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###### Department of Transportation

###### Federal Aviation Administration

          - 14 CFR Part 39
          - [Docket No. FAA-2006-24956; Directorate Identifier 2006-CE-32-AD; Amendment 39-14835; AD 2006-24-06]
          - RIN 2120-AA64

# AGENCY:

Federal Aviation Administration (FAA), Department of Transportation (DOT).

# ACTION:

Final rule. 

# 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 ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor. We are issuing this AD to require actions that are intended to address the unsafe condition described in the MCAI.

# DATES:

This AD becomes effective January 3, 2007.

                        The Director of the                         **Federal Register**                         approved the incorporation by reference of certain publications listed in this AD as of January 3, 2007.                    

# ADDRESSES:

                        You may examine the AD docket on the Internet at                         *http://dms.dot.gov*                         or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC.                    

# FOR FURTHER INFORMATION CONTACT:

Gregory A. Davison, Aerospace Engineer, ACE-112, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4130; 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 August 9, 2006 (71 FR 45471). That NPRM proposed to require that you inspect and replace the pressure lines. The MCAI states that ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor were found during a requested maintenance event after engine trouble in the range between maximum continuous power and take off power. The cracks can be a result of non-complete temperature resistance.                

## Comments

We gave the public the opportunity to participate in developing this AD. We have considered the comments received.

Jack Buster with the Modification and Replacement Parts Association provides comments on the MCAI AD process pertaining to how the FAA addresses publishing manufacturer service information as part of a proposed AD action. The commenter states that the proposed rule attempt to require compliance with a public law by reference to a private writing (as referenced in paragraph (e) of the proposed AD). The commenter would like the FAA to incorporate by reference (IBR) the Stemme service bulletin.

We agree with Mr. Buster. However, we do not IBR any document in a proposed AD action; instead we IBR the document in the final rule. Since we are issuing the proposal as a final rule AD action, Stemme F&D Design Org. Service Bulletin A31-10-073, Am. Index 01.a, dated June 22, 2005, is incorporated by reference.

                    Mr. Buster requests IBR documents be made available to the public by publication in the                     **Federal Register**                     or in the Docket Management System (DMS).                

We are currently reviewing issues surrounding the posting of service bulletins in the Department of Transportation's DMS as part of the AD docket. Once we have thoroughly examined all aspects of this issue and have made a final determination, we will consider whether our current practice needs to be revised.

## Conclusion

We reviewed the available data, including the comments received, 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 a U.S. court of law. 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. These requirements, if any, take precedence over the actions copied from the MCAI.

## Costs of Compliance

                    We estimate that this AD will affect 43 products of U.S. registry. We also estimate that it will take about 4 work-hours per product to comply with this AD. The average labor rate is $80 per work-hour. Required parts will cost about $10 per product. Where the service information lists required parts                           ( print page 68998)                        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 $14,190 or $330 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 in 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                     *http://dms.dot.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 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

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

# PART 39—AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follow: 

Authority:49 U.S.C. 106(g), 40113, 44701.

§ 39.13 

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

**2006-24-06 STEMME GMBH & CO. AG:**                             Amendment 39-14835; Docket No. FAA-2006-24956; Directorate Identifier 2006-CD-32-AD.                        

## Effective Date

(a) This airworthiness directive (AD) becomes effective January 3, 2007.

## Affected ADs

(b) None.

## Applicability

(c) This AD applies to STEMME Model S10-VT sailplanes; certificated in any U.S. category:

(1) Serial numbers (S/Ns) 11-89 through 11-096; and

(2) All S/Ns where pressure lines were replaced between July 27, 2004, and June 22, 2005, inclusive, and the parts were provided by Stemme Gmbh & Co. AG (Stemme).

## Reason

(d) The mandatory continuing airworthiness information (MCAI) states that ripped pressure lines betweeen Airbox-Carburator-Differential fuel pressure sensor were found during a requested maintenance event after engine trouble in the range between maximum continuous power and take off power. The cracks can be a result of non complete temperature resistance. This type of pressure line was installed since July 27, 2004. It was used for serial production and spare parts.

## Actions and Compliance

(e) Unless already done, do the following actions.

(1) Within 30 days after the effective date of this AD, inspect all 0.15 - 0.27 inch (4 x 7mm) pressure lines for porousness or cracks in particular areas of T-splits parts, clamps, or connections. The free areas between the white plastic covers must also be checked. If cracks or porosity are found, before further flight, replace all pressure lines with ROTAX part number (P/N) 860 660 or Stemme P/N HZ-KLS041 (or FAA-approved equivalent P/Ns) pressure lines following STEMME F&D Design Org. Service Bulletin A31-10-73, Am. Index 01.a, dated June 22, 2005.

Within 60 days after the effective date of this AD, unless already done, replace all installed 0.15 x 0.27 inch (4 x 7 mm) pressure lines with ROTAX P/N 860 660 or Stemme P/N HZ-KLS041 (or FAA-approved equivalent P/Ns) pressure lines following STEMME F&D Design Org. Service Bulletin A31-10-073, Am. Index 01.a, dated June 22, 2005.

## 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: Gregory A. Davison, Aerospace Safety Engineer, FAA, Small Airplane Directorate, 901 Locuse, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4130; 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) Return to Airworthiness: When complying with this AD, do the FAA-approved corrective actions before returning the product to an airworthy condition.

(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056.

## Related Information

(h) This AD is related to MCAI Luftfahrt-Bundesamt AD D-2005-228, dated June 24, 2005, which references STEMME F & D Design Org. Service Bulletin A31-10-073, Am.-Index 01.a, dated June 22, 2005.

## Material Incorporated by Reference

(i) You must use STEMME F&D Design Org. Service Bulletin A31-10-073, Am.-Index 01.a, dated June 22, 2005, 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 Stemme GmbH & Co. AG, Flugplatzstraβe F 2, Nr. 7, D-15344 Strausberg, Germany; telephone + 49 33 41 36 12 0; facsimile: + 49 33 41 36 12 30.

                            (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:                             *http://www.archives.gov/​federal-register/​cfr/​ibr-locations.html*.                        

      ( print page 68999)    
Issued in Kansas City, Missouri, on November 20, 2006.

David R. Showers,

Acting Manager, Small Airplane Directorate, Aircraft Certification Service.

[FR Doc. 06-9428 Filed 11-28-06; 8:45am]

BILLING CODE 4910-13-M