Airworthiness Directive

AD 98-15-16 63 FR 39491 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-19484
Amendment
39-10667
Published
1998-07-23
Effective
1998-08-07
Models covered
1
Last live check
2026-10-01
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AD

98-15-16

FR doc 98-19484 · 63 FR 39491

AD 98-15-16Published 1998-07-23Effective 1998-08-07

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 installation of an improved fuel pump and fuel supply tube.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to Bombardier-Rotax GmbH 912 F series reciprocating engines. This action requires installation of an improved fuel pump and fuel supply tube. This amendment is prompted by reports of fuel leaks at the outlet port of the fuel pump. The actions specified in this AD are intended to prevent fuel leaks from the fuel pump, which could result in undetected loss of fuel in flight or, an engine fire.

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All Rotax 912 directives

Applies to 1 model in our index