Airworthiness directives: SOCATA-Groupe Aerospatiale,

[Federal Register: April 24, 2007 (Volume 72, Number 78)]

[Proposed Rules]

[Page 20300-20302]

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

[DOCID:fr24ap07-16]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27432; Directorate Identifier 2007-CE-017-AD]

RIN 2120-AA64

Airworthiness Directives; SOCATA--Groupe AEROSPATIALE Model TB 9, TB 10, and TB 200 Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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:

* * * a new life limit for engine and Nose Landing Gear (NLG) mounts installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as defined in the updated Airworthiness Limitations Section (ALS) of the relevant Aircraft Maintenance Manuals (AMM).

[[Page 20301]]

The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by May 24, 2007.

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

DOT Docket Web Site: Go to http://dms.dot.gov and follow

the instructions for sending your comments electronically.

Fax: (202) 493-2251.

Mail: Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590-0001.

Hand Delivery: Room PL-401 on the plaza level of the Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

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

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 this proposed AD, 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.

FOR FURTHER INFORMATION CONTACT: Albert J. Mercado, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; 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. This 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 proposed AD references the MCAI and related service information that we considered in forming the engineering basis to correct the unsafe condition. The proposed AD contains text copied from the MCAI and for this reason might not follow our plain language principles.

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-2007- 27432; Directorate Identifier 2007-CE-017-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://dms.dot.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 European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued AD No. 2007-0034, dated February 22, 2007 (referred to after this as ``the MCAI''), to correct an unsafe condition for the specified products. The MCAI states:

* * * a new life limit for engine and Nose Landing Gear (NLG) mounts installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as defined in the updated Airworthiness Limitations Section (ALS) of the relevant Aircraft Maintenance Manuals (AMM).

The MCAI requires: * * * introduction of the new 10 000 Flight Hour life limit for engine and NLG mounts into the operator's maintenance program through the Revision 18 of the AMM.

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

Relevant Service Information

SOCATA--Groupe AEROSPATIALE has issued:

SOCATA TB 9 Model Maintenance Manual, Original version dated September 1991, Revision 18, dated September 2006;

SOCATA TB 10 Model Maintenance Manual, Original version dated September 1991, Revision 18, dated September 2006; and

SOCATA TB 200 Model Maintenance Manual, Original version dated September 1991, Revision 18, dated September 2006.

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 146 products of U.S. registry. We also estimate that it would take about 0.5 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $80 per work-hour.

Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $5,840, or $40 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

[[Page 20302]]

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 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:

   SOCATA--Groupe AEROSPATIALE: Docket No. FAA-2007-27432; Directorate Identifier 2007-CE-017-AD.

   Comments Due Date

   (a) We must receive comments by May 24, 2007.

   Affected ADs

   (b) None.

   Applicability

   (c) This AD applies to Model TB 9, TB 10, and TB 200 airplanes, all serial numbers, certificated in any category.

   Subject

   (d) Air Transport Association of America (ATA) Code 5: Time Limits.

   Reason

   (e) The mandatory continuing airworthiness information (MCAI) states:

   * * * a new life limit for engine and Nose Landing Gear (NLG) mounts installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as defined in the updated Airworthiness Limitations Section (ALS) of the relevant Aircraft Maintenance Manuals (AMM).

   Actions and Compliance

   (f) Unless already done, within the next 30 days after the effective date of this AD, incorporate the life limits in the Airworthiness Limitations documents presented in paragraphs (f)(1), (f)(2), or (f)(3) of this AD into the FAA-approved maintenance program. This may be done by updating the Airworthiness Limitations Section of the Airplane Maintenance Manual (AMM) and inserting the following applicable revision. The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may do this action. Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).

   (1) For Model TB 9 airplanes: Use SOCATA TB 9 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006, or later revision that incorporates the same life limit for the engine mount and NLG mount as the above referenced Revision 18;

   (2) For Model TB 10 airplanes: Use SOCATA TB 10 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006, or later revision that incorporates the same life limit for the engine mount and NLG mount as the above referenced Revision 18; or

   (3) For Model TB 200 airplanes: Use SOCATA TB 200 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006, or later revision that incorporates the same life limit for the engine mount and NLG mount as the above referenced Revision 18.

   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 Staff, FAA, ATTN: Albert J. Mercado, Aerospace Safety Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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, 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 2120-0056.

   Related Information

   (h) Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2007-0034, dated February 22, 2007; SOCATA TB 9 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006; SOCATA TB 10 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006; and SOCATA TB 200 Model Maintenance Manual, 04, Airworthiness Limitations, Original version dated September 1991, Revision 18, dated September 2006, for related information.

   Issued in Kansas City, Missouri, on April 17, 2007. Charles L. Smalley, Acting Manager, Small Airplane Directorate, Aircraft Certification Service.

   [FR Doc. E7-7756 Filed 4-23-07; 8:45 am]

   BILLING CODE 4910-13-P