Special Conditions: Textron Aviation Inc. (Textron) Model 560XL Airplane; Hydrophobic Windshield Coatings, 66543-66545 [2024-18425]
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66543
Rules and Regulations
Federal Register
Vol. 89, No. 159
Friday, August 16, 2024
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents.
DEPARTMENT OF AGRICULTURE
Animal and Plant Health Inspection
Service
customs territory of the United States,
either as a preassigned condition of
entry or as a remedial measure ordered
following the inspection of the
consignment, must pay an AQI user
fee.’’ is corrected to read ‘‘Each importer
of a consignment of articles that require
treatment upon arrival from a place
outside of the customs territory of the
United States, either as a preassigned
condition of entry or as a remedial
measure ordered following the
inspection of the consignment, must pay
an AQI user fee.’’.
Done in Washington, DC, this 26th day of
July 2024.
Jennifer Moffitt,
Under Secretary for Marketing and Regulatory
Programs.
7 CFR Part 354
[Docket No. APHIS–2022–0023]
RIN 0579–AE71
User Fees for Agricultural Quarantine
and Inspection Services; Correction
Animal and Plant Health
Inspection Service, USDA.5
ACTION: Final rule; correction.
[FR Doc. 2024–18206 Filed 8–15–24; 8:45 am]
BILLING CODE 3410–34–P
AGENCY:
DEPARTMENT OF TRANSPORTATION
This document corrects a
typographical error in the final rule
entitled ‘‘User Fees for Agricultural
Quarantine and Inspection Services,’’
which was published in the Federal
Register on May 7, 2024, and has an
effective date of October 1, 2024.
DATES: This document is effective on
October 1, 2024.
FOR FURTHER INFORMATION CONTACT: Mr.
George Balady, Senior Regulatory Policy
Specialist, PPQ, APHIS, 4700 River
Road, Unit 36, Riverdale, MD 20737;
(301) 851–2338; aqi.user.fees@usda.gov.
SUPPLEMENTARY INFORMATION: In the
Federal Register of May 7, 2024 (89 FR
38596–38644), we published a final rule
entitled ‘‘User Fees for Agricultural
Quarantine’’ that listed the designation
for paragraph (h)(1) twice in 7 CFR
354.3. This document corrects that
error.
SUMMARY:
Correction
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In FR Doc. 2024–09348, appearing on
pages 38596–38644 in the Federal
Register of Tuesday, May 7, 2024, the
following correction is made:
§ 354.3
[Corrected]
On page 38643, in the second column,
in § 354.3, paragraph (h)(1), the first
sentence after the paragraph heading
‘‘(1) Each importer of a consignment of
articles that require treatment upon
arrival from a place outside of the
■
VerDate Sep<11>2014
16:32 Aug 15, 2024
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Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2024–1626; Special
Conditions No. 25–867–SC]
Special Conditions: Textron Aviation
Inc. (Textron) Model 560XL Airplane;
Hydrophobic Windshield Coatings
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for the Textron Model 560XL
airplane. This airplane will have a novel
or unusual design feature when
compared to the state of technology
envisioned in the airworthiness
standards for transport-category
airplanes. This design feature is
hydrophobic windshield coatings to
maintain a clear view. The applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for this design feature. These special
conditions contain the additional safety
standards that the Administrator
considers necessary to establish a level
of safety equivalent to that established
by the existing airworthiness standards.
DATES: This action is effective on
Textron on August 16, 2024. Send
comments on or before September 30,
2024.
SUMMARY:
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Send comments identified
by Docket No. FAA–2024–1626 using
any of the following methods:
• Federal eRegulations Portal: Go to
www.regulations.gov and follow the
online instructions for sending your
comments electronically.
• Mail: Send comments to Docket
Operations, M–30, U.S. Department of
Transportation (DOT), 1200 New Jersey
Avenue SE, Room W12–140, West
Building Ground Floor, Washington, DC
20590–0001.
