Special Conditions: Learjet Model 45 Series Airplanes; Isolation or Security Protection of the Aircraft Control Domain and the Airline Information Services Domain From the Passenger Services Domain, 65155-65156 [2013-25851]
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Federal Register / Vol. 78, No. 211 / Thursday, October 31, 2013 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2013–0919; Special
Conditions No. 25–13–11–SC]
Special Conditions: Learjet Model 45
Series Airplanes; Isolation or Security
Protection of the Aircraft Control
Domain and the Airline Information
Services Domain From the Passenger
Services Domain
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special condition; request
for comments.
AGENCY:
These special conditions are
issued for the Learjet Model 45 series
airplanes. These airplanes will have
novel or unusual design features
associated with 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: The effective date of these
special conditions is October 31, 2013.
We must receive your comments by
December 16, 2013.
ADDRESSES: Send comments identified
by docket number FAA–2013–0919
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
wreier-aviles on DSK5TPTVN1PROD with RULES
SUMMARY:
VerDate Mar<15>2010
15:19 Oct 30, 2013
Jkt 232001
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 the 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 Branch, 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: The FAA
has determined that notice of, and
opportunity for prior public comment
on, these special conditions are
impracticable because these procedures
would significantly delay issuance of
the design approval and thus delivery of
the affected aircraft. In addition, the
substance of these special conditions
has been subject to the public comment
process in several prior instances with
no substantive comments received. The
FAA therefore finds that good cause
exists for making these special
conditions effective upon publication in
the Federal Register.
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 by the closing date for
comments. We may change these special
conditions based on the comments we
receive.
Background
On April 21, 2010, Learjet applied for
both a change to Type Certificate No.
T00008WI and for a supplemental type
certificate (STC) change in the digital
systems architecture in the Learjet
Model 45 series airplanes. The Learjet
Model No. 45 series airplanes are a
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
65155
swept-wing aircraft equipped with two
Honeywell TFE731–40BR turbojet
engines, weighing 13,890 pounds empty
and capable of carrying up to nine
passengers plus two crew members.
The proposed Learjet Model 45
architecture is new and novel for
commercial transport airplanes by
allowing connection to previously
isolated data networks connected to
systems that perform functions required
for the safe operation of the airplane.
This proposed data network and design
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 this type of
system architecture or electronic access
to aircraft systems. Furthermore,
regulations and current system safety
assessment policy and techniques do
not address potential security
vulnerabilities, which could be caused
by unauthorized access to aircraft data
buses and servers. The intent of these
special conditions is to ensure that
security, integrity, and availability of
aircraft systems are not compromised by
certain wired or wireless electronic
connections between airplane data
busses and networks. A separate Learjet
Model 45 project special condition
addresses aircraft electronic system
security protection from unauthorized
external access.
Type Certification Basis
Under Title 14, Code of Federal
Regulations (14 CFR) 21.17, Learjet must
show that the Model 45 series meets the
applicable provisions of 14 CFR part 25,
as amended by Amendments 25–1
through 25–128.
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 Model 45 series because of a
novel or unusual design feature, special
conditions are prescribed under § 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, the proposed special
conditions would also apply to the other
model under § 21.101.
In addition to the applicable
airworthiness regulations and proposed
special conditions, the Learjet Model 45
series airplane must comply with the
fuel vent and exhaust emission
requirements of 14 CFR part 34 and the
noise certification requirements of 14
E:\FR\FM\31OCR1.SGM
31OCR1
65156
Federal Register / Vol. 78, No. 211 / Thursday, October 31, 2013 / Rules and Regulations
CFR part 36 and the FAA must issue a
finding of regulatory adequacy under
§ 611 of Public Law 92–574, the ‘‘Noise
Control Act of 1972.’’
The FAA issues special conditions, as
defined in 14 CFR 11.19, under § 11.38,
and they become part of the typecertification basis under § 21.17(a)(2).
wreier-aviles on DSK5TPTVN1PROD with RULES
Novel or Unusual Design Features
The Learjet Model 45 series airplanes
will incorporate the following novel or
unusual design features: The proposed
architecture and network configuration
may be used for, or interfaced with, a
diverse set of functions, including:
1. Flight-safety related control,
communication, and navigation systems
(aircraft control domain);
2. Operator business and
administrative support (operator
information domain); and
3. Passenger information and
entertainment systems (passenger
entertainment domain).
