Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-2A13 Airplanes; Airplane Electronic-System Security Protection From Authorized Internal Access, 56474-56475 [2016-19994]
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56474
Federal Register / Vol. 81, No. 162 / Monday, August 22, 2016 / Rules and Regulations
Issued in Renton, Washington, on August
11, 2016.
Paul Bernado,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2016–19993 Filed 8–19–16; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2015–6359; Special
Conditions No. 25–633–SC]
Special Conditions: Bombardier Inc.
Model BD–700–2A12 and BD–700–
2A13 Airplanes; Airplane ElectronicSystem Security Protection From
Authorized Internal Access
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for the Bombardier Inc.
(Bombardier) Model BD–700–2A12 and
BD–700–2A13 airplanes. These
airplanes will have novel or unusual
design features, specifically, digital
systems architecture composed of
several connected data networks that
will have the capability to allow
connectivity of the passenger-service
computer systems to the airplane
critical systems and data networks. 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
Bombardier on August 22, 2016. We
must receive your comments by October
6, 2016.
ADDRESSES: Send comments identified
by docket number FAA–2015–6359
using any of the following methods:
• Federal eRegulations Portal: Go to
https://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
Lhorne on DSK30JT082PROD with RULES
SUMMARY:
VerDate Sep<11>2014
15:11 Aug 19, 2016
Jkt 238001
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.
Privacy: The FAA will post all
comments it receives, without change,
to https://www.regulations.gov/,
including any personal information the
commenter provides. Using the search
function of the docket Web site, anyone
can find and read the electronic form of
all comments received into any FAA
docket, including the name of the
individual sending the comment (or
signing the comment for an association,
business, labor union, etc.). DOT’s
complete Privacy Act Statement can be
found in the Federal Register published
on April 11, 2000 (65 FR 19477–19478),
as well as at https://DocketsInfo.dot.
gov/.
Docket: Background documents or
comments received may be read at
https://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:
Varun Khanna, FAA, Airplane and
Flight Crew Interface, ANM–111,
Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue
SW., Renton, Washington 98057–3356;
telephone 425–227–1298; facsimile
425–227–1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite 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.
We will consider all comments we
receive on or before the closing date for
comments. We may change these special
conditions based on the comments we
receive.
Background
On May 30, 2012, Bombardier applied
for an amendment to type certificate no.
T00003NY to include the new Model
BD–700–2A12 and BD–700–2A13
airplanes. These airplanes are
derivatives of the Model BD–700 series
of airplanes currently approved under
type certificate no. T00003NY, and are
marketed as the Bombardier Global 7000
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
(Model BD–700–2A12) and Global 8000
(Model BD–700–2A13). These airplanes
are ultra-long-range, executive-interior
business jets.
Type Certification Basis
Under the provisions of Title 14, Code
of Federal Regulations (14 CFR) 21.101,
Bombardier must show that the Model
BD–700–2A12 and BD–700–2A13
airplanes meet the applicable provisions
of the regulations listed in type
certificate no. T00003NY, 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
(i.e., 14 CFR part 25) do not contain
adequate or appropriate safety standards
for the BD–700–2A12 and BD–700–
2A13 airplanes 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 Model BD–700–2A12
and BD–700–2A13 airplanes must
comply with the fuel-vent and 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.
Novel or Unusual Design Features
The Model BD–700–2A12 and BD–
700–2A13 airplanes will incorporate the
following novel or unusual design
feature:
Digital systems architecture composed
of several connected data networks.
This network architecture and
configuration may be used for, or
interfaced with, a diverse set of
functions, including:
• Flight-safety-related control,
communication, and navigation systems
(airplane-control domain);
E:\FR\FM\22AUR1.SGM
22AUR1
Federal Register / Vol. 81, No. 162 / Monday, August 22, 2016 / Rules and Regulations
• Operation and administrative
support (operator-information-services
domain); and
• Passenger information and
entertainment systems (passengerentertainment domain).
In addition, this digital systems
architecture will have the capability to
allow access to or by external network
sources.
Discussion
The Model BD–700–2A12 and BD–
700–2A13 airplane digital systems
network architecture is different from
existing production (and retrofitted)
airplanes as it allows new kinds of user
access to previously isolated data
networks connected to systems that
perform functions required for the safe
operation of the airplane. This proposed
data-network design and integration
may result in security vulnerabilities
from intentional or unintentional
corruption of data and systems critical
to the safety and maintenance of the
airplane.
