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PROPOSED AD ALPHA AVIATION CONCEPT LIMITED (TYPE CERTIFICATE PREVIOUSLY HELD BY ALPHA AVIATION DESIGN LIMITED): Docket No. FAA-2012-0279; Directorate Identifier 2012-CE-007-AD.
(a) COMMENTS DUE DATE

    We must receive comments by May 3, 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 the effective date of this
    AD,  replace  the  oil  hose  lines  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 the effective date of this AD, do not install any oil hose lines
    with part  number 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:
    karl.schletzbaum@faa.gov.  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 7843 8040;  email:
    customer.support@alphaaviation.co.nz;
    Internet: http://www.alphaaviation.co.nz. 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.

Issued in  Kansas City,  Missouri,  on  March 12, 2012.  James E. Jackson,
Acting  Manager,  Small   Airplane  Directorate,  Aircraft   Certification
Service.

DATES: We must receive comments on this proposed AD by May 3, 2012.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0279; Directorate Identifier 2012-CE-007-AD]
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: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for
Alpha Aviation Concept Limited Model R2160 airplanes. This proposed AD
results from 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 oil lines fitted to affected aircraft are not
fire resistant. We are issuing this proposed AD to require actions to
address the unsafe condition on these products.

DATES: We must receive comments on this proposed AD by May 3, 2012.

ADDRESSES: You may send comments by any of the following methods:

Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the
instructions for submitting comments.

Fax: (202) 493-2251.

Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.

Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.

For service information identified in this proposed 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: customer.support@alphaaviation.co.nz; Internet:
http://www.alphaaviation.co.nz. 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.

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 this
proposed AD, 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.

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:
karl.schletzbaum@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include "Docket No. FAA-2012-0279;
Directorate Identifier 2012-CE-007-AD" at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.

We will post all comments we receive, without change, to http://regulations.gov,
including any personal information you provide. We will also post a report
summarizing each substantive verbal contact we receive about this proposed AD.

Discussion

The Civil Aviation Authority (CAA), which is the aviation authority
for New Zealand, has issued AD DCA/R2000/40, dated February 23, 2012
(referred to after this as "the MCAI"), 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.

Relevant Service Information

Alpha Aviation has issued Service Bulletin AA-SB-79-001, Revision
0, dated February 2012; and Apex Aircraft has issued Service Bulletin
No. 020310, dated June 3, 2002. The actions described in this service
information are intended to correct the unsafe condition identified in
the MCAI.

FAA's Determination and Requirements of the Proposed AD

This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with this State of Design Authority, they
have notified us of the unsafe condition described in the MCAI and
service information referenced above. We are proposing this AD because
we evaluated all information and determined the unsafe condition exists
and is likely to exist or develop on other products of the same type
design.

Costs of Compliance

We estimate that this proposed 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 proposed 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 proposed 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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 proposed
regulation:

(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.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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]

2. The FAA amends Sec. 39.13 by adding the following new AD: