Published 2017-10-23 · Federal Register document 2017-22564
Airworthiness Directives; Dassault Aviation Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for all Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. This AD was prompted by reports of defective fire extinguisher tubes. This AD requires replacement of the affected fire extinguisher tubes with improved fire extinguisher tubes. We are issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:54.997910+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2017-90ba553c3b802c53
- Source row
- results[321]
- Raw source SHA-256
- 90ba553c3b802c5316e8d18f30db5da9f7731a87f58278ec2965f199ef4375e9
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2017-21-01
- Effective date printed in this edition
- 2017-11-27
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective November 27, 2017.
Exact source excerpt. Text positions 13056–13121, end exclusive, in the original decoded publication. SHA-256: 3ccbc70f853218fe7dfecd12c9fafd3bd0f4b419b93f87613c92d0138791d51a
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 13121–13150, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD, certificated in any category.
(1) Dassault Aviation Model FAN JET FALCON, FAN JET FALCON
SERIES C, D, E, F, and G airplanes, all manufacturer serial numbers.
(2) Dassault Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5,
and 20-F5 airplanes, all manufacturer serial numbers.
Exact source excerpt. Text positions 13150–13549, end exclusive, in the original decoded publication. SHA-256: eabdc94fee6fe0fbe39860e1cd9aebea2a2b0c6e7f5f17320695262bfdb11a0a
Subject
(d) Subject
Air Transport Association (ATA) of America Code 26, Fire
protection.
Exact source excerpt. Text positions 13549–13637, end exclusive, in the original decoded publication. SHA-256: d2a9cf8a8912242590075a047b779e20ffaf976cb7811f4525197162c9aaae16
Reason
(e) Reason
This AD was prompted by reports of defective fire extinguisher
tubes. We are issuing this AD to prevent fire extinguisher failure.
Such a failure could result in the inability to extinguish a fire in
the rear compartment, and possible damage to the airplane and injury
to the occupants.
Exact source excerpt. Text positions 13637–13945, end exclusive, in the original decoded publication. SHA-256: df95eceef0b00af7d81005f4ecc3097036e24a53f2c2c9048c7e0fd710e19901
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 13945–14047, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Fire Extinguisher Tubes Replacement
(g) Fire Extinguisher Tubes Replacement
Within 450 flight cycles or 450 flight hours, whichever occurs
later after the effective date of this AD, replace each affected
fire extinguisher tube, part number (P/N) MY20791-121 and P/N
MY20791-122, with a serviceable fire extinguisher tube, P/N MY20791-
121-1 or P/N MY20791-122-1, as applicable, in accordance with the
Accomplishment Instructions of Dassault Service Bulletin F20-790,
dated September 14, 2016.
Exact source excerpt. Text positions 14047–14515, end exclusive, in the original decoded publication. SHA-256: 2d9cd219b7fc0a3274c038af3381f4e9224407d87da7e2a4bcd015f8ae7404c1
Parts Installation Prohibition
(h) Parts Installation Prohibition
No person may install a fire extinguisher tube, P/N MY20791-121
or P/N MY20791-122, on any airplane, as of the applicable time
specified in paragraph (h)(1) or (h)(2) of this AD.
(1) For an airplane equipped with an affected fire extinguisher
tube as of the effective date of this AD: After modification of that
airplane as required by paragraph (g) of this AD.
(2) For an airplane that is not equipped with an affected fire
extinguisher tube as of the effective date of this AD: As of the
effective date of this AD.
Exact source excerpt. Text positions 14515–15087, end exclusive, in the original decoded publication. SHA-256: b523ba54fd768e716106c49ca6adfd3e2948cf76eca0bb57bf010565988131ad
Other FAA AD Provisions
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (j)(2) of this AD. Information
may be emailed to: [email protected]. Before using any
approved AMOC, notify your appropriate
[[Page 48915]]
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Aviation
Safety Agency (EASA); or Dassault Aviation's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
Exact source excerpt. Text positions 15087–16403, end exclusive, in the original decoded publication. SHA-256: 86e0da868a76eb6bb025279f02f107b6b9993a5f3c77d024c55cd537267412eb
Related Information
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0154, dated July 28, 2016,
for related information. This MCAI may be found in the AD docket on
the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2016-9500.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone
425-227-1137; fax 425-227-1149.
Exact source excerpt. Text positions 16403–16965, end exclusive, in the original decoded publication. SHA-256: 316ab3856c2c882010a40a70ed4efe414a75ab09f1404e03f1e079dce6067f4e
Material Incorporated by Reference
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Dassault Service Bulletin F20-790, dated September 14, 2016.
