Airworthiness Directive

AD 2002-19-09 67 FR 60120 Active

Federal Aviation Administration · 14 CFR part 39

Requires initial and repetitive visual inspections and tests of the fuel pump assembly for fuel leakage.

FR document
02-24280
Amendment
39-12889
Published
2002-09-25
Effective
2002-10-10
Models covered
1

Last live check: 2026-08-19

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AD

2002-19-09

FR doc 02-24280 · 67 FR 60120

AD 2002-19-09Published 2002-09-25Effective 2002-10-10

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 and tests of the fuel pump assembly for fuel leakage.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to all Bombardier-Rotax GmbH 912 F series and 912 S series reciprocating engines with fuel pump assembly part number (P/N) 996.596 installed. This action requires initial and repetitive visual inspections and tests of the fuel pump assembly for fuel leakage. This amendment is prompted by two reports of fuel pump assembly fuel leaks. The actions specified in this AD are intended to prevent in-flight fuel leaks of the fuel pump assembly, which could result in an engine fire.

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Applies to 1 model in our index