Document
reformatted for the the world wide web
Geoffrey D. Gosling
Aviation System Planning Consultant
Berkeley, CA
February 15, 2001
U.S. Army Corps of Engineers
Regulatory Branch
P.O. Box 3755
Seattle, WA 98124
Attn: Jonathan Freedman, Project Manager
Washington State Department of Ecology
Shorelands & Environmental Assistance Program
3190 – 160th Ave., S.E.
Bellevue, WA 98008-5452
Attn: Ann Kenny, Environmental Specialist
RE: Port of Seattle, Ref. No. 1996-4-02325
Comments relating to Seattle-Tacoma International Airport Project
Third Runway – Aviation Technology and Safety Issues
Dear Mr. Freedman and Ms. Kenny:
At the request of the Airport Communities Coalition (ACC), I have undertaken
a further review of potential technology alternatives to the construction
of a third runway at Seattle-Tacoma International Airport as described
in the Final Environmental Impact Statement (FEIS) and Final Supplemental
Environmental Impact Statement (FSEIS) for the Proposed Master Plan Update
Development Actions for Seattle-Tacoma International Airport (Sea-Tac). This
letter supplements my initial findings submitted to the ACC in a letter
report dated November 24, 1999. It reviews recent developments in relevant
communication, navigation and surveillance (CNS) and air traffic management
(ATM) technologies, and discusses the potential for these technologies
to enhance the capacity of Sea-Tac.
At the request of the ACC, I have also given some consideration
to the operational factors that will arise at Sea-Tac as a consequence
of operating three parallel runways simultaneously, and the implications
of these factors for both airfield delays and runway safety.
As discussed in more detail below, the major conclusions
from this review are that:
1) The previous analysis of technology-based alternatives to the proposed
third runway described in the FEIS and FSEIS failed to address recent
developments in advanced air traffic management technologies, some of
which have occurred since that analysis was undertaken, and thus fails
to adequately reflect the potential of these technologies to enhance
the capacity of the existing runways at Sea-Tac; and
2) The increase in the number of runway crossings that will occur if
the proposed third runway is constructed will increase the risk of runway
incursions over present conditions, and may well limit the operational
benefits that can be obtained from the new runway.
In my opinion, further study of both these issues is therefore necessary
before the U.S. Army Corps of Engineers can properly assess the merits
of the proposed third runway compared to other alternatives to enhance
the capacity of the airport. The information presented in the FEIS of
the safety consequences of operating three runways in the manner proposed
does not adequately address the issues involved, for the reasons discussed
below, and a careful study of this issue would need to be undertaken
before any firm conclusion can be drawn regarding the extent to which
the third runway would affect safety levels at Sea-Tac.
For the record, I have attached a copy of a resume
of my qualifications and experience in undertaking research and consulting
activities relevant to the issues involved in this subject (Attachment
A).
Technology Alternatives to the Proposed Third Runway
My previous report discussed the potential for recent advances in CNS
and ATM technologies to open possibilities for entirely new ways to control
air traffic that can overcome many of the limitations of the existing
procedures based on radar and voice communications between pilots and
controllers, and that could allow simultaneous instrument approaches
to parallel runways separated by much smaller distances than currently
allowed. The key to these capabilities lies in the integration of Automated
Dependent Surveillance –Broadcast (ADS-B) technology, in which each aircraft
monitors its position using Global Positioning System (GPS) signals and
broadcasts this information to surrounding aircraft, Differential GPS
(DGPS) technology that greatly enhances the precision of the GPS information,
and either the use of enhanced Cockpit Display of Traffic Information
(CDTI) to allow the pilot to maintain safe separation for nearby aircraft
under instrument conditions or the direct feed of the ADS-B information
for other aircraft into the aircraft’s Flight Management System (FMS),
the automated flight control system, so that the aircraft automatically
maintains a safe separation from other traffic.
At the time of my previous report, three research and
development efforts were underway to pursue the opportunities presented
by these technologies.
