Amendment to Class B Airspace; Detroit, MI, 3305-3315 [2014-00622]
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Federal Register / Vol. 79, No. 13 / Tuesday, January 21, 2014 / Rules and Regulations
3305
TABLE 1 TO PARAGRAPH (e)—Continued
P/N
Part description
S–70, S–70A,
S–70C service
life
70400–08115–043, –045, –046, and –047 ....
70400–08162–042 ..........................................
70400–08166–041 ..........................................
70410–06520–044 through –046 ....................
Left Tie Rod Assembly ...................................
Forward Bellcrank Support Assembly ............
Lateral Servo Bellcrank ..................................
Tail Rotor Servo Assembly ............................
14,000
14,000/2,500 3
20,000
15,000
UH–60M
service life
4,600
5,600
11,000
11,000
SH–60B/F
service life
6,300
7,600
14,000
1 N/A
1 There is no service life limit listed because the parts on Model SH–60B/F have a different P/N than the parts on Models S–70, S–70A, and
S–70C.
2 For serial number (S/N) 32479930 through 324791859, with CAGE code 60078, the life limit is 1,300 hours TIS.
For S/N A241–07543 through A241–07594, A241–07706 through A241–07755, A241–07768 through A241–07771, A241–07800 through
A241–07831, R241–00101 through R241–00355, R241–00701 through R241–00966, and R241–01001 through R241–01166, the life limit is
2,500 hours TIS.
3 For S/N A–367–00001 through A367–00035, with CAGE code 78286, the life limit is 2,500 hours TIS.
(iii) Record the newly-established life limit
of each part on the part’s component log card
or equivalent record.
(2) After establishing the new life limit,
replace each part that has reached or
exceeded its new life limit with an airworthy
part before further flight.
(3) Do not install the following parts on a
Model S–70, S–70A, or S–70C helicopter if
they have been previously installed on a
Model UH–60M helicopter:
(i) Bolt, self retaining, P/N 70103–08801–
102;
(ii) Bifilar, P/N 70107–08400–046;
(iii) Aft Bellcrank, P/N 70400–08102–045;
(iv) Aft Walking Beam Assembly, P/N
70400–08104–048; or
(v) Close Tolerance Bolt, P/N 70400–
26802–102 and –103.
(f) Alternative Methods of Compliance
(AMOC)
(1) The Manager, Boston Aircraft
Certification Office, FAA, may approve
AMOCs for this AD. Send your proposal to:
Michael Davison, Flight Test Engineer,
Boston Aircraft Certification Office, Engine &
Propeller Directorate, 12 New England
Executive Park, Burlington, Massachusetts
01803; telephone (781) 238–7156; email
michael.davison@faa.gov.
(2) For operations conducted under a 14
CFR part 119 operating certificate or under
14 CFR part 91, subpart K, we suggest that
you notify your principal inspector, or
lacking a principal inspector, the manager of
the local flight standards district office or
certificate holding district office before
operating any aircraft complying with this
AD through an AMOC.
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(g) Subject
Joint Aircraft Service Component (JASC)
Code: 6220 Main Rotor Hub, 6230 Main Rotor
Mast/Swashplate, 6320 Main Rotor Gearbox,
6310 Engine/Transmission Coupling, 6510
Tail Rotor Drive Shaft.
(h) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
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16:01 Jan 17, 2014
Jkt 232001
(i) Pages 1–25 and 1–26, Section 1.1.3,
Component Life Prorating, of Sikorsky
Technical Manual TM 1–70–23AW–2,
Change 3, dated April 15, 2012.
(ii) Reserved.
(3) For Sikorsky service information
identified in this AD, contact Sikorsky
Aircraft Corporation, Customer Service
Engineering, 124 Quarry Road, Trumbull, CT
06611; telephone 1–800–Winged–S or 203–
416–4299; email sikorskywcs@sikorsky.com.
(4) You may view this service information
at FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd.,
Room 663, Fort Worth, Texas 76137. For
information on the availability of this
material at the FAA, call (817) 222–5110.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
(202) 741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Fort Worth, Texas, on December
5, 2013.
Kim Smith,
Directorate Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 2013–31459 Filed 1–17–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2012–0661; Airspace
Docket No. 09–AWA–4]
RIN 2120–AA66
Amendment to Class B Airspace;
Detroit, MI
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action modifies the
Detroit, MI, Class B airspace area to
contain aircraft conducting published
instrument procedures at Detroit
SUMMARY:
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Metropolitan Wayne County Airport
(DTW), Detroit, MI, within Class B
airspace. The FAA is taking this action
to support containment of aircraft
operations using the three existing dual
Simultaneous Independent Instrument
Landing System (SIILS) configurations,
runways 22R/21L, runways 4L/3R and
runways 27L/27R, as well as support
containment of aircraft operations for
triple SIILS operations to runways 4L/
4R/3R and runways 21L/22L/22R. This
action will enhance safety, improve the
flow of air traffic, and reduce the
potential for midair collisions in the
DTW terminal area, while
accommodating the concerns of all
airspace users. Furthermore, this effort
supports the FAA’s national airspace
redesign goal of optimizing terminal and
enroute airspace areas to reduce aircraft
delays and improve system capacity.
DATES: Effective Date: 0901 UTC, April
3, 2014. The Director of the Federal
Register approves this incorporation by
reference action under 3 CFR part 51,
subject to the annual revision of FAA
Order 7400.9 and publication of
conforming amendments.
FOR FURTHER INFORMATION CONTACT:
Colby Abbott, Airspace Policy and
Regulations Group, Office of Airspace
Services, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
History
On August 14, 2012, the FAA
published in the Federal Register a
notice of proposed rulemaking (NPRM)
to modify the Detroit Class B airspace
area (77 FR 48476). This action
proposed to expand the lateral and
vertical limits of the Detroit Class B
airspace area to provide additional
airspace needed to contain dual SIILS
procedures and associated traffic
patterns supporting runways 22R/21L,
runways 4L/3R, and runways 27L/27R
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simultaneous operations within Class B
airspace. The action also supports
airspace requirements necessary for
planned triple SIILS procedures and
associated traffic patterns to runways
4L/4R/3R and runways 21L/22L/22R
operations within Class B airspace.
In addition, the FAA published in the
Federal Register a document correcting
the 5-mile arc of the DXO VOR/DME
boundary reference information
published in the Areas C, D, and E
regulatory text descriptions to the 15mile arc of the DXO VOR/DME (77 FR
53159, August 31, 2012). Interested
parties were invited to participate in
this rulemaking effort by submitting
written comments on the proposed
action. Twenty-three written comments
were received in response to the notice.
The FAA considered all substantive
comments received before making a
determination on this final rule.
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Discussion of Comments
One commenter suggested that the
meetings associated with Detroit Class B
airspace modification were held in
secret, and without notice to the general
public. The commenter stated the
groups that attended were specifically
invited and were not representing the
interests of the flight schools in the area
impacted by the proposed changes.
The FAA considers the comment to be
specific to the Ad Hoc Committee
process the FAA follows during the
initial airspace design phase prior to the
initiation of rulemaking. To ensure local
user needs and suggestions are
considered during the initial airspace
design phase, an Ad Hoc Committee is
formed. The Ad Hoc Committee’s
purpose is to obtain suggestions from a
cross section of users and aviation
organizations that could be affected by
a proposed airspace change before the
FAA develops a proposed airspace
design. The committee makeup and size
is determined by the local situation or
requirements and includes
representatives of local users and
aviation organizations.
As noted in the NPRM in the
Discussion of Ad Hoc Committee
Recommendations and Comments
section, the interests of the flight
schools were represented by the Ad Hoc
Committee. The committee made
recommendations to the FAA
addressing the western boundary
remaining basically unchanged in
support of outlaying airports, glider
activities, and parachute operations; an
ATC advisory service to VFR pilots in
areas of intensive flight training; and
boundary changes to maintain the
ability to fly practice approaches at
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airports without the need for Class B
airspace services.
Additionally, the FAA hosted three
informal airspace meetings for the
general public on July 20, 21, and 22,
2010, that were intended to inform the
general public, affected airspace users,
and aviation organizations of the
proposed airspace changes and to gather
facts and information relevant to the
planned regulatory action. The FAA
published notice of the meetings in the
Federal Register (May 13, 2010; 75 FR
11496) and mailed 14,852 informal
airspace meeting notification letters to
all registered pilots that resided within
100 miles of DTW. As a result, the FAA
received comments from 29 individuals.
Five commenters addressed public
involvement in the regulatory process
proposing to modify the DTW Class B
airspace. One commenter praised the
FAA’s decision to limit western
expansion of the DTW Class B airspace
contained in the proposal following
industry and community input.
Conversely, four other commenters
believed the FAA largely ignored the
concerns and recommendations of the
Ad Hoc Committee and public in
developing the proposed DTW Class B
airspace modification. In general, they
argued that the FAA was going through
the motions of gathering public
comments, but had no intention of
modifying the proposal to address the
concerns raised by the committee and
the public.
The purpose of modifying the DTW
Class B airspace is to contain large
turbine-powered aircraft conducting
instrument procedures within Class B
airspace once they entered it, enhance
flight safety by segregating large turbinepowered aircraft and non-participating
VFR aircraft flying in the vicinity of the
DTW Class B airspace area, and contain
the instrument procedures and
associated traffic flows and patterns
supporting those procedures at DTW
within Class B airspace. The DTW Class
B airspace design was influenced by Ad
Hoc Committee and public comments
and recommendations received
throughout the airspace regulatory
process addressing VFR aircraft training
areas and activities west of DTW;
protection of an uncharted VFR flyway
over the Detroit River; the glider,
parachute, and ultra-light activities
located around DTW; the geographic
location and proximity of satellite
airports around DTW; and potential
impacts to non-participant VFR aircraft
transiting the DTW terminal area.
In direct response to comments and
recommendations received, the FAA
made numerous adjustments to the
Class B airspace area proposal. This
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included reducing the western
boundary and associated Class B
airspace shelves, adjusting multiple
Class B airspace sub-area boundaries
and floor altitudes, retaining an
uncharted VFR flyway, and aligning
airspace boundaries with easily
identifiable geographic landmarks.
The FAA removed the airspace area
west of DTW from the Class B airspace
proposal, from the DXO 333 radial
counterclockwise to the SVM 217 radial
west of Ann Arbor and Willow Run
airports, and terminated the Class B
airspace shelf located 25 nautical miles
(NM) to 30 NM southwest of DTW and
east of Meyers-Divers Airport (3TE). The
reduced western boundary provides the
minimum amount of Class B airspace
necessary to contain large turbinepowered aircraft flying the instrument
procedures and associated traffic
patterns to/from DTW within Class B
airspace while minimizing impact to
VFR aircraft flying in existing training
areas, parachute and glider activities,
and airport operations all located west
of DTW.
After originally planning to lower
Class B airspace north of DTW in the
vicinity of the highways from 4,000 feet
MSL to 3,000 feet MSL, the FAA raised
the proposed shelf to a minimum of
3,500 feet MSL along the entire length
of Interstate 696 (I–696). That change
specifically responded to concerns
about a reduced volume of airspace
being squeezed between the Class B
airspace floor, the obstructions along I–
696, and aircraft flying in and out of
Oakland-Troy Airport (VLL) depicted in
the original design.
With respect to recommendations for
a single Class B airspace floor overlying
Class D airspace areas, the FAA
minimized the proposed Class B
airspace to the extent practical to ensure
containment of large turbine-powered
aircraft flying instrument procedures
within Class B airspace. The FAA does
not agree with establishing a single
Class B airspace floor over the two
airports affected by this
recommendation (Ann Arbor Municipal
Airport (ARB) and Coleman A. Young
Municipal Airport (DET)) because this
would be excessive to what is required
and unnecessarily include navigable
airspace that would otherwise be
available to non-participating VFR
aircraft.
Based on recommendations not to
lower the 3,000-foot MSL Class B
airspace floor above an uncharted VFR
flyway over the Detroit River, the FAA
moved the proposed 2,500-foot MSL
Class B airspace shelf boundary closer
to DTW to a 10 NM arc of the DXO
VOR/DME and reduced the proposed
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Class B airspace surface area boundary
to an 8 NM arc of the DXO VOR/DME.
These adjustments ensure that the
existing uncharted VFR flyway will be
unaffected, allow easier access at the
southern end of the Detroit River, and
enable practice approaches at Grosse Ile
Municipal Airport (ONZ) without
needing a Class B airspace clearance.
The FAA also used landmarks to
assist VFR pilots in non-GPS equipped
aircraft with easily determining their
position relative Class B airspace
boundaries. As recommended by the Ad
Hoc Committee and airspace users, this
rule adopts boundary modifications that
align with Interstate highways I–696
and I–94, the Ford World Headquarters
building, and the Detroit River and Lake
Erie shoreline. Additionally, the FAA
retained numerous landmarks depicted
on the Detroit VFR Terminal Area Chart
to assist VFR pilots.
Fourteen comments addressed the
proposed vertical expansion of the DTW
Class B airspace ceiling from 8,000 feet
MSL to 10,000 feet MSL. Four
commenters challenged the operational
necessity of the Class B airspace ceiling
being raised. Eleven of the commenters
argued that raising the Class B airspace
area ceiling to 10,000 feet MSL does not
increase safety.
Raising the ceiling of the DTW Class
B airspace area is necessary to enhance
flight safety for all airspace users in the
DTW terminal area. As mentioned in the
NPRM, DTW arrivals enter the terminal
area at 12,000 feet MSL, enter the traffic
patterns abeam DTW descending out of
11,000 feet MSL, and are then vectored
by the final controller beginning at
9,000 feet MSL on the downwind and
8,000 feet MSL on base leg of the
patterns to the final approaches. As a
result, a 3,000 foot gap of airspace exists
between the altitude that DTW arrivals
are descending out of to enter the traffic
pattern at 11,000 feet MSL and the Class
B ceiling of 8,000 feet. Large turbinepowered aircraft arriving DTW and nonparticipating VFR aircraft, not
communicating with Detroit Terminal
Radar Approach Control (D21), are
operating simultaneously within this
gap of airspace today.
The FAA identified several issues
with the 8,000 foot MSL ceiling. It does
not segregate large turbine-powered
aircraft arriving/departing DTW from
the conflicting non-participant VFR
aircraft flying over the DTW Class B
airspace at 8,500 and 9,500 feet MSL.
Additionally, VHF Omnidirectional
Range (VOR) Federal airways V–2, V–
10, V–65, V–116, V–133, V–176, V–188,
V–276, V–383, V–410, and V–426
traverse the DTW terminal area and
enable VFR aircraft, not communicating
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16:01 Jan 17, 2014
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with D21, to fly over the DTW Class B
airspace area and conflict with the DTW
arrival/departure flows operating in the
same airspace area. Raising the ceiling
of the DTW Class B airspace will
enhance flight safety by segregating the
large turbine-powered aircraft arriving/
departing DTW and the nonparticipating VFR aircraft overflying
DTW.
