Rulemaking Advisory Committee; Transport Airplane Performance and Handling Characteristics-New Task, 15112-15114 [2013-05230]
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15112
Federal Register / Vol. 78, No. 46 / Friday, March 8, 2013 / Notices
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Notice of Intent To Rule on Request To
Release Airport Property at the SeattleTacoma International Airport, Seattle,
Washington
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of Request to Release
Airport Property.
mstockstill on DSK4VPTVN1PROD with NOTICES
AGENCY:
SUMMARY: The FAA proposes to rule and
invite public comment on the release of
land at the Seattle-Tacoma International
Airport under the provisions of Section
125 of the Wendell H. Ford Aviation
Investment Reform Act for the 21st
Century (AIR 21), now 49 U.S.C.
47107(h)(2).
DATES: Comments must be received on
or before April 8, 2013.
ADDRESSES: Comments on this
application may be mailed or delivered
to the FAA at the following address: Ms.
Carol Suomi, Manager, Federal Aviation
Administration, Northwest Mountain
Region, Airports Division, Seattle
Airports District Office, 1601 Lind
Avenue SW., Suite 250, Renton,
Washington 98057–3356.
In addition, one copy of any
comments submitted to the FAA must
be mailed or delivered to Mr. Allan
Royal, Port of Seattle Real Estate
Development, at the following address:
Mr. Allan Royal, Port of Seattle Real
Estate Development, P.O. Box 68727,
Seattle, Washington 98168.
FOR FURTHER INFORMATION CONTACT: Mr.
Peter Doyle, Project Manager, Federal
Aviation Administration, Northwest
Mountain Region, Seattle Airports
District Office, 1601 Lind Avenue SW.,
Suite 250, Renton, Washington 98057–
3356.
The request to release property may
be reviewed, by appointment, in person
at this same location.
SUPPLEMENTARY INFORMATION: The FAA
invites public comment on the request
to release property at the SeattleTacoma International Airport under the
provisions of the AIR 21 (49 U.S.C.
47107(h)(2)).
On February 22, 2013, the FAA
determined that the request to release
property at Seattle-Tacoma International
Airport submitted by the airport meets
the procedural requirements of the
Federal Aviation Administration. The
FAA may approve the request, in whole
or in part, no later than April 8, 2013.
The following is a brief overview of
the request:
The Seattle-Tacoma International
Airport is proposing the release of
VerDate Mar<15>2010
18:44 Mar 07, 2013
Jkt 229001
approximately 15,628 square feet of
airport property to the City of SeaTac.
This property is located on International
Blvd. and 160th Street in the City of
SeaTac, and is required for road
improvements to mitigate traffic
generated by the Rental Car Facility
constructed on airport property. This
mitigation measure is required by the
environmental analysis to reduce the
likely significant adverse environmental
traffic impacts to a nonsignificant level.
The value of the property is a
component of the overall cost of the
Rental Car Facility project.
Any person may inspect, by
appointment, the request in person at
the FAA office listed above under FOR
FURTHER INFORMATION CONTACT. In
addition, any person may, upon
appointment and request, inspect the
application, notice and other documents
germane to the application in person at
the Seattle-Tacoma International
Airport, 17801 International Blvd.,
Seattle, Washington 98158.
Issued in Renton, Washington, on February
22, 2013.
Carol Suomi,
Manager, Seattle Airports District Office.
[FR Doc. 2013–05453 Filed 3–7–13; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Aviation
Rulemaking Advisory Committee;
Transport Airplane Performance and
Handling Characteristics—New Task
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of new task assignment
for the Aviation Rulemaking Advisory
Committee (ARAC).
AGENCY:
SUMMARY: The FAA assigned ARAC a
new task to prioritize potential topic
areas for development of new or revised
requirements and guidance material for
airplane performance and handling
characteristics in new transport category
airplanes. The output of this task is
intended to support FAA planning for
subsequent ARAC taskings in these
topic areas. This notice is to inform the
public of this ARAC activity.
FOR FURTHER INFORMATION CONTACT: Joe
Jacobsen, Airplane & Flight Crew
Interface Branch, ANM–111, Transport
Airplane Directorate, Federal Aviation
Administration, 1601 Lind Ave. SW.,
Renton, Washington 98057–3356;
telephone (425) 227–2011, facsimile
(425) 227– 1149; email
joe.jacobsen@faa.gov.