A NASA research program termed the Terminal Area Productivity Program
was exploring ways to increase the capacity of the existing airport and
terminal area system. One component of this program was a joint effort
with Honeywell Technology Center and Honeywell Airport Systems to develop
two related systems, the Airborne Information for Lateral Spacing (AILS)
and the Closely Spaced Parallel Approaches (CASPER), that were designed
to allow aircraft to perform independent instrument approaches to parallel
runways spaced as close as 2,500 feet apart. NASA and Honeywell performed
in-flight demonstrations of the systems at Minneapolis-St Paul International
Airport in November 1999.
The Cargo Airline Association (CAA), in partnership with the FAA Safe
Flight 21 Program and a range of other industry organizations, had co-sponsored
a large-scale Operational Evaluation test of ADS-B and CDTI technologies
at Wilmington, Ohio in July 1999. The test involved 12 cargo aircraft
from three airlines, 12 other aircraft, including three FAA aircraft,
a NASA Boeing 757, a U.S. Navy P-3 Orion and several light aircraft,
and a ground vehicle. ADS-B data were received by two ground stations,
fused with radar data from an existing air traffic control surveillance
radar and displayed on an air traffic control workstation. During the
test, pilots performed a variety of procedures using the traffic information
displayed in the cockpit, including identification of other traffic and
maneuvers to assist in the sequencing of arriving traffic and improve
the efficiency of arrivals and departures. The immediate goal of the
CAA initiative was to allow the FAA to approve the use of ADS-B for traffic
alert and conflict resolution functions in place of the current Traffic
Alert and Collision Avoidance System (TCAS) equipment, which is based
on radar transponder signals. However, the larger interest of the CAA
and the FAA Safe Flight 21 Program in the use of ADS-B is that it is
not only potentially more accurate than existing TCAS equipment, but
it can support a much wider range of future capabilities.
RTCA, Inc. had established Special Committee 186 to develop operational
requirements and minimum performance standards for ADS-B. A subgroup
of Working Group 1, which was examining operations and implementation,
had also been addressing closely-spaced parallel approaches, and had
generated a number of concept papers that explored how ADS-B technology
might be used to allow IFR operations on much closer spaced runways,
including the existing runways at San Francisco International and Seattle-Tacoma
International airports. A paired approach concept is described in an
October 1998 paper by Rocky Stone of United Airlines.
Subsequent developments in each of these areas are
discussed in the following section.
In addition to more advanced CNS/ATM technologies, which will take some
time to reach a stage where they can be implemented in a routine basis,
there are existing radar and air traffic control display technologies
that can support new operational procedures that could increase the capacity
of the existing Sea-Tac runways in some weather conditions that currently
restrict landings to one runway. This display equipment, the Precision
Runway Monitor (PRM), in conjunction with a high-update-rate radar and
an offset Instrument Landing System (ILS) localizer and glideslope, allows
a procedure known as Simultaneous Offset Instrument Approach (SOIA). In
this procedure, arriving aircraft approach one of two closely spaced
runways on a course that is offset by a few degrees from the runway centerline. This
allows the aircraft on the two approach paths to be laterally separated
at the missed approach point by 3,000 feet, the minimum required for
simultaneous instrument approaches with a PRM. After the missed approach
point the aircraft need to have visual contact with other traffic and
complete the approach under visual flight rules. This procedure therefore
requires a minimum ceiling and visibility to enable aircraft to operate
under visual flight rules between the missed approach point and the runway. Thus
it cannot be used in all instrument meteorological conditions, but allows
simultaneous instrument approaches under some conditions that would otherwise
restrict operations to a single runway. It is anticipated that this
procedure could allow approaches to be performed with ceilings as low
as 1,600 feet above ground level and visibility as low as 4 miles (FAA, 2000
Aviation Capacity Enhancement Plan, December 2000). Efforts are
currently underway to implement SOIA procedures at San Francisco International
Airport.
Other ATM technologies that are currently being fielded have important
benefits for the implementation of such procedures as SOIA and the use
of ADS-B for paired approaches. These include components of the Center-TRACON
Automation System (CTAS), such as the Final Approach Spacing Tool. These
tools allow controllers to better position aircraft in the terminal airspace,
in order to minimize the separation between successive aircraft and optimize
the assignment of aircraft to different runways. These tools are currently
in the process of being fielded at selected ATC facilities as part of
the FAA Free Flight Phase 1 Program.
