AD 2007-04-25
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Alpha Aviation Concept Limited | R2160 | Airworthiness Directives; Alpha Aviation Design Limited R2160 Airplanes |
Unsafe Condition
Deficiency in compliance with 14 CFR 23.967(d), where production aircraft may lack a metal barrier between the cabin and the fuel tank bay, allowing flammable fuel vapors to enter the cabin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the aircraft to determine if a metal barrier is installed between the cabin and the fuel tank bay. If not installed, install a metal barrier as required by 14 CFR 23.967(d).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Alpha Aviation Design Limited R2160 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for the products listed above. 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 a deficiency in compliance with 14 CFR 23.967(d). There have been instances indicating that production aircraft may not have a metal barrier between the cabin and the fuel tank bay. Lack of a barrier could allow flammable fuel vapors to enter the cabin. We are issuing this AD to require actions to correct the unsafe condition on these products.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 72, Number 38 (Tuesday, February 27, 2007)]
[Rules and Regulations]
[Pages 8613-8615]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E7-3163]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26496 Directorate Identifier 2006-CE-81-AD;
Amendment 39-14958; AD 2007-04-25]
RIN 2120-AA64
Airworthiness Directives; Alpha Aviation Design Limited R2160
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. 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 a
deficiency in compliance with 14 CFR 23.967(d). There have been
instances indicating that production aircraft may not have a metal
barrier between the cabin and the fuel tank bay. Lack of a barrier
could allow flammable fuel vapors to enter the cabin. We are issuing
this AD to require actions to correct the unsafe condition on these
products.
DATES: This AD becomes effective April 3, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of April 3,
2007.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> or in person at the Docket Management Facility, U.S.
Department
[[Page 8614]]
of Transportation, 400 Seventh Street SW., Nassif Building, Room PL-
401, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. The streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
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 January 5, 2007 (72
FR 481). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states that there have been instances
indicating that production aircraft may not have a metal barrier
between the cabin and the fuel tank bay. Lack of a barrier could allow
flammable fuel vapors to enter the cabin. The MCAI requires that you,
to ensure that the aircraft is in compliance with 14 CFR 23.967(d),
inspect the aircraft to determine if a metal barrier is installed
behind the seats and, if not installed, to manufacture and install a
barrier.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
We reviewed the available data and determined that air safety and
the public interest require adopting the AD as proposed.
Differences Between this AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
described in a separate paragraph of the AD, and take precedence over
the actions copied from the MCAI.
Costs of Compliance
We estimate that this AD will affect 10 products of U.S. registry.
We also estimate that it will take about 3 work-hours per product to
comply with this AD. The average labor rate is $80 per work-hour.
Required parts will cost about $300 per product. Where the service
information lists required parts costs that are covered under warranty,
we have assumed that there will be no charge for these parts. As we do
not control warranty coverage for affected parties, some parties may
incur costs higher than estimated here. Based on these figures, we
estimate the cost of this AD to the U.S. operators to be $5,400 or $540
per product.
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 DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) 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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD Docket.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>; 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) 647-5227) 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
0
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:
2007-04-25 Alpha Aviation Design Limited: Amendment 39-14958; Docket
No. FAA-2006-26496; Directorate Identifier 2006-CE-81-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective April 3,
2007.
[[Page 8615]]
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model R2160 airplanes, serial numbers 001
through 378, certificated in any category.
Reason
(d) The mandatory continuing airworthiness information (MCAI)
states that there have been instances indicating that production
aircraft may not have a metal barrier between the cabin and the fuel
tank bay. Lack of a barrier could allow flammable fuel vapors to
enter the cabin. The MCAI requires that, to ensure that the aircraft
is in compliance with 14 CFR 23.967(d), inspect the aircraft to
determine if a metal barrier is installed behind the seats and, if
not installed, to manufacture and install a barrier.
Actions and Compliance
(e) Unless already done, do the following actions within the
next 100 hours time-in-service or within 6 months after April 3,
2007 (the effective date of this AD), whichever occurs first.
(1) Inspect the aircraft to determine if a metal barrier is
installed behind the seats per Alpha Aviation Service Bulletin AA-
SB-28-001, dated July 10, 2006.
(2) If a metal barrier is installed per Alpha Aviation Service
Bulletin AA-SB-28-001, dated July 10, 2006, and (e)(1) of this AD,
then no further action is required.
(3) If a metal barrier is not installed, manufacture and install
a barrier per Alpha Aviation Service Bulletin AA-SB-28-001, dated
July 10, 2006, and Alpha Aviation Drawing No. 60-53-119 (page 3 of 3
of the Service Bulletin).
FAA AD Differences
Note: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(f) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19.
(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, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.
Related Information
(g) Refer to MCAI Civil Aviation Authority of New Zealand AD
DCA/R2000/38, dated June 29, 2006, for related information.
Material Incorporated by Reference
(h) You must use Alpha Aviation Service Bulletin AA-SB-28-001,
dated July 10, 2006, to do the actions required by this AD, unless
the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact Alpha
Aviation Ltd, Ingram Road, Hamilton Airport RD 2, Hamilton 2021, New
Zealand; telephone: 011 64 7 843 7070; fax: 011 64 7 843 8040;
Internet: <a href="http://www.alphaaviation.co.nz">http://www.alphaaviation.co.nz</a>.
(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri
64106; or 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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Kansas City, Missouri, on February 15, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-3163 Filed 2-26-07; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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