PO 00000
Frm 00154
Fmt 4703
Sfmt 4703
SUPPLEMENTARY INFORMATION:
Background
The FAA established ARAC to
provide advice and recommendations to
the FAA Administrator on the FAA’s
rulemaking activities with respect to
aviation-related issues. This includes
obtaining advice and recommendations
on the FAA’s commitments to
harmonize FAA regulations with its
partners in Europe, Canada, and Brazil;
in this instance, on airplane
performance and handling
characteristics standards. ARAC will
address this task under the Transport
Airplane and Engine (TAE)
Subcommittee, and will reestablish the
Flight Test Harmonization Working
Group (FTHWG) to assist in completion
of this task.
The FAA has established regulations
and policy in the areas of airplane
performance and handling
characteristics. However, existing
standards do not adequately address
airplane designs using fly-by-wire
technology. Additionally, there are a
number of issues, such as several items
in the areas of takeoff and landing
performance and flying qualities that
may not be adequately addressed by the
existing airworthiness requirements and
guidance material. Finally, there are
cases where guidance information
provided by the airworthiness
authorities is not harmonized,
sometimes leading to different
compliance findings.
The Task
The FAA tasked ARAC to consider
several areas within the airplane
performance and handling qualities
requirements of the 14 CFR part 25
airworthiness standards and guidance
for possible revision. The task includes
prioritizing the list of topic areas
provided in this notice based on
prioritization criteria established by the
FTHWG. The prioritization criteria
should consider harmonization of
regulatory requirements and associated
guidance material for airworthiness
certification of airplane designs.
Recommendations may result in
subsequent ARAC taskings for standards
recommendations in follow-on phases.
ARAC may also recommend additional
topics in the general area of airplane
performance and handling qualities that
are not on the list provided in this
notice
The working group will provide a
draft report to ARAC recommending
focus areas and work plans to address
those areas the FTHWG identified as
high priorities for airworthiness
standards development relative to new
E:\FR\FM\08MRN1.SGM
08MRN1
Federal Register / Vol. 78, No. 46 / Friday, March 8, 2013 / Notices
airplane designs. This report will
provide the rationale for the priority
recommended as well as identify those
items for which coordination with other
working groups or experts outside the
FTHWG may be needed. The report will
also include a proposed schedule for
accomplishment of the plan, including
whether multiple topics can be worked
simultaneously. If there is disagreement
within the working group, those items
should be documented, including the
rationale from each party and the
reasons for the disagreement. The
following subject areas should be
considered:
1. Fly-by-wire (FBW) Flight Controls.
Regulatory requirements and associated
guidance material for airworthiness
certification of airplane designs using
FBW technology to obviate
longstanding, repetitively used FBW
special conditions. Specific areas
include:
a. Applicability/adaptation of
Amendment 25–121 airplane
performance and handling
characteristics in icing conditions
requirements
b. Design maneuver requirements,*
c. Design dive speed,*
d. Side stick controls,*
e. Flight envelope protection, and *
f. Interaction of airplane systems and
structure.*
mstockstill on DSK4VPTVN1PROD with NOTICES
* Note: These items should be considered
for coordination with other working groups.
2. Takeoff and Landing Performance.
Regulatory requirements and associated
guidance material for airworthiness
certification in the following areas listed
below. (Note: This topic area excludes
items addressed by the Takeoff and
Landing Performance Assessment
Aviation Rulemaking Committee.)
a. Flight test methods used to
determine maximum tailwind and
crosswind capability. Additionally, for
crosswind testing, better define
intended operational use of
demonstrated maximum steady and
gusting crosswind performance.
b. Wet runway stopping performance.
Recent landing overruns on wet
runways have raised questions
regarding current wet runway stopping
performance requirements and methods.
Analyses indicate that the braking
coefficient of friction in each case was
significantly lower than expected for a
wet runway (i.e., lower than the level
specified in FAA regulations).
Consideration should also be given to
the scheduling of landing performance
on wet porous friction course and
grooved runway surfaces.
