Airworthiness Directive

AD 2017-10-02 82 FR 24045 Active

Federal Aviation Administration · 14 CFR part 39

Requires actions to address the unsafe condition on these products.

FR document
2017-10403
Amendment
39-18876
Published
2017-05-25
Effective
2017-06-29
Models covered
1

Last live check: 2026-08-19

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AD

2017-10-02

FR doc 2017-10403 · 82 FR 24045

AD 2017-10-02Published 2017-05-25Effective 2017-06-29

Supersedes 2015-11-01

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 superseding airworthiness directive (AD) 2015-11-01 for Slingsby Aviation Ltd. Models T67M260 and T67M260-T3A 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 failure of a brake master cylinder pivot pin, which could cause the rudder pedal mechanism to detach from the brake cylinder. We are issuing this AD to require actions to address the unsafe condition on these products.

More directives for Slingsby T67 Firefly

  1. AD 2015-11-01 Airworthiness Directives; Slingsby Aviation Ltd. Airplanes Effective 2015-06-16
  2. AD 2014-04-01 Airworthiness Directives; Slingsby Aviation Ltd. Airplanes Effective 2014-04-01

All Slingsby T67 Firefly directives

Applies to 1 model in our index