[Docket No. FAA-2015-1383; Directorate Identifier 2015-NE-15-AD] 

RIN 2120-AA64 

Airworthiness Directives; Technify Motors GmbH Reciprocating Engines 

AGENCY: Federal Aviation Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking (NPRM). 

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Technify 

Motors GmbH T AE 125-02 reciprocating engines with a dual mass flywheel installed. 

This proposed AD was prompted by reports of a gearbox drive shaft breaking during 

starting or restarting of the engine. This proposed AD would require installation of a start 

phase monitoring system and associated specified software. We are proposing this AD to 

prevent overload and failure of the gearbox drive shaft, which could lead to failure of the 

engine, in-flight shutdown, and loss of control of the airplane. 

DATES: We must receive comments on tllis proposed AD by (INSERT DATE 60 

DAYS AFTER DATE OF PUBLICA TfON IN THE FEDERAL REGISTER]. 

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. 
Monday through Friday, except Federal holidays. 

• Fax: 202-493-2251. 

For service information identified in this proposed AD, contact Technify Motors 

GmbH, Platanenstrasse 14, D-09356 Sankt Egidien, Germany; phone: +49 37204 696 0; 

fax: +49 37204 696 29125; email: info@centurion-engines.com; and Diamond Aircraft 

Industries GmbH, N. A. Otto-Strasse 5, 2700 Wiener Neustadt, Austria; phone: +43 2622 

26700; fax: +43 2622 26700 1369; email: airworthiness@diamond-air.at. You may view 

this service information at the FAA, Engine & Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. For information on the availability of this material at 

the FAA, call 781-238-7125. It is also available on the Internet at 

http://www.regulations.gov by searching for and locating Docket No. FAA-2015-1383. 

Examining the AD Docket 

You may examine the AD docket on the Internet at http://www.regulations.gov by 

searching for and locating Docket No. FAA-2015-1383; 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 proposed AD, the mandatory continuing 

airworthiness information (MCAI), the regulatory evaluation, any comments received, and other information. The 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. 

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SUPPLEMENTARY INFORMATION: 

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-2015-1383; Directorate Identifier 20 15-NE-15-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 based on 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 with FAA personnel 

conceming this proposed AD. 

Discussion 

The European Aviation Safety Agency (EASA), which is the Technical Agent for 

the Member States ofthe European Community, has issued EASA AD 2015-0055, dated 

March 31, 2015 (referred to hereinafter as "the MCAI"), to correct an unsafe condition 

for the specified products. The MCAl states: 

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This condition, if not corrected, could lead to engine power loss 

during flight, possibly resulting in loss of control of the aeroplane. 

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

the Internet at http://www.regulations.gov by searching for and locating Docket No. 

FAA-2015-1383. 

Related Service Information under 1 CFR Part 51 

Technify Motors GmbH (type certificate previously held by Thielert Aircraft 

Engines GmbH) issued Technify Motors Service Bulletin (SB) No. SB TMG 125-1018 

PI, Revision 1, dated February 5, 2015. The service information describes procedures for 

installing a start phase monitoring system and associated specified software mapping on 

particular airplane models. This service information is reasonably available because the 

interested parties have access to it through their nonnal course of business or by the 

means identified in the ADDRESSES section of this NPRM. 

Other Related Service Information 

Technify Motors GmbH has also issued Technify Motors SB No. TM T AE 000-

0007, Revision 28, dated February 5, 2015; Technify Motors Installation Manual No. IM02-02, Issue 4, Revision 2, dated January 30, 2015, with Chapter 02-IM-13-02, section 

13.8.16, Revision 1, dated November 28, 2014; Technify Motors SB No. SB TMG 601-

1007 PI, Revision 3, dated February 5, 2015; and Technify Motors SB No. SB TMG 

651-1004 Pl, Revision 2, dated February 5, 2015. 

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monitoring system and associated specified software mapping. 

FAA's Determination and Requirements of This Proposed AD 

This product has been approved by the aviation authority of Germany, and is 

approved for operation in the United States. Pursuant to our bilateral agreement with the 

European Community, EASA has notified us ofthe unsafe condition described in the 

MCAI and service information referenced above. We are proposing this AD because we 

evaluated all information provided by EASA and detem1ined the unsafe condition exists and is likely to exist or develop on other products of the same type design. This proposed 

AD would require installation of specified software mapping and a start phase monitoring 

system. 