Recommendations may include the
need for additional data gathering,
analysis, and possible rulemaking.
VerDate Mar<15>2010
18:44 Mar 07, 2013
Jkt 229001
c. Go-around performance,
specifically height lost in executing a
go-around. While airplanes may be able
to demonstrate the climb gradient
capability prescribed in 14 CFR/
European Aviation Safety Agency
(EASA) Certification Specification (CS)
25.121, it may not be able to achieve it
quickly enough, particularly when
executing a go-around close to the
ground.
d. Performance standards and
guidance regarding landing in abnormal
configurations.
e. Guidance regarding the function
and use of the amber band on airspeed
tapes. Manufacturers’ philosophies
differ regarding the meaning of the
amber band in an airspeed tape display,
as do U.S. and European regulatory
authorities’ policies regarding
acceptance of target airspeeds within
the amber band.
f. Guidance on piloting procedures
used to evaluate airplane tail clearance
during certification flight tests for
takeoff performance.
g. Landing distance performance for
autoland and landing distance
performance using heads-up-displays
(HUD). Use of autoland or HUD may
invalidate landing distance performance
determined for compliance to 14 CFR/
CS 25.125.
h. Steep approach landing
performance. Current airplane
certification standards are not
harmonized among the U.S., Canadian,
Brazilian, and European airworthiness
authorities.
i. Narrow runway operations. Current
airplane certification standards do not
identify minimum runway widths for
which the standards apply.
j. Reduced and derated takeoff thrust
procedures. Updates to existing
guidance material may be appropriate to
limit the number of derates permitted
for a specific airframe/engine
combination.
k. Guidance material for pressure
error measurement during takeoff until
out of ground effect to ensure proper
data reduction for calculation of takeoff
distance performance.
l. Guidance material addressing the
adverse effects on stall speed in ground
effect.
3. Handling Characteristics.
Regulatory requirements and associated
guidance material for airworthiness
certification in the following areas:
a. Guidance material for assessing
handling qualities. Advisory Circular
25–7C, ‘‘Flight Test Guide for
Certification of Transport Category
Airplanes,’’ provides an FAA Handling
Quality Rating Method (HQRM) that is
intended to provide a systematic way of
PO 00000
Frm 00155
Fmt 4703
Sfmt 4703
15113
determining appropriate minimum
handling qualities requirements and
evaluating those handling qualities for
failure conditions affecting an airplane’s
flying qualities. The FAA handling
quality rating system is not universally
accepted within industry, nor is it
accepted by EASA.
b. Guidance for assessing
susceptibility to pilot-induced
oscillations/airplane-pilot coupling
(PIO/APC). Guidance provided in AC
25–7C for evaluating PIO/APC is also
not well accepted by airplane
manufacturers, is not harmonized with
EASA, and has been superseded to some
extent in recent certification programs.
Modified guidance is needed to both
simplify and standardize the methods
for evaluating an airplane’s
susceptibility to PIO/APC.
Schedule
The required completion date for the
recommendation report is 9 months
after the FAA publishes the task in the
Federal Register. After receiving the
report, the FAA will consider the
recommendations and determine
subsequent development tasks. The
FAA expects to publish additional
ARAC taskings for follow on phases to
develop recommendations for the
selected standards and guidance.
ARAC Acceptance of Task
ARAC accepted the task and assigned
it to the FTHWG under the TAE
Subcommittee. The working group
serves as staff to ARAC and assists in
the analysis of assigned tasks. ARAC
must review and approve the working
group’s recommendations. If ARAC
accepts the working group’s
recommendations, it will forward them
to the FAA.
Working Group Activity
The FTHWG must comply with the
procedures adopted by ARAC. As part
of the procedures, the working group
must:
1. Develop a prioritized list of subject
areas (as provided in this notice or
added by the FTHWG) to focus
subsequent efforts and standards
development in follow-on phases for
consideration by ARAC.
2. Based on the priorities from item 1
above, recommend a work plan and
phasing for completion of each
prioritized task for review and approval
by ARAC.
3. Provide a status report at each
meeting of ARAC.
4. Provide a final recommendation
report to ARAC for review and approval.