Raising the DTW Class B airspace
ceiling to 10,000 feet MSL also provides
operational and safety advantages by
establishing additional airspace for ATC
to more efficiently vector and sequence
arrival and departure aircraft within the
Class B airspace, as well as segregate
them from non-participating VFR
aircraft that are operating in the same
volume of airspace overhead DTW, as
they do today. The raised ceiling
ensures departure aircraft achieve the
required 1,000 feet of standard
separation over the top of the
downwind arrival traffic flying at 9,000
feet MSL, while remaining 1,000 feet
below the traffic pattern aircraft at
11,000 feet MSL. Currently, aircraft
departing DTW and requesting to climb
to 10,000 feet MSL and above are
impacted when D21 must vector the
aircraft, at low altitudes, to avoid
conflicting non-participant VFR traffic
overflying the DTW Class B airspace
area. In some instances, D21 must stop
all departures until the conflicting
traffic is clear. Raising the Class B
airspace ceiling to 10,000 feet MSL
requires non-participant VFR over flight
traffic, which opt to obtain Class B
airspace services, to communicate with
D21. This will enhance the operational
and flight safety benefits for all aircraft
operating above DTW, up to 10,000 feet
MSL, by enabling D21 to efficiently
sequence and separate arriving,
departing, and non-participant VFR over
flight aircraft simultaneously operating
within DTW Class B airspace.
Also, as noted in the NPRM, the
eastern portion of the DTW Class B
airspace area extends into Canadian
airspace. The equivalent Canadian
airspace to Class B airspace, as
designated in the United States, is Class
C airspace. NAV CANADA, the
Canadian air service navigation
provider, generally designates Class C
airspace with a 12,500 feet MSL ceiling,
however, has advised the FAA of its
willingness to establish corresponding
Canadian Class C airspace adjoining the
FAA’s DTW Class B airspace with a
ceiling of 10,000 feet MSL.
Additionally, NAV CANADA advised it
would make the Canadian Class C
airspace action effective to match the
effective date of this DTW Class B
airspace modification action.
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3307
Six commenters asserted that there
was insufficient justification to expand
the Class B airspace area boundary from
20 NM to 30 NM and that the proposed
expansion was based solely on future
procedures. One of the commenters
further argued that extending the lateral
boundaries of DTW Class B airspace to
30 NM will greatly affect the VFR flight
areas for airports like Brighton and
Livingston County for aircraft without
electrical systems.
Extending the DTW Class B airspace
to a 30 NM boundary is designed to
address current and future issues of
containing aircraft executing instrument
procedures within the confines of Class
B airspace. Today, large turbinepowered aircraft conducting dual SIILS
procedures are unable to be contained
within existing Class B airspace and are
entering, exiting, and reentering DTW
Class B airspace while flying the
published instrument approach
procedures and associated traffic
patterns. There are approximately 1,770
operations daily at DTW and D21 is
experiencing an average of 156 Class B
airspace excursions by large turbinepowered aircraft per day. As a result,
large turbine-powered aircraft and nonparticipating VFR aircraft flying in the
vicinity of the Class B airspace
boundaries, not in communication with
D21, are operating simultaneously in the
same volume of airspace.
The existing dual SIILS approaches in
use today enable an arrival capacity of
72 arrivals an hour. The expanded
boundary provides the minimum
amount of airspace essential to contain
the large turbine-powered aircraft
arriving from multiple arrival streams
being sequenced for and conducting the
SIILS procedures. Aircraft flying dual
SIILS procedures are assigned altitudes
that differ by at least 1,000 feet and they
are turned on to SIILS approaches so as
to ensure they are established on the
localizer signal at or outside mandatory
turn on points. For dual SIILS approach
configurations to Runways 21L/22R, the
mandatory turn on point is 18 NM from
the runways; for Runways 3R/4L, the
mandatory turn on point is 18 NM from
the runways; and for Runways 27L/27R,
the mandatory turn on point is 20 NM
from the runways. These are the
minimum distances that large turbinepowered aircraft must be established on
the localizer signal for dual SIILS
approaches and facilitate D21
controllers to meet minimum aircraft
separation guidance requirements for
simultaneous independent ILS
approaches. During moderate to heavy
arrival rushes, the turn on distances
extend outward an additional four to ten
NM beyond the minimum turn on
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Federal Register / Vol. 79, No. 13 / Tuesday, January 21, 2014 / Rules and Regulations
distances; extending beyond the 20 NM
DTW Class B airspace boundary.
Although the existing dual SIILS
procedures enable an arrival capacity of
72 aircraft per hour, DTW demand
exceeds that level on a daily basis. To
address this shortcoming of capacity,
triple SIILS approach procedures, which
increase DTW is arrival capacity to 112
arrivals per hour, are planned for
implementation in spring 2014. As with
dual SIILS procedures, aircraft
conducting triple SIILS procedures will
be assigned altitudes differing by at least
1,000 feet and turned on to the SIILS
approaches so they are established on
the localizer signal at or outside
mandatory turn on points. For triple
SIILS approaches to a Runways 21L/
22L/22R configuration, the mandatory
turn on point is 21 NM from the
runways, and for a Runways 3R/4R/4L
configuration, the mandatory turn on
point is 20 NM from the runways. These
are the minimum distances aircraft must
be established on the localizer signal for
triple SIILS approaches, thereby
allowing D21 controllers to meet
minimum aircraft separation guidance
requirements for simultaneous
independent ILS approaches. And,
during moderate to heavy arrival rushes,
the turn on distances will again extend
an additional 4 to 10 NM beyond these
minimum turn on distances; extending
beyond the 20 NM DTW Class B
airspace boundary.
With respect to the comment that
extending the lateral boundaries to 30
NM will greatly affect the VFR flight
areas of airports like Brighton and
Livingston County for aircraft without
electrical systems, both airports fall
outside the 30 NM DTW Class B
airspace area boundary. As such, there
is no affect or impact expected to the
VFR flight areas of these airports for
aircraft with or without electrical
systems. Modifying the Class B airspace
boundary to extend to 30 NM is
necessary to enhance flight safety by
containing the large turbine-powered
aircraft flying instrument procedures at
DTW within Class B airspace, as well as
segregating those aircraft and nonparticipating VFR aircraft operating in
the vicinity of the DTW Class B airspace
area from one another.
Five commenters addressed the new
Class B airspace shelves included in the
proposal and the floor altitudes of those
areas. Specifically the commenters
contend that the FAA ignored user
feedback and requests to raise the newly
proposed outermost ring of Class B
airspace to a floor of 8,000 feet MSL and
commenting that the lower 6,000 foot
MSL floors were unjustified. They
further argued that the Class B airspace
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16:01 Jan 17, 2014
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shelves proposed southwest of DTW
that lowered a portion of an existing
Class B airspace from 4,000 feet MSL to
3,000 feet MSL and established two new
Class B airspace shelves with floors at
4,000 feet MSL and 6,000 feet MSL were
unnecessary.
The DTW Class B airspace area
boundary, extending to 30 NM north of
DTW clockwise to the southwest of
DTW, is necessary for the reasons stated
above. Specific to the comments
received about Class B airspace floor
altitudes, the Class B airspace
modifications accomplished by this
action establishing new Class B airspace
shelves with 3,000-foot MSL, 4,000-foot
MSL, and 6,000-foot MSL floors, which
are necessary to contain the large
turbine-powered aircraft being vectored
for and conducting instrument
procedures at DTW within Class B
airspace. Additionally, the amended
and new Class B airspace floor altitudes
are aligned with the glide slopes of all
the ILS approaches to ensure aircraft
flying the instrument procedures are
contained within Class B airspace
throughout the entire approach.
Operationally, aircraft conducting
dual SIILS approaches to any of the
three existing dual SIILS runway
configurations enter the DTW terminal
area at 12,000 feet MSL descending to
enter the traffic pattern at either 6,000
feet MSL, descending further to as low
as 4,000 feet MSL on a base leg, or at
7,000 feet MSL abeam DTW on a
downwind, descending further to as low
as 4,000 feet MSL on a base leg.
Regardless of traffic flow (north, south,
or west), or the direction from which the
aircraft enters the DTW terminal area,
all aircraft are descended to as low as
4,000 feet MSL in preparation for turn
on to the final approach course prior to
the mandatory turn on points
mentioned previously. When the
planned triple SIILS procedures are
implemented to either of the triple SIILS
runway configurations, aircraft assigned
the ‘‘middle runway’’ will enter the
terminal area at 12,000 feet MSL, be
delivered to, and vectored by, the final
controller at 9,000 feet MSL on the
downwind and at 8,000 feet MSL on a
base leg. The aircraft assigned the
outboard runways will continue to enter
the traffic pattern at 6,000 feet MSL and
7,000 feet MSL abeam DTW on a
downwind, descending to as low as
4,000 feet MSL on base leg, as described
above for dual SIILS procedures.
The DTW Class B airspace area floor
altitudes established by this rule,
extending to 30 NM, ensure
containment of large turbine-powered
aircraft being vectored for and
conducting SIILS approaches to the
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three existing dual SIILS configurations
today (runways 4L/3R, runways 22R/
21L, and runways 27L/27R) within
Class B airspace; assure segregation of
large turbine-powered aircraft and nonparticipating VFR aircraft from
operating simultaneously in the same
airspace; and provide a Class B airspace
configuration that ensures future
containment needs when DTW
implements triple SIILS procedures to
meet arrival capacity requirements.
Six commenters contended that there
are safety concerns associated with the
Class B airspace modifications. Five of
the commenters submitted that the
proposed changes would force nonparticipating VFR aircraft to fly at lower
altitudes to circumnavigate Class B
airspace and would compress this
transient VFR traffic into the same
airspace areas that general aviation
airports are operating, thereby creating a
dangerous situation due to increased
congestion and risk of mid-air collision.
One commenter objected to the
proposed changes stating that the
modifications would decrease the
usability and safety of Detroit’s airspace.
The primary purpose of a Class B
airspace area is to reduce the potential
for midair collisions in the airspace
surrounding airports with high density
air traffic operations by providing an
area in which all aircraft are subject to
certain operating rules and equipment
requirements. FAA directives require
Class B airspace areas be designed to
contain all instrument procedures, and
that air traffic controllers vector aircraft
as appropriate to remain within Class B
airspace after entry.
With the DTW Class B airspace
configuration established in 1987,
arriving large turbine-powered aircraft
routinely enter, exit, and then re-enter
Class B airspace while flying published
instrument procedures today, which is
contrary to FAA directives. The
procedural requirements for establishing
these aircraft on the final approach
courses, to conduct simultaneous
independent approaches to the existing
parallel runways, has resulted in aircraft
exceeding the lateral boundaries of the
Class B airspace by up to 10 NM during
moderate to heavy arrival rushes. The
DTW Class B airspace modified by this
rule enhances flight safety by containing
all instrument approach procedures and
associated traffic patterns within the
boundaries of Class B airspace,
supporting increased operations to the
current dual and planned triple SIILS
runways, and better segregating the
large turbine-powered aircraft arriving/
departing DTW and non-participating
VFR aircraft operating in the vicinity of
DTW Class B airspace from one another.
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Federal Register / Vol. 79, No. 13 / Tuesday, January 21, 2014 / Rules and Regulations
The FAA acknowledges and
recognizes that VFR pilots electing to fly
below the floor of Class B airspace may
be compressed. However, the lower
floors are necessary to segregate those
aircraft operations from the large
turbine-powered aircraft arriving and
departing DTW. The Detroit terminal
area encompasses the world’s eleventh
(out of fifty) busiest airport (with over
443,000 airport operations in CY 2011),
plus numerous other airports situated in
and around the Detroit terminal area.
These factors create a complex, high
density airspace environment
containing a highly diverse mix of
aircraft types and aviation activities. In
some areas, large turbine-powered
aircraft and non-participating VFR
aircraft are flying simultaneously in the
same airspace. It is essential to segregate
the large turbine-powered aircraft
arriving/departing DTW and the nonparticipating VFR aircraft that may not
be in communication with ATC.
Consequently, some non-participating
VFR aircraft may have to fly further, or
at different altitudes, in order to remain
clear of the modified DTW Class B
airspace area. Ultimately, it is the pilot’s
responsibility to evaluate all factors that
could affect a planned flight and
determine the safest course of action
whether it is circumnavigating the Class
B airspace, flying over or beneath the
Class B airspace, utilizing a charted VFR
flyway, or requesting Class B clearance
and services from D21.
Six commenters asserted that the
Class B airspace modifications will
place an undue burden on general
aviation operators wishing to conduct
VFR training flights. The commenters
claimed that the modifications will have
a negative impact on training and
further believed that there will not be
sufficient altitudes available to conduct
most maneuvers.
The DTW Class B airspace will not
cause any VFR training practice areas to
be lost due to the modified design. The
FAA acknowledges that the floor of the
Class B airspace established by this
action could impact the available
altitudes in portions of some training
areas located southwest of DTW and a
portion of one training area northwest of
DTW, should VFR training aircraft
choose not to request Class B services
with D21. However, by adopting a
number of recommendation submitted
by the Ad Hoc Committee and during
informal airspace meetings, the FAA
adjusted the western boundary of Class
B airspace to alleviate many practice
area impacts. The result is that the
practice areas west and north of Ann
Arbor would be unaffected.
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The Class B airspace established
southwest of DTW is required to contain
large turbine-powered aircraft
conducting dual SIILS arrival
procedures to Runways 4L/3R, as well
as arrivals entering the DTW terminal
airspace via the POLAR1 STAR. It
extends over approximately three
quarters of the Eastern Michigan
University (EMU) Aviation flight
school’s southern practice area with
3,500-foot MSL, 4,000-foot MSL, and
6,000-foot MSL Class B airspace floors.
The EMU southern practice area is
subdivided into four sub-areas with
virtually no impact to the west
northwest sub-area and minor impacts
to the southern sub-area, but training
activities in the northeast and southeast
sub-areas will be limited to 4,000 feet
MSL, unless pilots receive a Class B
airspace clearance. The FAA does not
expect a substantive change to the
concentration of VFR training aircraft or
training activities conducted in that
practice area or the other practice areas
located further southwest of DTW under
the 6,000-foot MSL Class B airspace
shelf. The training activities conducted
in those practice areas today could
continue under the DTW Class B
airspace or within Class B airspace with
the appropriate Class B airspace
clearance.
The VFR practice area near the
General Motors Proving Ground, located
north of DTW and southwest of PTK, is
partially under a DTW Class B airspace
shelf with a 6,000-foot MSL floor;
however, VFR training flight activities
above 6,000 feet MSL are not normally
accomplished there and the 6,000-foot
MSL Class B airspace floor will have
negligible impact.