• Hand Delivery or Courier: Take
comments to Docket Operations in
Room W12–140 of the West Building
Ground Floor at 1200 New Jersey
Avenue SE, Washington, DC, between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays.
• Fax: Fax comments to Docket
Operations at 202–493–2251.
Docket: Background documents or
comments received may be read at
www.regulations.gov at any time.
Follow the online instructions for
accessing the docket or go to Docket
Operations in Room W12–140 of the
West Building Ground Floor at 1200
New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT: Eric
Brown, Flight Test and Human Factors,
AIR–621A, Technical Policy Branch,
Policy and Standards Division, Aircraft
Certification Service, Federal Aviation
Administration, 2200 S 216th Street,
Des Moines, Washington 98198,
telephone and (206) 231–3563; email
Eric.M.Brown@faa.gov.
SUPPLEMENTARY INFORMATION: The
substance of these special conditions
has been published in the Federal
Register for public comment in several
prior instances with no substantive
comments received. Therefore, the FAA
finds, pursuant to 14 CFR 11.38(b), that
new comments are unlikely, and notice
and comment prior to this publication
are unnecessary.
ADDRESSES:
Privacy
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in title 14,
Code of Federal Regulations (14 CFR)
11.35, the FAA will post all comments
received without change to
www.regulations.gov, including any
personal information you provide. The
E:\FR\FM\16AUR1.SGM
16AUR1
66544
Federal Register / Vol. 89, No. 159 / Friday, August 16, 2024 / Rules and Regulations
FAA will also post a report
summarizing each substantive verbal
contact received about these special
conditions.
Confidential Business Information
Confidential Business Information
(CBI) is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to these special
conditions contain commercial or
financial information that is customarily
treated as private, that you actually treat
as private, and that is relevant or
responsive to these special conditions, it
is important that you clearly designate
the submitted comments as CBI. Please
mark each page of your submission
containing CBI as ‘‘PROPIN.’’ The FAA
will treat such marked submissions as
confidential under the FOIA, and the
indicated comments will not be placed
in the public docket of these proposed
special conditions. Send submissions
containing CBI to the individual listed
in the For Further Information Contact
section above. Comments the FAA
receives, which are not specifically
designated as CBI, will be placed in the
public docket for these proposed special
conditions.
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Comments Invited
The FAA invites interested people to
take part in this rulemaking by sending
written comments, data, or views. The
most helpful comments reference a
specific portion of the special
conditions, explain the reason for any
recommended change, and include
supporting data.
The FAA will consider all comments
received by the closing date for
comments. The FAA may change these
special conditions based on the
comments received.
Aviation Inc. Model 560XL airplane, as
changed, continues to meet the
applicable provisions of the regulations
listed in Type Certificate No. A22CE or
the applicable regulations in effect on
the date of application for the change,
except for earlier amendments as agreed
upon by the FAA.
If the Administrator finds that the
applicable airworthiness regulations
(e.g., 14 CFR part 25) do not contain
adequate or appropriate safety standards
for the Textron Model 560XL airplane
because of a novel or unusual design
feature, special conditions are
prescribed under the provisions of
§ 21.16.
Special conditions are initially
applicable to the model for which they
are issued. Should the type certificate
for that model be amended later to
include any other model that
incorporates the same novel or unusual
design feature, or should any other
model already included on the same
type certificate be modified to
incorporate the same novel or unusual
design feature, these special conditions
would also apply to the other model
under § 21.101.
In addition to the applicable
airworthiness regulations and special
conditions, the Textron Model 560XL
airplane must comply with the exhaustemission requirements of 14 CFR part
34, and the noise-certification
requirements of 14 CFR part 36.
The FAA issues special conditions, as
defined in 14 CFR 11.19, in accordance
with § 11.38, and they become part of
the type certification basis under
§ 21.101.
Background
On June 30, 2021, Textron applied for
a change to Type Certificate No. A22CE
for hydrophobic coatings in lieu of
windshield wipers on the Model 560XL.
