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

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

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Technical Center. Indicated air speeds of 180 knots (kn) were<br />

assigned for turbojets, 150 kn for turboprops, and 120 kn for<br />

twin engine piston aircraft. Preliminary data indicated that<br />

during the simulation, a total of 746 blunders were initiated,<br />

376 for the triple approach configuration and 370 for the<br />

quadruple approach configuration. Approximately 74 percent of<br />

all blundering aircraft did not respond to air traffic control<br />

(ATC) commands.<br />

Preliminary data analyses indicated that the test criterion<br />

violations (TCV's) (aircraft separated by less than or equal to<br />

500 feet) exceeded the test criterion rate of 2 percent set to<br />

evaluate the operation. However, the number of NBO's and NTZ<br />

entries was acceptable based on the criteria set by the TWG.<br />

Qualitative data from the controller questionnaires indicated<br />

that when the ARTS IIIA display was used, it was "very difficultvv<br />

to perform the monitor controller task. The controllers also<br />

disagreed with the statement that Ittriple independent IFR<br />

approaches to runways spaced 5280 and 7600 ft apart can be safely<br />

conducted as simulated.11<br />

After reviewing the preliminary data, controller opinions, and<br />

technical observer comments, it was decided that an additional<br />

high density altitude simulation should be conducted using the<br />

Full Digital ARTS I11 Display System (FDADS) and data specific to<br />

DIA. To make this simulation site specific to DIA, additional<br />

information about air traffic and airport operations was<br />

requested from representatives from the Northwest Mountain Region<br />

and the Air Traffic Division of the <strong>FAA</strong>.<br />

1.1.1.2 Simulation Usina the FDADS.<br />

A second simulation was conducted to evaluate the performance of<br />

controllers monitoring triple simultaneous approaches to parallel<br />

runways using the FDADS. In this simulation, assigned aircraft<br />

speeds were kept at 170 kn for all turbojet and turboprop<br />

aircraft. Additionally, twin-engine piston aircraft were<br />

assigned a 150 kn IAS. The three-week simulation began on<br />

November 16, 1992, but was terminated on November 18, 1992,<br />

because preliminary data indicated that the operation would not<br />

meet performance goals set by the TWG.<br />

Preliminary data for aircraft separation, NBO's, and NTZ entries<br />

were reviewed daily. At the end of the second day of simulation,<br />

1169 aircraft were handled, 87 blunders were initiated into<br />

flight simulators, and 5 TCV's were reported. Although the data<br />

for NTZ entries and NBO's appeared to be within the goals set by<br />

the TWG, this sample of data (5 TCV's out of 87 blunders = 5.7<br />

percent TCV rate) exceeded the blunder resolution performance<br />

goal set by the TWG. Additionally, TWG members, simulation<br />

participants, and observers from <strong>FAA</strong> Headquarters and the<br />

4

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