Recent Developments in Advanced CNS/ATM Technologies
Since the end of 1999, several significant developments have occurred
in the potential use of ADS-B technologies to enhance airport capacity. The
NASA Terminal Automation Program terminated at the end of fiscal year
2000, having met all its program goals and considered the AILS technology
as sufficiently mature to hand off to industry for further development. In
May 2000, the AILS research team was awarded the NASA Turning Goals into
Reality Award for exceptional progress toward affordable air travel. The
FAA Safe Flight 21 Program continued to work with the CAA and others
on additional Operational Evaluations of ADS-B technology in the Ohio
River Valley. A second Operational Evaluation was conducted in late
October 2000 at Louisville, Kentucky. The goal of this Operational Evaluation
was to evaluate air traffic controller use of ADS-B in the terminal area
environment, concentrating on the following Safe Flight 21 Master Plan
applications: approach spacing, departure spacing/clearance, runway
and final approach occupancy awareness, and airport surface situational
awareness. Further details are available on the Safe Flight 21 web site
(www.faa.gov/safeflight21).
Most significantly for potential future applications at Sea-Tac, in
December 2000 the Safe Flight 21 Program announced that it had entered
into a cooperative venture with United Airlines and NASA to develop and
evaluate the operational procedures for a Paired Approach landing concept
that could be applied at San Francisco International and similar airports. This
concept exploits the features available in aircraft equipped with ADS-B
and CDTI, and is based on concepts formulated by the Closely Spaced Parallel
Approaches Sub-Group of Working Group 1 of the RTCA Special Committee
186 discussed in my initial report. The program announcement is attached
as Attachment B. This concept is of particular relevance to the discussion
of CNS/ATM technology applications at Sea-Tac because the runways at
San Francisco International are even closer together than at Sea-Tac. By
keeping the trailing aircraft in each pair within 6,000 feet of the lead
aircraft and on the upwind approach path, it is anticipated that the
trailing aircraft will be close enough to the lead aircraft to remain
clear of any wake vortices. This solution to the capacity constraints
caused by wake vortex considerations could negate the concern raised
by the Port of Seattle in its responses to comments on the Master Plan
Update Development Actions that wake vortex considerations would prevent
simultaneous instrument approaches to parallel runways closer than 2,500
feet (e.g. see General Response 5 in Response to Comments on
Permit Reference No. 1996-4-02325 – Master Plan Update Development Actions
at Seattle-Tacoma International Airport, March 2000).
While it is certainly true that the paired approach concept will not
allow independent simultaneous instrument approaches to both runways
(the paired aircraft are obviously highly dependent), neither will the
third runway under current air traffic control rules. In any event,
what matters is not whether approaches are independent or not, but the
capacity provided by a given procedure.
The RTCA Special Committee 186 is continuing to meet and is currently
working on developing Minimum Operational Performance Standards for cockpit
display of traffic information, as well as Airborne Surveillance and
Separation Assurance Processing. Further details are on the RTCA web
site (www.rtca.org).
Potential Implications for the Capacity of Sea-Tac Airport
If the paired approach concept being pursued by the Safe Flight 21 Program
is found to be technically feasible, then in principle aircraft could
continue to use the two existing runways in conditions of bad weather
(low cloud and/or poor visibility) at similar arrival rates to those
currently achieved in good weather. However, this would require all
aircraft using the airport to be suitably equipped and their crews approved
to perform the relevant procedures. To the extent that only a proportion
of the aircraft fleet would be so equipped, at least initially, the capacity
benefits would be reduced.
Whether the delay reduction benefits from the implementation of a paired
approach concept using ADS-B technology would ever be as great as those
offered by the proposed third runway, and how any difference in delay
reduction benefits compares to the likely difference in implementation
costs and environmental impacts, cannot be determined from the information
presented in the FEIS and FSEIS. This is not only because the paired
approach concept was not considered in the discussion of technology alternatives
in the FEIS and FSEIS, but also because the analyses of airfield capacity
and delay upon which the FEIS and FSEIS were based were undertaken well
before the details of the paired approach concept had been articulated.