The Textron Model 560XL airplane is a
derivative of the Model 560XLS+ and is
currently approved under Type
Certificate No. A22CE. The Model
560XL is a twin-engine business jet,
with a maximum seating capacity for 12
passengers, and a maximum take-off
weight of 20,330 pounds.
Novel or Unusual Design Features
The modified Textron Model 560XL
series airplane will incorporate the
following novel or unusual design
feature:
Hydrophobic windshield coatings to
maintain a clear view. The airplane
flightdeck design incorporates
hydrophobic windshield coating that,
during precipitation, provides an
adequate outside view from the pilot
compartment. Sole reliance on such
coating, without windshield wipers,
constitutes a novel or unusual design
feature for which the applicable
airworthiness regulations do not contain
adequate or appropriate safety
standards. Therefore, special conditions
are required to provide a level of safety
equivalent to that established by the
regulations.
Type Certification Basis
Under the provisions of title 14, Code
of Federal Regulations (14 CFR) 21.101,
Textron must show that the Textron
Discussion
Title 14 CFR 25.773(b)(1) requires a
means to maintain a clear portion of the
windshield for both pilots to have a
VerDate Sep<11>2014
16:32 Aug 15, 2024
Jkt 262001
PO 00000
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Fmt 4700
Sfmt 4700
sufficiently extensive view along the
flight path during precipitation
conditions. The regulations require this
means to maintain such an area during
precipitation in heavy rain at speeds up
to 1.5 VSR1.
Effective December 26, 2002,
amendment 25–108 changed the speed
for effectiveness of the means to
maintain an area of clear vision from up
to 1.6 VS1 to 1.5 VSR1 to accommodate
the redefinition of the reference stall
speed from the minimum speed in the
stall, VS1, to greater than or equal to the
1g stall speed, VSR1. As noted in the
preamble to the final rule for that
amendment, the reduced factor of 1.5 on
VSR1 is to maintain approximately the
same speed as the 1.6 factor on VS1.
Textron was granted an Equivalent
Level of Safety (ELOS) to
§ 25.773(b)(1)(i) amendment 25–136 to
use 1.6 Vs1 instead of 1.5 VSR1 as
documented in ELOS Memorandum No.
TXTAV–18571–SM–03, dated December
6, 2023.
The requirement that the means to
maintain a clear area of forward vision
must function at high speeds and high
precipitation rates is based on the use of
windshield wipers as the means to
maintain an adequate area of clear
vision in precipitation conditions. The
effectiveness of windshield wipers to
maintain an area of clear vision
normally degrades as airspeed and
precipitation rates increase. It is
assumed that because high speeds and
high precipitation rates represent
limiting conditions for windshield
wipers, they will also be effective at
lower speeds and precipitation levels.
Accordingly, § 25.773(b)(1)(i) does not
require maintenance of a clear area of
forward vision at lower speeds or lower
precipitation rates.
A forced airflow blown directly over
the windshield has also been used to
maintain an area of clear vision in
precipitation. The limiting conditions
for this technology are comparable to
those for windshield wipers.
Accordingly, introduction of this
technology did not present a need for
special conditions to maintain the level
of safety embodied in the existing
regulations.
Hydrophobic windshield coatings
may depend to some degree on airflow
to maintain a clear vision area. The
heavy rain and high-speed conditions
specified in the current rule do not
necessarily represent the limiting
condition for this new technology. For
example, airflow over the windshield,
which may be necessary to remove
moisture from the windshield, may not
be adequate to maintain a sufficiently
clear area of the windshield in low-
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Federal Register / Vol. 89, No. 159 / Friday, August 16, 2024 / Rules and Regulations
speed flight or during surface
operations. Alternatively, airflow over
the windshield may be disturbed during
such critical times as the approach to
land, where the airplane is at a higherthan-normal pitch attitude. In these
cases, areas of airflow disturbance or
separation on the windshield could
cause failure to maintain a clear vision
area on the windshield.
