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CFR Citation: 14 CFR Part 39

Docket ID: [Docket No. FAA-2008-0055; Directorate Identifier 2007-CE-099-AD]

RIN ID: RIN 2120-AA64

NOTICE: PROPOSED RULES

ACTION: Airworthiness Directives:

DOCUMENT ACTION: Notice of proposed rulemaking (NPRM).

SUBJECT CATEGORY: Airworthiness Directives; Pacific Aerospace Limited Models FU24- 954 and FU24A-954 Airplanes

DATES: We must receive comments on this proposed AD by February 25, 2008.

DOCUMENT SUMMARY: We propose to adopt a new airworthiness directive (AD) for the products listed above. 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:

This AD is prompted by reports of loosening rivets securing the threaded inserts in the ends of the aileron control pushrods P/N 08 240151. Aileron pushpull rods P/N 08240151 have been installed on aircraft embodying PAC/FU/0340.
The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

SUMMARY: Pacific Aerospace Limited Models FU24-954 and FU24A-954 Airplanes,

SUPPLEMENTAL INFORMATION

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. FAA20080055; Directorate Identifier 2007CE099AD'' 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://www.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 of New Zealand (CAA), which is the aviation authority for New Zealand, has issued DCA/FU24/177, dated November 28, 2007, to correct an unsafe condition for the specified products. The MCAI states:

This AD is prompted by reports of loosening rivets securing the threaded inserts in the ends of the aileron control pushrods P/N 08 240151. Aileron pushpull rods P/N 08240151 have been installed on aircraft embodying PAC/FU/0340.
The MCAI requires an initial and repetitive inspection of the aileron and elevator control pushrods and requires corrective action as necessary.

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You may obtain further information by examining the MCAI in the AD docket.

Relevant Service Information

Pacific Aerospace Limited has issued PACSB/FU/091, Issue 2, dated November 12, 2007. 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.
Differences Between This Proposed 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 proposed different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a NOTE within the proposed AD.

Costs of Compliance

Based on the service information, we estimate that this proposed AD would affect about 2 products of U.S. registry. We also estimate that it would take about 1 workhour per product to comply with the basic requirements of this proposed AD. The average labor rate is $80 per workhour.

Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $160, or $80 per product.

In addition, we estimate that any necessary followon actions would take about 5 workhours and require parts costing $100, for a cost of $500 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 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); 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 proposed AD and placed it in the AD docket. List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, 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 39AIRWORTHINESS 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: Pacific Aerospace Limited: Docket No. FAA20080055; Directorate Identifier 2007CE099AD.
Comments Due Date
(a) We must receive comments by February 25, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to models FU24954 and FU24A954 airplanes, all serial numbers, certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 27: Flight Controls.
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:

This AD is prompted by reports of loosening rivets securing the threaded inserts in the ends of the aileron control pushrods P/N 08 240151. Aileron pushpull rods P/N 08240151 have been installed on aircraft embodying PAC/FU/0340.
The MCAI requires an initial and repetitive inspection of the aileron and elevator control pushrods and requires corrective action as necessary.
Actions and Compliance
(f) Unless already done, do the following actions:
(1) Within the next 50 hours timeinservice (TIS) after the effective date of this AD, inspect the pushrod ends on the aileron and elevator control pushrods part number (P/N) 08240151 following Pacific Aerospace Limited Service Bulletin No. PACSB/FU/091, Issue 2, dated November 12, 2007. Repetitively inspect thereafter at intervals not to exceed 150 hours TIS.
(2) Before further flight after any inspection where any rivets are found on aileron and elevator control pushrods P/N 08240151 that have detectable play between the pushrod and the insert or evidence of working rivets, replace the rivets following Pacific Aerospace Limited Service Bulletin No. PACSB/FU/091, Issue 2, dated November 12, 2007.

FAA AD Differences

Note: This AD differs from the MCAI and/or service information as follows: No differences.
Other FAA AD Provisions
(g) 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
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64106; telephone: (816) 3294146; fax: (816) 3294090. 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 FAAapproved. Corrective actions are considered FAAapproved 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 21200056.
Related Information
(h) Refer to MCAI Civil Aviation Authority of New Zealand (CAA), which is the aviation authority for New Zealand, DCA/FU24/177, dated November 28, 2007; and Pacific Aerospace Limited Service Bulletin No. PACSB/FU/091, Issue 2, dated November 12, 2007, for related information.

Issued in Kansas City, Missouri, on January 16, 2008. James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E81137 Filed 12308; 8:45 am]
BILLING CODE 491013P

FOR FURTHER INFORMATION CONTACT Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 3294146; fax: (816) 3294090.