Therefore in order to compare the potential capacity benefits of the
paired approach concept to those of the proposed third runway, it would
be necessary to perform a detailed simulation analysis of the paired
approach concept at varying levels of aircraft equipage. Until such
an analysis is undertaken, it is simply not possible to say whether the
proposed third runway would provide greater delay reduction benefits
in the long term than implementation of the paired approach concept,
or how the two approaches would compare in the nearer term. Such an
analysis would need to consider the effect of different implementation
schedules for the paired approach concept, as well as different future
traffic growth scenarios. Clearly, fairly rapid implementation combined
with slow traffic growth will give a very different outcome than a much
slower implementation schedule combined with a rapid growth in traffic.
Whether or not the paired approach concept can be implemented at Sea-Tac,
the combination of SOIA procedures and CTAS tools would appear to offer
the prospect of significantly reducing delays during intermediate weather
conditions (down to the ceiling and visibility limits of the SOIA procedure). How
effective this will be in reducing total delay will require a careful
analysis that considers how often these intermediate weather conditions
occur. While this will not eliminate delays during very bad weather,
it is critical to assessing this issue to know how often these conditions
occur. It is not sufficient to simply know what percent of the time
these conditions occur. What matters is how long they persist when they
do occur. There is a huge difference from a delay standpoint in a condition
that occurs for one or two hours a day on many days a year and a condition
that lasts all day on far fewer days per year. In the former case, although
delays build up while the conditions persist, once the weather improves
and capacity returns to an unconstrained level, delays will gradually
reduce as the backlog of flights is eliminated. However, in the latter
case delays will continue to build all day to such levels that it will
become necessary to start canceling a large number of flights to preserve
the integrity of the system.
While the capacity and delay analysis undertaken during the 1995 Capacity
Enhancement Study Update for Sea-Tac, and used as the basis for the delay
projections in the FEIS and FSEIS, considered the occurrence of different
weather conditions over a ten-year period, the weather categories used
in that study do not conform to the likely ceiling and visibility limits
that would be allowable with a SOIA procedure. Thus it would be necessary
to re-run the analysis for both the third runway and the SOIA procedure
in order to compare the delays under the revised weather categories.
Operational Considerations with Three Parallel Runways
Implementation of the proposed third runway will create a situation
in which aircraft taxiing between the new runway and the passenger terminal
complex will have to cross the two existing runways. This has both delay
and safety implications.
During periods of heavy arrival traffic and poor weather, arrivals will
need to use the two outboard runways in order to be able to operate dependent
instrument approaches to two runways, which require the full separation
between the outboard runways under current air traffic control rules. In
this situation, departures will generally be assigned to the middle runway
to avoid needing to increase the separation between successive arrivals
to a given runway in order to be able to release a departure. However,
some departures may need to use the longest runway, Runway 16L/34R, which
will generally require that a gap be created in the arrival flow to that
runway, reducing the arrival capacity. This also means that most departures
will need to cross Runway 16L/34R to reach to middle runway. This will
significantly complicate the departure flow, since departing aircraft
cannot be cleared across the arrival runway when an arriving aircraft
is within 2 miles of the threshold, and there is limited space between
the two existing runways to hold aircraft waiting to take off. This
is particularly problematical under north flow conditions since the thresholds
of Runways 34L and 34R are not aligned, and departing traffic has to
cross Runway 34R well down the runway. Thus by the time an arrival on
Runway 34R has passed the crossing taxiway, the next arrival may be too
close to the threshold to allow a departure to cross. Furthermore, the
departure queue would obstruct the parallel taxiways in front of the
South Satellite Terminal.