E:\FR\FM\08MRN1.SGM
08MRN1
15114
Federal Register / Vol. 78, No. 46 / Friday, March 8, 2013 / Notices
DEPARTMENT OF TRANSPORTATION
The FTHWG is composed of technical
experts having expertise in the subject
matter and an interest in the assigned
task. A working group member need not
be a representative or a member of
ARAC.
If you have expertise in the subject
matter and wish to become a member of
the working group, write to the person
listed under the caption FOR FURTHER
INFORMATION CONTACT expressing that
desire. Describe your interest in the task
and state the expertise you would bring
to the working group. We must receive
all requests by April 5, 2013. ARAC and
the FAA will review the requests and
advise you whether or not your request
is approved.
If you are chosen for membership on
the working group, you must represent
your aviation community segment and
actively participate in the working
group by attending all meetings and
providing written comments when
requested to do so. You must devote the
resources necessary to support the
working group in meeting any assigned
deadlines. You must keep your
management chain and those you may
represent advised of working group
activities and decisions to ensure that
the proposed technical solutions do not
conflict with your sponsoring
organization’s position when the subject
being negotiated is presented to ARAC
for approval. Once the working group
has begun deliberations, members will
not be added or substituted without the
approval of the FAA and the Working
Group Co-Chairs.
The Secretary of Transportation
determined that the formation and use
of ARAC is necessary and in the public
interest in connection with the
performance of duties imposed on the
FAA by law. ARAC and the TAE
Subcommittee meetings are open to the
public. Meetings of the Flight Test
Harmonization Working Group will not
be open to the public, except to the
extent individuals with an interest and
expertise are selected to participate. The
FAA will make no public
announcement of working group
meetings.
mstockstill on DSK4VPTVN1PROD with NOTICES
Participation in the Working Group
National Highway Traffic Safety
Administration
Issued in Washington, DC, on March 1,
2013.
Lirio Liu,
Designated Federal Officer, Aviation
Rulemaking Advisory Committee.
[FR Doc. 2013–05230 Filed 3–7–13; 8:45 am]
18:44 Mar 07, 2013
Group Lotus plc; Grant of Petition for
a Temporary Exemption From an
Advanced Air Bag Requirement of
FMVSS No. 208
National Highway Traffic
Safety Administration (NHTSA),
Department of Transportation (DOT).
ACTION: Notice of grant of a petition for
a temporary exemption from a provision
of Federal Motor Vehicle Safety
Standard (FMVSS) No. 208, Occupant
Crash Protection.
AGENCY:
SUMMARY: This notice grants the petition
of Group Lotus plc (Lotus) for a
temporary exemption of the front
passenger position of its Evora model
from one advanced air bag requirement
of FMVSS No. 208, i.e., the higher
maximum speed (56 km/h (35 mph))
belted test requirement using 5th
percentile adult female dummies. The
agency finds that achieving compliance
with that requirement would cause
substantial economic hardship to Lotus
and that the company has tried to
comply with the requirement in good
faith.
The exemption remains in effect
until March 8, 2014.
FOR FURTHER INFORMATION CONTACT:
David Jasinski, Office of the Chief
Counsel, NCC–112, National Highway
Traffic Safety Administration, 1200 New
Jersey Avenue SE., West Building 4th
Floor, Room W41–326, Washington, DC
20590. Telephone: (202) 366–2992; Fax:
(202) 366–3820.
SUPPLEMENTARY INFORMATION:
DATES:
I. Advanced Air Bag Requirements and
Small Volume Manufacturers
In 2000, NHTSA published a final
rule upgrading the requirements for air
bags in passenger cars and light trucks,
requiring what are commonly known as
‘‘advanced air bags.’’ 1 The upgrade was
designed to meet the twin goals of
improving protection for occupants of
all sizes, belted and unbelted, in
moderate-to-high-speed crashes, and of
minimizing the risks posed by air bags
to infants, children, and other
occupants, especially in low-speed
crashes. Prior to this rule, crash tests
under FMVSS No. 208 used only one
size dummy, a 50th percentile adult
male dummy. However, the advanced
air bag rule specified the use of both
2 See
BILLING CODE 4910–13–P
VerDate Mar<15>2010
[Docket No. NHTSA–2012–0086]
50th percentile adult male and 5th
percentile adult female dummies for the
standard’s crash tests.
