AD 2012-11-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Alpha Aviation Concept Limited | R2160 | Airworthiness Directives; Alpha Aviation Concept Limited (Type Certificate Previously Held by Alpha Aviation Design Limited) Airplanes |
Unsafe Condition
Oil lines and oil pressure transducer hose fitted to affected aircraft are not fire resistant.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the oil hose lines and oil pressure transducer hose with fire-resistant lines as specified in the referenced service bulletins. Do not install non-compliant oil hose lines on affected aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service after July 12, 2012.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Alpha Aviation Concept Limited Model R2160 airplanes, serial numbers 001 through 378, certificated in any category.
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 Alpha Aviation Concept Limited Model R2160 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 oil lines fitted to affected aircraft are not fire resistant. We are issuing this AD to require actions to address the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Alpha Aviation Concept Limited Model R2160
airplanes, serial numbers 001 through 378, certificated in any
category.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 77, Number 110 (Thursday, June 7, 2012)]
[Rules and Regulations]
[Pages 33622-33624]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2012-13558]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0279; Directorate Identifier 2012-CE-007-AD;
Amendment 39-17073; AD 2012-11-10]
RIN 2120-AA64
Airworthiness Directives; Alpha Aviation Concept Limited (Type
Certificate Previously Held by Alpha Aviation Design Limited) 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 Alpha
Aviation Concept Limited Model R2160 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 oil lines fitted to affected aircraft are not fire
resistant. We are issuing this AD to require actions to address the
unsafe condition on these products.
DATES: This AD is effective July 12, 2012.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of July 12, 2012.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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 Alpha
Aviation Concept Limited, Ingram Road, Hamilton Airport, RD 2, Hamilton
2021, New Zealand; telephone: 011 64 7 843 7070; fax: 011 64 7843 8040;
email: <a href="/cdn-cgi/l/email-protection#4f2c3a3c3b20222a3d613c3a3f3f203d3b0f2e233f272e2e39262e3b262021612c20612135"><span class="__cf_email__" data-cfemail="096a7c7a7d66646c7b277a7c7979667b7d496865796168687f60687d606667276a66276773">[email protected]</span></a>; Internet: <a href="http://www.alphaaviation.co.nz">http://www.alphaaviation.co.nz</a>. 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: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090; email:
<a href="/cdn-cgi/l/email-protection#dfb4beadb3f1acbcb7b3baaba5bdbeaab29fb9bebef1b8b0a9"><span class="__cf_email__" data-cfemail="8fe4eefde3a1fcece7e3eafbf5edeefae2cfe9eeeea1e8e0f9">[email protected]</span></a>.
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 March 19, 2012 (77
FR 15980). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
It has been determined that the oil lines fitted to affected
aircraft are not fire resistant and not compliant with the
requirements in FAR 23.1183. To correct this unsafe condition the
Civil Aviation Authority of New Zealand issued DCA/R2000/34
requiring the replacement of oil lines with fire resistant lines.
Since the issue of that AD it has been determined that the oil
transmitter hoses are also not compliant with FAR 23.1183. DCA/
R2000/40 retains the requirements in superseded DCA/R2000/34. The AD
requirement expanded to include the replacement of the oil pressure
transducer hoses.
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 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 15980, March 19, 2012) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 15980, March 19, 2012).
[[Page 33623]]
Costs of Compliance
We estimate that this AD will affect 10 products of U.S. registry.
We also estimate that it would take about 4 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts would cost about $510 per product.
Based on these figures, we estimate the cost of the AD on U.S.
operators to be $8,500, or $850 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 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 <a href="http://www.regulations.gov">http://www.regulations.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) 647-5527) 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:
2012-11-10 Alpha Aviation Concept Limited: Amendment 39-17073;
Docket No. FAA-2012-0279; Directorate Identifier 2012-CE-007-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective July 12,
2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Alpha Aviation Concept Limited Model R2160
airplanes, serial numbers 001 through 378, certificated in any
category.