(ii) Reserved.
(3) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call 425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 16965–18145, end exclusive, in the original decoded publication. SHA-256: 0ce05e1ccee92196af588d0d730f115ddb914758f4bde8c13d521c346b601eea
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2017-21-01 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 7dc2917632216781f4ffa05668ffbc02e80ba110b01566597ec1a52fdb66270f. Source manifest: 42a930a647ace082154a61e5702ebe960b907c1975e88496133632cfe9417848.
Official source · 2017-10-23
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 82, Number 203 (Monday, October 23, 2017)]
[Rules and Regulations]
[Pages 48912-48915]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-22564]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-9500; Product Identifier 2016-NM-140-AD; Amendment
39-19072; AD 2017-21-01]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for all
Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E,
F, and G; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5
airplanes. This AD was prompted by reports of defective fire
extinguisher tubes. This AD requires replacement of the affected fire
extinguisher tubes with improved fire extinguisher tubes. We are
issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective November 27, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 27,
2017.
ADDRESSES: For service information identified in this final rule,
contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box
2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet
http://www.dassaultfalcon.com. You may view this referenced service
information at the FAA, Transport Standards Branch, 1601 Lind Avenue
SW., Renton, WA. For information on the availability
[[Page 48913]]
of this material at the FAA, call 425-227-1221. It is also available on
the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2016-9500.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9500; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is Docket Management Facility, U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Section, Transport Standards Branch, FAA, 1601 Lind
Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-
1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to all Dassault Aviation Model
FAN JET FALCON, and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5
airplanes. The NPRM published in the Federal Register on December 20,
2016 (81 FR 92747) (``the NPRM''). The NPRM was prompted by reports of
defective fire extinguisher tubes. The NPRM proposed to require
replacement of the affected fire extinguisher tubes with improved fire
extinguisher tubes. We are issuing this AD to prevent fire extinguisher
failure. Such a failure could result in the inability to extinguish a
fire in the rear compartment, and possible damage to the airplane and
injury to the occupants.
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Union, has issued EASA
Airworthiness Directive 2016-0154, dated July 28, 2016 (referred to
after this as the Mandatory Continuing Airworthiness Information, or
``the MCAI''), to correct an unsafe condition for all Dassault Aviation
Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G; and
Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. The MCAI
states:
Several defective extinguisher tubes have been found on certain
Dassault Aviation Fan Jet Falcon aeroplanes. The results of the
investigations concluded that these occurrences were caused by
corrosion.
This condition, if not corrected, could impact the capability to
extinguish a fire in the rear compartment of the aeroplane, possibly
resulting in damage to the aeroplane and injury to the occupants.
For the reason described above, this [EASA] AD requires the
replacement of the affected tubes with improved fire extinguisher
tube. In addition, this [EASA] AD prohibits (re)installation of the
affected fire extinguisher tubes on an aeroplane.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9500.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM and
the FAA's response to each comment.
Request To Change Compliance Time From Flight Cycles to Flight Hours
Dassault Aviation noted that paragraph (g) of the proposed AD
specified a compliance time of 450 flight cycles but the MCAI specified
a compliance time of 450 flight hours. Dassault Aviation requested that
we change the compliance time in the proposed AD to specify flight
hours.
We acknowledge the commenter's request and agree that we
inadvertently referred to ``flight cycles'' instead of ``flight hours''
in paragraph (g) of the proposed AD. Using flight cycles gives
operators approximately 3 additional months to comply with the proposed
action based on the average fleet utilization of these airplanes.
However, to reduce the compliance time of the proposed AD would
necessitate (under the provisions of the Administrative Procedure Act)
reissuing the notice, reopening the period for public comment, and
eventually issuing a final rule. Those actions would add even more time
to the rulemaking process and further delay mitigation of the unsafe
condition. We find that delaying issuance of this final rule is
inappropriate in light of the identified unsafe condition. Most ADs,
including this one, permit operators to accomplish the requirements of
an AD at a time earlier than the specified compliance time. To more
closely match the EASA specified compliance time without compromising
safety, we have changed the compliance time in paragraph (g) of this AD
to ``within 450 flight cycles or 450 flight hours, whichever occurs
later after the effective date of this AD.''
