Airworthiness Directive

AD 2013-15-19 78 FR 48795 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2013-18528
Amendment
39-17535
Published
2013-08-12
Effective
2013-08-27
Models covered
2
Last live check
2026-10-01
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AD

2013-15-19

FR doc 2013-18528 · 78 FR 48795

AD 2013-15-19Published 2013-08-12Effective 2013-08-27

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 a report that additional engine cylinder heads are likely to be affected.

Full official abstract

We are superseding an existing airworthiness directive (AD) for all BRP-Powertrain GmbH & Co KG Rotax model 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; 912 S4; 914 F2; 914 F3; and 914 F4 reciprocating engines. That AD required a one-time visual inspection for excessive oil or carbon deposits on the cylinder No. 2 and No. 3 (\2/3\) spark plug center and grounding electrodes, and if found, replacement of the cylinder head before further flight. This AD was prompted by a report that additional engine cylinder heads are likely to be affected. We are issuing this AD to prevent excessive oil consumption, which could result in an in-flight engine shutdown, forced landing, and damage to the airplane.

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All Rotax 912 directives

Applies to 2 models in our index