(d) Subject
Air Transport Association of America (ATA) Code 79: Engine Oil.
(e) Reason
This AD was prompted by a determination that the oil lines and
the oil pressure transducer hose fitted to affected aircraft are not
fire resistant. We are issuing this AD to detect and replace non-
fire resistant oil lines, which, if not corrected, could lead to an
inflight fire.
(f) Actions and Compliance
Unless already done, do the following actions:
(1) Within 50 hours time-in-service (TIS) after July 12, 2012
(the effective date of this AD), replace the oil hose lines (part
number (P/N) 41-23-56-000, 53-11-10-000, 53-20-13-000, 53-20-14-000,
53-34-10-010, 53-18-02-030, 53-21-14-000, or 53-22-01-000) following
Apex Aircraft Service Bulletin No. 020310, dated June 3, 2002, and
replace the oil pressure transducer hose and associated hardware
following Alpha Aviation Service Bulletin AA-SB-79-001, Revision 0,
dated February 2012.
(2) As of July 12, 2012 (the effective date of this AD), do not
install any oil hose lines with P/N 41-23-56-000, 53-11-10-000, 53-
20-13-000, 53-20-14-000, 53-34-10-010, 53-18-02-030, 53-21-14-000,
or 53-22-01-000 on the affected aircraft.
(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: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090;
email: <a href="/cdn-cgi/l/email-protection#670c06150b4914040f0b02131d0506120a2701060649000811"><span class="__cf_email__" data-cfemail="d8b3b9aab4f6abbbb0b4bdaca2bab9adb598beb9b9f6bfb7ae">[email protected]</span></a>. 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 Civil Aviation Authority of New Zealand AD DCA/
R2000/40, dated February 23, 2012; Apex Aircraft Service Bulletin
No. 020310, dated June 3, 2002; and Alpha Aviation Service Bulletin
AA-SB-79-001, Revision 0, dated February 2012, for related
information. For service information related to this AD, contact
Alpha Aviation Concept Limited, Ingram Road, Hamilton Airport, RD 2,
Hamilton 2021, New Zealand; telephone: 011 64 7 843 7070; fax: 011
64
[[Page 33624]]
7843 8040; email: <a href="/cdn-cgi/l/email-protection#6d0e181e190200081f431e181d1d021f192d0c011d050c0c1b040c19040203430e02430317"><span class="__cf_email__" data-cfemail="97f4e2e4e3f8faf2e5b9e4e2e7e7f8e5e3d7f6fbe7fff6f6e1fef6e3fef8f9b9f4f8b9f9ed">[email protected]</span></a>; Internet:
<a href="http://www.alphaaviation.co.nz">http://www.alphaaviation.co.nz</a>. 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.
(i) Material Incorporated by Reference
(1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) under 5 U.S.C. 552(a) and 1 CFR part 51:
(i) Apex Aircraft Service Bulletin No. 020310, dated June 3,
2002; and
(ii) Alpha Aviation Service Bulletin AA-SB-79-001, Revision 0,
dated February 2012.
(2) For service information identified in this AD, contact Alpha
Aviation Concept Limited, Ingram Road, Hamilton Airport, RD 2,
Hamilton 2021, New Zealand; telephone: 011 64 7 843 7070; fax: 011
64 7843 8040; email: <a href="/cdn-cgi/l/email-protection#2b485e585f44464e5905585e5b5b44595f6b4a475b434a4a5d424a5f424445054844054551"><span class="__cf_email__" data-cfemail="caa9bfb9bea5a7afb8e4b9bfbabaa5b8be8aaba6baa2ababbca3abbea3a5a4e4a9a5e4a4b0">[email protected]</span></a>; Internet:
<a href="http://www.alphaaviation.co.nz">http://www.alphaaviation.co.nz</a>.
(3) You may review copies of the 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.
(4) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at an NARA facility, call 202-741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
Issued in Kansas City, Missouri, on May 29, 2012.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012-13558 Filed 6-6-12; 8:45 am]
BILLING CODE 4910-13-P
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