Request To Change the Compliance Method
One commenter, Robert Bowers, requested that we change the
compliance method in the proposed AD to match that specified in AD
2015-20-08, Amendment 39-18287 (80 FR 60795, October 8, 2015) (``AD
2015-20-08''). AD 2015-20-08 requires that certain other fire
extinguisher tubes be inspected every 13 months, until they need to be
replaced by a new tube. The commenter added that he has inspected two
Falcon airplanes and finds no reason to replace these fire extinguisher
tubes at this time.
We disagree with the commenter's request. The location of the fire
extinguisher tubes addressed by this AD is more critical from a design
perspective than that of the fire extinguisher tubes addressed by AD
2015-20-08. The applicable fire extinguisher tubes must be replaced
with tubes having an improved design to address the unsafe condition.
We have not changed this AD in this regard.
Explanation of Change to NPRM
In the proposed AD, we stated the applicability included ``Dassault
Aviation Model FAN JET FALCON'' airplanes and inadvertently left out
``SERIES C, D, E, F, and G'' from the description. For clarity, we have
revised the applicability to read ``Dassault Aviation Model FAN JET
FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes . . .'' in
this final rule. This change does not expand the scope of the final
rule or add airplanes to the applicability.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the changes described previously and minor editorial
changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.
Related Service Information Under 1 CFR Part 51
Dassault Aviation has issued Service Bulletin F20-790, dated
September 14,
[[Page 48914]]
2016. This service information describes procedures for the replacement
of affected fire extinguisher tubes with improved fire extinguisher
tubes. This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
We estimate that this AD affects 133 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Fire extinguisher tube replacement.... 3 work-hours x $85 per $3,100 $3,355 $446,215
hour = $255.
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes to
the Director of the System Oversight Division.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2017-21-01 Dassault Aviation: Amendment 39-19072; Docket No. FAA-
2016-9500; Product Identifier 2016-NM-140-AD.
(a) Effective Date
This AD is effective November 27, 2017.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD, certificated in any category.
(1) Dassault Aviation Model FAN JET FALCON, FAN JET FALCON
SERIES C, D, E, F, and G airplanes, all manufacturer serial numbers.
(2) Dassault Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5,
and 20-F5 airplanes, all manufacturer serial numbers.
(d) Subject
Air Transport Association (ATA) of America Code 26, Fire
protection.
(e) Reason
This AD was prompted by reports of defective fire extinguisher
tubes. We are issuing this AD to prevent fire extinguisher failure.
Such a failure could result in the inability to extinguish a fire in
the rear compartment, and possible damage to the airplane and injury
to the occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Fire Extinguisher Tubes Replacement
Within 450 flight cycles or 450 flight hours, whichever occurs
later after the effective date of this AD, replace each affected
fire extinguisher tube, part number (P/N) MY20791-121 and P/N
MY20791-122, with a serviceable fire extinguisher tube, P/N MY20791-
121-1 or P/N MY20791-122-1, as applicable, in accordance with the
Accomplishment Instructions of Dassault Service Bulletin F20-790,
dated September 14, 2016.
(h) Parts Installation Prohibition
No person may install a fire extinguisher tube, P/N MY20791-121
or P/N MY20791-122, on any airplane, as of the applicable time
specified in paragraph (h)(1) or (h)(2) of this AD.
(1) For an airplane equipped with an affected fire extinguisher
tube as of the effective date of this AD: After modification of that
airplane as required by paragraph (g) of this AD.
(2) For an airplane that is not equipped with an affected fire
extinguisher tube as of the effective date of this AD: As of the
effective date of this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Section, Transport Standards Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the International Section, send it to the attention of
the person identified in paragraph (j)(2) of this AD. Information
may be emailed to: [email protected]. Before using any
approved AMOC, notify your appropriate
[[Page 48915]]
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, International
Section, Transport Standards Branch, FAA; or the European Aviation
Safety Agency (EASA); or Dassault Aviation's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0154, dated July 28, 2016,
for related information. This MCAI may be found in the AD docket on
the Internet at http://www.regulations.gov by searching for and
locating Docket No. FAA-2016-9500.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Section, Transport Standards
Branch, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone
425-227-1137; fax 425-227-1149.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Dassault Service Bulletin F20-790, dated September 14, 2016.
(ii) Reserved.
(3) For service information identified in this AD, contact
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000,
South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 1601 Lind Avenue SW., Renton, WA. For information
on the availability of this material at the FAA, call 425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on October 11, 2017.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2017-22564 Filed 10-20-17; 8:45 am]
BILLING CODE 4910-13-P
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