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2014-04-02: Landing Gear

FAA order 2014-04-02 is an airworthiness directive in force since April 1, 2014. The FAA's subject line: Landing Gear. It names Dornier DORNIER 228: about 11 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: landing gear.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Dornier Luftfahrt GmbH
Models
Dornier 228-212
On this site
Dornier DORNIER 228 11 registered

Dates and paperwork

In force since
April 1, 2014
Published
February 25, 2014 (signed February 10, 2014)
Docket
FAA-2013-0962
Status
Current
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 DORNIER LUFTFAHRT GmbH Model 228-212 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as main landing gear axle failure caused by initial fatigue cracking and small pre-damage by corrosion. We are issuing this AD to require actions to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,630 characters)
Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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 AD: 2014-04-02 Dornier Luftfahrt GmbH: Amendment 39-17760; Docket No. FAA-2013-0962; Directorate Identifier 2013-CE-028-AD. (a) Effective Date This airworthiness directive (AD) becomes effective April 1, 2014. (b) Affected ADs None. [[Page 10350]] (c) Applicability This AD applies to DORNIER LUFTFAHRT GmbH Model 228-212 airplanes, all serial numbers, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 32: Landing Gear. (e) Reason This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as improper restoration of corrosion protection as the likely cause of initial fatigue cracking of the main landing gear (MLG) axle. We are issuing this AD to detect and correct possible corrosion and cracking of the MLG axle, which could lead to failure of the MLG axle resulting in a runway excursion with consequent damage to the airplane and injury to the occupants. (f) Actions and Compliance Unless already done, do the actions in paragraphs (f)(1) and (f)(2) of this AD: (1) Inspect the MLG axle following the Accomplishment Instructions in RUAG Aerospace Services GmbH Dornier 228 Service Bulletin No. SB-228-300, Revision 1, dated April 25, 2013, at the time specified in paragraphs (f)(1)(i) or (f)(1)(ii) of this AD. (i) If, as of April 1, 2014 (the effective date of this AD), the main landing gear (MLG) has 6,000 or more hours time-in-service (TIS) since new or is 10 years old or is more than 10 years old: Within the next 400 hours TIS after April 1, 2014 (the effective date of this AD) or within the next 6 months after April 1, 2014 (the effective date of this AD), whichever occurs first. (ii) If, as of April 1, 2014 (the effective date of this AD), the MLG has less than 6,000 hours TIS since new or is between 5 to 10 years old: Before or upon accumulating 6,400 hours TIS or within 6 months after April 1, 2014 (the effective date of this AD), whichever occurs first. (2) If, during the inspection required in paragraph (f)(1) of this AD, any discrepancies are found outside the limits specified in RUAG Aerospace Services GmbH Dornier 228 Service Bulletin No. SB- 228-300, Revision 1, dated April 25, 2013, before further flight, make all necessary corrective actions following the Accomplishment Instructions in RUAG Aerospace Services GmbH Dornier 228 Service Bulletin No. SB-228-300, Revision 1, dated April 25, 2013. (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4123; fax: (816) 329-4090; email: karl.schletzbaum@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, a federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (h) Related Information Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 2013-0209, dated September 10, 2013, for related information. The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2013-0962-0002. (i) Material Incorporated by Reference (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. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) RUAG Aerospace Services GmbH Dornier 228 Service Bulletin No. SB-228-300, Revision 1, dated April 25, 2013. (ii) Reserved. (3) For RUAG Aerospace Services GmbH service information identified in this AD, contact RUAG Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box 1253, 82231 Wessling, Germany; telephone: +49-(0)8153-30-2280; fax: +49-(0)8153-30-3030; Internet: http://www.ruag.com/en/Aviation/Aviation_Home. (4) You may view this service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (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.

Related safety bulletins advice on the same designs, not orders

2008-05-23CE-08-25 · Propellers/Propulsion - Controlling

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 October 5, 2026. Connections as data: /graph/directive/2014-04-02.json · aircraft systems.