Special Conditions: Dassault Falcon Fan Jet, Fan Jet Series D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and Mystere-Falcon 200 Airplanes; High-Intensity Radiated Fields (HIRF), 20933-20935 [E7-8112]
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20933
Rules and Regulations
Federal Register
Vol. 72, No. 81
Friday April 27, 2007
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. Prices of
new books are listed in the first FEDERAL
REGISTER issue of each week.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM377; Special Conditions No.
25–353–SC]
Special Conditions: Dassault Falcon
Fan Jet, Fan Jet Series D, Series E,
Series F, Mystere-Falcon 20–C5, 20–
D5, 20–E5, 20–F5, and Mystere-Falcon
200 Airplanes; High-Intensity Radiated
Fields (HIRF)
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
cprice-sewell on PROD1PC66 with RULES
AGENCY:
SUMMARY: These special conditions are
issued for Dassault Falcon Fan Jet, Fan
Jet Series D, Series E, Series F, MystereFalcon 20–C5, 20–D5, 20–E5, 20–F5,
and Mystere-Falcon 200 airplanes
modified by 3S Certification, LLC.
These modified airplanes will have
novel or unusual design features when
compared with the state of technology
envisioned in the airworthiness
standards for transport category
airplanes. The modification installs
Thommen AD 30 Repeater Altimeters
and a Skylight ADC 600 Air Data
Converter Unit. The applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for protecting these systems from effects
of high-intensity radiated fields (HIRF).
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 for these
special conditions is April 20, 2007. We
must receive your comments by June 11,
2007.
ADDRESSES: You may mail or deliver
comments on these special conditions
VerDate Aug<31>2005
15:13 Apr 26, 2007
Jkt 211001
in duplicate to: Federal Aviation
Administration, Transport Airplane
Directorate, Attention: Rules Docket
(ANM–113), Docket No. NM377, 1601
Lind Avenue, SW., Renton, Washington
98057–3356. You must mark your
comments Docket No. NM377. You may
inspect comments in the Rules Docket
weekdays, except Federal holidays,
between 7:30 a.m. and 4 p.m.
FOR FURTHER INFORMATION CONTACT: Greg
Dunn, 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) 227–2799;
facsimile (425) 227–1320.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA has determined that notice
and opportunity for prior public
comment for these special conditions is
impracticable, because these procedures
would significantly delay certification
and 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. We therefore find that good
cause exists for making these special
conditions effective upon issuance.
However, we invite interested persons
to take part in this rulemaking by
submitting written comments. The most
helpful comments reference a specific
portion of the special conditions,
explain the reason for any
recommended change, and include
supporting data. We ask that you send
us two copies of written comments.
We will file in the docket all
comments we receive as well as a report
summarizing each substantive public
contact with FAA personnel about these
special conditions. You may inspect the
docket before and after the comment
closing date. If you wish to review the
docket in person, go to the address in
the ADDRESSES section of this preamble
between 7:30 a.m. and 4 p.m., Monday
through Friday, except Federal holidays.
We will consider all comments we
receive by the closing date for
comments. We will consider comments
filed late if it is possible to do so
without incurring expense or delay. We
may change these special conditions
based on the comments we receive.
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Fmt 4700
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If you want the FAA to acknowledge
receipt of your comments on these
special conditions, include with your
comments a pre-addressed, stamped
postcard on which the docket number
appears. We will stamp the date on the
postcard and mail it back to you.
Background
On December 21, 2006, 3S
Certification, LLC of Nixa, MO, applied
to the Wichita Aircraft Certification
Office for a Supplemental Type
Certificate to modify Dassault Falcon
Fan Jet, Fan Jet Series D, Series E, Series
F, Mystere-Falcon 20–C5, 20–D5, 20–E5,
20–F5, and Mystere-Falcon 200
airplanes approved under Type
Certificate No. A7EU. These are
transport category airplanes powered by
two turbojet engines with maximum
takeoff weights of up to 18,000 pounds.
The airplanes operate with a 2-pilot
crew and can seat up to 8 passengers.
The proposed modification installs
Thommen AD 30 Repeater Altimeters
and a Skylight ADC 600 Air Data
Converter Unit. These systems have a
potential to be vulnerable to HIRF
external to the airplane.