One solution to this problem would be to have departures cross both
existing runways and form a departure queue on a parallel taxiway between
Runway 16R/34L and the new runway. The proposed taxiway system is well
configured to support this during south flow conditions, but not at all
well configured for north flow conditions. Departures on Runway 34L
would have to taxi all the way to the parallel taxiway adjacent to the
new runway before looping back to the end of Runway 34L, resulting in
longer taxi distances than necessary. In both south and north flow,
there is only one crossing taxiway that is well positioned to handle
departing traffic. Since each route involves two runway crossings, that
generally will require a hold between the two runways, this is likely
to result in traffic backing up onto the parallel taxiways in front of
the terminals and may well require both arrival and departure rates to
be temporarily reduced to allow enough departures across the runways
to maintain the departure queue. While this solution would prevent the
arrivals on Runway 16L/34R from limiting the departure capacity, it will
significantly increase the number of runway crossings. This has potential
safety implications, as discussed below.
Aircraft arriving on the new runway would need to cross the two existing
runways to reach the terminal complex. Apart from the delays inherent
in any crossing of an active runway, the need for the local controller
responsible for the existing runways to coordinate crossings in both
directions will significantly increase the control task complexity and
further delay crossing aircraft. Each aircraft waiting to cross the
runway will need to be given a separate clearance, and the time required
to issue as many as four clearances (two crossings in each direction)
will reduce the number of opportunities to clear aircraft across the
runways without increasing the intervals between arriving and departing
aircraft. Since the space between the two existing runways generally
only allows one aircraft to be held on each perpendicular crossing taxiway,
the controller will need to clear an aircraft waiting between the runways
to cross the runway in front of it before clearing the following aircraft
into the hold position between the runways.
During peak departure periods and poor weather, there are two ways in
which the airfield could be operated. The first would have departures
use both existing runways and assign most arrivals to the new runway. The
second would have departures use Runway 16L/34R and the new runway, while
most arrivals use Runway 16R/34L. The former has the advantage that
an increase in arrival rate can be handled by dependent instrument approaches
to the outboard runways, as in the peak arrival case. This would also
make the transition between arrival and departure peaks relatively easy. However,
the arrivals on the new runway would have to cross two departure runways,
although this is easier than crossing an arrival and a departure runway,
since departures can be held for crossing traffic, while arrivals cannot.
The large number of runway crossings that would have to be coordinated
under these various operating conditions obviously increase the potential
for runway incursions, either due to pilot or controller errors. (A
runway incursion is defined by the FAA as any occurrence at an airport
involving an aircraft, vehicle, person, or object on the ground that
creates a collision hazard or results in a loss of separation with an
aircraft taking off, intending to take off, landing, or intending to
land). Although most runway incursions do not result in collisions,
the few that do are often associated with great loss of life. The worst
accident in civil aviation history involved a runway collision at Tenerife
in the Canary Islands between two Boeing 747 aircraft. Several of the
recent air carrier accidents in the U.S. have also involved runway collisions. The
FAA is rightfully concerned about the number of runway incursions that
occur each year, and has a major program underway to reduce the frequency
with which they occur. However, to date this has not been particularly
effective, and the number of reported runway incursions last year increased
significantly over the previous year.
Among the factors that are believed to increase the risk of a runway
incursion occurring are traffic intensity, airfield complexity, and poor
visibility or darkness, for fairly self-evident reasons. Thus it appears
highly likely that the operational conditions that will occur at Sea-Tac
if the third runway is constructed will tend to increase the risk of
a runway incursion over the present conditions. Whether this increase
in risk is significant enough to be of concern, and whether steps can
be taken to offset or reduce it, is not clear without a careful study
of the issues involved. Of particular concern is the possibility that
operational procedures that may turn out to be necessary to reduce the
risk of runway incursions could result in greater delays than predicted
by the delay analysis undertaken thus far and upon which the FEIS and
FSEIS are based.