And, as noted in the NPRM, the FAA
will continue working with the local
flight training schools to discuss and
pursue aircraft training program
activities, scheduling, and airspace
alternatives, as required, independent of
this Class B airspace modification
action.
Three commenters challenged the
DTW Class B airspace modifications
arguing that they increase the waste of
fuel, time, and cost to the VFR traffic
that currently uses the airspace areas
being established as Class B airspace.
One commenter contends that there
would be increases to the cost of flight
training to clear the Class B airspace
area completely, while another
commenter allege that the Class B
airspace hampers the effectiveness of
the General Aviation (GA) community
in the Detroit Metropolitan area and
costs them more to operate in and
around DTW.
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The FAA recognizes the Class B
airspace modifications could increase
fuel burn for non-participating VFR
aircraft. To remain clear of the DTW
Class B airspace area, non-participating
VFR pilots who elect not to contact D21
for Class B services may end up flying
at lower altitude or further distances to
circumnavigate the Class B airspace.
However, this action is necessary to
separate them from the large turbinepowered aircraft being contained within
the Class B airspace while flying
instrument procedures and associated
traffic flows/patterns. While some GA
pilots will opt to fly additional distance
or different altitudes to circumnavigate
the Class B airspace, the FAA believes
any increase in fuel burn or cost to be
minimal and justified by the overall
increase in flight safety. The DTW Class
B airspace has no impact to the routes
or altitudes assigned to IFR and
participating VFR aircraft flying in the
Detroit terminal area. Additionally, the
VFR flyways that are charted on the
Detroit VFR Terminal Area Chart remain
available for use by GA pilots to transit
north and south or east and west under
and around the DTW Class B airspace
area.
As addressed previously, the Class B
airspace design incorporated
recommended changes received from
the Ad Hoc Committee and informal
airspace meetings to prevent impacts,
operationally and economically, to the
non-participating VFR training aircraft
flying in the vicinity of the DTW Class
B airspace area.
Fifteen comments were received from
the public regarding the fair and
equitable access to the DTW Class B
airspace area. Eleven of the commenters
asserted that the Class B airspace design
unfairly affects the activities of the local
GA community, limiting their access,
without a demonstrated need. Three
commenters stated that D21 routinely
denies Class B airspace entry requests,
or ignores the requests altogether, to
highlight the limited access.
The FAA remains committed to
providing Class B airspace services to
all National Airspace System (NAS)
users operating in the airspace
surrounding DTW in a manner that
keeps the Detroit terminal area safe for
all users. As mentioned previously, the
primary purpose of a Class B airspace
area is to reduce the potential for midair
collisions in the airspace surrounding
airports with high density air traffic
operations by providing an area in
which all aircraft are subject to certain
operating rules and equipment
requirements.
Class B airspace services are not
restricted to only those aircraft landing
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or departing the primary airports around
which the Class B airspace is
established. Various types of aircraft are
routinely cleared into and through DTW
Class B airspace when traffic conditions
permit doing so safely. Based on
historical data and forecast trends, the
D21 average daily traffic count includes
684 air carrier, 707 air taxi, 364 general
aviation, 15 military IFR operations and
69 VFR operations. When VFR aircraft
request Class B services to transit the
DTW Class B airspace, they are initially
told to remain outside the Class B
airspace until radar identification is
established; unfortunately and
oftentimes, this is misunderstood as
denial of Class B services. In 2012, D21
provided Class B services to 25,216 VFR
aircraft operations. Routinely, D21
provides Class B airspace clearances
and services to VFR aircraft requesting
access into and through the DTW Class
B airspace when the arrival/departure
traffic volume and airspace capacity
conditions enable doing so safely.
tkelley on DSK3SPTVN1PROD with RULES
Differences From the NPRM
Editorial corrections have been made
to the Detroit Class B airspace
description for clarity and for
standardization. Areas A, C, D, F, and H
have editorial corrections whereas, the
Detroit Class B airspace header and all
Areas with reference to ‘‘DXO VOR–
DME’’ have been corrected to read
‘‘DXO VOR/DME’’ for standardization.
Also, in the NPRM description of Area
A, a typographical error that listed a
geographic reference as ‘‘lat. 42°5′17″
N., long. 83°26′04″ W.’’ on the 4.4-mile
radius of the Detroit Willow Run
Airport has been corrected to read ‘‘lat.
42°15′17″ N., long. 83°26′04″ W.’’. With
the exception of the above noted
changes and minor editorial corrections,
this rule reflects the same Class B
airspace area as that published in the
NPRM.
The Rule
The FAA is amending Title 14 of the
Code of Federal Regulations (14 CFR)
part 71 to modify the Detroit Class B
airspace area. This action (depicted on
the chart in Figure 1—Amendment of
the Detroit, MI Class B Airspace Area)
lowers the floor of Class B airspace in
portions of the Detroit Class B airspace
area; extends Class B airspace out to 30
NM to the north, east (designated Class
C airspace in Canada), and south of
DTW; and raises the ceiling of the entire
Class B airspace area from 8,000 feet
MSL to 10,000 feet MSL. These
modifications provide the airspace
needed to contain large turbine-powered
aircraft conducting instrument
procedures within the confines of Class
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B airspace, especially when flying
existing dual and planned triple SIILS
approaches. Additionally, these airspace
modifications will ensure efficient
airspace utilization and enhance safety
by better segregating the large turbinepowered IFR aircraft arriving/departing
DTW and the non-participating VFR
aircraft operating in the vicinity of the
Detroit Class B airspace area. The
modifications to the Detroit Class B
airspace area are summarized below:
Area A. Area A extends from the
ground upward to 10,000 feet MSL,
centered on the Detroit VOR/DME
antenna. The surface area is expanded
by relocating the southern boundary
approximately 2.5 NM further south and
lowering the Class B airspace floor in
that expanded portion of existing Class
B airspace from 2,500 feet MSL to the
surface.
Area B. Area B extends upward from
2,500 feet MSL to 10,000 feet MSL. The
Area B extends from north clockwise to
the southwest of DTW between the 8
NM and the 10 NM arcs of the Detroit
VOR/DME antenna. The Class B
airspace floor is lowered from 3,000 feet
MSL to 2,500 feet MSL in the expanded
portions of existing Class B airspace
northeast and southeast of DTW.
Area C. Area C continues to surround
Areas A and B and extends upward
from 3,000 feet MSL to 10,000 feet MSL.
The Area C boundary from east
clockwise to the southwest of DTW is
expanded to match the 20 NM arc of the
Detroit VOR/DME antenna and from
north clockwise to the northeast of DTW
is expanded to match the 15 NM arc of
the Detroit VOR/DME antenna. The
Class B airspace floor is lowered from
4,000 feet MSL to 3,000 feet MSL in the
expanded portions of existing Class B
airspace and established at 4,000 feet
MSL for the expanded portions that
were previously outside the Detroit
Class B airspace area.
Area D. Area D is redefined to extend
upward from 3,500 feet MSL to 10,000
feet MSL. Area D overlays the
southeastern half of the Ann Arbor Class
D airspace area and extends
approximately 7 NM south of the Ann
Arbor Class D airspace area between the
15 NM and 20 NM arcs of the Detroit
VOR/DME antenna. The Class B
airspace floor is raised from 3,000 feet
MSL to 3,500 feet MSL for a portion of
existing Class B airspace area, lowered
from 4,000 feet MSL to 3,500 feet MSL
for another portion of existing Class B
airspace area, and established at 3,500
feet MSL for the portion that was
previously outside the Detroit Class B
airspace area.
Area E. Area E is a new subarea that
extends upward from 3,500 feet MSL to
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10,000 feet MSL. Area E is located north
clockwise to northeast of DTW between
the 15 NM and 20 NM arcs of the Detroit
VOR/DME antenna. The Class B
airspace floor is lowered from 4,000 feet
MSL to 3,500 feet MSL in the portion of
existing Class B airspace and
established at 3,500 feet MSL for the
portions that were previously outside
the Detroit Class B airspace area.
Area F. Area F is a new subarea that
extends upward from 4,000 feet MSL to
10,000 feet MSL. This area is
established from north clockwise to
west southwest of DTW between the 20
NM and 25 NM arcs of the Detroit VOR/
DME antenna. The Class B airspace floor
is raised from 3,000 feet MSL to 4,000
feet MSL in the portion of existing Class
B airspace located west of DTW and
established at 4,000 feet MSL for the
portion that was previously outside the
Detroit Class B airspace area.
Area G. Area G is a new subarea that
extends upward from 6,000 feet MSL to
10,000 feet MSL. This new area is
located southwest of DTW between the
25 NM and 30 NM arcs of the Detroit
VOR/DME antenna. This area abuts
Area F and I (described below) and
establishes the Class B airspace floor at
6,000 feet MSL in airspace previously
outside of the Detroit Class B airspace
area.
Area H. Area H is also a new subarea
that extends upward from 6,000 feet
MSL to 10,000 feet MSL. This new area
is located from north northwest
clockwise to southeast of DTW and
abuts Areas C, E, F, and I (described
below) extending to the 25 NM arc of
the Detroit VOR/DME antenna. The
Class B airspace floor is established at
6,000 feet MSL in airspace previously
outside of the Detroit Class B airspace
area.
Area I. Area I is another new subarea
that extends upward from 9,000 feet
MSL to 10,000 feet MSL. This new area
is established south of DTW and abuts
Areas F, G, and H extending to the 30
NM arc of the Detroit VOR/DME
antenna. The Class B airspace floor is
established at 9,000 feet MSL in
airspace previously outside the Detroit
Class B airspace area.
Finally, this action updates the DTW
airport reference point coordinates to
reflect current NAS data; includes all
airports and navigation aids, with
geographic coordinates, used to describe
the Detroit Class B airspace in the
Detroit Class B airspace area legal
description header; and describes the
Detroit Class B airspace area centered on
the Detroit VOR/DME (DXO) antenna.
All radials listed in the Detroit Class
B airspace area description in this rule
are stated in degrees relative to True
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North. All geographic coordinates listed
in the Detroit Class B airspace area
description in this rule are stated in
degrees, minutes, and seconds based on
North American Datum 83. And, all
mileages listed in the Detroit Class B
airspace area description in this rule are
nautical miles.
Class B airspace areas are published
in paragraph 3000 of FAA Order
7400.9X, Airspace Designations and
Reporting Points, dated August 7, 2013,
and effective September 15, 2013, which
is incorporated by reference in 14 CFR
section 71.1. The Class B airspace area
listed in this rule will be published
subsequently in the Order.
Environmental Review
The FAA has determined that this
action qualifies for categorical exclusion
under the National Environmental
Policy Act in accordance with FAA
Order 1050.1E, ‘‘Environmental
Impacts: Policies and Procedures,’’
paragraph 311a. This airspace action is
not expected to cause any potentially
significant environmental impacts, and
no extraordinary circumstances exist
that warrant preparation of an
environmental assessment.
tkelley on DSK3SPTVN1PROD with RULES
Paperwork Reduction Act
The Paperwork Reduction Act of 1995
(44 U.S.C. 3507(d)) requires that the
FAA consider the impact of paperwork
and other information collection
burdens imposed on the public. We
have determined that there is no new
information collection requirement
associated with this rule.
Regulatory Evaluation Summary
Changes to Federal regulations must
undergo several economic analyses.
First, Executive Order 12866 and
Executive Order 13563 direct that each
Federal agency shall propose or adopt a
regulation only upon a reasoned
determination that the benefits of the
intended regulation justify its costs.
Second, the Regulatory Flexibility Act
of 1980 (Pub. L. 96–354) requires
agencies to analyze the economic
impact of regulatory changes on small
entities. Third, the Trade Agreements
Act (Pub. L. 96–39) prohibits agencies
from setting standards that create
unnecessary obstacles to the foreign
commerce of the United States. In
developing U.S. standards, the Trade
Act requires agencies to consider
international standards and, where
appropriate, that they be the basis of
U.S. standards. Fourth, the Unfunded
Mandates Reform Act of 1995 (Pub. L.
104–4) requires agencies to prepare a
written assessment of the costs, benefits,
and other effects of proposed or final
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rules that include a Federal mandate
likely to result in the expenditure by
State, local, or tribal governments, in the
aggregate, or by the private sector, of
$100 million or more annually (adjusted
for inflation with base year of 1995).
This portion of the preamble
summarizes the FAA’s analysis of the
economic impacts of this final rule.
Department of Transportation Order
DOT 2100.5 prescribes policies and
procedures for simplification, analysis,
and review of regulations. If the
expected cost impact is so minimal that
a proposed or final rule does not
warrant a full evaluation, this order
permits that a statement to that effect
and the basis for it be included in the
preamble if a full regulatory evaluation
of the cost and benefits is not prepared.
Such a determination has been made for
this final rule. The reasoning for this
determination follows:
In conducting these analyses, the FAA
has determined that this final rule:
(1) Imposes minimal incremental
costs and provides benefits,
(2) Is not an economically ‘‘significant
regulatory action’’ as defined in section
3(f) of Executive Order 12866,
(3) Is not significant as defined in
DOT’s Regulatory Policies and
Procedures;
(4) Will not have a significant
economic impact on a substantial
number of small entities;
(5) Will not have a significant effect
on international trade; and
(6) Will not impose an unfunded
mandate on state, local, or tribal
governments, or on the private sector by
exceeding the monetary threshold
identified.
These analyses are summarized below.
This final rule modifies the Detroit,
MI, Class B airspace to contain aircraft
conducting published instrument
procedures at Detroit Metropolitan
Wayne County (DTW), Detroit, MI,
within Class B airspace. The FAA is
taking this action to support all three
existing Simultaneous Instrument
Landing System (SILS) configurations
today; runways 22/21, runways 4/3 and
runways 27L/27R, as well as to support
containment for triple SILS operations
planned for the very near future for
runways 4L/4R/3R and runways 21L/
22L/22R.
The benefits of this rule are enhanced
safety, improved flow of air traffic, and
reduced potential for midair collisions
in the DTW terminal area. In addition,
this rule supports the FAA’s national
airspace redesign goal of optimizing
terminal and enroute airspace areas to
reduce aircraft delays and improve
system capacity.
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As described in the NPRM, the costs
of this final rule will include the costs
of general aviation aircraft that might
have to fly further. However, the FAA
believes that any such costs will be
minimal because the FAA designed the
airspace to minimize the effect on
aviation users who would not fly in the
Class B airspace. In addition the FAA
held a series of meetings to solicit
comments from people who thought
that they might be affected by the
proposal. Wherever possible the FAA
included the comments from those
meetings in this final rule.
The FAA received no comments on
the FAA’s request for comments on the
minimal cost determination. Therefore,
the FAA has determined that this final
rule is not a ‘‘significant regulatory
action’’ as defined in section 3(f) of
Executive Order 12866, and is not
‘‘significant’’ as defined in DOT’s
Regulatory Policies and Procedures.
Regulatory Flexibility Determination
The Regulatory Flexibility Act of 1980
(Pub. L. 96–354) (RFA) establishes ‘‘as a
principle of regulatory issuance that
agencies shall endeavor, consistent with
the objective of the rule and of
applicable statutes, to fit regulatory and
informational requirements to the scale
of the business, organizations, and
governmental jurisdictions subject to
regulation.’’ To achieve that principle,
the RFA requires agencies to solicit and
consider flexible regulatory proposals
and to explain the rationale for their
actions to assure that such proposals are
given serious consideration. The RFA
covers a wide-range of small entities,
including small businesses, not-forprofit organizations and small
governmental jurisdictions.
Agencies must perform a review to
determine whether a proposed or final
rule will have a significant economic
impact on a substantial number of small
entities. If the agency determines that it
will, the agency must prepare a
regulatory flexibility analysis as
described in the Act.
However, if an agency determines that
a proposed or final rule is not expected
to have a significant economic impact
on a substantial number of small
entities, section 605(b) of the 1980 RFA
provides that the head of the agency
may so certify and a regulatory
flexibility analysis is not required. The
certification must include a statement
providing the factual basis for this
determination, and the reasoning should
be clear.
In the Initial Regulatory Flexibility
Analysis the FAA determined that the
proposed rule was expected to improve
safety by redefining Class B airspace
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boundaries and was expected to impose
only minimal costs on small entities.
The FAA requested comments on this
determination.
The FAA received no comments on
small entity considerations.
Therefore, the FAA Administrator
certifies that this final rule will not have
a significant economic impact on a
substantial number of small entities.
International Trade Impact Assessment
The Trade Agreements Act of 1979
(Pub. L. 96–39), as amended by the
Uruguay Round Agreements Act (Pub.
L. 103–465), prohibits Federal agencies
from establishing standards or engaging
in related activities that create
unnecessary obstacles to the foreign
commerce of the United States.
Pursuant to these Acts, the
establishment of standards is not
considered an unnecessary obstacle to
the foreign commerce of the United
States, so long as the standard has a
legitimate domestic objective, such as
the protection of safety, and does not
operate in a manner that excludes
imports that meet this objective. The
statute also requires consideration of
international standards and, where
appropriate, that they be the basis for
U.S. standards.
The FAA assessed the potential effect
of this proposed rule in the NPRM and
determined that it would encourage
international cooperation between the
United States and Canada and increase
safety in both the United States and
Canada because the proposal affects
airspace in both these countries. The
FAA received no comments on this
determination.
Therefore, the FAA has determined
that this final rule will encourage
international cooperation and increase
safety between the United States and
Canada.
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Unfunded Mandates Assessment
Title II of the Unfunded Mandates
Reform Act of 1995 (Pub. L. 104–4)
requires each Federal agency to prepare
a written statement assessing the effects
of any Federal mandate in a proposed or
final agency rule that may result in an
expenditure of $100 million or more
(adjusted annually for inflation) in any
one year by State, local, and tribal
governments, in the aggregate, or by the
private sector; such a mandate is
deemed to be a ‘‘significant regulatory
action.’’ The FAA currently uses an
inflation-adjusted value of $143.1
million in lieu of $100 million. This
final rule does not contain such a
mandate; therefore the requirements of
Title II do not apply.
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List of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference,
Navigation (air).
Adoption of the Amendment
In consideration of the foregoing, the
Federal Aviation Administration
amends 14 CFR part 71 as follows:
PART 71—DESIGNATION OF CLASS A,
B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND
REPORTING POINTS
1. The authority citation for part 71
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40103, 40113,
40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959–
1963 Comp., p. 389.
§ 71.1
[Amended]
2. The incorporation by reference in
14 CFR 71.1 of the Federal Aviation
Administration Order 7400.9X, Airspace
Designations and Reporting Points,
dated August 7, 2013, and effective
September 15, 2013, is amended as
follows:
■
Paragraph 3000
Airspace
Subpart B—Class B
*
*
*
*
*
AGL MI B Detroit, MI
Detroit Metropolitan Wayne County Airport,
MI (Primary Airport)
(Lat. 42°12′45″ N., long. 83°21′12″ W.)
Detroit, Willow Run Airport, MI
(Lat. 42°14′21″ N., long. 83°31′51″ W.)
Ann Arbor Municipal Airport, MI
(Lat. 42°13′23″ N., long. 83°44′44″ W.)
Coleman A. Young Municipal Airport, MI
(Lat. 42°24′33″ N., long. 83°00′36″ W.)
Detroit (DXO) VOR/DME
(Lat. 42°12′47″ N., long. 83°22′00″ W.)
Salem (SVM) VORTAC
(Lat. 42°24′32″ N., long. 83°35′39″ W.)
Area A. That airspace extending upward
from the surface to and including 10,000 feet
MSL within an area bounded by a line
beginning at lat. 42°17′18″ N., long. 83°27′27″
W. on the 4.4-mile radius of the Detroit
Willow Run Airport; thence northeast to lat.
42°20′47″ N., long. 83°22′12″ W. on the 8mile arc of the DXO VOR/DME; thence
clockwise along the 8-mile arc of the DXO
VOR/DME to intercept the 4.4-mile radius of
the Detroit Willow Run Airport at lat.
42°09′57″ N., long. 83°32′04″ W.; thence
counterclockwise along the 4.4-mile radius of
the Detroit Willow Run Airport to lat.
42°12′08″ N., long. 83°26′44″ W.; thence
north to lat. 42°15′17″ N., long. 83°26′04″ W.
on the 4.4-mile radius of the Detroit Willow
Run Airport; thence counterclockwise along
the 4.4-mile radius of the Detroit Willow Run
Airport to the point of beginning.
Area B. That airspace extending upward
from 2,500 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the DXO
VOR/DME 354° radial and the Detroit Willow
Run Airport 047° bearing; thence north along
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the DXO VOR/DME 354° radial to intercept
the 10-mile arc of the DXO VOR/DME; thence
clockwise along the 10-mile arc of the DXO
VOR/DME to intercept the DXO VOR/DME
234° radial; thence northeast along the DXO
VOR/DME 234° radial to intercept the 8-mile
arc of the DXO VOR/DME; thence
counterclockwise along the 8-mile arc of the
DXO VOR/DME arc to lat. 42°20′47″ N., long.
83°22′12″ W.; thence southwest to the point
of beginning.
Area C. That airspace extending upward
from 3,000 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the 5-mile arc
of the SVM VORTAC and the 15-mile arc of
the DXO VOR/DME at lat. 42°26′42″ N., long.
83°29′34″ W.; thence clockwise along the 15mile arc of the DXO VOR/DME to intercept
the DXO VOR/DME 063° radial; thence
northeast along the DXO VOR/DME 063°
radial to intercept the 4.1-mile radius of the
Coleman A. Young Municipal Airport at lat.
42°20′30″ N., long. 83°01′31″ W.; thence
counterclockwise along the 4.1-mile radius of
the Coleman A. Young Municipal Airport to
intercept the 20-mile arc of the DXO VOR/
DME at lat. 42°21′09″ N., long. 82°57′31″ W.;
thence clockwise along the DXO 20-mile arc
to intercept the DXO VOR/DME 234° radial;
thence northeast along the DXO 234° radial
to intercept the 15-mile arc of the DXO VOR/
DME; thence clockwise along the 15-mile arc
of the DXO VOR/DME to intercept the 4.4mile radius of the Ann Arbor Municipal
Airport at lat. 42°09′36″ N., long. 83°41′43″
W.; thence counterclockwise along the 4.4mile radius of the Ann Arbor Municipal
Airport to intercept the SVM VORTAC 214°
radial at lat. 42°17′21″ N., long. 83°42′10″ W.;
thence northeast along the SVM VORTAC
214° radial to intercept the 5-mile arc of the
SVM VORTAC at lat. 42°20′23″ N., long.
83°39′25″ W.; thence counterclockwise along
the 5-mile arc of the SVM VORTAC to the
point of beginning, excluding Areas A and B.
Area D. That airspace extending upward
from 3,500 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the SVM
VORTAC 214° radial and the 20-mile arc of
the DXO VOR/DME; thence counterclockwise
along the 20-mile arc of the DXO VOR/DME
to intercept the DXO VOR/DME 234° radial;
thence northeast along the DXO VOR/DME
234° radial to intercept the 15-mile arc of the
DXO VOR/DME at lat. 42°03′57″ N., long.
83°38′18″ W.; thence clockwise along the 15mile arc of the DXO VOR/DME to intercept
the 4.4-mile radius of the Ann Arbor
Municipal Airport at lat. 42°09′36″ N., long.
83°41′43″ W.; thence counterclockwise along
the 4.4-mile radius of the Ann Arbor
Municipal Airport to intercept the SVM
VORTAC 214° radial at lat. 42°17′21″ N.,
long. 83°42′10″ W.; thence southwest along
the SVM VORTAC 214° radial to the point of
beginning.
Area E. That airspace extending upward
from 3,500 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the 5-mile arc
of the SVM VORTAC and the 15-mile arc of
the DXO VOR/DME at lat. 42°26′42″ N., long.
83°29′34″ W.; thence clockwise along the 15mile arc of the DXO VOR/DME to intercept
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the DXO VOR/DME 063° radial; thence
northeast along the DXO VOR/DME 063°
radial to intercept the 4.1-mile radius of the
Coleman A. Young Municipal Airport at lat.
42°20′30″ N., long. 83°01′31″ W.; thence
counterclockwise along the 4.1-mile radius of
the Coleman A. Young Municipal Airport to
intercept the 20-mile arc of the DXO VOR/
DME at lat. 42°21′09″ N., long. 82°57′31″ W.;
thence counterclockwise along the 20-mile
arc of the DXO VOR/DME to intercept the
SVM VORTAC 044° radial; thence southwest
along the SVM VORTAC 044° radial to
intercept the 5-mile arc of the SVM VORTAC
at lat. 42°28′08″ N., long. 83°30′58″ W.;
thence clockwise along the 5-mile arc of the
SVM VORTAC to the point of beginning.
Area F. That airspace extending upward
from 4,000 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the SVM
VORTAC 044° radial and the 25-mile arc of
the DXO VOR/DME; thence clockwise along
the 25-mile arc of the DXO VOR/DME to lat.
41°48′32″ N., long. 83°13′49″ W.; thence west
to intercept the 25-mile arc of the DXO VOR/
DME at lat. 41°48′11″ N., long. 83°28′00″ W.;
thence clockwise along the 25-mile arc of the
DXO VOR/DME to intercept the SVM
VORTAC 214° radial; thence northeast along
the SVM VORTAC 214° radial to intercept
the 20-mile arc of the DXO VOR/DME at lat.
42°10′10″ N., long. 83°48′40″ W.; thence
counterclockwise along the 20-mile arc of the
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DXO VOR/DME to intercept the SVM
VORTAC 044° radial; thence northeast along
the SVM VORTAC 044° radial to the point of
beginning.
Area G. That airspace extending upward
from 6,000 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at the intersection of the SVM
VORTAC 214° radial and the 25-mile arc of
the DXO VOR/DME at lat. 42°04′33″ N., long.
83°53′44″ W.; thence counterclockwise along
the 25-mile arc of the DXO VOR/DME to lat.
41°48′11″ N., long. 83°28′00″ W.; thence west
to intercept the 30-mile arc of the DXO VOR/
DME at lat. 41°47′43″ N., long. 83°44′08″ W.;
thence clockwise along the 30-mile arc of the
DXO VOR/DME to lat. 41°51′00″ N., long.
83°49′42″ W.; thence north to the point of
beginning.
Area H. That airspace extending upward
from 6,000 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at a point on the DXO VOR/DME
327° radial at 30-miles at lat. 42°37′56″ N.,
long. 83°44′08″ W.; thence clockwise along
the 30-mile arc of the DXO VOR/DME to lat.
41°46′30″ N., long. 83°02′36″ W.; thence
northwest to lat. 41°48′44″ N., long. 83°05′28″
W.; thence west to intercept the 25-mile arc
of the DXO VOR/DME at lat. 41°48′32″ N.,
long. 83°13′49″ W.; thence counterclockwise
along the 25-mile arc of the DXO VOR/DME
until intercepting the SVM VORTAC 044°
radial; thence southwest along the SVM
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3313
VORTAC 044° radial until intercepting the 5mile arc of the SVM VORTAC; thence
clockwise along the 5-mile arc of the SVM
VORTAC to intercept the DXO VOR/DME
327° radial at lat. 42°21′52″ N., long.
83°29′57″ W.; thence northwest along the
DXO VOR/DME 327° radial to the point of
beginning.
Area I. That airspace extending upward
from 9,000 feet MSL to and including 10,000
feet MSL within an area bounded by a line
beginning at lat. 41°47′43″ N., long. 83°44′08″
W. on the 30-mile arc of the DXO VOR/DME;
thence counterclockwise along the 30-mile
arc of the DXO VOR/DME to lat. 41°46′30″
N., long. 83°02′36″ W.; thence northwest to
lat. 41°48′44″ N., long. 83°05′28″ W.; thence
west to the point of beginning.
Note: The Canadian airspace depicted in
Areas C, F, and H above are included in the
legal description for the Detroit Class B to
accommodate charting. This accommodation
reflects airspace established by Transport
Canada to complete the Detroit Class B
airspace area.
Issued in Washington, DC, on January 9,
2014.
Gary A. Norek,
Manager, Airspace Policy and Regulations
Group.
BILLING CODE 4910–13–P
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Federal Register / Vol. 79, No. 13 / Tuesday, January 21, 2014 / Rules and Regulations
Figure 1
Modification of the Detroit, MI Class B Airspace Area
(Docket No.09-AWA-4)
OMTC
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For Information Only - Not For Navigation
Federal Register / Vol. 79, No. 13 / Tuesday, January 21, 2014 / Rules and Regulations
[FR Doc. 2014–00622 Filed 1–17–14; 8:45 am]
BILLING CODE 4910–13–C
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2012–1168; Airspace
Docket No. 07–AWA–3]
RIN 2120–AA66
Modification of the Dallas/Fort Worth
Class B Airspace Area; TX
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action modifies the
Dallas/Fort Worth, TX, Class B airspace
area to ensure containment of large
turbine-powered aircraft flying
instrument procedures to and from the
Dallas/Fort Worth International Airport
(DFW) and Dallas Love Field Airport
(DAL) within Class B airspace. The FAA
is taking this action to further support
its national airspace redesign goal of
optimizing terminal and en route
airspace areas to enhance safety,
improve the flow of air traffic, and
reduce the potential for near midair
collision in the DFW terminal area.
DATES: Effective Date: 0901 UTC, March
6, 2014. The Director of the Federal
Register approves this incorporation by
reference action under 3 CFR part 51,
subject to the annual revision of FAA
Order 7400.9 and publication of
conforming amendments.
FOR FURTHER INFORMATION CONTACT:
Colby Abbott, Airspace Policy and
Regulations Group, AJV–11, Office of
Airspace Services, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
SUMMARY:
tkelley on DSK3SPTVN1PROD with RULES
History
On January 22, 2013, the FAA
published in the Federal Register a
notice of proposed rulemaking (NPRM)
to modify the Dallas/Fort Worth, TX,
Class B airspace area (78 FR 4356). This
action proposed to expand the lateral
and vertical dimensions of the Dallas/
Fort Worth Class B airspace area to
provide additional airspace needed to
contain large turbine-powered aircraft
flying instrument procedures to and
from the Dallas/Fort Worth International
Airport (DFW) and Dallas Love Field
Airport (DAL) within Class B airspace.
The NPRM noted that large turbinepowered aircraft routinely entered,
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exited, and then re-entered Class B
airspace while flying published
instrument approach procedures to
DFW runway13R and DAL runways
13L/13R and 31R/31L, which is contrary
to FAA policy.
Interested parties were invited to
participate in this rulemaking effort by
submitting written comments on the
proposal. A total of 73 responses to the
NPRM were received; of which, 13
responses opposed the proposed action
and did not provide any rationale or
information for consideration. On April
25, 2013, and subsequent to the close of
the public comment period, the FAA
received an inquiry from two
Congressional members requesting that
the FAA withdraw the NPRM and
consider the alternative solution
submitted by a commenter to the NPRM.
This inquiry was added to the docket
(making 74 responses total) and
considered along with the responses
received during the comment period.
The FAA considered all substantive
comments received before making a
determination on the final rule.
Discussion of Comments
Of the 74 responses received to the
NPRM, 61 concerned the airspace in the
vicinity of Addison Airport (ADS). All
of these commenters opposed the
proposed modification to Area F,
contending that it would result in lower
flight paths for DAL arrivals and ADS
arrivals and departures, and lead to
various adverse impacts such as
compression of VFR aircraft, safety of
flight issues, increased noise, air
pollution and health issues, lower
property values, detrimental effect on
local businesses, and decreased
commerce at ADS.
The above perceived impacts appear
to be based on the belief that the Class
B airspace modification would lead to
an increased number of IFR and VFR
flights operating at lower altitudes than
they do today. This is incorrect. The
Class B airspace modifications,
including Area F, are based on the need
to contain existing large turbinepowered IFR aircraft that are now
operating below Class B airspace. It is
important to note that existing DAL IFR
arrival and departure operating
altitudes, flight paths, traffic patterns,
and procedures will not change. As
stated in the NPRM, the Area F
modification will continue to support
IFR and VFR aircraft arriving and
departing ADS as they do today without
compression and ensure large turbinepowered aircraft flying instrument
procedures to DAL runways 13L/13R
are contained within Class B airspace.
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Five commenters argued that the FAA
should not lower the Class B airspace
over the entire Addison Class D airspace
area. They believed it would create an
unsafe condition with arrivals and
departures to from ADS from the north
and east would be forced to operate at
the same, or close to the same altitudes;
create the possibility of unintentional
airspace incursions; and have
operational issues associated with
separation from the existing DAL traffic
patterns at 1,600 feet MSL and 2,000
feet MSL. Additionally, one of the
commenters also argued that lowering
the entire ADS Class D airspace to a
2,500-foot MSL ceiling under the 3,000foot MSL Class B airspace floor would
result in a wedge of uncontrolled
airspace above ADS to the north and
east.
As noted in the NPRM, the FAA
reduced the lateral dimensions of Area
F over the ADS Class D airspace to only
extend from the 10-nautical mile (NM)
arc from the Point of Origin to the 13–
NM arc from the Point of Origin;
matching the outer boundary with the
adjacent Area B outer boundary at 13–
NM arc from the Point of Origin, and
not overlay the entire ADS Class D
airspace. The ADS Class D airspace
beyond the 13–NM arc is unchanged
and the existing 3,000-foot MSL ceiling
is unaffected by this rule. By lowering
only the portion of Class B airspace
necessary to contain aircraft flying
instrument procedures to DAL within
Class B airspace [Area F] and retaining
the existing arrival/departure traffic
flows, altitudes, and procedures, the
concerns that the ADS arrival/departure
aircraft from the north and east would
be operating at the same altitudes are
addressed. ADS arrival and departure
aircraft will be unaffected and are not
expected to create any unintentional
Class B incursions or impact the two
existing ADS traffic patterns. Finally,
the ADS Class D airspace beyond the
13–NM arc of the Point of Origin will
remain unchanged by this airspace
action.
Thirty commenters stated that VFR
flights operating at ADS would be
compressed as a result of establishing
Area F with a 2,500 feet MSL floor over
a portion of the ADS Class D airspace.
They further argue that this
compression into less airspace at ADS,
below Area F, could result in the loss of
operational flexibility and options for
VFR aircraft to vary from air traffic
control (ATC) recommended arrival and
departure altitudes; the introduction of
new flight safety hazards to VFR pilots
forced to fly 500 feet lower; a greater
potential for midair collision; and
inadvertent incursions into Class B
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Agencies
[Federal Register Volume 79, Number 13 (Tuesday, January 21, 2014)]
[Rules and Regulations]
[Pages 3305-3315]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-00622]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA-2012-0661; Airspace Docket No. 09-AWA-4]
RIN 2120-AA66
Amendment to Class B Airspace; Detroit, MI
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: This action modifies the Detroit, MI, Class B airspace area to
contain aircraft conducting published instrument procedures at Detroit
Metropolitan Wayne County Airport (DTW), Detroit, MI, within Class B
airspace. The FAA is taking this action to support containment of
aircraft operations using the three existing dual Simultaneous
Independent Instrument Landing System (SIILS) configurations, runways
22R/21L, runways 4L/3R and runways 27L/27R, as well as support
containment of aircraft operations for triple SIILS operations to
runways 4L/4R/3R and runways 21L/22L/22R. This action will enhance
safety, improve the flow of air traffic, and reduce the potential for
midair collisions in the DTW terminal area, while accommodating the
concerns of all airspace users. Furthermore, this effort supports the
FAA's national airspace redesign goal of optimizing terminal and
enroute airspace areas to reduce aircraft delays and improve system
capacity.
DATES: Effective Date: 0901 UTC, April 3, 2014. The Director of the
Federal Register approves this incorporation by reference action under
3 CFR part 51, subject to the annual revision of FAA Order 7400.9 and
publication of conforming amendments.
FOR FURTHER INFORMATION CONTACT: Colby Abbott, Airspace Policy and
Regulations Group, Office of Airspace Services, Federal Aviation
Administration, 800 Independence Avenue SW., Washington, DC 20591;
telephone: (202) 267-8783.
SUPPLEMENTARY INFORMATION:
History
On August 14, 2012, the FAA published in the Federal Register a
notice of proposed rulemaking (NPRM) to modify the Detroit Class B
airspace area (77 FR 48476). This action proposed to expand the lateral
and vertical limits of the Detroit Class B airspace area to provide
additional airspace needed to contain dual SIILS procedures and
associated traffic patterns supporting runways 22R/21L, runways 4L/3R,
and runways 27L/27R
[[Page 3306]]
simultaneous operations within Class B airspace. The action also
supports airspace requirements necessary for planned triple SIILS
procedures and associated traffic patterns to runways 4L/4R/3R and
runways 21L/22L/22R operations within Class B airspace.
In addition, the FAA published in the Federal Register a document
correcting the 5-mile arc of the DXO VOR/DME boundary reference
information published in the Areas C, D, and E regulatory text
descriptions to the 15-mile arc of the DXO VOR/DME (77 FR 53159, August
31, 2012). Interested parties were invited to participate in this
rulemaking effort by submitting written comments on the proposed
action. Twenty-three written comments were received in response to the
notice. The FAA considered all substantive comments received before
making a determination on this final rule.
Discussion of Comments
One commenter suggested that the meetings associated with Detroit
Class B airspace modification were held in secret, and without notice
to the general public. The commenter stated the groups that attended
were specifically invited and were not representing the interests of
the flight schools in the area impacted by the proposed changes.
The FAA considers the comment to be specific to the Ad Hoc
Committee process the FAA follows during the initial airspace design
phase prior to the initiation of rulemaking. To ensure local user needs
and suggestions are considered during the initial airspace design
phase, an Ad Hoc Committee is formed. The Ad Hoc Committee's purpose is
to obtain suggestions from a cross section of users and aviation
organizations that could be affected by a proposed airspace change
before the FAA develops a proposed airspace design. The committee
makeup and size is determined by the local situation or requirements
and includes representatives of local users and aviation organizations.
As noted in the NPRM in the Discussion of Ad Hoc Committee
Recommendations and Comments section, the interests of the flight
schools were represented by the Ad Hoc Committee. The committee made
recommendations to the FAA addressing the western boundary remaining
basically unchanged in support of outlaying airports, glider
activities, and parachute operations; an ATC advisory service to VFR
pilots in areas of intensive flight training; and boundary changes to
maintain the ability to fly practice approaches at airports without the
need for Class B airspace services.
Additionally, the FAA hosted three informal airspace meetings for
the general public on July 20, 21, and 22, 2010, that were intended to
inform the general public, affected airspace users, and aviation
organizations of the proposed airspace changes and to gather facts and
information relevant to the planned regulatory action. The FAA
published notice of the meetings in the Federal Register (May 13, 2010;
75 FR 11496) and mailed 14,852 informal airspace meeting notification
letters to all registered pilots that resided within 100 miles of DTW.
As a result, the FAA received comments from 29 individuals.
Five commenters addressed public involvement in the regulatory
process proposing to modify the DTW Class B airspace. One commenter
praised the FAA's decision to limit western expansion of the DTW Class
B airspace contained in the proposal following industry and community
input. Conversely, four other commenters believed the FAA largely
ignored the concerns and recommendations of the Ad Hoc Committee and
public in developing the proposed DTW Class B airspace modification. In
general, they argued that the FAA was going through the motions of
gathering public comments, but had no intention of modifying the
proposal to address the concerns raised by the committee and the
public.
The purpose of modifying the DTW Class B airspace is to contain
large turbine-powered aircraft conducting instrument procedures within
Class B airspace once they entered it, enhance flight safety by
segregating large turbine-powered aircraft and non-participating VFR
aircraft flying in the vicinity of the DTW Class B airspace area, and
contain the instrument procedures and associated traffic flows and
patterns supporting those procedures at DTW within Class B airspace.
The DTW Class B airspace design was influenced by Ad Hoc Committee and
public comments and recommendations received throughout the airspace
regulatory process addressing VFR aircraft training areas and
activities west of DTW; protection of an uncharted VFR flyway over the
Detroit River; the glider, parachute, and ultra-light activities
located around DTW; the geographic location and proximity of satellite
airports around DTW; and potential impacts to non-participant VFR
aircraft transiting the DTW terminal area.
In direct response to comments and recommendations received, the
FAA made numerous adjustments to the Class B airspace area proposal.
This included reducing the western boundary and associated Class B
airspace shelves, adjusting multiple Class B airspace sub-area
boundaries and floor altitudes, retaining an uncharted VFR flyway, and
aligning airspace boundaries with easily identifiable geographic
landmarks.
The FAA removed the airspace area west of DTW from the Class B
airspace proposal, from the DXO 333 radial counterclockwise to the SVM
217 radial west of Ann Arbor and Willow Run airports, and terminated
the Class B airspace shelf located 25 nautical miles (NM) to 30 NM
southwest of DTW and east of Meyers-Divers Airport (3TE). The reduced
western boundary provides the minimum amount of Class B airspace
necessary to contain large turbine-powered aircraft flying the
instrument procedures and associated traffic patterns to/from DTW
within Class B airspace while minimizing impact to VFR aircraft flying
in existing training areas, parachute and glider activities, and
airport operations all located west of DTW.
After originally planning to lower Class B airspace north of DTW in
the vicinity of the highways from 4,000 feet MSL to 3,000 feet MSL, the
FAA raised the proposed shelf to a minimum of 3,500 feet MSL along the
entire length of Interstate 696 (I-696). That change specifically
responded to concerns about a reduced volume of airspace being squeezed
between the Class B airspace floor, the obstructions along I-696, and
aircraft flying in and out of Oakland-Troy Airport (VLL) depicted in
the original design.
With respect to recommendations for a single Class B airspace floor
overlying Class D airspace areas, the FAA minimized the proposed Class
B airspace to the extent practical to ensure containment of large
turbine-powered aircraft flying instrument procedures within Class B
airspace. The FAA does not agree with establishing a single Class B
airspace floor over the two airports affected by this recommendation
(Ann Arbor Municipal Airport (ARB) and Coleman A. Young Municipal
Airport (DET)) because this would be excessive to what is required and
unnecessarily include navigable airspace that would otherwise be
available to non-participating VFR aircraft.
Based on recommendations not to lower the 3,000-foot MSL Class B
airspace floor above an uncharted VFR flyway over the Detroit River,
the FAA moved the proposed 2,500-foot MSL Class B airspace shelf
boundary closer to DTW to a 10 NM arc of the DXO VOR/DME and reduced
the proposed
[[Page 3307]]
Class B airspace surface area boundary to an 8 NM arc of the DXO VOR/
DME. These adjustments ensure that the existing uncharted VFR flyway
will be unaffected, allow easier access at the southern end of the
Detroit River, and enable practice approaches at Grosse Ile Municipal
Airport (ONZ) without needing a Class B airspace clearance.
The FAA also used landmarks to assist VFR pilots in non-GPS
equipped aircraft with easily determining their position relative Class
B airspace boundaries. As recommended by the Ad Hoc Committee and
airspace users, this rule adopts boundary modifications that align with
Interstate highways I-696 and I-94, the Ford World Headquarters
building, and the Detroit River and Lake Erie shoreline. Additionally,
the FAA retained numerous landmarks depicted on the Detroit VFR
Terminal Area Chart to assist VFR pilots.
Fourteen comments addressed the proposed vertical expansion of the
DTW Class B airspace ceiling from 8,000 feet MSL to 10,000 feet MSL.
Four commenters challenged the operational necessity of the Class B
airspace ceiling being raised. Eleven of the commenters argued that
raising the Class B airspace area ceiling to 10,000 feet MSL does not
increase safety.
