23 June 2011. Two notices.
Aircraft Protection Against Electronic Hi-jack
[Federal Register Volume 76, Number 121 (Thursday, June 23, 2011)]
[Rules and Regulations]
[Pages 36861-36862]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-15705]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM447; Special Conditions No. 25-436-SC]
Special Conditions: Gulfstream Model GVI Airplane; Electronic
Systems Security Isolation or Protection From Unauthorized Passenger
Systems Access
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
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SUMMARY: These special conditions are issued for the Gulfstream GVI
airplane. This airplane will have novel or unusual design features
associated with connectivity of the passenger domain computer systems
to the airplane
[[Page 36862]]
critical systems and data networks. The applicable airworthiness
regulations do not contain adequate or appropriate safety standards for
these design features. 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: Effective Date: July 25, 2011.
FOR FURTHER INFORMATION CONTACT: Will Struck, FAA, Airplane and Flight
Crew Interface Branch, ANM-111, Transport Standards Staff, Transport
Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue,
SW., Renton, Washington 98055-4056; telephone (425) 227-2764; facsimile
(425) 227-1320.
SUPPLEMENTARY INFORMATION:
Background
On March 29, 2005, Gulfstream Aerospace Corporation (hereafter
referred to as ``Gulfstream'') applied for an FAA type certificate for
its new Gulfstream Model GVI passenger airplane. Gulfstream later
applied for, and was granted, an extension of time for the type
certificate, which changed the effective application date to September
28, 2006. The Gulfstream Model GVI airplane will be an all-new, two-
engine jet transport airplane. The maximum takeoff weight will be
99,600 pounds, with a maximum passenger count of 19 passengers.
Type Certification Basis
Under provisions of Title 14, Code of Federal Regulations (14 CFR)
21.17, Gulfstream must show that the Gulfstream Model GVI airplane
(hereafter referred to as ``the GVI'') meets the applicable provisions
of 14 CFR part 25, as amended by Amendments 25-1 through 25-119, 25-
122, and 25-124. 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 GVI 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 features, the special conditions would also apply to the
other model under provisions of Sec. 21.101.
In addition to complying with the applicable airworthiness
regulations and special conditions, the GVI 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 must also issue a
finding of regulatory adequacy pursuant to section 611 of Public Law
92-574, the ``Noise Control Act of 1972.''
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. 21.17(a)(2).
Novel or Unusual Design Features
The Gulfstream Model GVI airplane will incorporate the following
novel or unusual design features: Digital systems architecture composed
of several connected networks. 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. Airline business and administrative support (airline information
domain),
3. Passenger information and entertainment systems (passenger
entertainment domain), and
4. The capability to allow access to or by external sources.
Discussion
The GVI integrated network configuration 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 Gulfstream airplane models.
This may allow the exploitation of network security vulnerabilities and
increase risks potentially resulting in unsafe conditions for the
airplane and its 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 and a means of
compliance 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 networks and the passenger
entertainment domain.
Discussion of Comments
Notice of proposed special conditions No. 25-11-06-SC for
Gulfstream GVI airplanes was published in the Federal Register on
February 25, 2011 (76 FR 10528). Only one comment was received, which
was supportive, so these special conditions are adopted as proposed.
Applicability
As discussed above, these special conditions are applicable to the
Gulfstream Model GVI airplane. Should Gulfstream apply at a later date
for a change to the type certificate to include another model
incorporating the same novel or unusual design features, these special
conditions would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
of the GVI. It is not a rule of general applicability.
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 Condition
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special condition is issued as part of the
type certification basis for Gulfstream GVI airplanes.
The design must isolate or provide protection from any
inadvertent or malicious change to, and any adverse effect on any
systems, software, or data in the aircraft control domain or airline
information domain from any point within the passenger entertainment
domain.
