
[Federal Register: April 15, 2008 (Volume 73, Number 73)]
[Rules and Regulations]               
[Page 20159-20161]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr15ap08-2]                         

=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0304; Directorate Identifier 2008-NE-08-AD; 
Amendment 39-15470; AD 2008-06-52]
RIN 2120-AA64

 
Airworthiness Directives; Thielert Aircraft Engines GmbH (TAE) 
Model TAE 125-02-99 Engines

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

ACTION: Final rule; request for comments.

-----------------------------------------------------------------------

SUMMARY: This document publishes in the Federal Register an amendment 
adopting emergency airworthiness directive (AD) 2008-06-52 that was 
sent previously to all known U.S. owners and operators of certain TAE 
Model TAE 125-02-99 engines. This AD requires, before further flight, 
replacing the high-pressure fuel line and installing a high-pressure 
fuel line support. This AD results from reports of in-flight engine 
shutdown incidents on airplanes equipped with TAE 125-02-99 engines. We 
are issuing this AD to prevent an in-flight engine shutdown or engine 
fire due to a cracked fuel line.

DATES: This AD becomes effective April 30, 2008 to all persons except 
those persons to whom it was made immediately effective by emergency AD 
2008-06-52, issued on March 12, 2008, which contained the requirements 
of this amendment. The Director of the Federal Register approved the 
incorporation by reference of certain publications listed in the 
regulations as of April 30, 2008.
    We must receive any comments on this AD by June 16, 2008.

ADDRESSES: Use one of the following addresses to comment on this AD.
     Federal eRulemaking Portal: Go to http://
www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility, U.S. Department of 
Transportation, 1200 New Jersey Avenue, SE., West Building Ground 
Floor, Room W12-140, Washington, DC 20590-0001.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
     Fax: (202) 493-2251.
    Contact Thielert Aircraft Engines GmbH, Platanenstrasse 14 D-09350, 
Lichtenstein, Germany, telephone: +49-37204-696-0; fax: +49-37204-696-
55; e-mail: info@centurion-engines.com, for the service information 
identified in this AD.

FOR FURTHER INFORMATION CONTACT: Jason Yang, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; e-mail 
jason.yang@faa.gov; telephone (781) 238-7747; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: On March 12, 2008, the FAA issued emergency 
AD 2008-06-52, that applies to TAE model TAE 125-02-99 engines with a 
serial number from 02-02-1500 through 02-02-2279. That AD requires, 
before further flight, replacing the high-pressure fuel line and 
installing a high-pressure fuel line support. That AD resulted from 
reports of in-flight engine shutdown incidents on airplanes equipped 
with TAE 125-02-99 engines. This was found to be the result of a 
cracked high-pressure fuel line between the high-pressure pump and fuel 
rail. These cracks were caused by excessive vibration of the fuel line. 
This condition, if not corrected, could result in an in-flight engine 
shutdown or engine fire due to a cracked fuel line.

Relevant Service Information

    We have reviewed and approved the technical contents of TAE Service 
Bulletin (SB) No. TM TAE 125-1005 P1, Revision 1, dated February 11, 
2008, and SB No. TM TAE 125-1005 P1, Revision 2, dated March 6, 2008. 
Those SBs describe procedures for installing a new high-pressure fuel 
line and a high-pressure fuel line bracket.

FAA's Determination and Requirements of This AD

    Since the unsafe condition described is likely to exist or develop 
on other engines of the same type design, we issued emergency AD 2008-
06-52 to prevent an in-flight engine shutdown or engine fire due to a 
cracked fuel line. This AD requires, before further flight, replacing 
the high-pressure fuel line and installing a high-pressure fuel line 
support. You must use the service information described previously to 
perform the actions required by this AD.

FAA's Determination of the Effective Date

    Since an unsafe condition exists that requires the immediate 
adoption of this AD, we have found that notice and opportunity for 
public comment before issuing this AD are impracticable, and that good 
cause existed to make the AD effective immediately on March 12, 2008, 
to all known U.S. owners and operators of certain TAE 125-02-99 
engines. These conditions still exist, and we are publishing the AD in 
the Federal Register as an amendment to Section 39.13 of part 39 of the 
Code of Federal Regulations (14 CFR part 39) to make it effective to 
all persons.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety and was not preceded by notice and an opportunity for public 
comment. However, we invite you to send us any written relevant data, 
views, or arguments regarding this AD. Send your comments to an address 
listed under ADDRESSES. Include ``AD Docket No. FAA-2008-0304; 
Directorate Identifier 2008-NE-08-AD'' in the subject line of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the rule that might 
suggest a need to modify it.
    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 
with FAA personnel concerning this AD. Using the search function of the 
Web site, anyone can find and read the comments in any of our dockets, 
including, if provided, the name of the individual who sent the comment 
(or signed the comment on behalf of an association, business, labor 
union, etc.). You may review the DOT's complete Privacy Act Statement 
in the Federal Register published on April 11, 2000 (65 FR 19477-78).