In addition to potentially depending
on airflow to function effectively,
hydrophobic coatings may also be
dependent on water-droplet size for
effective precipitation removal. For
example, precipitation in the form of a
light mist may not be sufficient for the
coating’s properties to result in
maintaining a clear area of vision.
The current regulations identify speed
and precipitation rate requirements that
represent limiting conditions for
windshield wipers and blowers, but not
for hydrophobic coatings. Likewise, it is
necessary to issue special conditions to
maintain the level of safety represented
by the current regulations.
These special conditions provide an
appropriate safety standard for the
hydrophobic-coating technology as the
means to maintain a clear area of vision
by requiring coating to be effective at
low speeds and low precipitation rates,
as well as at the higher speeds and
precipitation rates identified in the
current regulation.
These special conditions contain the
additional safety standards that the
Administrator considers necessary to
establish a level of safety equivalent to
that established by the existing
airworthiness standards.
Applicability
As discussed above, these special
conditions are applicable to the Textron
Model 560XL airplane. Should Textron
apply at a later date for a change to the
type certificate to include another
model incorporating the same novel or
unusual design feature, these special
conditions would apply to that model as
well.
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Conclusion
This action affects only a certain
novel or unusual design feature on the
Textron Model 560XL airplane. It is not
a rule of general applicability.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting
and recordkeeping requirements.
Authority Citation
The authority citation for these
special conditions is as follows:
Authority: 49 U.S.C. 106(f), 106(g), 40113,
44701, 44702, and 44704.
VerDate Sep<11>2014
16:32 Aug 15, 2024
Jkt 262001
The Special Conditions
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the following special
conditions are issued as part of the type
certification basis for Textron Model
560XL.
The airplane must have a means to
maintain a clear portion of the
windshield, during precipitation
conditions, enough for both pilots to
have a sufficiently extensive view along
the ground or flight path in normal taxi
and flight altitudes of the airplane. This
means must be designed to function,
without continuous attention on the
part of the crew, in conditions from
light misting precipitation to heavy rain,
at speeds from fully stopped in still air,
to 1.6 VS with lift and drag devices
retracted.
Issued in Kansas City, Missouri, on August
8, 2024.
Patrick R. Mullen,
Manager, Technical Policy Branch, Policy and
Standards Division, Aircraft Certification
Service.
[FR Doc. 2024–18425 Filed 8–15–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
RIN 2120–AA66
Amendment of Class D Airspace; Fort
Liberty, NC; Correction
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
Fmt 4700
FOR FURTHER INFORMATION CONTACT:
Justin T. Rhodes, Operations Support
Group, Eastern Service Center, Federal
Aviation Administration, 1701
Columbia Avenue, College Park, GA
30337; telephone: (404) 305–5478.
SUPPLEMENTARY INFORMATION:
History
The FAA published a final rule in the
Federal Register on July 18, 2024 (89 FR
58262) for Docket No. FAA–2024–0383,
updating the Class D airspace for Fort
Liberty, NC, by excluding 1,400 feet
MSL from the vertical limits (previously
‘‘including’’), updating the airport’s
geographic coordinates, replacing
‘‘Notice to Airmen’’ with ‘‘Notice to Air
Missions’’ in the description, and
updating the reference to ‘‘Chart
Supplement’’ (previously ‘‘Airport
Facility Directory’’). After publication,
the FAA found updates to the FAA’s
database rendering the Airport
Reference Point (ARP) data incorrect,
which, as dependent upon the ARP,
rendered other airspace description
information incorrect. This action
corrects these errors.
Sfmt 4700
In FR Doc 2024–15483 at 58262,
published in the Federal Register on
July 18, 2024, the FAA makes the
following corrections:
On page 58263, in the second column,
correct the ASO NC D description for
Fort Liberty, NC, to read as follows:
*
The FAA is correcting a final
rule that was published in the Federal
Register on July 18, 2024. The final rule
amended Class D airspace extending
upward from the surface for Fort
Liberty, NC. This action corrects errors
in the Class D legal description.
DATES: Effective 0901 UTC, October 31,
2024. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA
Order JO 7400.11 and publication of
conforming amendments.