Unfortunately, the analysis of air traffic safety presented in Chapter
IV of the FEIS is based on some fairly simplistic, and erroneous, assumptions. A
separate analysis was performed for aircraft accidents and incidents
and pilot deviations. No consideration appears to have been given to
analyzing controller operational errors. The analysis of aircraft accidents
and incidents assumed a constant ratio of accidents and incidents to
aircraft operations, based on the average ratio over the period from
1984 to 1993. This was used to project the number of accidents and incidents
in the future. The discussion of Future Conditions for aircraft accidents
and incidents begins with the following, unsupported, statement:
No direct correlation exists between accidents and
incidents and the number of aircraft operations at a particular airport. (FEIS,
p. IV.7-18)
The analysis then proceeded to assume the very correlation that it had
just claimed did not exist. Since the projected number of accidents
and incidents in a given year depended only on the forecast traffic level,
it follows that the same number was obtained irrespective of the development
alternative being considered. This clearly makes no sense at all. The
analysis made an implicit assumption that the different alternatives
being considered had no effect on the accident or incident rates, and
then concluded that there was no difference between alternatives.
The analysis of pilot deviations was based on 122 occurrences over an
unspecified period since October 1987. Most of the occurrences were
airspace deviations and most were by general aviation pilots. There
were 9 runway incursions during this period, a rate of about 1.4 per
year by 1994. These were projected for future years for the do-nothing
alternative based on a constant ratio to aircraft operations. In the
case of development alternatives, the number of runway incursions was
projected for future years based on the projected increase in runway
crossings due to the new runway. However, the increase in the number
of runway crossings assumed appears implausibly low, varying from about
44 percent for 2000 to 42 percent in 2020. Since each operation on the
third runway generates two runway crossings, while each operation on
Runway 16R/34L only generates one under current conditions and of course
operations on Runway 16L/34R do not generate any, even if the new runway
only handles half as many operations as Runway 16R/34L the number of
runway crossings would double. If the departure queue for Runway 16R/34L
is located to the west of the runway, as discussed above, or the new
runway handles a larger share of the traffic, then the increase in the
number of runway crossings would be even greater.
Another concern with the analysis is the assumption that the likelihood
of a runway incursion occurring depends only on the number of runway
crossings, and not where those crossings take place. With the current
operating pattern, most runway crossings in poor weather involve arriving
traffic crossing a departure runway (Runway 16L/34R), since arrivals
cannot use both runways under these conditions. It is inherently easier
for controllers to manage traffic crossing a departure runway, because
departures can be held at the end of the runway to allow aircraft to
cross, whereas inbound arrivals cannot be stopped, nor can aircraft be
cleared to cross the runway if an arrival is within 2 miles of the threshold.
The discussion of runway crossings makes the following
statement:
No direct correlation exists between the increase in runway crossings and safety,
as the separation standards used by air traffic control will ensure
adequate separation between aircraft, and aircraft and service vehicles. (FEIS,
p. IV.7-21)
This demonstrates a misplaced faith in the infallibility of both controllers
and flight crew. If this were true, obviously no runway incursions would
ever occur. It may well be the case that the risk of a runway incursion
depends on more factors than just the number of runway crossings, but
that is very different from saying that there is no correlation between
runway crossings and incursions.
Because of these deficiencies in the analysis, the
information presented in the FEIS of the safety consequences of operating
three runways in the manner proposed does not adequately address the
issues involved, and a more careful study of this issue would need
to be undertaken before any firm conclusion can be drawn regarding
the extent to which the third runway would affect safety levels at
Sea-Tac.
Conclusion
The discussion of the potential contribution
of advanced CNS/ATM technology to enhancing the capacity of Sea-Tac and
the safety considerations involved in operating three parallel runways,
that is contained in the FEIS, FSEIS, and subsequent responses by the
Port of Seattle to public comments on these issues, has failed to consider
several important recent developments and has not adequately analyzed
the issues involved. Therefore further studies of these issues should
be undertaken before the U.S. Army Corps of Engineers can properly consider
the potential role of new technology to enhance the capacity of Sea-Tac
Airport, as well as assess any change in the risk of runway incursions
that could result from the construction of the third runway.
Sincerely,
Geoffrey D. Gosling
Attachment A
Resume
Attachment B
Description of FAA Safe Flight 21 Project
Source: http://www.faa.gov/safeflight21 (Downloaded
2/14/01)
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San Francisco
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The FAA has initiated a program to develop
and evaluate the operational concept and procedures
for a Paired Approach landing technique which
exploits the features available in aircraft
equipped with Automatic Dependent Surveillance-Broadcast
(ADS-B) and Cockpit Display of Traffic Information
(CDTI). The activity will be conducted by the
FAA's Safe Flight 21 Product Team in a cooperative
venture with United Airlines and NASA. The
motivation, concept and benefits are explained
below. The ADS-B concept and CDTI display are
illustrated in the accompanying two figures.