The existing regulations and guidance
material did not anticipate these types
of system architectures or access to
airplane systems. Furthermore, 14 CFR
regulations, and current system safetyassessment policy and techniques, do
not address potential security
vulnerabilities that could be caused by
unauthorized access to airplane data
busses and servers. Therefore, these
special conditions are issued to ensure
that the security, integrity, and
availability of airplane systems are not
compromised by certain wired or
wireless electronic connections between
airplane data busses and networks.
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.
Lhorne on DSK30JT082PROD with RULES
Applicability
As discussed above, these special
conditions are applicable to the Model
BD–700–2A12 and BD–700–2A13
airplanes. Should Bombardier 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 the other model as well.
Conclusion
This action affects only certain novel
or unusual design features on
Bombardier Model BD–700–2A12 and
BD–700–2A13 airplanes. It is not a rule
of general applicability.
The substance of these special
conditions has been subjected to the
VerDate Sep<11>2014
15:11 Aug 19, 2016
Jkt 238001
56475
notice and comment period in several
prior instances and has been derived
without substantive change from those
previously issued. It is unlikely that
prior public comment would result in a
significant change from the substance
contained herein. Therefore, the FAA
has determined that prior public notice
and comment are unnecessary, and good
cause exists for adopting these special
conditions upon publication in the
Federal Register.
The FAA is requesting comments to
allow interested persons to submit
views that may not have been submitted
in response to the prior opportunities
for comment described above.
DEPARTMENT OF TRANSPORTATION
List of Subjects in 14 CFR Part 25
SUMMARY:
Aircraft, Aviation safety, Reporting
and recordkeeping requirements.
The authority citation for these
special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 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 typecertification basis for the Bombardier
Inc. Model BD–700–2A12 and BD–700–
2A13 airplanes.
1. The applicant must ensure that the
design provides isolation from, or
airplane electronic system security
protection against, access by
unauthorized sources internal to the
airplane. The design must prevent
inadvertent and malicious changes to,
and all adverse impacts upon, airplane
equipment, systems, networks, or other
assets required for safe flight and
operations.
2. The applicant must establish
appropriate procedures to allow the
operator to ensure that continued
airworthiness of the airplane is
maintained, including all post type
certification modifications that may
have an impact on the approved
electronic system security safeguards.
Issued in Renton, Washington, on August
11, 2016.
Paul Bernado,
Acting Manager, Transport Airplane
Directorate Aircraft Certification Service.
[FR Doc. 2016–19994 Filed 8–19–16; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2016–8029; Special
Conditions No. 25–634–SC]
Special Conditions: Garmin
International, Beechcraft Corporation
Model 400A Airplanes; Airplane
Electronic-System Security Protection
From Unauthorized External Access
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for the Beechcraft Corporation
(Beechcraft) Model 400A airplane. This
airplane, as modified by Garmin
International (Garmin), will have a
novel or unusual design feature when
compared to the state of technology
envisioned in the airworthiness
standards for transport-category
airplanes. These airplanes will have a
digital-systems network architecture
composed of several connected
networks that may allow access to or by
external computer systems and
networks, and may otherwise result in
airplane electronic-system security
vulnerabilities without appropriate
protection. 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
Garmin on August 22, 2016. We must
receive your comments by October 6,
2016.
ADDRESSES: Send comments identified
by docket number FAA–2016–8029
using any of the following methods:
• Federal eRegulations Portal: Go to
https://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.
E:\FR\FM\22AUR1.SGM
22AUR1
Agencies
[Federal Register Volume 81, Number 162 (Monday, August 22, 2016)]
[Rules and Regulations]
[Pages 56474-56475]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-19994]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2015-6359; Special Conditions No. 25-633-SC]
Special Conditions: Bombardier Inc. Model BD-700-2A12 and BD-700-
2A13 Airplanes; Airplane Electronic-System Security Protection From
Authorized Internal Access
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Bombardier Inc.
(Bombardier) Model BD-700-2A12 and BD-700-2A13 airplanes. These
airplanes will have novel or unusual design features, specifically,
digital systems architecture composed of several connected data
networks that will have the capability to allow connectivity of the
passenger-service computer systems to the airplane critical systems and
data networks. 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 Bombardier on August 22, 2016. We
must receive your comments by October 6, 2016.
ADDRESSES: Send comments identified by docket number FAA-2015-6359
using any of the following methods:
Federal eRegulations Portal: Go to https://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.
Privacy: The FAA will post all comments it receives, without
change, to https://www.regulations.gov/, including any personal
information the commenter provides. Using the search function of the
docket Web site, anyone can find and read the electronic form of all
comments received into any FAA docket, including the name of the
individual sending the comment (or signing the comment for an
association, business, labor union, etc.). DOT's complete Privacy Act
Statement can be found in the Federal Register published on April 11,
2000 (65 FR 19477-19478), as well as at https://DocketsInfo.dot.gov/ gov/.