[[Page 20160]]

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Operations office 
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 Operations office (telephone (800) 647-5527) is the same as 
the Mail address provided in the ADDRESSES section. Comments will be 
available in the AD docket shortly after receipt.

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 have 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 that this AD:
    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 summary of the costs to comply with this AD and 
placed it in the AD Docket. You may get a copy of this summary at the 
address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Under the authority delegated to me by the Administrator, the Federal 
Aviation Administration amends part 39 of the Federal Aviation 
Regulations (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 adding the following new airworthiness 
directive:

2008-06-52 Thielert Aircraft Engines GmbH: Amendment 39-15470. 
Docket No. FAA-2008-0304; Directorate Identifier 2008-NE-08-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective April 
30, 2008, to all persons except those persons to whom it was made 
immediately effective by emergency AD 2008-06-52, issued March 12, 
2008, which contained the requirements of this amendment.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Thielert Aircraft Engines GmbH (TAE) 
model TAE 125-02-99 engines with a serial number (SN) from 02-02-
1500 through 02-02-2279. These engines are installed on, but not 
limited to, Cessna 172 and (Reims-built) F172 series (STC No. 
SA01303WI); and Diamond DA42 airplanes.

Unsafe Condition

    (d) This AD results from reports of in-flight engine shutdown 
incidents on airplanes equipped with TAE 125-02-99 engines. This was 
found to be the result of a cracked high-pressure fuel line between 
the high-pressure pump and fuel rail. These cracks were caused by 
excessive vibration of the fuel line. We are issuing this AD to 
prevent an in-flight engine shutdown or engine fire due to a cracked 
fuel line.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed before the next flight after the effective date of this 
AD, unless the actions have already been done.

Corrective Action

    (f) Before the next flight, install a new high-pressure fuel 
line and a high-pressure fuel line bracket using TAE Service 
Bulletin (SB) No. TM TAE 125-1005 P1, Revision 2, dated March 6, 
2008, or TAE SB No. TM TAE 125-1005 P1, Revision 1, dated February 
11, 2008.

Alternative Methods of Compliance

    (g) The Manager, Engine Certification Office, has the authority 
to approve alternative methods of compliance for this AD if 
requested using the procedures found in 14 CFR 39.19.

Special Flight Permits

    (h) We are limiting special flight permits to relocating the 
airplane to the next maintenance station, to a maximum flight 
duration of 2 hours, and to visual flight rules.

Related Information

    (i) EASA Emergency Airworthiness Directive (EAD) No. 2008-
0056R1-E, dated March 11, 2008, and EASA EAD No. 2008-0027-E, dated 
February 13, 2008, also address the subject of this AD.
    (j) Contact Jason Yang, Aerospace Engineer, Engine Certification 
Office, FAA, Engine and Propeller Directorate, 12 New England 
Executive Park, Burlington, MA 01803; e-mail: jason.yang@faa.gov; 
telephone: (781) 238-7747; fax: (781) 238-7199, for more information 
about this AD.

Material Incorporated by Reference

    (k) You must use the service information specified in Table 1 of 
this AD to perform the actions required by this AD. The Director of 
the Federal Register approved the incorporation by reference of the 
documents listed in Table 1 of this AD in accordance with 5 U.S.C. 
552(a) and 1 CFR part 51. You can get a copy from Thielert Aircraft 
Engines GmbH, Platanenstrasse 14 D-09350, Lichtenstein, Germany, 
telephone: +49-37204-696-0; fax: +49-37204-696-55; e-mail: 
info@centurion-engines.com. You may review copies at the FAA, New 
England Region, 12 New England Executive Park, Burlington, MA; 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.

                                      Table 1.--Incorporation by Reference
----------------------------------------------------------------------------------------------------------------
          Service Bulletin No.                     Page            Revision                  Date
----------------------------------------------------------------------------------------------------------------
TM TAE 125-1005 P1, Total Pages--6......  ALL..................            1  February 11, 2008.
TM TAE 125-1005 P1, Total Pages--6......  ALL..................            2  March 6, 2008.
----------------------------------------------------------------------------------------------------------------



[[Page 20161]]

    Issued in Burlington, Massachusetts, on April 10, 2008.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E8-8118 Filed 4-14-08; 8:45 am]

BILLING CODE 4910-13-P