Raising the ceiling of the DTW Class B airspace area is necessary
to enhance flight safety for all airspace users in the DTW terminal
area. As mentioned in the NPRM, DTW arrivals enter the terminal area at
12,000 feet MSL, enter the traffic patterns abeam DTW descending out of
11,000 feet MSL, and are then vectored by the final controller
beginning at 9,000 feet MSL on the downwind and 8,000 feet MSL on base
leg of the patterns to the final approaches. As a result, a 3,000 foot
gap of airspace exists between the altitude that DTW arrivals are
descending out of to enter the traffic pattern at 11,000 feet MSL and
the Class B ceiling of 8,000 feet. Large turbine-powered aircraft
arriving DTW and non-participating VFR aircraft, not communicating with
Detroit Terminal Radar Approach Control (D21), are operating
simultaneously within this gap of airspace today.
The FAA identified several issues with the 8,000 foot MSL ceiling.
It does not segregate large turbine-powered aircraft arriving/departing
DTW from the conflicting non-participant VFR aircraft flying over the
DTW Class B airspace at 8,500 and 9,500 feet MSL. Additionally, VHF
Omnidirectional Range (VOR) Federal airways V-2, V-10, V-65, V-116, V-
133, V-176, V-188, V-276, V-383, V-410, and V-426 traverse the DTW
terminal area and enable VFR aircraft, not communicating with D21, to
fly over the DTW Class B airspace area and conflict with the DTW
arrival/departure flows operating in the same airspace area. Raising
the ceiling of the DTW Class B airspace will enhance flight safety by
segregating the large turbine-powered aircraft arriving/departing DTW
and the non-participating VFR aircraft overflying DTW.
Raising the DTW Class B airspace ceiling to 10,000 feet MSL also
provides operational and safety advantages by establishing additional
airspace for ATC to more efficiently vector and sequence arrival and
departure aircraft within the Class B airspace, as well as segregate
them from non-participating VFR aircraft that are operating in the same
volume of airspace overhead DTW, as they do today. The raised ceiling
ensures departure aircraft achieve the required 1,000 feet of standard
separation over the top of the downwind arrival traffic flying at 9,000
feet MSL, while remaining 1,000 feet below the traffic pattern aircraft
at 11,000 feet MSL. Currently, aircraft departing DTW and requesting to
climb to 10,000 feet MSL and above are impacted when D21 must vector
the aircraft, at low altitudes, to avoid conflicting non-participant
VFR traffic overflying the DTW Class B airspace area. In some
instances, D21 must stop all departures until the conflicting traffic
is clear. Raising the Class B airspace ceiling to 10,000 feet MSL
requires non-participant VFR over flight traffic, which opt to obtain
Class B airspace services, to communicate with D21. This will enhance
the operational and flight safety benefits for all aircraft operating
above DTW, up to 10,000 feet MSL, by enabling D21 to efficiently
sequence and separate arriving, departing, and non-participant VFR over
flight aircraft simultaneously operating within DTW Class B airspace.
Also, as noted in the NPRM, the eastern portion of the DTW Class B
airspace area extends into Canadian airspace. The equivalent Canadian
airspace to Class B airspace, as designated in the United States, is
Class C airspace. NAV CANADA, the Canadian air service navigation
provider, generally designates Class C airspace with a 12,500 feet MSL
ceiling, however, has advised the FAA of its willingness to establish
corresponding Canadian Class C airspace adjoining the FAA's DTW Class B
airspace with a ceiling of 10,000 feet MSL. Additionally, NAV CANADA
advised it would make the Canadian Class C airspace action effective to
match the effective date of this DTW Class B airspace modification
action.
Six commenters asserted that there was insufficient justification
to expand the Class B airspace area boundary from 20 NM to 30 NM and
that the proposed expansion was based solely on future procedures. One
of the commenters further argued that extending the lateral boundaries
of DTW Class B airspace to 30 NM will greatly affect the VFR flight
areas for airports like Brighton and Livingston County for aircraft
without electrical systems.
Extending the DTW Class B airspace to a 30 NM boundary is designed
to address current and future issues of containing aircraft executing
instrument procedures within the confines of Class B airspace. Today,
large turbine-powered aircraft conducting dual SIILS procedures are
unable to be contained within existing Class B airspace and are
entering, exiting, and reentering DTW Class B airspace while flying the
published instrument approach procedures and associated traffic
patterns. There are approximately 1,770 operations daily at DTW and D21
is experiencing an average of 156 Class B airspace excursions by large
turbine-powered aircraft per day. As a result, large turbine-powered
aircraft and non-participating VFR aircraft flying in the vicinity of
the Class B airspace boundaries, not in communication with D21, are
operating simultaneously in the same volume of airspace.
The existing dual SIILS approaches in use today enable an arrival
capacity of 72 arrivals an hour. The expanded boundary provides the
minimum amount of airspace essential to contain the large turbine-
powered aircraft arriving from multiple arrival streams being sequenced
for and conducting the SIILS procedures. Aircraft flying dual SIILS
procedures are assigned altitudes that differ by at least 1,000 feet
and they are turned on to SIILS approaches so as to ensure they are
established on the localizer signal at or outside mandatory turn on
points. For dual SIILS approach configurations to Runways 21L/22R, the
mandatory turn on point is 18 NM from the runways; for Runways 3R/4L,
the mandatory turn on point is 18 NM from the runways; and for Runways
27L/27R, the mandatory turn on point is 20 NM from the runways. These
are the minimum distances that large turbine-powered aircraft must be
established on the localizer signal for dual SIILS approaches and
facilitate D21 controllers to meet minimum aircraft separation guidance
requirements for simultaneous independent ILS approaches. During
moderate to heavy arrival rushes, the turn on distances extend outward
an additional four to ten NM beyond the minimum turn on
[[Page 3308]]
distances; extending beyond the 20 NM DTW Class B airspace boundary.
Although the existing dual SIILS procedures enable an arrival
capacity of 72 aircraft per hour, DTW demand exceeds that level on a
daily basis. To address this shortcoming of capacity, triple SIILS
approach procedures, which increase DTW is arrival capacity to 112
arrivals per hour, are planned for implementation in spring 2014. As
with dual SIILS procedures, aircraft conducting triple SIILS procedures
will be assigned altitudes differing by at least 1,000 feet and turned
on to the SIILS approaches so they are established on the localizer
signal at or outside mandatory turn on points. For triple SIILS
approaches to a Runways 21L/22L/22R configuration, the mandatory turn
on point is 21 NM from the runways, and for a Runways 3R/4R/4L
configuration, the mandatory turn on point is 20 NM from the runways.
These are the minimum distances aircraft must be established on the
localizer signal for triple SIILS approaches, thereby allowing D21
controllers to meet minimum aircraft separation guidance requirements
for simultaneous independent ILS approaches. And, during moderate to
heavy arrival rushes, the turn on distances will again extend an
additional 4 to 10 NM beyond these minimum turn on distances; extending
beyond the 20 NM DTW Class B airspace boundary.
With respect to the comment that extending the lateral boundaries
to 30 NM will greatly affect the VFR flight areas of airports like
Brighton and Livingston County for aircraft without electrical systems,
both airports fall outside the 30 NM DTW Class B airspace area
boundary. As such, there is no affect or impact expected to the VFR
flight areas of these airports for aircraft with or without electrical
systems. Modifying the Class B airspace boundary to extend to 30 NM is
necessary to enhance flight safety by containing the large turbine-
powered aircraft flying instrument procedures at DTW within Class B
airspace, as well as segregating those aircraft and non-participating
VFR aircraft operating in the vicinity of the DTW Class B airspace area
from one another.
Five commenters addressed the new Class B airspace shelves included
in the proposal and the floor altitudes of those areas. Specifically
the commenters contend that the FAA ignored user feedback and requests
to raise the newly proposed outermost ring of Class B airspace to a
floor of 8,000 feet MSL and commenting that the lower 6,000 foot MSL
floors were unjustified. They further argued that the Class B airspace
shelves proposed southwest of DTW that lowered a portion of an existing
Class B airspace from 4,000 feet MSL to 3,000 feet MSL and established
two new Class B airspace shelves with floors at 4,000 feet MSL and
6,000 feet MSL were unnecessary.
The DTW Class B airspace area boundary, extending to 30 NM north of
DTW clockwise to the southwest of DTW, is necessary for the reasons
stated above. Specific to the comments received about Class B airspace
floor altitudes, the Class B airspace modifications accomplished by
this action establishing new Class B airspace shelves with 3,000-foot
MSL, 4,000-foot MSL, and 6,000-foot MSL floors, which are necessary to
contain the large turbine-powered aircraft being vectored for and
conducting instrument procedures at DTW within Class B airspace.
Additionally, the amended and new Class B airspace floor altitudes are
aligned with the glide slopes of all the ILS approaches to ensure
aircraft flying the instrument procedures are contained within Class B
airspace throughout the entire approach.
Operationally, aircraft conducting dual SIILS approaches to any of
the three existing dual SIILS runway configurations enter the DTW
terminal area at 12,000 feet MSL descending to enter the traffic
pattern at either 6,000 feet MSL, descending further to as low as 4,000
feet MSL on a base leg, or at 7,000 feet MSL abeam DTW on a downwind,
descending further to as low as 4,000 feet MSL on a base leg.
Regardless of traffic flow (north, south, or west), or the direction
from which the aircraft enters the DTW terminal area, all aircraft are
descended to as low as 4,000 feet MSL in preparation for turn on to the
final approach course prior to the mandatory turn on points mentioned
previously. When the planned triple SIILS procedures are implemented to
either of the triple SIILS runway configurations, aircraft assigned the
``middle runway'' will enter the terminal area at 12,000 feet MSL, be
delivered to, and vectored by, the final controller at 9,000 feet MSL
on the downwind and at 8,000 feet MSL on a base leg. The aircraft
assigned the outboard runways will continue to enter the traffic
pattern at 6,000 feet MSL and 7,000 feet MSL abeam DTW on a downwind,
descending to as low as 4,000 feet MSL on base leg, as described above
for dual SIILS procedures.
The DTW Class B airspace area floor altitudes established by this
rule, extending to 30 NM, ensure containment of large turbine-powered
aircraft being vectored for and conducting SIILS approaches to the
three existing dual SIILS configurations today (runways 4L/3R, runways
22R/21L, and runways 27L/27R) within Class B airspace; assure
segregation of large turbine-powered aircraft and non-participating VFR
aircraft from operating simultaneously in the same airspace; and
provide a Class B airspace configuration that ensures future
containment needs when DTW implements triple SIILS procedures to meet
arrival capacity requirements.
Six commenters contended that there are safety concerns associated
with the Class B airspace modifications. Five of the commenters
submitted that the proposed changes would force non-participating VFR
aircraft to fly at lower altitudes to circumnavigate Class B airspace
and would compress this transient VFR traffic into the same airspace
areas that general aviation airports are operating, thereby creating a
dangerous situation due to increased congestion and risk of mid-air
collision. One commenter objected to the proposed changes stating that
the modifications would decrease the usability and safety of Detroit's
airspace.
The primary purpose of a Class B airspace area is to reduce the
potential for midair collisions in the airspace surrounding airports
with high density air traffic operations by providing an area in which
all aircraft are subject to certain operating rules and equipment
requirements. FAA directives require Class B airspace areas be designed
to contain all instrument procedures, and that air traffic controllers
vector aircraft as appropriate to remain within Class B airspace after
entry.
With the DTW Class B airspace configuration established in 1987,
arriving large turbine-powered aircraft routinely enter, exit, and then
re-enter Class B airspace while flying published instrument procedures
today, which is contrary to FAA directives. The procedural requirements
for establishing these aircraft on the final approach courses, to
conduct simultaneous independent approaches to the existing parallel
runways, has resulted in aircraft exceeding the lateral boundaries of
the Class B airspace by up to 10 NM during moderate to heavy arrival
rushes. The DTW Class B airspace modified by this rule enhances flight
safety by containing all instrument approach procedures and associated
traffic patterns within the boundaries of Class B airspace, supporting
increased operations to the current dual and planned triple SIILS
runways, and better segregating the large turbine-powered aircraft
arriving/departing DTW and non-participating VFR aircraft operating in
the vicinity of DTW Class B airspace from one another.
[[Page 3309]]
The FAA acknowledges and recognizes that VFR pilots electing to fly
below the floor of Class B airspace may be compressed. However, the
lower floors are necessary to segregate those aircraft operations from
the large turbine-powered aircraft arriving and departing DTW. The
Detroit terminal area encompasses the world's eleventh (out of fifty)
busiest airport (with over 443,000 airport operations in CY 2011), plus
numerous other airports situated in and around the Detroit terminal
area. These factors create a complex, high density airspace environment
containing a highly diverse mix of aircraft types and aviation
activities. In some areas, large turbine-powered aircraft and non-
participating VFR aircraft are flying simultaneously in the same
airspace. It is essential to segregate the large turbine-powered
aircraft arriving/departing DTW and the non-participating VFR aircraft
that may not be in communication with ATC. Consequently, some non-
participating VFR aircraft may have to fly further, or at different
altitudes, in order to remain clear of the modified DTW Class B
airspace area. Ultimately, it is the pilot's responsibility to evaluate
all factors that could affect a planned flight and determine the safest
course of action whether it is circumnavigating the Class B airspace,
flying over or beneath the Class B airspace, utilizing a charted VFR
flyway, or requesting Class B clearance and services from D21.
Six commenters asserted that the Class B airspace modifications
will place an undue burden on general aviation operators wishing to
conduct VFR training flights. The commenters claimed that the
modifications will have a negative impact on training and further
believed that there will not be sufficient altitudes available to
conduct most maneuvers.
The DTW Class B airspace will not cause any VFR training practice
areas to be lost due to the modified design. The FAA acknowledges that
the floor of the Class B airspace established by this action could
impact the available altitudes in portions of some training areas
located southwest of DTW and a portion of one training area northwest
of DTW, should VFR training aircraft choose not to request Class B
services with D21. However, by adopting a number of recommendation
submitted by the Ad Hoc Committee and during informal airspace
meetings, the FAA adjusted the western boundary of Class B airspace to
alleviate many practice area impacts. The result is that the practice
areas west and north of Ann Arbor would be unaffected.
The Class B airspace established southwest of DTW is required to
contain large turbine-powered aircraft conducting dual SIILS arrival
procedures to Runways 4L/3R, as well as arrivals entering the DTW
terminal airspace via the POLAR1 STAR. It extends over approximately
three quarters of the Eastern Michigan University (EMU) Aviation flight
school's southern practice area with 3,500-foot MSL, 4,000-foot MSL,
and 6,000-foot MSL Class B airspace floors. The EMU southern practice
area is subdivided into four sub-areas with virtually no impact to the
west northwest sub-area and minor impacts to the southern sub-area, but
training activities in the northeast and southeast sub-areas will be
limited to 4,000 feet MSL, unless pilots receive a Class B airspace
clearance. The FAA does not expect a substantive change to the
concentration of VFR training aircraft or training activities conducted
in that practice area or the other practice areas located further
southwest of DTW under the 6,000-foot MSL Class B airspace shelf. The
training activities conducted in those practice areas today could
continue under the DTW Class B airspace or within Class B airspace with
the appropriate Class B airspace clearance.