Approaches to airports with parallel runways
have different restrictions depending on the
weather conditions. During visual meteorological
conditions (VMC), visual approaches can be
conducted by aircraft operating under an instrument
flight rules (IFR) flight plan. Visual approaches
were originally designed to reduce pilot and
controller workload and to shorten flight paths
to an airport (FAA, 1999 AIM). The pilot must
report either the airport or the preceding
aircraft in sight to conduct the visual approach.
Upon accepting the visual approach, the pilot
is responsible for "maintaining a safe
approach interval and adequate wake turbulence
separation" (FAA, 1999 AIM). Simultaneous
visual approaches can be conducted if runways
are at least 700 feet apart.
To conduct visual approaches, reported weather
must be VMC (1000 feet and 3 miles or greater)
but visual approaches are discontinued at much
higher minima. In fact, capacity at airports
is greatly reduced when weather drops below
good VMC because aircraft cannot be vectored
for approaches when the ceiling is below minimum
vectoring altitude (MVA) plus 500 feet. In
actual practice, visual approaches are suspended
well above even these minima. Once visual approaches
are suspended, a reduction in capacity generally
occurs. For example, Boston Logan and San Francisco
International (SFO) airports experience a reduction
in capacity of approximately 40% when they
are unable to conduct visual approaches and
have to resort to a single runway.
Aircraft equipped with ADS-B and CDTI will
have a far superior situational awareness in
the cockpit in the form of air-to-air surveillance
displayed on the CDTI. This provides identity,
position, and altitude, heading and airspeed
of all aircraft within the vicinity. During
transition to ADS-B equipage, ADS-B equipped
aircraft may also receive Traffic Information
System-Broadcast (TIS-B) on their CDTI showing
ground surveillance data for non-equipped aircraft.
Aircraft equipped to conduct paired approach
will have a CDTI display mode with a display
range of approximately 2 to 4 miles and relevant
display information to permit pilots to conduct
paired approaches similar to that which would
be conducted visually in good VMC. The paired
approach CDTI display will highlight the aircraft
in the pair throughout the approach after the
pair assignments.
Approach control will assign lead and trail
aircraft pairing, runway assignments and altitude
based on aircraft input to the Airlines operations
Center and/or the Traffic Management Unit.
Upon verification of speeds, aircraft pairing
assignments will be made at ranges of approximately
45 nmi. Physical pairing (initial positioning)
will occur at approximately 20 miles from the
airport. Longitudinal / lateral spacing and
altitude difference will be adjusted next.
The final controllers will issue speed instructions
to the Final Approach Fix (FAF) and clear the
pair for paired approach at least 12 nmi from
the FAF.
After pairing, the lead aircraft conducts
its normal straight-in approach and fly a defined
deceleration profile after the FAF. The trailing
aircraft on adjacent approach is responsible
for maintaining spacing behind the lead aircraft.
The CDTI display on the trailing aircraft is
used to assist the pilot in maintaining appropriate
spacing through the use of a longitudinal "safe
zone" which is shown as a set of brackets
as well as an arrow to indicate the target
spacing to achieve prior to FAF. The trailing
aircraft stays within the "safe zone" and
achieves the target position to avoid blunders
and wake turbulence from the lead aircraft.
It is expected that Paired Approach will increase
and potentially restore capacity at major airports
during deteriorated weather conditions. This
will allow participating airlines to increase
their schedule reliability. It should also
reduce holding delays on the ground and in
the air, provide operational cost savings and
facilitate more efficient use of the terminal
airspace. While many details must be worked
out before flight tests can be considered,
major simulation efforts utilizing experienced
controllers and pilots have shown sufficient
promise to support this cooperative program
by the FAA's Safe Flight 21 Product Team, United
Airlines and NASA.
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Paired
Approach CDTI Enhancement
(4 Mile Range)
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