ADDRESSES: FAA Order JO 7400.11H,
Airspace Designations, and Reporting
Points, and subsequent amendments can
be viewed online at https://
www.faa.gov/air_traffic/publications/.
For further information, you can contact
SUMMARY:
Frm 00003
the Rules and Regulations Group,
Federal Aviation Administration, 800
Independence Avenue SW, Washington,
DC 20591; telephone: (202) 267–8783.
Correction to the Final Rule
[Docket No. FAA–2024–0383; Airspace
Docket No. 24–ASO–2]
PO 00000
66545
*
ASO NC D
*
*
*
Simmons AAF, NC [Corrected]
Simmons AAF, NC
(Lat. 35°07′56″ N, long. 78°56′07″ W)
That airspace extending upward from the
surface to but not including 1,400 feet MSL
within a 3.9-mile radius of Simmons AAF,
excluding the portion northwest of a line
extending from lat. 35°11′48″ N, long.
78°55′35″ W; to lat. 35°06′19″ N, long.
79°00′27″ W, excluding the portion within
the Fayetteville, NC, Class C airspace area.
This Class D airspace area is effective during
the specific dates and times established in
advance by a Notice to Air Missions. The
effective date and time will thereafter be
continuously published in the Chart
Supplement.
*
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*
*
16AUR1
*
*
Agencies
[Federal Register Volume 89, Number 159 (Friday, August 16, 2024)]
[Rules and Regulations]
[Pages 66543-66545]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-18425]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2024-1626; Special Conditions No. 25-867-SC]
Special Conditions: Textron Aviation Inc. (Textron) Model 560XL
Airplane; Hydrophobic Windshield Coatings
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Textron Model
560XL airplane. This airplane will have a novel or unusual design
feature when compared to the state of technology envisioned in the
airworthiness standards for transport-category airplanes. This design
feature is hydrophobic windshield coatings to maintain a clear view.
The applicable airworthiness regulations do not contain adequate or
appropriate safety standards for this design feature. These special
conditions contain the additional safety standards that the
Administrator considers necessary to establish a level of safety
equivalent to that established by the existing airworthiness standards.
DATES: This action is effective on Textron on August 16, 2024. Send
comments on or before September 30, 2024.
ADDRESSES: Send comments identified by Docket No. FAA-2024-1626 using
any of the following methods:
Federal eRegulations Portal: Go to www.regulations.gov and
follow the online instructions for sending your comments
electronically.
Mail: Send comments to Docket Operations, M-30, U.S.
Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room
W12-140, West Building Ground Floor, Washington, DC 20590-0001.
Hand Delivery or Courier: Take comments to Docket
Operations in Room W12-140 of the West Building Ground Floor at 1200
New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Fax: Fax comments to Docket Operations at 202-493-2251.
Docket: Background documents or comments received may be read at
www.regulations.gov at any time. Follow the online instructions for
accessing the docket or go to Docket Operations in Room W12-140 of the
West Building Ground Floor at 1200 New Jersey Avenue SE, Washington,
DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays.
FOR FURTHER INFORMATION CONTACT: Eric Brown, Flight Test and Human
Factors, AIR-621A, Technical Policy Branch, Policy and Standards
Division, Aircraft Certification Service, Federal Aviation
Administration, 2200 S 216th Street, Des Moines, Washington 98198,
telephone and (206) 231-3563; email [email protected].
SUPPLEMENTARY INFORMATION: The substance of these special conditions
has been published in the Federal Register for public comment in
several prior instances with no substantive comments received.
Therefore, the FAA finds, pursuant to 14 CFR 11.38(b), that new
comments are unlikely, and notice and comment prior to this publication
are unnecessary.
Privacy
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in title
14, Code of Federal Regulations (14 CFR) 11.35, the FAA will post all
comments received without change to www.regulations.gov, including any
personal information you provide. The
[[Page 66544]]
FAA will also post a report summarizing each substantive verbal contact
received about these special conditions.
