[Federal Register Volume 83, Number 125 (Thursday, June 28, 2018)]
[Rules and Regulations]
[Pages 30316-30317]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-13948]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2018-0602; Special Conditions No. 25-729-SC]
Special Conditions: Airbus Model A318, A319, A320 and A321 Series
Airplanes; Electronic System Security Protection From Unauthorized
Internal Access
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
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SUMMARY: These special conditions are issued for the Airbus Model A318,
A319, A320 and A321 series airplanes. These airplanes 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 airplane electronic systems and
networks that allow access, from aircraft internal sources (e.g.,
wireless devices, internet connectivity), to the airplane's previously
isolated, internal, electronic components. 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 Airbus on June 28, 2018. Send
comments on or before August 13, 2018.
ADDRESSES: Send comments identified by Docket No. FAA-2018-0602 using
any of the following methods:
Federal eRegulations Portal: Go to http://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 http://www.regulations.gov/, including any personal
information the commenter provides. Using the search function of the
docket website, 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).
Docket: Background documents or comments received may be read at
http://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, Airplane and Flight Crew
Interface Section, AIR-671, Transport Standards Branch, Policy and
Innovation Division, Aircraft Certification Service, Federal Aviation
Administration, 2200 South 216th Street, Des Moines, Washington 98198;
telephone and fax 206-231-3159; email [email protected].
SUPPLEMENTARY INFORMATION: The substance of these special conditions
previously has been published in the Federal Register for public
comment. These special conditions have 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 finds that, for the same
reason, good cause exists for adopting these special conditions 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.
[[Page 30317]]
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 February 2, 2017, Airbus applied for a change to Type
Certificate No. A28NM for the installation of electronic network system
architecture or Flight Operations and Maintenance Exchanger (FOMAX)
equipment in the Model A318, A319, A320 and A321 series airplanes. The
Airbus Model A318, A319, A320 and A321 series airplanes are twin-
engine, transport category airplanes with a passenger seating capacity
of 136 to 230 and a maximum takeoff weight of 123,458 to 213,848
pounds, depending on the specific design.
Type Certification Basis
Under the provisions of title 14, Code of Federal Regulations (14
CFR) 21.101, Airbus must show that the Model A318, A319, A320 and A321
series airplanes as changed, continue to meet the applicable provisions
of the regulations listed in Type Certificate No. A28NM 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 Airbus Model A318, A319, A320 and
A321 series 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 Airbus Model A318, A319, A320 and A321 series 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 Airbus Model A318, A319, A320 and A321 series airplanes will
incorporate the following novel or unusual design feature:
The installation and activation of electronic network system
architecture or Flight Operations and Maintenance Exchanger (FOMAX)
equipment that allows access from internal sources (e.g., wireless
devices, internet connectivity) to the airplane's once isolated
internal electronic components.
Discussion
The Airbus Model A318, A319, A320 and A321 series airplanes
architecture is novel or unusual for commercial transport airplanes
because it allows connection to previously isolated data networks
connected to systems that perform functions required for the safe
operation of the airplane. This 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, 14 CFR regulations and the 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 to ensure that the security of airplane systems and
networks is not compromised by unauthorized wired or wireless internal
access.
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 A318, A319, A320 and A321 series airplanes. Should Airbus 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 Airbus Model A318, A319, A320 and A321 series airplanes. 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,
44704.
The Special Conditions
0
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 Airbus Model A318, A319, A320 and A321
series 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 aircraft is
maintained, including all post type certification modifications that
may have an impact on the approved electronic system security
safeguards.
Issued in Des Moines, Washington, on June 25, 2018.
Victor Wicklund,
Manager, Transport Standards Branch, Policy and Innovation Division,
Aircraft Certification Service.
[FR Doc. 2018-13948 Filed 6-27-18; 8:45 am]
BILLING CODE 4910-13-P