[Federal Register Volume 76, Number 2 (Tuesday, January 4, 2011)]
[Rules and Regulations]
[Pages 253-255]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-32798]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1286; Directorate Identifier 2010-CE-064-AD; 
Amendment 39-16563; AD 86-25-07 R1]
RIN 2120-AA64


Airworthiness Directives; ROLLADEN-SCHNEIDER Flugzeugbau GmbH 
Model LS6 Gliders

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: We are rescinding an existing airworthiness directive (AD) for 
the products listed above. The existing AD resulted 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:

    During flights at speeds between 250 to 270 km/h (135 to 145 
kts) aileron flutter occurred resulting in damage of control stick 
attachment.


[[Page 254]]


    Since issuance of that AD, we have determined that the AD is not 
applicable because the Model LS6 is not type certificated in the United 
States.

DATES: This AD is effective January 19, 2011.
    We must receive comments on this AD by February 18, 2011.

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.

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 AD, the regulatory evaluation, 
any comments received, and other information. The street address for 
the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. 
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aerospace Engineer, 
Small Airplane Directorate, FAA, 901 Locust, Room 301, Kansas City, 
Missouri 64106; phone: (816) 329-4165; fax: (816) 329-4090; e-mail: 
[email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    In 1986, we issued AD 86-25-07, Amendment 39-5487 (51 FR 44901, 
December 15, 1986). That AD required actions intended to address an 
unsafe condition on the products listed above. Since we issued AD 86-
25-07, we have determined that the AD is not applicable because the 
only version of the Model LS6 type certificated in the United States is 
the Model LS6-c. Since the Model LS6 is not type certificated in the 
United States, there are no airplanes affected by that AD. We have also 
determined that the unsafe condition does not exist in the Model LS6-c 
gliders.

FAA's Determination

    We are issuing this AD rescission because we evaluated all the 
relevant information and determined the existing AD is not applicable 
to the Model LS6 glider, and the unsafe condition described previously 
is not likely to exist or develop in the Model LS6-c gliders type 
design.

FAA's Justification and Determination of the Effective Date

    AD 86-25-07 is not applicable to the Model LS6 because it is not 
type certificated in the United States. Therefore, we find that notice 
and opportunity for prior public comment are unnecessary and that good 
cause exists for making this amendment effective in less than 30 days.

Comments Invited

    Although this is a final rule that was not preceded by notice and 
an opportunity for public comment, we invite you to submit any written 
relevant data, views, or arguments regarding this AD. Send your 
comments to an address listed under the ADDRESSES section. Include the 
docket number FAA-2010-1286 and Directorate Identifier 2010-CE-064-AD 
at the beginning of your comments. We specifically invite comments on 
the overall regulatory, economic, environmental, and energy aspects of 
this AD. We will consider all comments received by the closing date and 
may amend this 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 AD.

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

    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 that 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),
    (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, Safety.

Adoption of the Amendment

0
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 rescinding AD 86-25-07, Amendment 39-
5487 (51 FR 44901, December 15, 1986):

86-25-07 R1 ROLLADEN-SCHNEIDER Flugzeugbau GmbH: Amendment 39-16563; 
Docket No. FAA-2010-1286; Directorate Identifier 2010-CE-064-AD.

Effective Date

    (a) This AD is effective January 19, 2011.

Affected ADs

    (b) This AD rescinds AD 86-25-07.

Applicability

    (c) This AD rescission applies to Model LS6 gliders, all serial 
numbers, that are certified in any category.

Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 27, Flight Controls.


[[Page 255]]


    Issued in Kansas City, Missouri, on December 21, 2010.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010-32798 Filed 1-3-11; 8:45 am]
BILLING CODE 4910-13-P