In addition, the operating systems
(OS) for current aircraft systems are
usually and historically proprietary.
Therefore, they are not as susceptible to
corruption from worms, viruses, and
other malicious actions as more widely
used commercial operating systems,
such as Microsoft Windows NT, because
access to the design details of these
proprietary OS is limited to the system
developer and aircraft integrator. Some
systems installed on the Learjet Model
45 series airplanes will use operating
systems that are widely used and
commercially available from third party
software suppliers. The security
vulnerabilities of these operating
systems may be more widely known
than proprietary operating systems
currently used by avionics
manufacturers.
Discussion
The integrated network configurations
in the Learjet Model 45 series airplanes
may allow increased connectivity with
external network sources and will have
more interconnected networks and
systems, such as passenger
entertainment and information services
than previous airplane models. This
may allow the exploitation of network
security vulnerabilities and increased
risks potentially resulting in unsafe
conditions for the airplanes and
occupants. This potential exploitation of
security vulnerabilities may result in
intentional or unintentional destruction,
disruption, degradation, or exploitation
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. Furthermore, 14
VerDate Mar<15>2010
15:19 Oct 30, 2013
Jkt 232001
CFR regulations and current system
safety assessment policy and techniques
do not address potential security
vulnerabilities which could be exploited
by unauthorized access to airplane
networks and servers. Therefore, these
special conditions are being issued to
ensure that the security (i.e.,
confidentiality, integrity, and
availability) of airplane systems is not
compromised by unauthorized wired or
wireless electronic connections between
airplane systems and the passenger
entertainment services.
For the reasons discussed above, 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 Learjet
Model 45 series airplanes. Should
Learjet apply at a later date for a change
to the type certificate to include another
model incorporating the same novel or
unusual design feature, the special
conditions would apply to that model as
well.
Conclusion
This action affects only certain novel
or unusual design features on one model
series of 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, because a
delay would significantly affect the
certification of the airplane, which is
imminent, the FAA has determined that
prior public notice and comment are
unnecessary and impracticable, 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.
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
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 Learjet Model 45
series airplanes.
Isolation or Security Protection of the
Aircraft Control Domain and the Airline
Information Services Domain From the
Passenger Services Domain
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 aircraft is
maintained, including all post-typecertification modifications that may
have an impact on the approved
electronic system security safeguards.
Issued in Renton, Washington, on October
22, 2013.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2013–25851 Filed 10–30–13; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2013–0820; Notice No.
25–499–SC]
Special Conditions: Bombardier Inc.,
Models BD–500–1A10 and BD–500–
1A11 Series Airplanes; Interactions of
Systems and Structures
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for the Bombardier Inc. Models
BD–500–1A10 and BD–500–1A11 series
airplanes. These airplanes will have
novel or unusual features when
compared to the state of technology
envisioned in the airworthiness
standards for transport category
airplanes. These design features include
systems that, directly or as a result of
SUMMARY:
E:\FR\FM\31OCR1.SGM
31OCR1
Agencies
[Federal Register Volume 78, Number 211 (Thursday, October 31, 2013)]
[Rules and Regulations]
[Pages 65155-65156]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-25851]
[[Page 65155]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2013-0919; Special Conditions No. 25-13-11-SC]
Special Conditions: Learjet Model 45 Series Airplanes; Isolation
or Security Protection of the Aircraft Control Domain and the Airline
Information Services Domain From the Passenger Services Domain
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special condition; request for comments.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Learjet Model 45
series airplanes. These airplanes will have novel or unusual design
features associated with 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: The effective date of these special conditions is October 31,
2013. We must receive your comments by December 16, 2013.
ADDRESSES: Send comments identified by docket number FAA-2013-0919
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/.
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 the 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 Branch, 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: The FAA has determined that notice of, and
opportunity for prior public comment on, these special conditions are
impracticable because these procedures would significantly delay
issuance of the design approval and thus delivery of the affected
aircraft. In addition, the substance of these special conditions has
been subject to the public comment process in several prior instances
with no substantive comments received. The FAA therefore finds that
good cause exists for making these special conditions effective upon
publication in the Federal Register.
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 by the closing date for
comments. We may change these special conditions based on the comments
we receive.