Costs of Compliance 

We estimate that this proposed AD affects 97 engines installed on airplanes of 

U.S. registry. We also estimate that it would take about 3 hours per engine to comply 

with this proposed AD. The average labor rate is $85 per hour. For 13 ofthe engines, 

required parts cost about $285 per engine. For 84 of the engines, required parts cost about 

$206 per engine. Based on these figures, we estimate the cost of this proposed AD on 

U.S. operators to be $45,744. 

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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 detennined 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 11 034, February 26, 1979), 

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List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation safety, Incorporation by reference, 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. 1 06(g), 40113, 44701. 

§ 39.13 [Amended) 

2. The FAA amends § 39.1 3 by adding the followi ng new airworthiness directive 

(AD): 

Technify Motors GmbH (Type Certificate Previously Held by Thielert Aircraft 

Engines GmbH): Docket No. FAA-2015-1383; Directorate Identifier 2015-NE-15-AD. 

(a) Comments Due Date 

We must receive comments by [INSERT DATE 60 DAYS AFTER DATE OF 

PUBLICATION INTI fE FEDERAL REGISTER]. 

(b) Affected ADs 

None. 

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flywheel installed. 

(d) Reason 

This AD was prompted by reports of a gearbox drive shaft breaking during 

starting or restarting of the engine. We are issuing this AD to prevent overload and failure 

of the gearbox drive shaft, which could lead to failure of the engine, in-flight shutdown, 

and loss of control of the airplane. 

(e) Actions and Compliance 

Comply with this AD within the compliance times specified, unless already done. 

Within II 0 flight hours or at the next scheduled inspection after the effective date 

of this AD, whichever occurs fust, install a start phase monitoring system and software 

mapping. Use Technify Motors Service Bulletin (SB) No. SB TM 125-1018 P1, Revision 

1, dated February 5, 2015, to do the installation. 

(t) Installation Prohibition 

After the effective date of this AD, do not install onto any airplane any Technify 

Motors T AE 125-02-99 or T AE 125-02-114 reciprocating engine that is not equipped 

with a start phase monitoring system and software mapping. 

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(h) Related Information 

(1) For more infom1ation about this AD, contact Robert Green, Aerospace 

Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 01803; phone: 781-238-7754; fax: 781-238-

7199; email: robert.green@faa.gov. 

(2) Refer to MCAI European Aviation Safety Agency AD 2015-0055, dated 

March 31,2015, for more information. You may examine the MCAI in the AD docket on 

the Internet at http://www.regulations.gov by searching for and locating it in Docket No. 

FAA-2015-1383. 

(3) Technify Motors SB No. SB TMG 125-1018 PI, Revision 1, dated February 

5, 2015; Technify Motors SB No. TM TAE 000-0007, Revision 28, dated February 5, 

2015; Technify Motors Installation Manual No. IM-02-02, Issue 4, Revision 2, dated January 30,2015, with Chapter 02-IM-13-02, section 13.8.16, Revision 1, dated 

November 28, 2014; Technify Motors SB No. SB TMG 601-1007 PI, Revision 3, dated 

February 5, 2015; and Technify Motors SB No. SB TMG 651-1004 PI, Revision 2, dated 

February 5, 2015, can be obtained from Technify Motors GmbH, using the contact 

information in paragraph (h)(5) of this proposed AD. 

(4) Diamond Aircraft Industries GmbH MSB No. 42-109/1, dated February 4, 

2015; and DAl MSB No. 42-007/16, dated February 4, 2015, can be obtained from 

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phone: +49-37204-696-0; fax: +49-37204-696-55; email: info@centurion-engines.com. 

For DAI service information identified in this proposed AD, contact Diamond Aircraft 

Industries GmbH, N. A. Otto-Strasse 5, 2700 Wiener Neustadt, Austria; phone: +43 2622 

26700; fax: +43 2622 26700 1369; email: airworthiness@diamond-air.at. 

(6) You may view this service information at the FAA, Engine & Propeller 

Directorate, 12 New England Executive Park, Burlington, MA. For information on the 

availability of this material at the FAA, call 781-238-7125. 

Issued in Burlington, Massachusetts, on June 26, 2015. 

Ann C. Mollica, Acting Directorate Manager, Engine & Propeller Directorate, 

Aircraft Certification Service. 

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