Type Certification Basis
Under provisions of 14 CFR 21.101,
3S Certification, LLC must show that the
Dassault Falcon Fan Jet, Fan Jet Series
D, Series E, Series F, Mystere-Falcon
20–C5, 20–D5, 20–E5, 20–F5, and
Mystere-Falcon 200 airplanes, as
changed, continue to meet the
applicable provisions of the regulations
incorporated by reference in Type
Certificate No. A7EU or the applicable
regulations in effect on the date of
application for the change. The
regulations incorporated by reference in
the type certificate are commonly
referred to as the ‘‘original type
certification basis.’’ The type
certification basis for the modified
Dassault Falcon Fan Jet, Fan Jet Series
D, Series E, and Series F airplanes
includes the applicable paragraphs of
CAR 4b, as amended by Amendments
4b–1 through 4b–12; Special
Regulations SR–422B and 14 CFR part
25 as amended by provisions of
Amendment 25–4 in lieu of CAR
4b.350(e) and (f). The type certification
basis for the Dassault Mystere-Falcon
200 airplanes includes the applicable
paragraphs of CAR 4b, as amended by
Amendments 4b–1 through 4b–12;
E:\FR\FM\27APR1.SGM
27APR1
cprice-sewell on PROD1PC66 with RULES
20934
Federal Register / Vol. 72, No. 81 / Friday April 27, 2007 / Rules and Regulations
Special Regulations SR–422B and 14
CFR part 25 as amended by certain
sections of Amendments 25–1 through
25–46; SFAR 27 as amended by
Amendments 27–1 through 27–3; and
14 CFR part 36 as amended by
Amendments 36–1 through 36–12. The
type certification basis for the Dassault
Mystere-Falcon 20–C5, 20–D5, 20–E5,
and 20–F5 airplanes includes the
applicable paragraphs of CAR 4b, as
amended by Amendments 4b–1 through
4b–12; Special Regulations SR–422B
and 14 CFR part 25 as amended by
certain sections in Amendments 25–1
through 25–56; § 25.904 and Appendix
1 as amended by Amendment 25–62;
SFAR 27 as amended by Amendments
27–1 through 27–6; and 14 CFR part 36
as amended by Amendments 36–1
through 36–15. In addition, the type
certification basis includes certain later
amended sections of the applicable part
25 regulations that are not relevant to
these special conditions.
If the Administrator finds that the
applicable airworthiness regulations
(part 25, as amended) do not contain
adequate or appropriate safety standards
for the Dassault Falcon Fan Jet, Fan Jet
Series D, Series E, Series F, MystereFalcon 20–C5, 20–D5, 20–E5, 20–F5,
and Mystere-Falcon 200 airplanes
because of a novel or unusual design
feature, special conditions are
prescribed under the provisions of
§ 21.16.
In addition to the applicable
airworthiness regulations and special
conditions, the Dassault Falcon Fan Jet,
Fan Jet Series D, Series E, Series F,
Mystere-Falcon 20–C5, 20–D5, 20–E5,
20–F5, and Mystere-Falcon 200
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 § 11.19, under § 11.38, and
they become part of the type
certification basis under the provisions
of § 21.101.
Special conditions are initially
applicable to the model for which they
are issued. Should 3S Certification, LLC
apply later for a supplemental type
certificate to modify any other model
included on Type Certificate No. A7EU,
as applicable, to incorporate the same or
similar novel or unusual design feature,
these special conditions would also
apply to the other model under the
provisions of § 21.101.
Novel or Unusual Design Features
As noted earlier, the Dassault Falcon
Fan Jet, Fan Jet Series D, Series E, Series
F, Mystere-Falcon 20–C5, 20–D5, 20–E5,
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15:13 Apr 26, 2007
Jkt 211001
20–F5, and Mystere-Falcon 200
airplanes modified by 3S Certification,
LLC will incorporate repeater altimeters
and an air data converter unit, that will
perform critical functions. These
systems may be vulnerable to HIRF
external to the airplane. Current
airworthiness standards of part 25 do
not contain adequate or appropriate
safety standards for protecting this
equipment from adverse effects of HIRF.
Therefore, these systems are considered
to be novel or unusual design features.
Discussion
There is no specific regulation that
addresses protection for electrical and
electronic systems from HIRF. Increased
power levels from radio frequency
transmitters and the growing use of
sensitive avionics/electronics and
electrical systems to command and
control airplanes have made it necessary
to provide adequate protection.
