Airworthiness Directive

AD 2016-13-04 81 FR 40483 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-14789
Amendment
39-18568
Published
2016-06-22
Effective
2016-07-27
Models covered
2
Last live check
2026-10-01
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AD

2016-13-04

FR doc 2016-14789 · 81 FR 40483

AD 2016-13-04Published 2016-06-22Effective 2016-07-27

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.

Requires re-identification of the engine model and concurrent modification of the aircraft to indicate the maximum coolant temperature limit.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain BRP-Powertrain GmbH & Co KG Rotax 912 F2, 912 F3, 912 F4, 912 S2, 912 S3, 912 S4, 914 F2, 914 F3, and 914 F4 reciprocating engines. This AD requires re-identification of the engine model and concurrent modification of the aircraft to indicate the maximum coolant temperature limit. This AD was prompted by a design change introduced by the manufacturer that relocated the engine cylinder head temperature sensor to a different location and converted it to a coolant temperature sensor. We are issuing this AD to prevent exceeding engine coolant temperature limits, which could result in loss of engine coolant, damage to the engine, and loss of control of the airplane.

More directives for Rotax 912

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  5. AD 2019-21-12 Airworthiness Directives; BRP-Rotax GmbH & Co KG Engines 2019-11-04

All Rotax 912 directives

Applies to 2 models in our index