Docket: Background documents or comments received may be read at
https://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: Varun Khanna, FAA, Airplane and Flight
Crew Interface, ANM-111, Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-
3356; telephone 425-227-1298; facsimile 425-227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite 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.
We will consider all comments we receive on or before the closing
date for comments. We may change these special conditions based on the
comments we receive.
Background
On May 30, 2012, Bombardier applied for an amendment to type
certificate no. T00003NY to include the new Model BD-700-2A12 and BD-
700-2A13 airplanes. These airplanes are derivatives of the Model BD-700
series of airplanes currently approved under type certificate no.
T00003NY, and are marketed as the Bombardier Global 7000 (Model BD-700-
2A12) and Global 8000 (Model BD-700-2A13). These airplanes are ultra-
long-range, executive-interior business jets.
Type Certification Basis
Under the provisions of Title 14, Code of Federal Regulations (14
CFR) 21.101, Bombardier must show that the Model BD-700-2A12 and BD-
700-2A13 airplanes meet the applicable provisions of the regulations
listed in type certificate no. T00003NY, 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 (i.e., 14 CFR part 25) do not contain adequate or
appropriate safety standards for the BD-700-2A12 and BD-700-2A13
airplanes 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 Model BD-700-2A12 and BD-700-2A13 airplanes must comply
with the fuel-vent and 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 Model BD-700-2A12 and BD-700-2A13 airplanes will incorporate
the following novel or unusual design feature:
Digital systems architecture composed of several connected data
networks. This network architecture and configuration may be used for,
or interfaced with, a diverse set of functions, including:
Flight-safety-related control, communication, and
navigation systems (airplane-control domain);
[[Page 56475]]
Operation and administrative support (operator-
information-services domain); and
Passenger information and entertainment systems
(passenger-entertainment domain).
In addition, this digital systems architecture will have the
capability to allow access to or by external network sources.
Discussion
The Model BD-700-2A12 and BD-700-2A13 airplane digital systems
network architecture is different from existing production (and
retrofitted) airplanes as it allows new kinds of user access to
previously isolated data networks connected to systems that perform
functions required for the safe operation of the airplane. This
proposed data-network design and integration may result in security
vulnerabilities from intentional or unintentional corruption of data
and systems critical to the safety and maintenance of the airplane.
The existing regulations and guidance material did not anticipate
these types of system architectures or access to airplane systems.
Furthermore, 14 CFR regulations, and current system safety-assessment
policy and techniques, do not address potential security
vulnerabilities that could be caused by unauthorized access to airplane
data busses and servers. Therefore, these special conditions are issued
to ensure that the security, integrity, and availability of airplane
systems are not compromised by certain wired or wireless electronic
connections between airplane data busses and networks.
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
Model BD-700-2A12 and BD-700-2A13 airplanes. Should Bombardier 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 the other model as well.
Conclusion
This action affects only certain novel or unusual design features
on Bombardier Model BD-700-2A12 and BD-700-2A13 airplanes. It is not a
rule of general applicability.
The substance of these special conditions has been subjected to the
notice and comment period in several prior instances and has been
derived without substantive change from those previously issued. It is
unlikely that prior public comment would result in a significant change
from the substance contained herein. Therefore, the FAA has determined
that prior public notice and comment are unnecessary, and good cause
exists for adopting these special conditions upon publication in the
Federal Register.
The FAA is requesting comments to allow interested persons to
submit views that may not have been submitted in response to the prior
opportunities for comment described above.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 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 the Bombardier Inc. Model BD-700-2A12
and BD-700-2A13 airplanes.
1. The applicant must ensure that the design provides isolation
from, or airplane electronic system security protection against, access
by unauthorized sources internal to the airplane. The design must
prevent inadvertent and malicious changes to, and all adverse impacts
upon, airplane equipment, systems, networks, or other assets required
for safe flight and operations.
2. The applicant must establish appropriate procedures to allow the
operator to ensure that continued airworthiness of the airplane is
maintained, including all post type certification modifications that
may have an impact on the approved electronic system security
safeguards.
Issued in Renton, Washington, on August 11, 2016.
Paul Bernado,
Acting Manager, Transport Airplane Directorate Aircraft Certification
Service.
[FR Doc. 2016-19994 Filed 8-19-16; 8:45 am]
BILLING CODE 4910-13-P