AD 2004-06-09

Recurring final rule
Data completeness: 90%

Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

AD Number
2004-06-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2004-CE-07-AD
FR Citation
69 FR 15657

Applicability

TypeManufacturerModelDetails
aircraft Lancair Company Models LC40-550FG and LC42-550FG Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes

Unsafe Condition

Fuel pressure transducer wearing through at the threads where it attaches to the fuel line, potentially leading to failure of the transducer threaded fitting and resulting fuel leaks.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Repetitively inspect the fuel pressure transducer for evidence of chafing and measure the cross section diameter as necessary. Install a compliance kit based on the outcomes of the inspections and measurements. Installation of the kit terminates the repetitive inspection requirements.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 50 flight hours after the effective date of the AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

The Lancair Company Models LC40-550FG and LC42-550FG airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.