To ensure that a level of safety is
achieved equivalent to that intended by
the regulations incorporated by
reference, special conditions are needed
for the Dassault Falcon Fan Jet, Fan Jet
Series D, Series E, Series F, MystereFalcon 20–C5, 20–D5, 20–E5, 20–F5,
and Mystere-Falcon 200 airplanes
modified by 3S Certification, LLC.
These special conditions require that
new avionics/electronics and electrical
systems that perform critical functions
be designed and installed to preclude
component damage and interruption of
function because of HIRF.
High-Intensity Radiated Fields (HIRF)
With the trend toward increased
power levels from ground-based
transmitters, and the advent of space
and satellite communication coupled
with electronic command and control of
the airplane, the immunity of critical
digital avionics/electronics and
electrical systems to HIR must be
established.
It is not possible to precisely define
the HIRF to which the airplane will be
exposed in service. There is also
uncertainly concerning the effectiveness
of airframe shielding for HIRF.
Furthermore, coupling of
electromagnetic energy to cockpitinstalled equipment through the cockpit
window apertures is undefined. Based
on surveys and an analysis of existing
HIRF emitters, an adequate level of
protection exists when compliance with
the HIRF protection special condition is
shown with either paragraph 1 or 2
below:
1. A minimum environment of 100
volts rms (root-mean-square) per meter
electric field strength from 10 KHz to 18
GHz.
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a. System elements and their
associated wiring harnesses must be
exposed to the environment without
benefit of airframe shielding.
b. Demonstration of this level of
protection is established through system
tests and analysis.
2. An environment external to the
airframe of the field strengths shown in
the table below for the frequency ranges
indicated. Immunity to both peak and
average field strength components from
the table must be demonstrated.
Frequency
Field strength
(volts per meter)
Peak
10 kHz–100 kHz .......
100 kHz–500 kHz .....
500 kHz–2 MHz ........
2 MHz–30 MHz .........
30 MHz–70 MHz .......
70 MHz–100 MHz .....
100 MHz–200 MHz ...
200 MHz–400 MHz ...
400 MHz–700 MHz ...
700 MHz–1 GHz .......
1 GHz–2 GHz ...........
2 GHz–4 GHz ...........
4 GHz–6 GHz ...........
6 GHz–8 GHz ...........
8 GHz–12 GHz .........
12 GHz–18 GHz .......
18 GHz–40 GHz .......
50
50
50
100
50
50
100
100
700
700
2000
3000
3000
1000
3000
2000
600
Average
50
50
50
100
50
50
100
100
50
100
200
200
200
200
300
200
200
The field strengths are expressed in terms
of peak of the root-mean-square (rms) over
the complete modulation period.
The environment levels identified
above are the result of an FAA review
of existing studies on the subject of
HIRF and of the work of the
Electromagnetic Effects Harmonization
Working Group of the Aviation
Rulemaking Advisory Committee.
Applicability
These special conditions are
applicable to Dassault Falcon Fan Jet,
Fan Jet Series D, Series E, Series F,
Mystere-Falcon 20–C5, 20–D5, 20–E5,
20–F5, and Mystere-Falcon 200
airplanes modified by 3S Certification,
LLC. Should 3S Certification, LLC apply
later for a supplemental type certificate
to modify any other model included on
Type Certificate No. A7EU to
incorporate the same or similar novel or
unusual design feature, these special
conditions would apply to that model as
well under provisions of § 21.101.
Conclusion
This action affects only certain novel
or unusual design features on Dassault
Falcon Fan Jet, Fan Jet Series D, Series
E, Series F, Mystere-Falcon 20–C5, 20–
D5, 20–E5, 20–F5, and Mystere-Falcon
200 airplanes modified by 3S
Certification, LLC. It is not a rule of
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27APR1
Federal Register / Vol. 72, No. 81 / Friday April 27, 2007 / Rules and Regulations
general applicability and affects only
the applicant which applied to the FAA
for approval of these design features on
the airplane.
The substance of the special
conditions for these airplanes has been
subjected to the notice and comment
procedure in several prior instances and
has been derived without substantive
change from those previously issued.
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
immediately. The FAA is requesting
comments to allow interested people to
submit views that may not have been
submitted in response to the prior
opportunities for comment.
