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Airworthiness Directive

AD 2014-15-02 R1 79 FR 63502 Active

Federal Aviation Administration · 14 CFR part 39

Requires actions to address the unsafe condition on these products.

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FR document
2014-25287
Amendment
39-18001
Published
2014-10-24
Effective
2014-10-24
Models covered
1

Last live check: 2026-08-19

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This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2014-15-02 R1

FR doc 2014-25287 · 79 FR 63502

AD 2014-15-02 R1Published 2014-10-24Effective 2014-10-24

Revises 2014-15-02

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires actions to address the unsafe condition on these products.

Full official abstract

We are adopting a new airworthiness directive (AD) for Fiberglas-Technik Rudolf Lindner GmbH & Co. KG (type certificates formerly held by GROB-WERKE GMBH & CO KG and BURKHART GROB LUFT- UND RAUMFAHRT GmbH & CO KG) Models G102 STANDARD ASTIR III, G102 CLUB ASTIR III, G102 CLUB ASTIR IIIb, G103 TWIN II, G103A TWIN II ACRO, G103C TWIN III ACRO, and G 103 C Twin III SL gliders. This AD revises AD 2014-15- 02, which required inspection of the rudder control unit for installation of plastic cable pulleys and replacement of plastic cable pulleys with aluminum cable pulleys. This AD retains the actions of AD 2014-15-02 but clarifies the suffixes of serial numbers (S/Ns) in paragraph (c) Applicability. This AD was prompted by reports of plastic control cable pulleys developing cracks due to aging, which could lead to breaking of the pulley and potentially jamming the rudder control unit, possibly resulting in loss of control. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Grob

  1. AD 2025-20-07 Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG... Effective 2025-10-17
  2. AD 2022-05-14 Airworthiness Directives; GROB Aircraft SE (Type Certificate Previously ... Effective 2022-03-24
  3. AD 2022-03-08 Airworthiness Directives; Fiberglas-Technik Rudolf Lindner GmbH & Co. KG... Effective 2022-03-17
  4. AD 2017-08-12 Airworthiness Directives; GROB Aircraft AG Gliders Effective 2017-05-31
  5. AD 2016-12-08 Airworthiness Directives; GROB Aircraft AG Airplanes Effective 2016-07-20

All Grob directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index