The VFR practice area near the General Motors Proving Ground,
located north of DTW and southwest of PTK, is partially under a DTW
Class B airspace shelf with a 6,000-foot MSL floor; however, VFR
training flight activities above 6,000 feet MSL are not normally
accomplished there and the 6,000-foot MSL Class B airspace floor will
have negligible impact.
And, as noted in the NPRM, the FAA will continue working with the
local flight training schools to discuss and pursue aircraft training
program activities, scheduling, and airspace alternatives, as required,
independent of this Class B airspace modification action.
Three commenters challenged the DTW Class B airspace modifications
arguing that they increase the waste of fuel, time, and cost to the VFR
traffic that currently uses the airspace areas being established as
Class B airspace. One commenter contends that there would be increases
to the cost of flight training to clear the Class B airspace area
completely, while another commenter allege that the Class B airspace
hampers the effectiveness of the General Aviation (GA) community in the
Detroit Metropolitan area and costs them more to operate in and around
DTW.
The FAA recognizes the Class B airspace modifications could
increase fuel burn for non-participating VFR aircraft. To remain clear
of the DTW Class B airspace area, non-participating VFR pilots who
elect not to contact D21 for Class B services may end up flying at
lower altitude or further distances to circumnavigate the Class B
airspace. However, this action is necessary to separate them from the
large turbine-powered aircraft being contained within the Class B
airspace while flying instrument procedures and associated traffic
flows/patterns. While some GA pilots will opt to fly additional
distance or different altitudes to circumnavigate the Class B airspace,
the FAA believes any increase in fuel burn or cost to be minimal and
justified by the overall increase in flight safety. The DTW Class B
airspace has no impact to the routes or altitudes assigned to IFR and
participating VFR aircraft flying in the Detroit terminal area.
Additionally, the VFR flyways that are charted on the Detroit VFR
Terminal Area Chart remain available for use by GA pilots to transit
north and south or east and west under and around the DTW Class B
airspace area.
As addressed previously, the Class B airspace design incorporated
recommended changes received from the Ad Hoc Committee and informal
airspace meetings to prevent impacts, operationally and economically,
to the non-participating VFR training aircraft flying in the vicinity
of the DTW Class B airspace area.
Fifteen comments were received from the public regarding the fair
and equitable access to the DTW Class B airspace area. Eleven of the
commenters asserted that the Class B airspace design unfairly affects
the activities of the local GA community, limiting their access,
without a demonstrated need. Three commenters stated that D21 routinely
denies Class B airspace entry requests, or ignores the requests
altogether, to highlight the limited access.
The FAA remains committed to providing Class B airspace services to
all National Airspace System (NAS) users operating in the airspace
surrounding DTW in a manner that keeps the Detroit terminal area safe
for all users. As mentioned previously, the primary purpose of a Class
B airspace area is to reduce the potential for midair collisions in the
airspace surrounding airports with high density air traffic operations
by providing an area in which all aircraft are subject to certain
operating rules and equipment requirements.
Class B airspace services are not restricted to only those aircraft
landing
[[Page 3310]]
or departing the primary airports around which the Class B airspace is
established. Various types of aircraft are routinely cleared into and
through DTW Class B airspace when traffic conditions permit doing so
safely. Based on historical data and forecast trends, the D21 average
daily traffic count includes 684 air carrier, 707 air taxi, 364 general
aviation, 15 military IFR operations and 69 VFR operations. When VFR
aircraft request Class B services to transit the DTW Class B airspace,
they are initially told to remain outside the Class B airspace until
radar identification is established; unfortunately and oftentimes, this
is misunderstood as denial of Class B services. In 2012, D21 provided
Class B services to 25,216 VFR aircraft operations. Routinely, D21
provides Class B airspace clearances and services to VFR aircraft
requesting access into and through the DTW Class B airspace when the
arrival/departure traffic volume and airspace capacity conditions
enable doing so safely.
Differences From the NPRM
Editorial corrections have been made to the Detroit Class B
airspace description for clarity and for standardization. Areas A, C,
D, F, and H have editorial corrections whereas, the Detroit Class B
airspace header and all Areas with reference to ``DXO VOR-DME'' have
been corrected to read ``DXO VOR/DME'' for standardization. Also, in
the NPRM description of Area A, a typographical error that listed a
geographic reference as ``lat. 42[deg]5'17'' N., long. 83[deg]26'04''
W.'' on the 4.4-mile radius of the Detroit Willow Run Airport has been
corrected to read ``lat. 42[deg]15'17'' N., long. 83[deg]26'04'' W.''.
With the exception of the above noted changes and minor editorial
corrections, this rule reflects the same Class B airspace area as that
published in the NPRM.
The Rule
The FAA is amending Title 14 of the Code of Federal Regulations (14
CFR) part 71 to modify the Detroit Class B airspace area. This action
(depicted on the chart in Figure 1--Amendment of the Detroit, MI Class
B Airspace Area) lowers the floor of Class B airspace in portions of
the Detroit Class B airspace area; extends Class B airspace out to 30
NM to the north, east (designated Class C airspace in Canada), and
south of DTW; and raises the ceiling of the entire Class B airspace
area from 8,000 feet MSL to 10,000 feet MSL. These modifications
provide the airspace needed to contain large turbine-powered aircraft
conducting instrument procedures within the confines of Class B
airspace, especially when flying existing dual and planned triple SIILS
approaches. Additionally, these airspace modifications will ensure
efficient airspace utilization and enhance safety by better segregating
the large turbine-powered IFR aircraft arriving/departing DTW and the
non-participating VFR aircraft operating in the vicinity of the Detroit
Class B airspace area. The modifications to the Detroit Class B
airspace area are summarized below:
Area A. Area A extends from the ground upward to 10,000 feet MSL,
centered on the Detroit VOR/DME antenna. The surface area is expanded
by relocating the southern boundary approximately 2.5 NM further south
and lowering the Class B airspace floor in that expanded portion of
existing Class B airspace from 2,500 feet MSL to the surface.
Area B. Area B extends upward from 2,500 feet MSL to 10,000 feet
MSL. The Area B extends from north clockwise to the southwest of DTW
between the 8 NM and the 10 NM arcs of the Detroit VOR/DME antenna. The
Class B airspace floor is lowered from 3,000 feet MSL to 2,500 feet MSL
in the expanded portions of existing Class B airspace northeast and
southeast of DTW.
Area C. Area C continues to surround Areas A and B and extends
upward from 3,000 feet MSL to 10,000 feet MSL. The Area C boundary from
east clockwise to the southwest of DTW is expanded to match the 20 NM
arc of the Detroit VOR/DME antenna and from north clockwise to the
northeast of DTW is expanded to match the 15 NM arc of the Detroit VOR/
DME antenna. The Class B airspace floor is lowered from 4,000 feet MSL
to 3,000 feet MSL in the expanded portions of existing Class B airspace
and established at 4,000 feet MSL for the expanded portions that were
previously outside the Detroit Class B airspace area.
Area D. Area D is redefined to extend upward from 3,500 feet MSL to
10,000 feet MSL. Area D overlays the southeastern half of the Ann Arbor
Class D airspace area and extends approximately 7 NM south of the Ann
Arbor Class D airspace area between the 15 NM and 20 NM arcs of the
Detroit VOR/DME antenna. The Class B airspace floor is raised from
3,000 feet MSL to 3,500 feet MSL for a portion of existing Class B
airspace area, lowered from 4,000 feet MSL to 3,500 feet MSL for
another portion of existing Class B airspace area, and established at
3,500 feet MSL for the portion that was previously outside the Detroit
Class B airspace area.
Area E. Area E is a new subarea that extends upward from 3,500 feet
MSL to 10,000 feet MSL. Area E is located north clockwise to northeast
of DTW between the 15 NM and 20 NM arcs of the Detroit VOR/DME antenna.
The Class B airspace floor is lowered from 4,000 feet MSL to 3,500 feet
MSL in the portion of existing Class B airspace and established at
3,500 feet MSL for the portions that were previously outside the
Detroit Class B airspace area.
Area F. Area F is a new subarea that extends upward from 4,000 feet
MSL to 10,000 feet MSL. This area is established from north clockwise
to west southwest of DTW between the 20 NM and 25 NM arcs of the
Detroit VOR/DME antenna. The Class B airspace floor is raised from
3,000 feet MSL to 4,000 feet MSL in the portion of existing Class B
airspace located west of DTW and established at 4,000 feet MSL for the
portion that was previously outside the Detroit Class B airspace area.
Area G. Area G is a new subarea that extends upward from 6,000 feet
MSL to 10,000 feet MSL. This new area is located southwest of DTW
between the 25 NM and 30 NM arcs of the Detroit VOR/DME antenna. This
area abuts Area F and I (described below) and establishes the Class B
airspace floor at 6,000 feet MSL in airspace previously outside of the
Detroit Class B airspace area.
Area H. Area H is also a new subarea that extends upward from 6,000
feet MSL to 10,000 feet MSL. This new area is located from north
northwest clockwise to southeast of DTW and abuts Areas C, E, F, and I
(described below) extending to the 25 NM arc of the Detroit VOR/DME
antenna. The Class B airspace floor is established at 6,000 feet MSL in
airspace previously outside of the Detroit Class B airspace area.
Area I. Area I is another new subarea that extends upward from
9,000 feet MSL to 10,000 feet MSL. This new area is established south
of DTW and abuts Areas F, G, and H extending to the 30 NM arc of the
Detroit VOR/DME antenna. The Class B airspace floor is established at
9,000 feet MSL in airspace previously outside the Detroit Class B
airspace area.
Finally, this action updates the DTW airport reference point
coordinates to reflect current NAS data; includes all airports and
navigation aids, with geographic coordinates, used to describe the
Detroit Class B airspace in the Detroit Class B airspace area legal
description header; and describes the Detroit Class B airspace area
centered on the Detroit VOR/DME (DXO) antenna.
All radials listed in the Detroit Class B airspace area description
in this rule are stated in degrees relative to True
[[Page 3311]]
North. All geographic coordinates listed in the Detroit Class B
airspace area description in this rule are stated in degrees, minutes,
and seconds based on North American Datum 83. And, all mileages listed
in the Detroit Class B airspace area description in this rule are
nautical miles.
Class B airspace areas are published in paragraph 3000 of FAA Order
7400.9X, Airspace Designations and Reporting Points, dated August 7,
2013, and effective September 15, 2013, which is incorporated by
reference in 14 CFR section 71.1. The Class B airspace area listed in
this rule will be published subsequently in the Order.
Environmental Review
The FAA has determined that this action qualifies for categorical
exclusion under the National Environmental Policy Act in accordance
with FAA Order 1050.1E, ``Environmental Impacts: Policies and
Procedures,'' paragraph 311a. This airspace action is not expected to
cause any potentially significant environmental impacts, and no
extraordinary circumstances exist that warrant preparation of an
environmental assessment.
Paperwork Reduction Act
The Paperwork Reduction Act of 1995 (44 U.S.C. 3507(d)) requires
that the FAA consider the impact of paperwork and other information
collection burdens imposed on the public. We have determined that there
is no new information collection requirement associated with this rule.
Regulatory Evaluation Summary
Changes to Federal regulations must undergo several economic
analyses. First, Executive Order 12866 and Executive Order 13563 direct
that each Federal agency shall propose or adopt a regulation only upon
a reasoned determination that the benefits of the intended regulation
justify its costs. Second, the Regulatory Flexibility Act of 1980 (Pub.
L. 96-354) requires agencies to analyze the economic impact of
regulatory changes on small entities. Third, the Trade Agreements Act
(Pub. L. 96-39) prohibits agencies from setting standards that create
unnecessary obstacles to the foreign commerce of the United States. In
developing U.S. standards, the Trade Act requires agencies to consider
international standards and, where appropriate, that they be the basis
of U.S. standards. Fourth, the Unfunded Mandates Reform Act of 1995
(Pub. L. 104-4) requires agencies to prepare a written assessment of
the costs, benefits, and other effects of proposed or final rules that
include a Federal mandate likely to result in the expenditure by State,
local, or tribal governments, in the aggregate, or by the private
sector, of $100 million or more annually (adjusted for inflation with
base year of 1995). This portion of the preamble summarizes the FAA's
analysis of the economic impacts of this final rule.
Department of Transportation Order DOT 2100.5 prescribes policies
and procedures for simplification, analysis, and review of regulations.
If the expected cost impact is so minimal that a proposed or final rule
does not warrant a full evaluation, this order permits that a statement
to that effect and the basis for it be included in the preamble if a
full regulatory evaluation of the cost and benefits is not prepared.
Such a determination has been made for this final rule. The reasoning
for this determination follows:
In conducting these analyses, the FAA has determined that this
final rule:
(1) Imposes minimal incremental costs and provides benefits,
(2) Is not an economically ``significant regulatory action'' as
defined in section 3(f) of Executive Order 12866,
(3) Is not significant as defined in DOT's Regulatory Policies and
Procedures;
(4) Will not have a significant economic impact on a substantial
number of small entities;
(5) Will not have a significant effect on international trade; and
(6) Will not impose an unfunded mandate on state, local, or tribal
governments, or on the private sector by exceeding the monetary
threshold identified.
These analyses are summarized below.
This final rule modifies the Detroit, MI, Class B airspace to
contain aircraft conducting published instrument procedures at Detroit
Metropolitan Wayne County (DTW), Detroit, MI, within Class B airspace.
The FAA is taking this action to support all three existing
Simultaneous Instrument Landing System (SILS) configurations today;
runways 22/21, runways 4/3 and runways 27L/27R, as well as to support
containment for triple SILS operations planned for the very near future
for runways 4L/4R/3R and runways 21L/22L/22R.
The benefits of this rule are enhanced safety, improved flow of air
traffic, and reduced potential for midair collisions in the DTW
terminal area. In addition, this rule supports the FAA's national
airspace redesign goal of optimizing terminal and enroute airspace
areas to reduce aircraft delays and improve system capacity.
As described in the NPRM, the costs of this final rule will include
the costs of general aviation aircraft that might have to fly further.
However, the FAA believes that any such costs will be minimal because
the FAA designed the airspace to minimize the effect on aviation users
who would not fly in the Class B airspace. In addition the FAA held a
series of meetings to solicit comments from people who thought that
they might be affected by the proposal. Wherever possible the FAA
included the comments from those meetings in this final rule.
