Airworthiness Directive

AD 2007-24-06 72 FR 67245 Active

Federal Aviation Administration · 14 CFR part 39

Prompted by mandatory continuing airworthiness information (MCAI) provided by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on SMA SR305-230 and SR305-230-1 reciprocating engines.

FR document
E7-22812
Amendment
39-15272
Published
2007-11-28
Effective
2007-12-13
Models covered
1

Last live check: 2026-08-19

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AD

2007-24-06

FR doc E7-22812 · 72 FR 67245

AD 2007-24-06Published 2007-11-28Effective 2007-12-13

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.

Prompted by mandatory continuing airworthiness information (MCAI) provided by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on SMA SR305-230 and SR305-230-1 reciprocating engines.

Supersedes an earlier directive. See the official text.

Full official abstract

We are superseding an existing airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) provided by the European Aviation Safety Agency (EASA) to identify and correct an unsafe condition on SMA SR305-230 and SR305-230-1 reciprocating engines. The MCAI states the following:

More directives for SMA SR305

  1. AD 2009-04-05 Airworthiness Directives; Cessna Aircraft Company Models 182Q and 182R A... Effective 2009-03-27
  2. AD 2007-18-05 Airworthiness Directives; Societe de Motorisations Aeronautiques (SMA) S... Effective 2007-10-09
  3. AD 2006-23-08 Airworthiness Directives; Societe de Motorisations Aeronautiques (SMA) S... Effective 2006-11-22

All SMA SR305 directives

Applies to 1 model in our index