Airworthiness Directive

AD 2002-16-26 67 FR 53296 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-20679
Amendment
39-12865
Published
2002-08-15
Effective
2002-09-16
Models covered
2
Last live check
2026-10-01
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AD

2002-16-26

FR doc 02-20679 · 67 FR 53296

AD 2002-16-26Published 2002-08-15Effective 2002-09-16

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 initial and repetitive visual inspections of the engine crankcase for cracks.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain serial numbers (SN's) of Bombardier-Rotax GmbH type 912 F and 914 F series reciprocating engines. This action requires initial and repetitive visual inspections of the engine crankcase for cracks. This amendment is prompted by reports of several instances of engine crankcases found cracked in service. The actions specified in this AD are intended to prevent oil loss caused by cracks in the engine crankcase, which could lead to in-flight failure of the engine and forced landing.

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All Rotax 912 directives

Applies to 2 models in our index