The requirements for the vehicle
performance in an unbelted 32 km/h (20
mph) to 40 km/h (25 mph) rigid barrier
crash test and the belted rigid barrier
crash test with a maximum test speed of
48 km/h (30 mph) for both the 50th
percentile male dummy and the 5th
percentile female dummy were phased
in, beginning with the 2004 model year.
Small volume manufacturers were not
subject to these advanced air bag
requirements until the end of the phasein period, which was September 1,
2006.
A second phase-in period required
vehicles to be certified as meeting the
belted rigid barrier test requirements at
speeds up to 56 km/h (35 mph) using
the 50th percentile adult male dummy.
This requirement was phased in,
beginning with the 2008 model year.
Small volume manufacturers were not
subject to this requirement until the end
of the phase-in period, which was
September 1, 2010.
The 2000 final rule did not include a
higher speed belted rigid barrier test for
a 5th percentile adult female dummy.
Instead, NHTSA initiated testing to
examine the practicability of such a
requirement.2
On August 31, 2006, NHTSA
published a final rule that increased the
maximum test speed for the belted rigid
barrier test using the 5th percentile
adult female test dummy from
48 km/h (30 mph) to 56 km/h (35 mph).3
This new requirement was phased in,
beginning with the 2010 model year.
Small manufacturers were not subject to
this requirement until the completion of
the phase in period, which was
September 1, 2012.
In recent years, NHTSA has addressed
a number of petitions for exemption
from some of the initial advanced air
bag requirements of FMVSS No. 208.
The majority of these requests came
from small manufacturers, each of
which petitioned on the basis that
achieving compliance would cause it
substantial economic hardship and that
it has tried in good faith to comply with
the standard. In recognition of the more
limited resources and capabilities of
small manufacturers, authority to grant
exemptions based on substantial
economic hardship and good faith
efforts was given the agency in 1972 to
enable it to give those manufacturers
additional time to comply with the
Federal safety standards.
1 See
Jkt 229001
PO 00000
65 FR 30680 (May 12, 2000).
Frm 00156
Fmt 4703
Sfmt 4703
3 See
E:\FR\FM\08MRN1.SGM
65 FR 30690.
71 FR 51768.
08MRN1
Agencies
- DEPARTMENT OF TRANSPORTATION
- Federal Aviation Administration Aviation
[Federal Register Volume 78, Number 46 (Friday, March 8, 2013)]
[Notices]
[Pages 15112-15114]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-05230]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Aviation
Rulemaking Advisory Committee; Transport Airplane Performance and
Handling Characteristics--New Task
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of new task assignment for the Aviation Rulemaking
Advisory Committee (ARAC).
-----------------------------------------------------------------------
SUMMARY: The FAA assigned ARAC a new task to prioritize potential topic
areas for development of new or revised requirements and guidance
material for airplane performance and handling characteristics in new
transport category airplanes. The output of this task is intended to
support FAA planning for subsequent ARAC taskings in these topic areas.
This notice is to inform the public of this ARAC activity.
FOR FURTHER INFORMATION CONTACT: Joe Jacobsen, Airplane & Flight Crew
Interface Branch, ANM-111, Transport Airplane Directorate, Federal
Aviation Administration, 1601 Lind Ave. SW., Renton, Washington 98057-
3356; telephone (425) 227-2011, facsimile (425) 227- 1149; email
joe.jacobsen@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA established ARAC to provide advice and recommendations to
the FAA Administrator on the FAA's rulemaking activities with respect
to aviation-related issues. This includes obtaining advice and
recommendations on the FAA's commitments to harmonize FAA regulations
with its partners in Europe, Canada, and Brazil; in this instance, on
airplane performance and handling characteristics standards. ARAC will
address this task under the Transport Airplane and Engine (TAE)
Subcommittee, and will reestablish the Flight Test Harmonization
Working Group (FTHWG) to assist in completion of this task.