Confidential Business Information
Confidential Business Information (CBI) is commercial or financial
information that is both customarily and actually treated as private by
its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552),
CBI is exempt from public disclosure. If your comments responsive to
these special conditions contain commercial or financial information
that is customarily treated as private, that you actually treat as
private, and that is relevant or responsive to these special
conditions, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and the indicated comments will not be
placed in the public docket of these proposed special conditions. Send
submissions containing CBI to the individual listed in the For Further
Information Contact section above. Comments the FAA receives, which are
not specifically designated as CBI, will be placed in the public docket
for these proposed special conditions.
Comments Invited
The FAA invites interested people to take part in this rulemaking
by sending written comments, data, or views. The most helpful comments
reference a specific portion of the special conditions, explain the
reason for any recommended change, and include supporting data.
The FAA will consider all comments received by the closing date for
comments. The FAA may change these special conditions based on the
comments received.
Background
On June 30, 2021, Textron applied for a change to Type Certificate
No. A22CE for hydrophobic coatings in lieu of windshield wipers on the
Model 560XL. The Textron Model 560XL airplane is a derivative of the
Model 560XLS+ and is currently approved under Type Certificate No.
A22CE. The Model 560XL is a twin-engine business jet, with a maximum
seating capacity for 12 passengers, and a maximum take-off weight of
20,330 pounds.
Type Certification Basis
Under the provisions of title 14, Code of Federal Regulations (14
CFR) 21.101, Textron must show that the Textron Aviation Inc. Model
560XL airplane, as changed, continues to meet the applicable provisions
of the regulations listed in Type Certificate No. A22CE or the
applicable regulations in effect on the date of application for the
change, except for earlier amendments as agreed upon by the FAA.
If the Administrator finds that the applicable airworthiness
regulations (e.g., 14 CFR part 25) do not contain adequate or
appropriate safety standards for the Textron Model 560XL airplane
because of a novel or unusual design feature, special conditions are
prescribed under the provisions of Sec. 21.16.
Special conditions are initially applicable to the model for which
they are issued. Should the type certificate for that model be amended
later to include any other model that incorporates the same novel or
unusual design feature, or should any other model already included on
the same type certificate be modified to incorporate the same novel or
unusual design feature, these special conditions would also apply to
the other model under Sec. 21.101.
In addition to the applicable airworthiness regulations and special
conditions, the Textron Model 560XL airplane must comply with the
exhaust-emission requirements of 14 CFR part 34, and the noise-
certification requirements of 14 CFR part 36.
The FAA issues special conditions, as defined in 14 CFR 11.19, in
accordance with Sec. 11.38, and they become part of the type
certification basis under Sec. 21.101.
Novel or Unusual Design Features
The modified Textron Model 560XL series airplane will incorporate
the following novel or unusual design feature:
Hydrophobic windshield coatings to maintain a clear view. The
airplane flightdeck design incorporates hydrophobic windshield coating
that, during precipitation, provides an adequate outside view from the
pilot compartment. Sole reliance on such coating, without windshield
wipers, constitutes a novel or unusual design feature for which the
applicable airworthiness regulations do not contain adequate or
appropriate safety standards. Therefore, special conditions are
required to provide a level of safety equivalent to that established by
the regulations.
Discussion
Title 14 CFR 25.773(b)(1) requires a means to maintain a clear
portion of the windshield for both pilots to have a sufficiently
extensive view along the flight path during precipitation conditions.
The regulations require this means to maintain such an area during
precipitation in heavy rain at speeds up to 1.5 VSR1.
Effective December 26, 2002, amendment 25-108 changed the speed for
effectiveness of the means to maintain an area of clear vision from up
to 1.6 VS1 to 1.5 VSR1 to accommodate the
redefinition of the reference stall speed from the minimum speed in the
stall, VS1, to greater than or equal to the 1g stall speed,
VSR1. As noted in the preamble to the final rule for that
amendment, the reduced factor of 1.5 on VSR1 is to maintain
approximately the same speed as the 1.6 factor on VS1.
