OF CONTENTS Page EXECUTIVE SU
Page 12 and 13: An evaluation of NBO's and NTZ entr
Page 14 and 15: One specific effect of high density
Page 16 and 17: Technical Center. Indicated air spe
Page 18 and 19: -: zg cui r - I -----1 s: i I - OM
Page 20 and 21: sometimes instructed to disregard c
Page 22 and 23: ILS Localizer Cen tex line A Note:
Page 24 and 25: The Simulation Pilot Subsystem cons
Page 26 and 27: provided by ARTS displays, FMA's pr
Page 28 and 29: Controllers also submitted a report
Page 30 and 31: a. NTZ transgression frequency: b.
Page 32 and 33: 3.3.1.1 No-Controller Intervention
Page 34 and 35: analyses and the TWG operational as
Page 36 and 37: I [OOOO l'OS66) [OOS6'0SP6) [0006'0
Page 38 and 39: [OOSS' OSPS) [OOOS'OS6P) [OOSP' OSP
Page 41 and 42: TABLE 8. TCV DATA, TWA621/AAL204 Bl
Page 43 and 44: directed not to respond), the 17R c
Page 45 and 46: 4.2.6 Blunder Resolution Performanc
Page 47 and 48: [LSI [ssl [ESI L 35
Page 49 and 50: 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 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
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
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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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