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2018-18-02: Reciprocating Engine Power Section

FAA order 2018-18-02 is an airworthiness directive in force since November 29, 2018. The FAA's subject line: Reciprocating Engine Power Section. It names the Austro Engine E4P(series engine: about 148 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Engine
Makes
Austro Engine GmbH
Models
E4, E4P
Engine series
Austro Engine E4P(series 148 aircraft

Dates and paperwork

In force since
November 29, 2018
Published
October 25, 2018 (signed October 19, 2018)
Docket
FAA-2017-1138
Replaced by
2020-15-05
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Austro Engine GmbH model E4 engines and for all model E4P engines. This AD was prompted by reports of considerable wear on the timing chain on these engines. This AD requires replacement of the timing chain and amending certain airplane flight manuals to limit the use of windmill restarts. We are issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,551 characters)
Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): \n\nAD 2018-18-02; Austro Engine GmbH Engines: Amendment 39-19381; Docket No. FAA-2017-1138; Product Identifier 2017-NE-41-AD. \n\n(a) Effective Date \n\n\n\tThis AD is effective November 29, 2018. \n\n(b) Affected Ads \n\n\n\tNone. \n\n(c) Applicability \n\n\n\tThis AD applies to Austro Engine GmbH model E4 engines with serial numbers that have a ''-B'' or ''-C'' configuration and to model E4P engines, all serial numbers. \n\n(d) Subject \n\n\n\tJoint Aircraft System Component (JASC) Code 8520, Reciprocating Engine Power Section. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by reports of considerable wear on the timing chain on these engines. We are issuing this AD to prevent failure of the engine timing chain. The unsafe condition, if not addressed, could result in failure of the engine timing chain, loss of engine thrust control, and reduced control of the airplane. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Actions \n\n\n\t(1) Determine whether the engine is a Group 1 or Group 2 engine as follows. \n\t(i) A Group 1 engine is an engine equipped with a timing chain that was installed on an engine that experienced a windmill restart, or an engine in which it cannot be determined if the engine experienced any windmilling restarts. \n\t(ii) A Group 2 engine is an engine that is equipped with a timing chain that has not experienced any windmilling restarts. \n\t(2) For Group 1 engines: Before the affected timing chain exceeds 945 engine flight hours (EFHs) since installation on an engine, or within 110 EFHs after the effective date of this AD, whichever occurs later, replace the timing chain in accordance with the instructions in Technical Details, paragraph 2, in Austro Engine Mandatory Service Bulletin (MSB) No. MSB-E4-017/2, Revision 2, dated December 2, 2016. \n\t(3) For Group 1 and Group 2 engines: After the effective date of this AD, following each windmill restart of an engine, before the timing chain of that engine exceeds 945 EFHs since first installation on an engine, or within 110 EFHs after that windmilling restart, whichever occurs later, replace the timing chain in accordance with the instructions in Technical Details, paragraph 2, in Austro Engine MSB No. MSB-E4-017/2, Revision 2, dated December 2, 2016. \n\t(4) For Group 1 and Group 2 engines: Within 30 days after the effective date of this AD, amend the applicable airplane flight manual under emergency procedures by adding the information in figure 1 to paragraph (g)(4) of this AD to limit the use of a windmilling restart to only an emergency procedure. \n\n((Page 53805)) \n\n(GRAPHIC) (TIFF OMITTED) TR25OC18.000 \n\n\n\t(5) For affected Austro Engine GmbH model E4 engines installed on Diamond Aircraft Industries (DAI) model DA 42 NG and DA 42 M-NG airplanes and for Austro Engine GbmH model E4P engines installed on DAI model DA 62 airplanes, using Airplane Flight Manual (AFM) Temporary Revision (TR) TR-M(Auml)M-42-973, and AFM TR TR-M(Auml)M- 62-240, both dated August 12, 2016, respectively, to update the applicable AFM is an acceptable method to comply with paragraph (g)(4) of this AD. \n\n(h) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The manager, ECO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local flight standards district office, as appropriate. If sending information directly to the managerof the ECO Branch, send it to the attention of the person identified in paragraph (i)(1) of this AD. You may email your request to: [email protected]. \n\t(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office. \n\n(i) Related Information \n\n\n\t(1) For more information about this AD, contact Barbara Caufield, Aerospace Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7146; fax: 781-238-7199; email: [email protected]. \n\t(2) Refer to EASA AD 2017-0103, dated June 14, 2017, for more information. You may examine the EASA AD in the AD docket on the internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2017-1138. \n\n(j) Material Incorporated by Reference \n\n\n\t(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. \n\t(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. \n\t(i) Austro Engine Mandatory Service Bulletin No. MSB-E4-017/2, Revision 2, dated December 2, 2016. \n\t(ii) Diamond Aircraft Airplane Flight Manual (AFM) Temporary Revision (TR) TR-M(Auml)M-42-973, dated August 12, 2016. \n\t(iii) Diamond Aircraft AFM TR TR-M(Auml)M-62-240, dated August 12, 2016. \n\t(3) For Austro Engine GmbH service information identified in this AD, contact Austro Engine GmbH, Rudolf-Diesel-Strasse 11, A- 2700 Weiner Neustadt, Austria; phone +43 2622 23000; fax: +43 2622 23000-2711; internet: www.austroengine.at. For Diamond Aircraft Industries service information in this AD, contact Diamond Aircraft Industries, N. A., Otto-Stra(szlig)e 5, A-2700 Wiener Neustadt, phone: +43 2622 26700, Fax: +43 2622 26780; internet: www.diamondaircraft.com. \n\t(4) Youmay view this service information at FAA, Engine and Propeller Standards Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781-238-7759. \n\t(5) You may view this service information that is incorporated by reference 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. \n\n\n\n((Page 53806))

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2018-18-02.json · aircraft systems.