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
cprice-sewell on PROD1PC66 with RULES
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the following special
conditions are issued as part of the
supplemental type certification basis for
the Dassault Falcon Fan Jet, Fan Jet
Series D, Series E, Series F, MystereFalcon 20–C5, 20–D5, 20–E5, 20–F5,
and Mystere-Falcon 200 airplanes
modified by 3S Certification, LLC.
1. Protection From Unwanted Effects
of High-Intensity Radiated Fields
(HIRF).
Each electrical and electronic system
that performs critical functions must be
designed and installed to ensure that the
operation and operational capability of
these systems to perform critical
functions are not adversely affected
when the airplane is exposed to highintensity radiated fields.
2. For the purpose of these special
conditions, the following definition
applies: Critical Functions: Functions
whose failure would contribute to or
cause a failure condition that would
prevent continued safe flight and
landing of the airplane.
Issued in Renton, Washington, on April 20,
2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–8112 Filed 4–26–07; 8:45 am]
BILLING CODE 4910–13–P
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15:13 Apr 26, 2007
Jkt 211001
SOCIAL SECURITY ADMINISTRATION
20 CFR Part 401
[Docket No. SSA 2006–0074]
RIN 0960–AE88
Privacy and Disclosure of Official
Records and Information
Social Security Administration.
Final rules.
AGENCY:
ACTION:
SUMMARY: These final rules revise our
privacy and disclosure rules to clarify
certain provisions and to provide
expanded regulatory support for new
and existing responsibilities and
functions. These changes in the
regulations will increase Agency
efficiency and ensure consistency in the
implementation of the Social Security
Administration’s (SSA) policies and
responsibilities under the Privacy Act
and the Social Security Act.
DATES: These rules are effective May 29,
2007.
FOR FURTHER INFORMATION CONTACT:
Christine W. Johnson, Office of Public
Disclosure, 3–A–6 Operations Building,
6401 Security Boulevard, Baltimore, MD
21235–6401, (410) 965–8563 or TTY
(410) 965–5609. For information on
eligibility or filing for benefits, call our
national toll-free numbers, 1–800–772–
1213 or TTY 1–800–325–0778, or visit
our Internet Web site, Social Security
Online, at https://
www.socialsecurity.gov.
SUPPLEMENTARY INFORMATION:
Electronic Version
The electronic file of this document is
available on the date of publication in
the Federal Register at https://
www.gpoaccess.gov/FR/.
Background
We last revised the privacy and
disclosure regulations in 1980 when the
Social Security Administration (SSA)
was a part of the Department of Health
and Human Services (DHHS) (formerly
the Department of Health, Education
and Welfare) and subject to DHHS’
disclosure policy oversight. Since 1980,
significant changes have occurred in the
procedures. We are codifying these
changes in the procedures governing
access to, and disclosure of, personally
identifiable information. We are also
making minor housekeeping changes to
further clarify our procedures. In
general, these final rules reflect SSA’s
compliance with technological, legal
and legislative changes that have
occurred since 1980.
We are clarifying the provisions
regarding requests for access to
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Sfmt 4700
20935
information developed by medical
sources for Social Security programs,
fully describing the existing
responsibilities and functions of the
Privacy Officer position, establishing
the new senior agency official for
privacy as required by the Office of
Management and Budget (OMB) and
explaining the related responsibilities,
and implementing SSA’s new Privacy
Impact Assessment process in
accordance with the E-Government Act
of 2002, Pub. L. 107–347. As required by
OMB, we are requiring adequate
safeguards against inappropriate
disclosure of personal information by
electronic means, e.g., over the Internet,
and revising our procedures on
notification of, or access to, medical
records on behalf of another person, e.g.,
an adult or child.
These final rules also clarify SSA
policy concerning an individual’s access
to, or notification of, program records,
amend the language concerning appeal
requests under the Privacy Act to
include denial of access to the record,
and amend the language to insert the
word ‘‘written’’ prior to ‘‘consent’’ to
clarify that the requirement means
disclosure with written consent and
expands the language to more clearly
define what information we will
disclose with written consent. We are
revising the language to show that SSA
also has physical custody of personnel
records, and revising the language under
disclosure of personal information in
nonprogram records to show the new
name of the former General Accounting
Office.