The FAA received no comments on the FAA's request for comments on
the minimal cost determination. Therefore, the FAA has determined that
this final rule is not a ``significant regulatory action'' as defined
in section 3(f) of Executive Order 12866, and is not ``significant'' as
defined in DOT's Regulatory Policies and Procedures.
Regulatory Flexibility Determination
The Regulatory Flexibility Act of 1980 (Pub. L. 96-354) (RFA)
establishes ``as a principle of regulatory issuance that agencies shall
endeavor, consistent with the objective of the rule and of applicable
statutes, to fit regulatory and informational requirements to the scale
of the business, organizations, and governmental jurisdictions subject
to regulation.'' To achieve that principle, the RFA requires agencies
to solicit and consider flexible regulatory proposals and to explain
the rationale for their actions to assure that such proposals are given
serious consideration. The RFA covers a wide-range of small entities,
including small businesses, not-for-profit organizations and small
governmental jurisdictions.
Agencies must perform a review to determine whether a proposed or
final rule will have a significant economic impact on a substantial
number of small entities. If the agency determines that it will, the
agency must prepare a regulatory flexibility analysis as described in
the Act.
However, if an agency determines that a proposed or final rule is
not expected to have a significant economic impact on a substantial
number of small entities, section 605(b) of the 1980 RFA provides that
the head of the agency may so certify and a regulatory flexibility
analysis is not required. The certification must include a statement
providing the factual basis for this determination, and the reasoning
should be clear.
In the Initial Regulatory Flexibility Analysis the FAA determined
that the proposed rule was expected to improve safety by redefining
Class B airspace
[[Page 3312]]
boundaries and was expected to impose only minimal costs on small
entities. The FAA requested comments on this determination.
The FAA received no comments on small entity considerations.
Therefore, the FAA Administrator certifies that this final rule
will not have a significant economic impact on a substantial number of
small entities.
International Trade Impact Assessment
The Trade Agreements Act of 1979 (Pub. L. 96-39), as amended by the
Uruguay Round Agreements Act (Pub. L. 103-465), prohibits Federal
agencies from establishing standards or engaging in related activities
that create unnecessary obstacles to the foreign commerce of the United
States. Pursuant to these Acts, the establishment of standards is not
considered an unnecessary obstacle to the foreign commerce of the
United States, so long as the standard has a legitimate domestic
objective, such as the protection of safety, and does not operate in a
manner that excludes imports that meet this objective. The statute also
requires consideration of international standards and, where
appropriate, that they be the basis for U.S. standards.
The FAA assessed the potential effect of this proposed rule in the
NPRM and determined that it would encourage international cooperation
between the United States and Canada and increase safety in both the
United States and Canada because the proposal affects airspace in both
these countries. The FAA received no comments on this determination.
Therefore, the FAA has determined that this final rule will
encourage international cooperation and increase safety between the
United States and Canada.
Unfunded Mandates Assessment
Title II of the Unfunded Mandates Reform Act of 1995 (Pub. L. 104-
4) requires each Federal agency to prepare a written statement
assessing the effects of any Federal mandate in a proposed or final
agency rule that may result in an expenditure of $100 million or more
(adjusted annually for inflation) in any one year by State, local, and
tribal governments, in the aggregate, or by the private sector; such a
mandate is deemed to be a ``significant regulatory action.'' The FAA
currently uses an inflation-adjusted value of $143.1 million in lieu of
$100 million. This final rule does not contain such a mandate;
therefore the requirements of Title II do not apply.
List of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference, Navigation (air).
Adoption of the Amendment
In consideration of the foregoing, the Federal Aviation
Administration amends 14 CFR part 71 as follows:
PART 71--DESIGNATION OF CLASS A, B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND REPORTING POINTS
0
1. The authority citation for part 71 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40103, 40113, 40120; E.O. 10854, 24
FR 9565, 3 CFR, 1959-1963 Comp., p. 389.
Sec. 71.1 [Amended]
0
2. The incorporation by reference in 14 CFR 71.1 of the Federal
Aviation Administration Order 7400.9X, Airspace Designations and
Reporting Points, dated August 7, 2013, and effective September 15,
2013, is amended as follows:
Paragraph 3000 Subpart B--Class B Airspace
* * * * *
AGL MI B Detroit, MI
Detroit Metropolitan Wayne County Airport, MI (Primary Airport)
(Lat. 42[deg]12'45'' N., long. 83[deg]21'12'' W.)
Detroit, Willow Run Airport, MI
(Lat. 42[deg]14'21'' N., long. 83[deg]31'51'' W.)
Ann Arbor Municipal Airport, MI
(Lat. 42[deg]13'23'' N., long. 83[deg]44'44'' W.)
Coleman A. Young Municipal Airport, MI
(Lat. 42[deg]24'33'' N., long. 83[deg]00'36'' W.)
Detroit (DXO) VOR/DME
(Lat. 42[deg]12'47'' N., long. 83[deg]22'00'' W.)
Salem (SVM) VORTAC
(Lat. 42[deg]24'32'' N., long. 83[deg]35'39'' W.)
Area A. That airspace extending upward from the surface to and
including 10,000 feet MSL within an area bounded by a line beginning
at lat. 42[deg]17'18'' N., long. 83[deg]27'27'' W. on the 4.4-mile
radius of the Detroit Willow Run Airport; thence northeast to lat.
42[deg]20'47'' N., long. 83[deg]22'12'' W. on the 8-mile arc of the
DXO VOR/DME; thence clockwise along the 8-mile arc of the DXO VOR/
DME to intercept the 4.4-mile radius of the Detroit Willow Run
Airport at lat. 42[deg]09'57'' N., long. 83[deg]32'04'' W.; thence
counterclockwise along the 4.4-mile radius of the Detroit Willow Run
Airport to lat. 42[deg]12'08'' N., long. 83[deg]26'44'' W.; thence
north to lat. 42[deg]15'17'' N., long. 83[deg]26'04'' W. on the 4.4-
mile radius of the Detroit Willow Run Airport; thence
counterclockwise along the 4.4-mile radius of the Detroit Willow Run
Airport to the point of beginning.
Area B. That airspace extending upward from 2,500 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the DXO VOR/DME 354[deg] radial and
the Detroit Willow Run Airport 047[deg] bearing; thence north along
the DXO VOR/DME 354[deg] radial to intercept the 10-mile arc of the
DXO VOR/DME; thence clockwise along the 10-mile arc of the DXO VOR/
DME to intercept the DXO VOR/DME 234[deg] radial; thence northeast
along the DXO VOR/DME 234[deg] radial to intercept the 8-mile arc of
the DXO VOR/DME; thence counterclockwise along the 8-mile arc of the
DXO VOR/DME arc to lat. 42[deg]20'47'' N., long. 83[deg]22'12'' W.;
thence southwest to the point of beginning.
Area C. That airspace extending upward from 3,000 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the 5-mile arc of the SVM VORTAC
and the 15-mile arc of the DXO VOR/DME at lat. 42[deg]26'42'' N.,
long. 83[deg]29'34'' W.; thence clockwise along the 15-mile arc of
the DXO VOR/DME to intercept the DXO VOR/DME 063[deg] radial; thence
northeast along the DXO VOR/DME 063[deg] radial to intercept the
4.1-mile radius of the Coleman A. Young Municipal Airport at lat.
42[deg]20'30'' N., long. 83[deg]01'31'' W.; thence counterclockwise
along the 4.1-mile radius of the Coleman A. Young Municipal Airport
to intercept the 20-mile arc of the DXO VOR/DME at lat.
42[deg]21'09'' N., long. 82[deg]57'31'' W.; thence clockwise along
the DXO 20-mile arc to intercept the DXO VOR/DME 234[deg] radial;
thence northeast along the DXO 234[deg] radial to intercept the 15-
mile arc of the DXO VOR/DME; thence clockwise along the 15-mile arc
of the DXO VOR/DME to intercept the 4.4-mile radius of the Ann Arbor
Municipal Airport at lat. 42[deg]09'36'' N., long. 83[deg]41'43''
W.; thence counterclockwise along the 4.4-mile radius of the Ann
Arbor Municipal Airport to intercept the SVM VORTAC 214[deg] radial
at lat. 42[deg]17'21'' N., long. 83[deg]42'10'' W.; thence northeast
along the SVM VORTAC 214[deg] radial to intercept the 5-mile arc of
the SVM VORTAC at lat. 42[deg]20'23'' N., long. 83[deg]39'25'' W.;
thence counterclockwise along the 5-mile arc of the SVM VORTAC to
the point of beginning, excluding Areas A and B.
Area D. That airspace extending upward from 3,500 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the SVM VORTAC 214[deg] radial and
the 20-mile arc of the DXO VOR/DME; thence counterclockwise along
the 20-mile arc of the DXO VOR/DME to intercept the DXO VOR/DME
234[deg] radial; thence northeast along the DXO VOR/DME 234[deg]
radial to intercept the 15-mile arc of the DXO VOR/DME at lat.
42[deg]03'57'' N., long. 83[deg]38'18'' W.; thence clockwise along
the 15-mile arc of the DXO VOR/DME to intercept the 4.4-mile radius
of the Ann Arbor Municipal Airport at lat. 42[deg]09'36'' N., long.
83[deg]41'43'' W.; thence counterclockwise along the 4.4-mile radius
of the Ann Arbor Municipal Airport to intercept the SVM VORTAC
214[deg] radial at lat. 42[deg]17'21'' N., long. 83[deg]42'10'' W.;
thence southwest along the SVM VORTAC 214[deg] radial to the point
of beginning.
Area E. That airspace extending upward from 3,500 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the 5-mile arc of the SVM VORTAC
and the 15-mile arc of the DXO VOR/DME at lat. 42[deg]26'42'' N.,
long. 83[deg]29'34'' W.; thence clockwise along the 15-mile arc of
the DXO VOR/DME to intercept
[[Page 3313]]
the DXO VOR/DME 063[deg] radial; thence northeast along the DXO VOR/
DME 063[deg] radial to intercept the 4.1-mile radius of the Coleman
A. Young Municipal Airport at lat. 42[deg]20'30'' N., long.
83[deg]01'31'' W.; thence counterclockwise along the 4.1-mile radius
of the Coleman A. Young Municipal Airport to intercept the 20-mile
arc of the DXO VOR/DME at lat. 42[deg]21'09'' N., long.
82[deg]57'31'' W.; thence counterclockwise along the 20-mile arc of
the DXO VOR/DME to intercept the SVM VORTAC 044[deg] radial; thence
southwest along the SVM VORTAC 044[deg] radial to intercept the 5-
mile arc of the SVM VORTAC at lat. 42[deg]28'08'' N., long.
83[deg]30'58'' W.; thence clockwise along the 5-mile arc of the SVM
VORTAC to the point of beginning.
Area F. That airspace extending upward from 4,000 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the SVM VORTAC 044[deg] radial and
the 25-mile arc of the DXO VOR/DME; thence clockwise along the 25-
mile arc of the DXO VOR/DME to lat. 41[deg]48'32'' N., long.
83[deg]13'49'' W.; thence west to intercept the 25-mile arc of the
DXO VOR/DME at lat. 41[deg]48'11'' N., long. 83[deg]28'00'' W.;
thence clockwise along the 25-mile arc of the DXO VOR/DME to
intercept the SVM VORTAC 214[deg] radial; thence northeast along the
SVM VORTAC 214[deg] radial to intercept the 20-mile arc of the DXO
VOR/DME at lat. 42[deg]10'10'' N., long. 83[deg]48'40'' W.; thence
counterclockwise along the 20-mile arc of the DXO VOR/DME to
intercept the SVM VORTAC 044[deg] radial; thence northeast along the
SVM VORTAC 044[deg] radial to the point of beginning.
Area G. That airspace extending upward from 6,000 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at the intersection of the SVM VORTAC 214[deg] radial and
the 25-mile arc of the DXO VOR/DME at lat. 42[deg]04'33'' N., long.
83[deg]53'44'' W.; thence counterclockwise along the 25-mile arc of
the DXO VOR/DME to lat. 41[deg]48'11'' N., long. 83[deg]28'00'' W.;
thence west to intercept the 30-mile arc of the DXO VOR/DME at lat.
41[deg]47'43'' N., long. 83[deg]44'08'' W.; thence clockwise along
the 30-mile arc of the DXO VOR/DME to lat. 41[deg]51'00'' N., long.
83[deg]49'42'' W.; thence north to the point of beginning.
Area H. That airspace extending upward from 6,000 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at a point on the DXO VOR/DME 327[deg] radial at 30-miles
at lat. 42[deg]37'56'' N., long. 83[deg]44'08'' W.; thence clockwise
along the 30-mile arc of the DXO VOR/DME to lat. 41[deg]46'30'' N.,
long. 83[deg]02'36'' W.; thence northwest to lat. 41[deg]48'44'' N.,
long. 83[deg]05'28'' W.; thence west to intercept the 25-mile arc of
the DXO VOR/DME at lat. 41[deg]48'32'' N., long. 83[deg]13'49'' W.;
thence counterclockwise along the 25-mile arc of the DXO VOR/DME
until intercepting the SVM VORTAC 044[deg] radial; thence southwest
along the SVM VORTAC 044[deg] radial until intercepting the 5-mile
arc of the SVM VORTAC; thence clockwise along the 5-mile arc of the
SVM VORTAC to intercept the DXO VOR/DME 327[deg] radial at lat.
42[deg]21'52'' N., long. 83[deg]29'57'' W.; thence northwest along
the DXO VOR/DME 327[deg] radial to the point of beginning.
Area I. That airspace extending upward from 9,000 feet MSL to
and including 10,000 feet MSL within an area bounded by a line
beginning at lat. 41[deg]47'43'' N., long. 83[deg]44'08'' W. on the
30-mile arc of the DXO VOR/DME; thence counterclockwise along the
30-mile arc of the DXO VOR/DME to lat. 41[deg]46'30'' N., long.
83[deg]02'36'' W.; thence northwest to lat. 41[deg]48'44'' N., long.
83[deg]05'28'' W.; thence west to the point of beginning.
Note: The Canadian airspace depicted in Areas C, F, and H above
are included in the legal description for the Detroit Class B to
accommodate charting. This accommodation reflects airspace
established by Transport Canada to complete the Detroit Class B
airspace area.
Issued in Washington, DC, on January 9, 2014.
Gary A. Norek,
Manager, Airspace Policy and Regulations Group.
BILLING CODE 4910-13-P
[[Page 3314]]
[GRAPHIC] [TIFF OMITTED] TR21JA14.000
[[Page 3315]]
[FR Doc. 2014-00622 Filed 1-17-14; 8:45 am]
BILLING CODE 4910-13-C