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2010-09-23
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Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes
Rules and Regulations
D09002ee1bdea7626
D09002ee1bdea771f
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
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.
69 FR 15657
https://www.govinfo.gov/app/details/FR-2004-03-26/04-6498
04-6498
fr26mr04-2
RIN 2120-AA64
4910-13-P
Docket No. 2004-CE-07-AD
Amendment 39-13535
AD 2004-06-09
https://www.govinfo.gov/app/details/FR-2004-03-26/04-6498
https://www.govinfo.gov/content/pkg/FR-2004-03-26/html/04-6498.htm
https://www.govinfo.gov/content/pkg/FR-2004-03-26/pdf/04-6498.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
15657
15659
69 FR 15657
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; The Lancair Company Models LC40-550FG and LC42-550FG Airplanes; Federal Register Vol. 69, Issue
RULE
04-6498
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2004-05-03
Docket No. 2004-CE-07-AD
Amendment 39-13535
AD 2004-06-09
4910-13-P
04-6498
Final rule; request for comments.
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.
This AD becomes effective on May 3, 2004.
Jeff Morfitt, Aerospace Engineer, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98055; telephone: 425-917-6405; facsimile: 425-917-6590.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Lancair Co.,
9-ACE-7-Docket@faa.gov
Federal Register
Vol. 69, no. 59
Office of the Federal Register, National Archives and Records Administration
2004-03-26
continuing
daily
deposited
born digital
521 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-03-26
P0b002ee180980d1f
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr26mr04
https://www.govinfo.gov/app/details/FR-2004-03-26
https://www.govinfo.gov/content/pkg/FR-2004-03-26/pdf/FR-2004-03-26.pdf
https://www.govinfo.gov/content/pkg/FR-2004-03-26/xml/FR-2004-03-26.xml
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DGPO
2010-09-23
2023-05-04
FR-2004-03-26
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FR
FR-2004-03-26
69
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