These final rules amend the language
under disclosure of personal
information in program records to make
clear that we disclose information from
program records only when there is a
legitimate need for the information, and
revise the language under disclosures
required by law to show the current
name for Aid to Families with
Dependent Children. We are amending
the language under compatible purposes
to clearly state how we implement the
routine use provision of the Privacy Act
(5 U.S.C. 552a(b)(3)) and what we mean
by routine use in terms of the
information we can disclose, and
amending the language under law
enforcement purposes to clarify that
disclosures under 5 U.S.C. 552a(b)(7)
also require a written request. We are
amending the language under statistical
and research activities to reflect the
language in the new routine use of data
for research purposes, amending the
language in the General Accounting
Office section to correctly reflect the
new name of the agency, and clarifying
certain matters related to our rules on
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27APR1
]]>Agencies
[Federal Register Volume 72, Number 81 (Friday, April 27, 2007)]
[Rules and Regulations]
[Pages 20933-20935]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-8112]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
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.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.
========================================================================
Federal Register / Vol. 72, No. 81 / Friday April 27, 2007 / Rules
and Regulations
[[Page 20933]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM377; Special Conditions No. 25-353-SC]
Special Conditions: Dassault Falcon Fan Jet, Fan Jet Series D,
Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and
Mystere-Falcon 200 Airplanes; High-Intensity Radiated Fields (HIRF)
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for Dassault Falcon Fan
Jet, Fan Jet Series D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5,
20-E5, 20-F5, and Mystere-Falcon 200 airplanes modified by 3S
Certification, LLC. These modified airplanes will have novel or unusual
design features when compared with the state of technology envisioned
in the airworthiness standards for transport category airplanes. The
modification installs Thommen AD 30 Repeater Altimeters and a Skylight
ADC 600 Air Data Converter Unit. The applicable airworthiness
regulations do not contain adequate or appropriate safety standards for
protecting these systems from effects of high-intensity radiated fields
(HIRF). 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 for these special conditions is April 20,
2007. We must receive your comments by June 11, 2007.
ADDRESSES: You may mail or deliver comments on these special conditions
in duplicate to: Federal Aviation Administration, Transport Airplane
Directorate, Attention: Rules Docket (ANM-113), Docket No. NM377, 1601
Lind Avenue, SW., Renton, Washington 98057-3356. You must mark your
comments Docket No. NM377. You may inspect comments in the Rules Docket
weekdays, except Federal holidays, between 7:30 a.m. and 4 p.m.
FOR FURTHER INFORMATION CONTACT: Greg Dunn, 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) 227-2799; facsimile (425) 227-
1320.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA has determined that notice and opportunity for prior public
comment for these special conditions is impracticable, because these
procedures would significantly delay certification and 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. We therefore
find that good cause exists for making these special conditions
effective upon issuance. However, we invite interested persons to take
part in this rulemaking by submitting written comments. The most
helpful comments reference a specific portion of the special
conditions, explain the reason for any recommended change, and include
supporting data. We ask that you send us two copies of written
comments.
We will file in the docket all comments we receive as well as a
report summarizing each substantive public contact with FAA personnel
about these special conditions. You may inspect the docket before and
after the comment closing date. If you wish to review the docket in
person, go to the address in the ADDRESSES section of this preamble
between 7:30 a.m. and 4 p.m., Monday through Friday, except Federal
holidays.
We will consider all comments we receive by the closing date for
comments. We will consider comments filed late if it is possible to do
so without incurring expense or delay. We may change these special
conditions based on the comments we receive.
If you want the FAA to acknowledge receipt of your comments on
these special conditions, include with your comments a pre-addressed,
stamped postcard on which the docket number appears. We will stamp the
date on the postcard and mail it back to you.
Background
On December 21, 2006, 3S Certification, LLC of Nixa, MO, applied to
the Wichita Aircraft Certification Office for a Supplemental Type
Certificate to modify Dassault Falcon Fan Jet, Fan Jet Series D, Series
E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and Mystere-
Falcon 200 airplanes approved under Type Certificate No. A7EU. These
are transport category airplanes powered by two turbojet engines with
maximum takeoff weights of up to 18,000 pounds. The airplanes operate
with a 2-pilot crew and can seat up to 8 passengers. The proposed
modification installs Thommen AD 30 Repeater Altimeters and a Skylight
ADC 600 Air Data Converter Unit. These systems have a potential to be
vulnerable to HIRF external to the airplane.
