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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          ALL             1        February 11, 2008
    Total Pages – 6

    TM TAE 125-1005 P1          ALL             2        March 6, 2008
    Total Pages – 6
    ______________________________________________________________________

Issued in Burlington,  Massachusetts, on April  10, 2008. Peter  A. White,
Assistant   Manager,   Engine   and   Propeller   Directorate,    Aircraft
Certification Service.

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.
PREAMBLE 
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). 

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 

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 

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 airworthiness directive: