AD 2012-26-13

Airworthiness directive · Software mapping · Thielert Aircraft Engines TAE 125-01, TAE 125-02-114 and TAE 125-02-99

Effective
February 13, 2013
Published
January 9, 2013 · 78 FR 1733–1735
Issued
December 27, 2012
Supersedes
AD2011-07-09
Models
TAE 125-01, TAE 125-02-114, TAE 125-02-99
Data sheet
TCDSE00069EN
Registered aircraft
111 matched by model
Product
Aircraft · Large airplane
Amendment
39-17308
Docket
FAA-2010-0820
Project
2010-NE-31-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 2012-31605. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

We are superseding an existing airworthiness directive (AD) for all Thielert Aircraft Engines GmbH models TAE 125-01, TAE 125-02-99, and TAE 125-02-114 reciprocating engines. That AD currently requires installation of full-authority digital electronic control (FADEC) software version 2.91. This new AD requires removing all software mapping versions prior to 292, 301, or 302, applicable to the TAE engine model. This AD was prompted by reports of possible power loss on airplanes equipped with TAE 125 engines. We are issuing this AD to prevent engine power loss or in-flight shutdown, resulting in reduced control of or damage to the airplane.

The airworthiness directive

2012-26-13 Thielert Aircraft Engines GmbH: Amendment 39-17308; Docket No. FAA-2010-0820; Directorate Identifier 2010-NE-31-AD.

(a) Effective Date

PDF page 2

This airworthiness directive (AD) is effective February 13, 2013.

(b) Affected ADs

PDF page 2

This AD supersedes AD 2011-07-09, Amendment 39-16646 (76 FR 17757, March 31, 2011).

(c) Applicability

PDF page 2

This AD applies to Thielert Aircraft Engines GmbH models TAE 125-01, TAE 125-02-99, and TAE 125-02-114 reciprocating engines installed in, but not limited to, Cessna 172 and (Reims-built) F172 series (European Aviation Safety Agency (EASA) Supplemental Type Certificate (STC) No. EASA.A.S.01527); Piper PA-28 series (EASA STC No. EASA.A.S. 01632); APEX (Robin) DR 400 series (EASA STC No. A.S.01380); and Diamond Aircraft Industries Models DA 40, DA 42, and DA 42M NG airplanes.

(d) Unsafe Condition

PDF page 2

This AD was prompted by reports of possible power loss on airplanes equipped with TAE 125 engines. We are issuing this AD to prevent engine power loss or in-flight shutdown, resulting in reduced control of or damage to the airplane.

(e) Compliance

PDF page 2

Unless already done, do the following. Within 55 flight hours or within 3 months of the effective date of the AD, or during the next scheduled maintenance, whichever occurs first, remove all full-authority digital electronic control (FADEC) software prior to versions 292, 301, and 302. Tables 1, 2, and 3 to paragraph (e) provide the software mapping and respective part numbers for software versions 292, 301, and 302, installed on the TAE 125-01, TAE 125-02-99, and TAE-125-02-114 engines, respectively.

Table 1 to Paragraph ( e) for TAE 125-01 Engines
Software mappingPart No.
T14V292CES20-7610-55104R9.
T28V292CES20-7610-55105R7.
T14V292PIP40-7610-55106R9.
T28V292PIP40-7610-55107R7.
T14V292APEX60-7610-55106R9.
T14V292DIA50-7610-55105R9.
R28V292DIA50-7610-55107R5.
Table 2 to Paragraph ( e) for TAE 125-02-99 Engines
Software mappingPart No.
O14V301CES20-7610-E000110.
O28V301CES20-7610-E001110.
O14V301PIP40-7610-E000110.
O28V301PIP40-7610-E001110.
O14V301APEX60-7610-E000110.
O14V301DA4050-7610-E000110.
O28V301DA4252-7610-E000505.
Table 3 to Paragraph ( e) for TAE 125-02-114 Engines
Software mappingPart No.
P14V302CES20-7610-E002007.
P28V302CES20-7610-E003007.
P28V302PIP40-7610-E003007.
P14V302APEX60-7610-E002007.
P14V302DA4050-7610-E002007.

(f) Alternative Methods of Compliance (AMOCs)

PDF page 2

The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request.

(g) Related Information

PDF page 2

(1) For more information about this AD, contact Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; email: robert.green@faa.gov; phone: 781-238-7754; fax: 781-238 7199.

(2) Refer to MCAI European Aviation Safety Agency Airworthiness Directive No. 2012-0116, dated July 3, 2012, and Thielert Aircraft Engines Service Bulletin TM TAE 000-0007, Revision 19, dated August 31, 2012, for related information.

(3) For service information identified in this AD, contact Thielert Aircraft Engines GmbH, Platanenstrasse 14 D-09350, Lichtenstein, Germany, phone: +49-37204-696-0; fax: +49-37204-696-55; email: info@centurion-engines.com. 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.

(h) Material Incorporated by Reference

PDF page 2

None.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD is effective February 13, 2013.

AddressesPage 1

For service information identified in this AD, contact Thielert Aircraft Engines GmbH, Platanenstrasse 14 D-09350, Lichtenstein, Germany, phone: +49-37204-696-0; fax: +49-37204-696-55; email: info@centurion-engines.com. 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.

For further information contactPage 2

Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; email: robert.green@faa.gov; phone: 781-238-7754; fax: 781-238-7199.

DiscussionPage 2

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2011-07-09, Amendment 39-16646 (76 FR 17757, March 31, 2011). That AD applies to the specified products. The NPRM published in the Federal Register on September 17, 2012 (77 FR 57041). That NPRM proposed to require removing all software mapping versions prior to 292, 301, or 302, applicable to the TAE engine model.

CommentsPage 2

We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public.

ConclusionPage 2

We reviewed the relevant data and determined that air safety and the public interest require adopting the AD as proposed.

Costs of CompliancePage 2

We estimate that this AD will affect about 112 engines installed on airplanes of U.S. registry. We also estimate that it will take about 0.5 work hours per product to comply with this proposed AD. The average labor rate is $85 per work hour. Based on these figures, we estimate the cost of the AD to U.S. operators to be $4,760

Authority for This RulemakingPage 2

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 findingsPage 2

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 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.

Adoption of the AmendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

Adoption of the amendmentPage 2

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by removing airworthiness directive (AD) 2011-07-09, Amendment 39-16646 (76 FR 17757, March 31, 2011), and adding the following new AD:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 111

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Diamond Aircraft Ind81 aircraft
  • Piper27 aircraft
  • Cessna1 aircraft
  • Elwood Enterprises1 aircraft
  • Glasair Aviation USA1 aircraft
By year built
19832026
Registered aircraft by year built: 105 aircraft
19831
20053
200623
200743
20086
20141
20151
20221
20242
202513
202611

6 with no year recorded

By model

Aircraft

See all 111 aircraft