Type Certification Basis
Under provisions of 14 CFR 21.101, 3S Certification, LLC must show
that the Dassault Falcon Fan Jet, Fan Jet Series D, Series E, Series F,
Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and Mystere-Falcon 200
airplanes, as changed, continue to meet the applicable provisions of
the regulations incorporated by reference in Type Certificate No. A7EU
or the applicable regulations in effect on the date of application for
the change. The regulations incorporated by reference in the type
certificate are commonly referred to as the ``original type
certification basis.'' The type certification basis for the modified
Dassault Falcon Fan Jet, Fan Jet Series D, Series E, and Series F
airplanes includes the applicable paragraphs of CAR 4b, as amended by
Amendments 4b-1 through 4b-12; Special Regulations SR-422B and 14 CFR
part 25 as amended by provisions of Amendment 25-4 in lieu of CAR
4b.350(e) and (f). The type certification basis for the Dassault
Mystere-Falcon 200 airplanes includes the applicable paragraphs of CAR
4b, as amended by Amendments 4b-1 through 4b-12;
[[Page 20934]]
Special Regulations SR-422B and 14 CFR part 25 as amended by certain
sections of Amendments 25-1 through 25-46; SFAR 27 as amended by
Amendments 27-1 through 27-3; and 14 CFR part 36 as amended by
Amendments 36-1 through 36-12. The type certification basis for the
Dassault Mystere-Falcon 20-C5, 20-D5, 20-E5, and 20-F5 airplanes
includes the applicable paragraphs of CAR 4b, as amended by Amendments
4b-1 through 4b-12; Special Regulations SR-422B and 14 CFR part 25 as
amended by certain sections in Amendments 25-1 through 25-56; Sec.
25.904 and Appendix 1 as amended by Amendment 25-62; SFAR 27 as amended
by Amendments 27-1 through 27-6; and 14 CFR part 36 as amended by
Amendments 36-1 through 36-15. In addition, the type certification
basis includes certain later amended sections of the applicable part 25
regulations that are not relevant to these special conditions.
If the Administrator finds that the applicable airworthiness
regulations (part 25, as amended) do not contain adequate or
appropriate safety standards for the Dassault Falcon Fan Jet, Fan Jet
Series D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-
F5, and Mystere-Falcon 200 airplanes because of a novel or unusual
design feature, special conditions are prescribed under the provisions
of Sec. 21.16.
In addition to the applicable airworthiness regulations and special
conditions, the Dassault Falcon Fan Jet, Fan Jet Series D, Series E,
Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and Mystere-Falcon
200 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 Sec. 11.19, under
Sec. 11.38, and they become part of the type certification basis under
the provisions of Sec. 21.101.
Special conditions are initially applicable to the model for which
they are issued. Should 3S Certification, LLC apply later for a
supplemental type certificate to modify any other model included on
Type Certificate No. A7EU, as applicable, to incorporate the same or
similar novel or unusual design feature, these special conditions would
also apply to the other model under the provisions of Sec. 21.101.
Novel or Unusual Design Features
As noted earlier, the Dassault Falcon Fan Jet, Fan Jet Series D,
Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and
Mystere-Falcon 200 airplanes modified by 3S Certification, LLC will
incorporate repeater altimeters and an air data converter unit, that
will perform critical functions. These systems may be vulnerable to
HIRF external to the airplane. Current airworthiness standards of part
25 do not contain adequate or appropriate safety standards for
protecting this equipment from adverse effects of HIRF. Therefore,
these systems are considered to be novel or unusual design features.
Discussion
There is no specific regulation that addresses protection for
electrical and electronic systems from HIRF. Increased power levels
from radio frequency transmitters and the growing use of sensitive
avionics/electronics and electrical systems to command and control
airplanes have made it necessary to provide adequate protection.
To ensure that a level of safety is achieved equivalent to that
intended by the regulations incorporated by reference, special
conditions are needed for the Dassault Falcon Fan Jet, Fan Jet Series
D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and
Mystere-Falcon 200 airplanes modified by 3S Certification, LLC. These
special conditions require that new avionics/electronics and electrical
systems that perform critical functions be designed and installed to
preclude component damage and interruption of function because of HIRF.
High-Intensity Radiated Fields (HIRF)
With the trend toward increased power levels from ground-based
transmitters, and the advent of space and satellite communication
coupled with electronic command and control of the airplane, the
immunity of critical digital avionics/electronics and electrical
systems to HIR must be established.