The FAA has established regulations and policy in the areas of
airplane performance and handling characteristics. However, existing
standards do not adequately address airplane designs using fly-by-wire
technology. Additionally, there are a number of issues, such as several
items in the areas of takeoff and landing performance and flying
qualities that may not be adequately addressed by the existing
airworthiness requirements and guidance material. Finally, there are
cases where guidance information provided by the airworthiness
authorities is not harmonized, sometimes leading to different
compliance findings.
The Task
The FAA tasked ARAC to consider several areas within the airplane
performance and handling qualities requirements of the 14 CFR part 25
airworthiness standards and guidance for possible revision. The task
includes prioritizing the list of topic areas provided in this notice
based on prioritization criteria established by the FTHWG. The
prioritization criteria should consider harmonization of regulatory
requirements and associated guidance material for airworthiness
certification of airplane designs. Recommendations may result in
subsequent ARAC taskings for standards recommendations in follow-on
phases. ARAC may also recommend additional topics in the general area
of airplane performance and handling qualities that are not on the list
provided in this notice
The working group will provide a draft report to ARAC recommending
focus areas and work plans to address those areas the FTHWG identified
as high priorities for airworthiness standards development relative to
new
[[Page 15113]]
airplane designs. This report will provide the rationale for the
priority recommended as well as identify those items for which
coordination with other working groups or experts outside the FTHWG may
be needed. The report will also include a proposed schedule for
accomplishment of the plan, including whether multiple topics can be
worked simultaneously. If there is disagreement within the working
group, those items should be documented, including the rationale from
each party and the reasons for the disagreement. The following subject
areas should be considered:
1. Fly-by-wire (FBW) Flight Controls. Regulatory requirements and
associated guidance material for airworthiness certification of
airplane designs using FBW technology to obviate longstanding,
repetitively used FBW special conditions. Specific areas include:
a. Applicability/adaptation of Amendment 25-121 airplane
performance and handling characteristics in icing conditions
requirements
b. Design maneuver requirements,*
c. Design dive speed,*
d. Side stick controls,*
e. Flight envelope protection, and *
f. Interaction of airplane systems and structure.*
* Note: These items should be considered for coordination with
other working groups.
2. Takeoff and Landing Performance. Regulatory requirements and
associated guidance material for airworthiness certification in the
following areas listed below. (Note: This topic area excludes items
addressed by the Takeoff and Landing Performance Assessment Aviation
Rulemaking Committee.)
a. Flight test methods used to determine maximum tailwind and
crosswind capability. Additionally, for crosswind testing, better
define intended operational use of demonstrated maximum steady and
gusting crosswind performance.
b. Wet runway stopping performance. Recent landing overruns on wet
runways have raised questions regarding current wet runway stopping
performance requirements and methods. Analyses indicate that the
braking coefficient of friction in each case was significantly lower
than expected for a wet runway (i.e., lower than the level specified in
FAA regulations). Consideration should also be given to the scheduling
of landing performance on wet porous friction course and grooved runway
surfaces. Recommendations may include the need for additional data
gathering, analysis, and possible rulemaking.
c. Go-around performance, specifically height lost in executing a
go-around. While airplanes may be able to demonstrate the climb
gradient capability prescribed in 14 CFR/European Aviation Safety
Agency (EASA) Certification Specification (CS) 25.121, it may not be
able to achieve it quickly enough, particularly when executing a go-
around close to the ground.
d. Performance standards and guidance regarding landing in abnormal
configurations.
e. Guidance regarding the function and use of the amber band on
airspeed tapes. Manufacturers' philosophies differ regarding the
meaning of the amber band in an airspeed tape display, as do U.S. and
European regulatory authorities' policies regarding acceptance of
target airspeeds within the amber band.
f. Guidance on piloting procedures used to evaluate airplane tail
clearance during certification flight tests for takeoff performance.
g. Landing distance performance for autoland and landing distance
performance using heads-up-displays (HUD). Use of autoland or HUD may
invalidate landing distance performance determined for compliance to 14
CFR/CS 25.125.
h. Steep approach landing performance. Current airplane
certification standards are not harmonized among the U.S., Canadian,
Brazilian, and European airworthiness authorities.
i. Narrow runway operations. Current airplane certification
standards do not identify minimum runway widths for which the standards
apply.
j. Reduced and derated takeoff thrust procedures. Updates to
existing guidance material may be appropriate to limit the number of
derates permitted for a specific airframe/engine combination.
k. Guidance material for pressure error measurement during takeoff
until out of ground effect to ensure proper data reduction for
calculation of takeoff distance performance.
l. Guidance material addressing the adverse effects on stall speed
in ground effect.