Textron was granted an Equivalent Level of Safety (ELOS) to Sec.
25.773(b)(1)(i) amendment 25-136 to use 1.6 Vs1 instead of
1.5 VSR1 as documented in ELOS Memorandum No. TXTAV-18571-
SM-03, dated December 6, 2023.
The requirement that the means to maintain a clear area of forward
vision must function at high speeds and high precipitation rates is
based on the use of windshield wipers as the means to maintain an
adequate area of clear vision in precipitation conditions. The
effectiveness of windshield wipers to maintain an area of clear vision
normally degrades as airspeed and precipitation rates increase. It is
assumed that because high speeds and high precipitation rates represent
limiting conditions for windshield wipers, they will also be effective
at lower speeds and precipitation levels. Accordingly, Sec.
25.773(b)(1)(i) does not require maintenance of a clear area of forward
vision at lower speeds or lower precipitation rates.
A forced airflow blown directly over the windshield has also been
used to maintain an area of clear vision in precipitation. The limiting
conditions for this technology are comparable to those for windshield
wipers. Accordingly, introduction of this technology did not present a
need for special conditions to maintain the level of safety embodied in
the existing regulations.
Hydrophobic windshield coatings may depend to some degree on
airflow to maintain a clear vision area. The heavy rain and high-speed
conditions specified in the current rule do not necessarily represent
the limiting condition for this new technology. For example, airflow
over the windshield, which may be necessary to remove moisture from the
windshield, may not be adequate to maintain a sufficiently clear area
of the windshield in low-
[[Page 66545]]
speed flight or during surface operations. Alternatively, airflow over
the windshield may be disturbed during such critical times as the
approach to land, where the airplane is at a higher-than-normal pitch
attitude. In these cases, areas of airflow disturbance or separation on
the windshield could cause failure to maintain a clear vision area on
the windshield.
In addition to potentially depending on airflow to function
effectively, hydrophobic coatings may also be dependent on water-
droplet size for effective precipitation removal. For example,
precipitation in the form of a light mist may not be sufficient for the
coating's properties to result in maintaining a clear area of vision.
The current regulations identify speed and precipitation rate
requirements that represent limiting conditions for windshield wipers
and blowers, but not for hydrophobic coatings. Likewise, it is
necessary to issue special conditions to maintain the level of safety
represented by the current regulations.
These special conditions provide an appropriate safety standard for
the hydrophobic-coating technology as the means to maintain a clear
area of vision by requiring coating to be effective at low speeds and
low precipitation rates, as well as at the higher speeds and
precipitation rates identified in the current regulation.
These special conditions contain the additional safety standards
that the Administrator considers necessary to establish a level of
safety equivalent to that established by the existing airworthiness
standards.
Applicability
As discussed above, these special conditions are applicable to the
Textron Model 560XL airplane. Should Textron apply at a later date for
a change to the type certificate to include another model incorporating
the same novel or unusual design feature, these special conditions
would apply to that model as well.
Conclusion
This action affects only a certain novel or unusual design feature
on the Textron Model 560XL airplane. It is not a rule of general
applicability.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
Authority Citation
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701, 44702, and
44704.
The Special Conditions
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special conditions are issued as part of
the type certification basis for Textron Model 560XL.
The airplane must have a means to maintain a clear portion of the
windshield, during precipitation conditions, enough for both pilots to
have a sufficiently extensive view along the ground or flight path in
normal taxi and flight altitudes of the airplane. This means must be
designed to function, without continuous attention on the part of the
crew, in conditions from light misting precipitation to heavy rain, at
speeds from fully stopped in still air, to 1.6 VS with lift
and drag devices retracted.
Issued in Kansas City, Missouri, on August 8, 2024.
Patrick R. Mullen,
Manager, Technical Policy Branch, Policy and Standards Division,
Aircraft Certification Service.
[FR Doc. 2024-18425 Filed 8-15-24; 8:45 am]
BILLING CODE 4910-13-P