Published 2014-12-24 · Federal Register document 2014-29833
Airworthiness Directives; Alpha Aviation Concept Limited Airplanes
Publication 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 paint adherence defects inside the engine air intake box and cohesion defects inside the laminated ducting from the filter to the air intake box. 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 2026-09-03T22:23:45.694519+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2014-642efe379108139d
- Source row
- results[347]
- Raw source SHA-256
- 642efe379108139d70cbf0492188bfdaee07f4da1173b6bc01335f4de404a707
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2014-26-01
- Effective date printed in this edition
- 2015-01-28
Read 9 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) becomes effective January 28,
2015.
Exact source excerpt. Text positions 7974–8070, end exclusive, in the original decoded publication. SHA-256: 717bfc87629462b18e0f17bc7fa8dda922f34593a588aca7248e0a106833a835
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8070–8099, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Alpha Aviation Concept Limited Model R2160
airplanes, serial numbers 001 to 378, certificated in any category.
Exact source excerpt. Text positions 8099–8254, end exclusive, in the original decoded publication. SHA-256: 460799927a60d7576021ac44ecda8c773500664a47e57549f8d63949fd4d81d9
Subject
(d) Subject
Air Transport Association of America (ATA) Code 73: Engine Fuel
& Control.
Exact source excerpt. Text positions 8254–8348, end exclusive, in the original decoded publication. SHA-256: fd70899bb593313f613a5d6f4c3a61e04f9c2b425eb0ec2c7701a1a1bab1321a
Reason
(e) Reason
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated 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 paint adherence
defects inside the engine air intake box and cohesion defects inside
the laminated ducting from the filter to the air intake box. We are
issuing this AD to prevent paint defects from entering the engine
which could cause loss of power.
Exact source excerpt. Text positions 8348–8868, end exclusive, in the original decoded publication. SHA-256: 9e671618a678ca1b5200dbb46ff5f268fcdb36d99337cc1aec1028dd2ebf297b
Actions and Compliance
(f) Actions and Compliance
Unless already done, do the actions in paragraphs (f)(1) through
(f)(4) of this AD:
(1) Within the next 100 hours time-in-service (TIS) after
January 28, 2015 (the effective date of this AD) and repetitively
thereafter every 100 hours TIS, inspect any painted engine air
intake box (including the deflection flap) and the air intake
ducting (including the area downstream of the filter) for paint
adherence defects such as peeling, blistering, or bubbling following
Alpha Aviation Service Bulletin (SB) No. AA-SB-71-007, Revision 0,
dated August 2014.
(2) If any defects are found during the inspection required in
paragraph (f)(1) of this AD, before further flight, replace the
affected parts with airworthy parts following Alpha Aviation Service
Bulletin No. AA-SB-71-007, Revision 0, dated August 2014.
(3) As of January 28, 2015 (the effective date of this AD), do
not install a painted engine air intake box or a repaired engine air
duct on any affected airplane.
(4) The replacement of defective parts is not a terminating
action to the repetitive inspection of painted engine intake
components required in paragraph (f)(1) of this AD.
Exact source excerpt. Text positions 8868–10074, end exclusive, in the original decoded publication. SHA-256: 90fe2db51733a907eb1477f56deb3b00e1c4890b6e88b69660101511f1c68120
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: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; phone: (816) 329-4123; 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.
Exact source excerpt. Text positions 10074–11172, end exclusive, in the original decoded publication. SHA-256: c1e063977e74208807d0944509185b99abb72ff8c677c73844e909c17eb593d4
Related Information
(h) Related Information
Refer to MCAI Civil Aviation Authority (CAA) AD DCA/R2000/25A,
dated August 28, 2014, for related information. The MCAI can be
found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0759-0002.
Exact source excerpt. Text positions 11172–11440, end exclusive, in the original decoded publication. SHA-256: 058fb798128ab74ae13a1688f16b9e427fc19120996f7a763ce11b1731c4deff
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) Alpha Aviation Service Bulletin (SB) No. AA-SB-71-007,
Revision 0, dated August 2014.
(ii) Reserved.
(3) For Alpha Aviation Concept Limited service information
identified in this AD, contact Alpha Aviation, 59 Hautapu Road, RD
1, Cambridge 3493, New Zealand; telephone: +64 7 827 0528; fax: +64
7 929 2878; Internet: www.alphaaviation.co.nz.
(4) You may view this service information at the FAA, Small
Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For
[[Page 77376]]
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 11440–12694, end exclusive, in the original decoded publication. SHA-256: a1aab2bc95abc8a4f3bed92a9443cd65c7d4123f30bcffc4776aa8f3fce9f50e
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 2014-26-01 · 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: ab9a7b18c4a6a24fe728f53f4f87bd89bc34e72d029177ecbebf001390cfb549. Source manifest: 2e026bb34af8fc1f1a95c5ffbb1c0a187472dae0793924db5cdaaabf3b56c7a4.