3. Handling Characteristics. Regulatory requirements and associated
guidance material for airworthiness certification in the following
areas:
a. Guidance material for assessing handling qualities. Advisory
Circular 25-7C, ``Flight Test Guide for Certification of Transport
Category Airplanes,'' provides an FAA Handling Quality Rating Method
(HQRM) that is intended to provide a systematic way of determining
appropriate minimum handling qualities requirements and evaluating
those handling qualities for failure conditions affecting an airplane's
flying qualities. The FAA handling quality rating system is not
universally accepted within industry, nor is it accepted by EASA.
b. Guidance for assessing susceptibility to pilot-induced
oscillations/airplane-pilot coupling (PIO/APC). Guidance provided in AC
25-7C for evaluating PIO/APC is also not well accepted by airplane
manufacturers, is not harmonized with EASA, and has been superseded to
some extent in recent certification programs. Modified guidance is
needed to both simplify and standardize the methods for evaluating an
airplane's susceptibility to PIO/APC.
Schedule
The required completion date for the recommendation report is 9
months after the FAA publishes the task in the Federal Register. After
receiving the report, the FAA will consider the recommendations and
determine subsequent development tasks. The FAA expects to publish
additional ARAC taskings for follow on phases to develop
recommendations for the selected standards and guidance.
ARAC Acceptance of Task
ARAC accepted the task and assigned it to the FTHWG under the TAE
Subcommittee. The working group serves as staff to ARAC and assists in
the analysis of assigned tasks. ARAC must review and approve the
working group's recommendations. If ARAC accepts the working group's
recommendations, it will forward them to the FAA.
Working Group Activity
The FTHWG must comply with the procedures adopted by ARAC. As part
of the procedures, the working group must:
1. Develop a prioritized list of subject areas (as provided in this
notice or added by the FTHWG) to focus subsequent efforts and standards
development in follow-on phases for consideration by ARAC.
2. Based on the priorities from item 1 above, recommend a work plan
and phasing for completion of each prioritized task for review and
approval by ARAC.
3. Provide a status report at each meeting of ARAC.
4. Provide a final recommendation report to ARAC for review and
approval.
[[Page 15114]]
Participation in the Working Group
The FTHWG is composed of technical experts having expertise in the
subject matter and an interest in the assigned task. A working group
member need not be a representative or a member of ARAC.
If you have expertise in the subject matter and wish to become a
member of the working group, write to the person listed under the
caption FOR FURTHER INFORMATION CONTACT expressing that desire.
Describe your interest in the task and state the expertise you would
bring to the working group. We must receive all requests by April 5,
2013. ARAC and the FAA will review the requests and advise you whether
or not your request is approved.
If you are chosen for membership on the working group, you must
represent your aviation community segment and actively participate in
the working group by attending all meetings and providing written
comments when requested to do so. You must devote the resources
necessary to support the working group in meeting any assigned
deadlines. You must keep your management chain and those you may
represent advised of working group activities and decisions to ensure
that the proposed technical solutions do not conflict with your
sponsoring organization's position when the subject being negotiated is
presented to ARAC for approval. Once the working group has begun
deliberations, members will not be added or substituted without the
approval of the FAA and the Working Group Co-Chairs.
The Secretary of Transportation determined that the formation and
use of ARAC is necessary and in the public interest in connection with
the performance of duties imposed on the FAA by law. ARAC and the TAE
Subcommittee meetings are open to the public. Meetings of the Flight
Test Harmonization Working Group will not be open to the public, except
to the extent individuals with an interest and expertise are selected
to participate. The FAA will make no public announcement of working
group meetings.
Issued in Washington, DC, on March 1, 2013.
Lirio Liu,
Designated Federal Officer, Aviation Rulemaking Advisory Committee.
[FR Doc. 2013-05230 Filed 3-7-13; 8:45 am]
BILLING CODE 4910-13-P