Issued in Renton, Washington, on June 13, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-15705 Filed 6-22-11; 8:45 am]
BILLING CODE 4910-13-P
[Federal Register Volume 76, Number 121 (Thursday, June 23, 2011)]
[Rules and Regulations]
[Pages 36863-36864]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-15706]
[[Page 36863]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM448; Special Conditions No. 25-437-SC]
Special Conditions: Gulfstream Model GVI Airplane; Electronic
Systems Security Protection From Unauthorized External Access
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Gulfstream GVI
airplane. This airplane will have novel or unusual design features
associated with the architecture and connectivity capabilities of the
airplane's computer systems and networks, which may allow access by
external computer systems and networks. Connectivity by external
systems and networks may result in security vulnerabilities to the
airplane's systems. The applicable airworthiness regulations do not
contain adequate or appropriate safety standards for these design
features. 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: Effective Date: July 25, 2011.
FOR FURTHER INFORMATION CONTACT: Will Struck, FAA, Airplane and Flight
Crew Interface Branch, ANM-111, Transport Standards Staff, Transport
Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue,
SW., Renton, Washington 98055-4056; telephone (425) 227-2764; facsimile
(425) 227-1320.
SUPPLEMENTARY INFORMATION:
Background
On March 29, 2005, Gulfstream Aerospace Corporation (hereafter
referred to as ``Gulfstream'') applied for an FAA type certificate for
its new Gulfstream Model GVI passenger airplane. Gulfstream later
applied for, and was granted, an extension of time for the type
certificate, which changed the effective application date to September
28, 2006. The Gulfstream Model GVI airplane will be an all-new, two-
engine jet transport airplane. The maximum takeoff weight will be
99,600 pounds, with a maximum passenger count of 19 passengers.
Type Certification Basis
Under provisions of Title 14, Code of Federal Regulations (14 CFR)
21.17, Gulfstream must show that the Gulfstream Model GVI airplane
(hereafter referred to as ``the GVI'') meets the applicable provisions
of 14 CFR part 25, as amended by Amendments 25-1 through 25-119, 25-
122, and 25-124. 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 GVI 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 features, the special conditions would also apply to the
other model under provisions of Sec. 21.101.
In addition to complying with the applicable airworthiness
regulations and special conditions, the GVI 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 must also issue a
finding of regulatory adequacy pursuant to section 611 of Public Law
92-574, the ``Noise Control Act of 1972.''
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. 21.17(a)(2).
Novel or Unusual Design Features
The Gulfstream Model GVI airplane will incorporate the following
novel or unusual design features: Digital systems architecture composed
of several connected networks. 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. Airline business and administrative support (airline information
domain),
3. Passenger information and entertainment systems (passenger
entertainment domain), and
4. The capability to allow access to or by external sources.
Discussion
The proposed Model GVI architecture and network configuration may
allow increased connectivity to and access by external airplane sources
and airline operations and maintenance systems to the aircraft control
domain and airline information domain. The aircraft control domain and
airline information domain perform functions required for the safe
operation and maintenance of the airplane. Previously these domains had
very limited connectivity with external sources.
The architecture and network configuration may allow the
exploitation of network security vulnerabilities resulting in
intentional or unintentional destruction, disruption, degradation, or
exploitation of data, systems, and networks critical to the safety and
maintenance of the airplane.
The existing regulations and guidance material did not anticipate
these types of airplane 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 systems, data buses, and
servers. Therefore, these special conditions and a means of compliance
are 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.
Discussion of Comments
Notice of proposed special conditions No. 25-11-05-SC for
Gulfstream GVI airplanes was published in the Federal Register on
February 25, 2011 (76 FR 10529). Only one comment was received, which
was supportive, so this special condition is adopted as proposed.
Applicability
As discussed above, these special conditions are applicable to the
Gulfstream Model GVI airplane. Should Gulfstream apply at a later date
for a change to the type certificate to include another model
incorporating the same novel or unusual design features, these special
conditions would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
of the GVI. It is not a rule of general applicability.
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 Condition
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special condition is issued as part of the
type
[[Page 36864]]
certification basis for Gulfstream GVI airplanes.
1. The applicant must ensure electronic system security protection
for the aircraft control domain and airline information domain from
access by unauthorized sources external to the airplane, including
those possibly caused by maintenance activity.
2. The applicant must ensure that electronic system security
threats from external sources are identified and assessed, and that
effective electronic system security protection strategies are
implemented to protect the airplane from all adverse impacts on safety,
functionality, and continued airworthiness.
Issued in Renton, Washington, on June 13, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-15706 Filed 6-22-11; 8:45 am]
BILLING CODE 4910-13-P
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