Airworthiness Directive

AD 2004-06-09 69 FR 15657 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter (as necessary).

FR document
04-6498
Amendment
39-13535
Published
2004-03-26
Effective
2004-05-03
Models covered
1

Last live check: 2026-08-19

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AD

2004-06-09

FR doc 04-6498 · 69 FR 15657

AD 2004-06-09Published 2004-03-26Effective 2004-05-03

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 you to repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter (as necessary).

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain The Lancair Company (Lancair) Models LC40-550FG and LC42-550FG airplanes. This AD requires you to repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter (as necessary). The AD also requires you to install a compliance kit at a time dependent on the outcomes of the inspections and measurement. Installation of the kit is terminating action for the repetitive inspection requirements. This AD is the result of several reports of the fuel pressure transducer wearing through at the threads where it attached to the fuel line. We are issuing this AD to detect and correct chafing and wear of the fuel pressure transducer, which could result in failure of the transducer threaded fitting with a resulting fuel leak. These fuel leaks could lead to engine power loss or fire.

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Applies to 1 model in our index