It is not possible to precisely define the HIRF to which the
airplane will be exposed in service. There is also uncertainly
concerning the effectiveness of airframe shielding for HIRF.
Furthermore, coupling of electromagnetic energy to cockpit-installed
equipment through the cockpit window apertures is undefined. Based on
surveys and an analysis of existing HIRF emitters, an adequate level of
protection exists when compliance with the HIRF protection special
condition is shown with either paragraph 1 or 2 below:
1. A minimum environment of 100 volts rms (root-mean-square) per
meter electric field strength from 10 KHz to 18 GHz.
a. System elements and their associated wiring harnesses must be
exposed to the environment without benefit of airframe shielding.
b. Demonstration of this level of protection is established through
system tests and analysis.
2. An environment external to the airframe of the field strengths
shown in the table below for the frequency ranges indicated. Immunity
to both peak and average field strength components from the table must
be demonstrated.
------------------------------------------------------------------------
Field strength
(volts per meter)
Frequency ---------------------
Peak Average
------------------------------------------------------------------------
10 kHz-100 kHz.................................... 50 50
100 kHz-500 kHz................................... 50 50
500 kHz-2 MHz..................................... 50 50
2 MHz-30 MHz...................................... 100 100
30 MHz-70 MHz..................................... 50 50
70 MHz-100 MHz.................................... 50 50
100 MHz-200 MHz................................... 100 100
200 MHz-400 MHz................................... 100 100
400 MHz-700 MHz................................... 700 50
700 MHz-1 GHz..................................... 700 100
1 GHz-2 GHz....................................... 2000 200
2 GHz-4 GHz....................................... 3000 200
4 GHz-6 GHz....................................... 3000 200
6 GHz-8 GHz....................................... 1000 200
8 GHz-12 GHz...................................... 3000 300
12 GHz-18 GHz..................................... 2000 200
18 GHz-40 GHz..................................... 600 200
------------------------------------------------------------------------
The field strengths are expressed in terms of peak of the root-mean-
square (rms) over the complete modulation period.
The environment levels identified above are the result of an FAA
review of existing studies on the subject of HIRF and of the work of
the Electromagnetic Effects Harmonization Working Group of the Aviation
Rulemaking Advisory Committee.
Applicability
These special conditions are applicable to Dassault Falcon Fan Jet,
Fan Jet Series D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5, 20-
E5, 20-F5, and Mystere-Falcon 200 airplanes modified by 3S
Certification, LLC. Should 3S Certification, LLC apply later for a
supplemental type certificate to modify any other model included on
Type Certificate No. A7EU to incorporate the same or similar novel or
unusual design feature, these special conditions would apply to that
model as well under provisions of Sec. 21.101.
Conclusion
This action affects only certain novel or unusual design features
on Dassault Falcon Fan Jet, Fan Jet Series D, Series E, Series F,
Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5, and Mystere-Falcon 200
airplanes modified by 3S Certification, LLC. It is not a rule of
[[Page 20935]]
general applicability and affects only the applicant which applied to
the FAA for approval of these design features on the airplane.
The substance of the special conditions for these airplanes has
been subjected to the notice and comment procedure in several prior
instances and has been derived without substantive change from those
previously issued. 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 immediately. The FAA is requesting comments to allow
interested people to submit views that may not have been submitted in
response to the prior opportunities for comment.
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 supplemental type certification basis for the Dassault Falcon Fan
Jet, Fan Jet Series D, Series E, Series F, Mystere-Falcon 20-C5, 20-D5,
20-E5, 20-F5, and Mystere-Falcon 200 airplanes modified by 3S
Certification, LLC.
1. Protection From Unwanted Effects of High-Intensity Radiated
Fields (HIRF).
Each electrical and electronic system that performs critical
functions must be designed and installed to ensure that the operation
and operational capability of these systems to perform critical
functions are not adversely affected when the airplane is exposed to
high-intensity radiated fields.
2. For the purpose of these special conditions, the following
definition applies: Critical Functions: Functions whose failure would
contribute to or cause a failure condition that would prevent continued
safe flight and landing of the airplane.
Issued in Renton, Washington, on April 20, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-8112 Filed 4-26-07; 8:45 am]
BILLING CODE 4910-13-P