Background
On April 21, 2010, Learjet applied for both a change to Type
Certificate No. T00008WI and for a supplemental type certificate (STC)
change in the digital systems architecture in the Learjet Model 45
series airplanes. The Learjet Model No. 45 series airplanes are a
swept-wing aircraft equipped with two Honeywell TFE731-40BR turbojet
engines, weighing 13,890 pounds empty and capable of carrying up to
nine passengers plus two crew members.
The proposed Learjet Model 45 architecture is new and novel for
commercial transport airplanes by allowing connection to previously
isolated data networks connected to systems that perform functions
required for the safe operation of the airplane. This proposed data
network and design 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 this type of
system architecture or electronic access to aircraft systems.
Furthermore, regulations and current system safety assessment policy
and techniques do not address potential security vulnerabilities, which
could be caused by unauthorized access to aircraft data buses and
servers. The intent of these special conditions is to ensure that
security, integrity, and availability of aircraft systems are not
compromised by certain wired or wireless electronic connections between
airplane data busses and networks. A separate Learjet Model 45 project
special condition addresses aircraft electronic system security
protection from unauthorized external access.
Type Certification Basis
Under Title 14, Code of Federal Regulations (14 CFR) 21.17, Learjet
must show that the Model 45 series meets the applicable provisions of
14 CFR part 25, as amended by Amendments 25-1 through 25-128.
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 Model 45 series because of a novel
or unusual design feature, special conditions are prescribed under
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, the proposed special conditions would also
apply to the other model under Sec. 21.101.
In addition to the applicable airworthiness regulations and
proposed special conditions, the Learjet Model 45 series airplane must
comply with the fuel vent and exhaust emission requirements of 14 CFR
part 34 and the noise certification requirements of 14
[[Page 65156]]
CFR part 36 and the FAA must issue a finding of regulatory adequacy
under Sec. 611 of Public Law 92-574, the ``Noise Control Act of
1972.''
The FAA issues special conditions, as defined in 14 CFR 11.19,
under Sec. 11.38, and they become part of the type-certification basis
under Sec. 21.17(a)(2).
Novel or Unusual Design Features
The Learjet Model 45 series airplanes will incorporate the
following novel or unusual design features: The proposed architecture
and network configuration may be used for, or interfaced with, a
diverse set of functions, including:
1. Flight-safety related control, communication, and navigation
systems (aircraft control domain);
2. Operator business and administrative support (operator
information domain); and
3. Passenger information and entertainment systems (passenger
entertainment domain).
In addition, the operating systems (OS) for current aircraft
systems are usually and historically proprietary. Therefore, they are
not as susceptible to corruption from worms, viruses, and other
malicious actions as more widely used commercial operating systems,
such as Microsoft Windows NT, because access to the design details of
these proprietary OS is limited to the system developer and aircraft
integrator. Some systems installed on the Learjet Model 45 series
airplanes will use operating systems that are widely used and
commercially available from third party software suppliers. The
security vulnerabilities of these operating systems may be more widely
known than proprietary operating systems currently used by avionics
manufacturers.
Discussion
The integrated network configurations in the Learjet Model 45
series airplanes may allow increased connectivity with external network
sources and will have more interconnected networks and systems, such as
passenger entertainment and information services than previous airplane
models. This may allow the exploitation of network security
vulnerabilities and increased risks potentially resulting in unsafe
conditions for the airplanes and occupants. This potential exploitation
of security vulnerabilities may result in intentional or unintentional
destruction, disruption, degradation, or exploitation 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. Furthermore, 14 CFR regulations and
current system safety assessment policy and techniques do not address
potential security vulnerabilities which could be exploited by
unauthorized access to airplane networks and servers. Therefore, these
special conditions are being issued to ensure that the security (i.e.,
confidentiality, integrity, and availability) of airplane systems is
not compromised by unauthorized wired or wireless electronic
connections between airplane systems and the passenger entertainment
services.
For the reasons discussed above, 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
Learjet Model 45 series airplanes. Should Learjet apply at a later date
for a change to the type certificate to include another model
incorporating the same novel or unusual design feature, the special
conditions would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
on one model series of 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, because a delay would
significantly affect the certification of the airplane, which is
imminent, the FAA has determined that prior public notice and comment
are unnecessary and impracticable, 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 Learjet Model 45 series airplanes.
Isolation or Security Protection of the Aircraft Control Domain and the
Airline Information Services Domain From the Passenger Services Domain
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 aircraft 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 October 22, 2013.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-25851 Filed 10-30-13; 8:45 am]
BILLING CODE 4910-13-P