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2014-15-02: Flight Controls

FAA order 2014-15-02 is an airworthiness directive in force since August 27, 2014. The FAA's subject line: Flight Controls. It names Burkhart Grob Flugzeugbau G102, Burkhart Grob G-103: about 130 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Burkhart Grob Luft-Und; GROB-WERKE GMBH & CO KG
Models
G 103 C Twin III SL, G103 Twin II, G103A Twin II Acro, G103C Twin III Acro, G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, G102 Standard Astir III
On this site
Burkhart Grob Flugzeugbau G102 59 registered
Burkhart Grob G-103 71 registered

Dates and paperwork

In force since
August 27, 2014
Published
July 23, 2014 (signed July 14, 2014)
Docket
FAA-2014-0292
Replaced by
2014-15-02 R1
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 GROB- WERKE GMBH & CO KG Models G102 STANDARD ASTIR III, G102 CLUB ASTIR III, and G102 CLUB ASTIR IIIb gliders and BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG Models G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL 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 plastic control cable pulleys developing cracks due to aging. 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 (6,451 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: 2014-15-02 GROB-WERKE GMBH & CO KG and BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG: Amendment 39-17904; Docket No. FAA-2014- 0292; Directorate Identifier 2014-CE-011-AD. (a) Effective Date This airworthiness directive (AD) becomes effective August 27, 2014. (b) Affected ADs None. (c) Applicability This AD applies to GROB-WERKE GMBH & CO KG Models G102 STANDARD ASTIR III, G102 CLUB ASTIR III, and G102 CLUB ASTIR IIIb gliders and BURKHART GROB LUFT-UND RAUMFAHRT GmbH & CO KG Models G103 TWIN II, G103A TWIN II [[Page 42660]] ACRO, G103C TWIN III ACRO and Model G 103 C Twin III SL gliders with the following serial numbers (S/N), certificated in any category. (1) G102 STANDARD ASTIR III, S/N 5501 through 5652. (2) G102 CLUB ASTIR III, S/N 5501 through 5652. (3) G102 CLUB ASTIR IIIb, S/N 5501 through 5652. (4) G103 TWIN II, S/N 3730 through 34078. (5) G103A TWIN II ACRO, S/N 3730 through 34078. (6) G103C TWIN III ACRO, S/N 34101 through 34203. (7) G 103 C Twin III SL, S/N 35002 through 35051. (d) Subject Air Transport Association of America (ATA) Code 27: Flight Controls. (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 plastic control cable pulleys developing cracks due to aging. We are issuing this AD to detect and correct plastic control cable pulleys in the rudder control unit,which could lead to breaking of the pulley and potentially jamming the rudder control unit, possibly resulting in loss of control of the glider. (f) Actions and Compliance Comply with this AD within the compliance times specified in paragraphs (f)(1) through (f)(3) of this AD, unless already done. (1) For all Models G103C TWIN III ACRO and G 103 C Twin III SL gliders: Within 3 months after August 27, 2014 (the effective date of this AD), inspect the rudder control unit for installation of plastic cable pulleys. If plastic cable pulleys are installed, before further flight, replace the plastic cable pulleys with aluminum cable pulleys following the actions and instructions of Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Service Bulletin SB- G05 and Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Instructions A/I-G05, both dated January 17, 2014. (2) For all Models G102 STANDARD ASTIR III, G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, G103 TWIN II, and G103A TWIN II ACRO gliders: Within 1 month after August 27, 2014 (the effective date of this AD), inspect the rudder control unit for installation of plastic cable pulleys. If plastic cable pulleys are installed, before further flight, replace the plastic cable pulleys with aluminum cable pulleys following the actions and instructions of Fiberglas- Technik Rudolf Lindner GmbH & Co. KG Service Bulletin SB-G05 and Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Instructions A/I-G05, both dated January 17, 2014. (3) As of August 27, 2014 (the effective date of this AD), do not install any plastic control cable pulley in the rudder control unit of any glider identified in paragraphs (c)(1) through (c)(7) of this AD. (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 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. (h) Related Information Refer to European Aviation Safety Agency (EASA) AD No.: 2014- 0067, dated March 18, 2014, for related information. The MCAI can be found in the AD docket on the Internet at: http://www.regulations.gov/#!documentDetail;D=FAA-2014-0292-0002. (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) Fiberglas-Technik Rudolf Lindner GmbH & Co. KG Service Bulletin SB-G05, dated January 17, 2014. (ii) Fiberglas-Technik Rudolf Lindner GmbH & Co. Fiberglas- Technik Rudolf Lindner GmbH & Co. KG Instructions A/I-G05, dated January 17, 2014. (3) For Fiberglas-Technik Rudolf Lindner GmbH & Co. service information identified in this AD, contact Fiberglas-Technik Rudolf Lindner GmbH & Co. KG, Steige 3, D-88487 Walpertshofen, Germany; telephone: +49 (0) 7353/22 43; fax: +49 (0) 7353/30 96; email: Lindner.com">[email protected]; Web site: http://www.ltb-lindner.com/home.104.html. (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

2007-10-18CE-08-01 · Fuselage, Wing, & Stabilizer Structure
2006-06-21CE-06-49 ·

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 23, 2026. Connections as data: /graph/directive/2014-15-02.json · aircraft systems.