Airworthiness Directive

AD 2002-16-07 67 FR 53473 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-20266
Amendment
39-12846
Published
2002-08-16
Effective
2002-09-03
Models covered
2
Last live check
2026-10-01
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AD

2002-16-07

FR doc 02-20266 · 67 FR 53473

AD 2002-16-07Published 2002-08-16Effective 2002-09-03

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 replacement of the valve spring retainers, part number (P/N) 854.

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, 912 S and 914 F series reciprocating engines. This action requires replacement of the valve spring retainers, part number (P/N) 854.182, with the new-reinforced valve spring retainers, P/N 854.184. This amendment is prompted by reports of several cracked valve spring retainers discovered in-service. The actions specified in this AD are intended to prevent cracking of the valve spring retainers resulting in possible engine failure while in-flight.

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All Rotax 912 directives

Applies to 2 models in our index