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2014-07-08: Fuselage

FAA order 2014-07-08 is an airworthiness directive in force since May 27, 2014. The FAA's subject line: Fuselage. It names Centrair 101: about 37 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: airframe structure.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Centrair
Models
101, 101A, 101AP, 101P
On this site
Centrair 101 37 registered

Dates and paperwork

In force since
May 27, 2014
Published
April 22, 2014 (signed April 4, 2014)
Docket
FAA-2014-0018
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 Centrair Model 101, 101A, 101AP, and 101P gliders. 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 structural damage to the fuselage. 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 (6,631 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: 2014-07-08 Centrair: Amendment 39-17822; Docket No. FAA-2014-0018; Directorate Identifier 2013-CE-049-AD. (a) Effective Date This airworthiness directive (AD) becomes effective May 27, 2014. (b) Affected ADs None. (c) Applicability This AD applies to CENTRAIR Models 101, 101A, 101P, and 101AP gliders, all serial numbers, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 53: Fuselage. (e) Reason This AD was prompted by 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 structural damage to the fuselage. We are issuing this AD to detect and correct structural damage not identified during routine maintenance inspections, which could lead to reduced structural integrity of the glider. [[Page 22371]] (f) Actions and Compliance Unless already done, do the following actions in paragraphs (f)(1) through (f)(3) of this AD: (1) Within 25 days after May 27, 2014 (the effective date of this AD) and repetitively thereafter at intervals not to exceed every 12 months, inspect all fuselage frames and ribs following the instructions in Soci[eacute]t[eacute] Nouvelle CENTRAIR Mandatory Service Bulletin 101-06, Revision 1, dated August 5, 2013. (2) If structural damage is detected during any inspection required by paragraph (f)(1) of this AD, before further flight, contact Soci[eacute]t[eacute] Nouvelle CENTRAIR at the address specified in paragraph (i) of this AD to obtain FAA-approved repair instructions approved specifically for this AD, and before further flight, repair the glider using these repair instructions. (3) Accomplishment of a repair, as required by paragraph (f)(2) of this AD, does not constitute terminating action for the inspection required by paragraph (f)(1) of this AD. Note 1 to paragraph (f) of this AD: We recommend that you also inspect the fuselage frames and ribs after the occurrence of any of the following events following the instructions in Soci[eacute]t[eacute] Nouvelle CENTRAIR Mandatory Service Bulletin 101-06, Revision 1, dated August 5, 2013: Landing with retracted gear, landing gear retraction during landing run, ground looping during take-off or landing, hard landing, or damage of internal structure of the fuselage. If structural damage is detected during any of these inspections, we recommend you contact Soci[eacute]t[eacute] Nouvelle CENTRAIR at the address specified in paragraph (i) of this AD for FAA-approved repair instructions. (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: Jim Rutherford, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4165; fax: (816) 329-4090; email: [email protected]. 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 areconsidered 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.: 2013-0258, dated October 25, 2013, for related information. The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0018-0002. (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) Soci[eacute]t[eacute] Nouvelle CENTRAIR Mandatory Service Bulletin 101-06, Revision 1, dated August 5, 2013. (ii) Reserved. (3) For Centrair Gliders service information identified in this AD, contact Soci[eacute]t[eacute] Nouvelle CENTRAIR, Aerodrome B.P. 44, F- 36300 LeBlanc, France; telephone: +33(0)254370796, fax: +33(0)254374864, email: [email protected]; Internet: none. (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

2004-11-15CE-05-16 ·
2004-01-23CE-04-49 ·
2004-01-06CE-04-39 ·
2000-12-19CE-01-09 ·

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 22, 2026. Connections as data: /graph/directive/2014-07-08.json · aircraft systems.