Published 2013-02-21 · Federal Register document 2013-03704
Airworthiness Directives; Reims Aviation S.A. Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for Reims Aviation S.A. Model F406 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as improper material used in nose landing gear (NLG) attachment brackets could lead to failure of the NLG bracket with consequent damage to the airplane while landing. We are issuing this AD to require actions to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
- Source row
- results[62]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2013-04-02
- Effective date printed in this edition
- 2013-03-28
Read 9 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective March 28,
2013.
Exact source excerpt. Text positions 8125–8219, end exclusive, in the original decoded publication. SHA-256: 1db37eb9e07c82d7a5ed158026ac5153469fc45abed2adaee8181c58e73291b9
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8219–8248, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Reims Aviation S.A. F406 airplanes, all
serial numbers, certificated in any category.
Exact source excerpt. Text positions 8248–8378, end exclusive, in the original decoded publication. SHA-256: 5f770745c1e5ce9d94610867d0e07fa4aaccb6d25bab10440debc70b707f179e
Subject
(d) Subject
Air Transport Association of America (ATA) Code 32: Landing
Gear.
Exact source excerpt. Text positions 8378–8463, end exclusive, in the original decoded publication. SHA-256: be0ce89d2ed88efecf440760782df50a3f0087f20af4d42e538b61070a049ed5
Reason
(e) Reason
This AD was prompted by reports of improper material used in
nose landing gear (NLG) attachment brackets that could lead to
failure of the NLG bracket with consequent damage to the airplane
while landing. We are issuing this AD to ensure the proper NLG
attachment bracket is installed.
Exact source excerpt. Text positions 8463–8770, end exclusive, in the original decoded publication. SHA-256: 9adb4dea91a88a76c4ce93c304a4ee866e9536f1b442ed09562360285f7f7eec
Actions and Compliance
(f) Actions and Compliance
Unless already done, do the following actions following the
Accomplishment Instructions numbers 1 through 5 in Reims Aviation
Industries Service Bulletin No. F406-74, dated September 26, 2012:
(1) Within the next 25 hours time-in-service (TIS) after March
28, 2013 (the effective date of this AD) or within the next 30 days
after March 28, 2013 (the effective date of this AD), whichever
occurs first, inspect the nose landing gear (NLG) attachment
brackets, part number (P/N) 6013119-1, to verify if they are made of
steel and not aluminum alloy.
(2) If during the inspection required in paragraph (f)(1) of
this AD, you find that a NLG attachment bracket made of aluminum
alloy is installed, before further flight, replace with an airworthy
steel NLG attachment bracket, P/N 6013119-1.
(3) As of March 28, 2013 (the effective date of this AD), do not
install any NLG attachment bracket P/N 6013119-1 unless it is made
of steel.
Exact source excerpt. Text positions 8770–9757, end exclusive, in the original decoded publication. SHA-256: 83c2a354e4465b3aa145323195a5d26c36299d24338fd2466a5032291eec3e6b
Other FAA AD Provisions
(g) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Albert Mercado, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4119; fax: (816) 329-4090; email:
[email protected]. Before using any approved AMOC on any
airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information
subject to the requirements of the Paperwork Reduction Act unless
that collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 5 minutes per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.
Exact source excerpt. Text positions 9757–11846, end exclusive, in the original decoded publication. SHA-256: 48e38f9caf6e4d98b2da308287dbad28374db583f5c4a91f23ddd898911241db
Related Information
(h) Related Information
Refer to MCAI European Aviation Safety Agency (EASA) AD No.
2012-0202, dated October 1, 2012; and Reims Aviation Industries
Service Bulletin No. F406-74, dated September 26, 2012, for related
information.
[[Page 11980]]
Exact source excerpt. Text positions 11846–12100, end exclusive, in the original decoded publication. SHA-256: c1b87ebe62427d093605cdecdba1e65fc6dd1b1ecadbb43c4b83e0c279c586fe
Material Incorporated by Reference
(i) 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 the AD specifies otherwise.
(i) Reims Aviation Industries Service Bulletin No. F406-74,
dated September 26, 2012.
(ii) Reserved.
(3) For Reims Aviation Industries service information identified
in this AD, contact Reims Aviation Industries, A[eacute]rodrome de
Reims Prunay, 51360 Prunay, France; telephone + 33 3 26 48 46 65;
fax + 33 3 26 49 18 57; email: [email protected];
Internet: www.geciaviation.com/en/f406.html.
(4) You may view this service information at FAA, Small Airplane
Directorate, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
(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 12100–13384, end exclusive, in the original decoded publication. SHA-256: 2a8c6c3ed268ec10eb496e5a78eed0ebac644ed8581e67672af05ce074430715
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 2013-04-02 · 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: 9cc7d2580c756ae6e3a42612f50eb20fefbf337312ac66e9ce80a9ff3f4e4f9f. Source manifest: 4ce47a314cea2d706c28413b19c61cd8e6ed77f3ac9ba9e9c68ec4d66bb2bea7.
Official source · 2013-02-21
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 78, Number 35 (Thursday, February 21, 2013)]
[Rules and Regulations]
[Pages 11978-11980]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-03704]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-1274; Directorate Identifier 2012-CE-042-AD;
Amendment 39-17359; AD 2013-04-02]
RIN 2120-AA64
Airworthiness Directives; Reims Aviation S.A. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for Reims
Aviation S.A. Model F406 airplanes. This AD results from mandatory
continuing airworthiness information (MCAI) issued by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as improper material used in nose landing gear (NLG)
attachment brackets could lead to failure of the NLG bracket with
consequent damage to the airplane while landing. We are issuing this AD
to require actions to address the unsafe condition on these products.
