Airworthiness Directive

AD 95-17-08 60 FR 44422 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-20276
Amendment
39-9338
Published
1995-08-28
Effective
1995-10-10
Models covered
1

Last live check: 2026-08-19

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AD

95-17-08

FR doc 95-20276 · 60 FR 44422

AD 95-17-08Published 1995-08-28Effective 1995-10-10

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 modifying the rudder control cable system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Stemme GmbH (Stemme) S10 gliders. This action requires modifying the rudder control cable system. Rupture of a turnbuckle eye bolt in the rudder control cable system on one of the affected gliders prompted this action. The actions specified by this AD are intended to prevent rudder control cable system failure caused by rupture of the turnbuckle eye bolt, which, if not detected and corrected, could result in loss of rudder control and eventual loss of control of the glider.

More directives for Stemme S10/S12

  1. AD 2026-15-08 Airworthiness Directives; Stemme GmbH Gliders Effective 2026-09-03
  2. AD 2026-15-04 Airworthiness Directives; Stemme GmbH Gliders Effective 2026-07-24
  3. AD 2023-02-03 Airworthiness Directives; Stemme AG Gliders Effective 2023-03-01
  4. AD 2022-14-11 Airworthiness Directives; Stemme AG (Type Certificate Previously Held by... Effective 2022-07-26
  5. AD 2022-03-07 Airworthiness Directives; Stemme AG Gliders Effective 2022-03-02

All Stemme S10/S12 directives

Applies to 1 model in our index