Official source · 2014-12-24
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 79, Number 247 (Wednesday, December 24, 2014)]
[Rules and Regulations]
[Pages 77374-77376]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2014-29833]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0759; Directorate Identifier 2014-CE-028-AD;
Amendment 39-18052; AD 2014-26-01]
RIN 2120-AA64
Airworthiness Directives; Alpha Aviation Concept Limited
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
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 paint adherence defects inside the engine air intake box
and cohesion defects inside the laminated ducting from the filter to
the air intake box. We are issuing this AD to require actions to
address the unsafe condition on these products.
DATES: This AD is effective January 28, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of January 28,
2015.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0759; 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, 59 Hautapu Road, RD 1, Cambridge 3493, New Zealand;
telephone: +64 7 827 0528; fax: +64 7 929 2878; Internet:
www.alphaaviation.co.nz. You may review this 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,
901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816)
329-4123; 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 add an AD that would apply to Alpha Aviation Concept Limited
Model R2160 airplanes. The NPRM was published in the Federal Register
on October 2, 2014 (79 FR 59465). The NPRM proposed to correct an
unsafe condition for the specified products and was based on mandatory
continuing airworthiness information (MCAI) originated by an aviation
authority of another country. The MCAI states:
To prevent loss of engine power due to a possible paint
adherence defect inside the engine air intake box, accomplish the
following:
Inspect the engine air intake box (including the deflection
flap) and the engine air intake ducting (include the area downstream
of the filter) per Alpha Aviation Service Bulletin No. AA-SB-71-007
dated August 2014 or later approved revisions.
If any defects are found, replace affected parts per SB No. AA-
SB-71-007 before further flight.
The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0759-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 59465, October 2,
2014) 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 (79 FR 59465, October 2, 2014) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 59465, October 2, 2014).
Costs of Compliance
We estimate that this AD will affect 10 products of U.S. registry.
We also estimate that it would take about 1 work-hour per product to
comply with 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 $850, or $85 per product.
In addition, we estimate that any necessary follow-on actions would
take
[[Page 77375]]
about 6 work-hours and require parts costing $1,000, for a cost of
$1,510 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 by searching for and locating Docket No. FAA-2014-
0759; 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:
2014-26-01 Alpha Aviation Concept Limited: Amendment 39-18052;
Docket No. FAA-2014-0759; Directorate Identifier 2014-CE-028-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective January 28,
2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Alpha Aviation Concept Limited Model R2160
airplanes, serial numbers 001 to 378, certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 73: Engine Fuel
& Control.
(e) Reason
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated 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 paint adherence
defects inside the engine air intake box and cohesion defects inside
the laminated ducting from the filter to the air intake box. We are
issuing this AD to prevent paint defects from entering the engine
which could cause loss of power.
(f) Actions and Compliance
Unless already done, do the actions in paragraphs (f)(1) through
(f)(4) of this AD:
(1) Within the next 100 hours time-in-service (TIS) after
January 28, 2015 (the effective date of this AD) and repetitively
thereafter every 100 hours TIS, inspect any painted engine air
intake box (including the deflection flap) and the air intake
ducting (including the area downstream of the filter) for paint
adherence defects such as peeling, blistering, or bubbling following
Alpha Aviation Service Bulletin (SB) No. AA-SB-71-007, Revision 0,
dated August 2014.
(2) If any defects are found during the inspection required in
paragraph (f)(1) of this AD, before further flight, replace the
affected parts with airworthy parts following Alpha Aviation Service
Bulletin No. AA-SB-71-007, Revision 0, dated August 2014.
(3) As of January 28, 2015 (the effective date of this AD), do
not install a painted engine air intake box or a repaired engine air
duct on any affected airplane.
(4) The replacement of defective parts is not a terminating
action to the repetitive inspection of painted engine intake
components required in paragraph (f)(1) of this AD.
(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; phone: (816) 329-4123; 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.
(h) Related Information
Refer to MCAI Civil Aviation Authority (CAA) AD DCA/R2000/25A,
dated August 28, 2014, for related information. The MCAI can be
found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0759-0002.
(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) Alpha Aviation Service Bulletin (SB) No. AA-SB-71-007,
Revision 0, dated August 2014.
(ii) Reserved.
(3) For Alpha Aviation Concept Limited service information
identified in this AD, contact Alpha Aviation, 59 Hautapu Road, RD
1, Cambridge 3493, New Zealand; telephone: +64 7 827 0528; fax: +64
7 929 2878; Internet: www.alphaaviation.co.nz.
(4) You may view this service information at the FAA, Small
Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For
[[Page 77376]]
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 December 15, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-29833 Filed 12-23-14; 8:45 am]
BILLING CODE 4910-13-P
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