DATES: This AD is effective March 28, 2013.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of March 28,
2013.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at Document 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 service information identified in this AD, contact Reims
Aviation Industries, A[eacute]rodrome de Reims Prunay, 51360 Prunay,
France; telephone + 33 3 26 48 46 65; fax + 33 3 26 49 18 57; email:
[email protected]; Internet: www.geciaviation.com/en/f406.html. You may review copies of the referenced service information
at the FAA, Small Airplane Directorate, 901 Locust, Kansas City,
Missouri 64106. For information on the availability of this material at
the FAA, call (816) 329-4148.
FOR FURTHER INFORMATION CONTACT: Albert Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090; email:
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on December 5, 2012 (77
FR 72252). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
During the manufacturing process, RAI found that some of the
nose landing gear (NLG) attachment brackets, Part Number (P/N)
6013119-1, were made of aluminum alloy, instead of steel. The
results of the investigations showed that some of these aluminum
alloy brackets are likely to be installed on aeroplanes currently in
service.
This condition, if not detected and corrected, could lead to
failure of the NLG attachment bracket and jamming of the NLG
extension/retraction mechanism, possibly resulting in a runway
excursion and consequent damage to the aeroplane and injury to the
occupants.
For the reasons described above, this AD requires inspection of
the NLG attachment bracket P/N 6013119-1 and, depending on findings,
replacement with a serviceable bracket made of steel.
In addition, as some aluminum alloy P/N 6013119-1 NLG attachment
brackets may have been supplied as spares, this AD also requires
determination that the part is made of steel, prior to installation.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (77 FR 72252, December 5,
2012) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 72252, December 5, 2012) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the (77 FR 72252, December 5, 2012).
Costs of Compliance
We estimate that this AD will affect 7 products of U.S. registry.
We also estimate that it would take about .5 work-hour per product to
comply with
[[Page 11979]]
the basic requirements of this AD. The average labor rate is $85 per
work-hour.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $42.50, or $297.50 per product.
In addition, we estimate that any necessary follow-on actions would
take about 3 work-hours and require parts costing $500, for a cost of
$755 per product. We have no way of determining the number of products
that may need these actions.
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.
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 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.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; 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 the NPRM, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
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 AD:
2013-04-02 Reims Aviation S.A.: Amendment 39-17359; Docket No. FAA-
2012-1274; Directorate Identifier 2012-CE-042-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective March 28,
2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Reims Aviation S.A. F406 airplanes, all
serial numbers, certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 32: Landing
Gear.
(e) Reason
This AD was prompted by reports of improper material used in
nose landing gear (NLG) attachment brackets that could lead to
failure of the NLG bracket with consequent damage to the airplane
while landing. We are issuing this AD to ensure the proper NLG
attachment bracket is installed.
(f) Actions and Compliance
Unless already done, do the following actions following the
Accomplishment Instructions numbers 1 through 5 in Reims Aviation
Industries Service Bulletin No. F406-74, dated September 26, 2012:
(1) Within the next 25 hours time-in-service (TIS) after March
28, 2013 (the effective date of this AD) or within the next 30 days
after March 28, 2013 (the effective date of this AD), whichever
occurs first, inspect the nose landing gear (NLG) attachment
brackets, part number (P/N) 6013119-1, to verify if they are made of
steel and not aluminum alloy.
(2) If during the inspection required in paragraph (f)(1) of
this AD, you find that a NLG attachment bracket made of aluminum
alloy is installed, before further flight, replace with an airworthy
steel NLG attachment bracket, P/N 6013119-1.
(3) As of March 28, 2013 (the effective date of this AD), do not
install any NLG attachment bracket P/N 6013119-1 unless it is made
of steel.
(g) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Albert Mercado, Aerospace Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4119; fax: (816) 329-4090; email:
[email protected]. Before using any approved AMOC on any
airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, a federal agency may not conduct or sponsor, and a person
is not required to respond to, nor shall a person be subject to a
penalty for failure to comply with a collection of information
subject to the requirements of the Paperwork Reduction Act unless
that collection of information displays a current valid OMB Control
Number. The OMB Control Number for this information collection is
2120-0056. Public reporting for this collection of information is
estimated to be approximately 5 minutes per response, including the
time for reviewing instructions, completing and reviewing the
collection of information. All responses to this collection of
information are mandatory. Comments concerning the accuracy of this
burden and suggestions for reducing the burden should be directed to
the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:
Information Collection Clearance Officer, AES-200.
(h) Related Information
Refer to MCAI European Aviation Safety Agency (EASA) AD No.
2012-0202, dated October 1, 2012; and Reims Aviation Industries
Service Bulletin No. F406-74, dated September 26, 2012, for related
information.
[[Page 11980]]
(i) 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 the AD specifies otherwise.
(i) Reims Aviation Industries Service Bulletin No. F406-74,
dated September 26, 2012.
(ii) Reserved.
(3) For Reims Aviation Industries service information identified
in this AD, contact Reims Aviation Industries, A[eacute]rodrome de
Reims Prunay, 51360 Prunay, France; telephone + 33 3 26 48 46 65;
fax + 33 3 26 49 18 57; email: [email protected];
Internet: www.geciaviation.com/en/f406.html.
(4) You may view this service information at FAA, Small Airplane
Directorate, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
(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 Kansas City, Missouri, on February 12, 2013.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-03704 Filed 2-20-13; 8:45 am]
BILLING CODE 4910-13-P
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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:56:52.359806+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
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- Text SHA-256
- 9cc7d2580c756ae6e3a42612f50eb20fefbf337312ac66e9ce80a9ff3f4e4f9f
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.