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2010-09-23
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Airworthiness Directives; Great Lakes Aircraft Company, LLC, Models 2T-1A-1 and 2T-1A-2 Airplanes
Rules and Regulations
D09002ee1bde4abab
D09002ee1bde4ac47
United States
Department of Transportation
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United States Government Agency or Subagency
United States
Federal Aviation Administration
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United States Government Agency or Subagency
The FAA supersedes Airworthiness Directive (AD) 79-20-08, which applies to all Great Lakes Aircraft Company, LLC, (Great Lakes) Models 2T-1A-1 and 2T-1A-2 airplanes with a Lycoming IO-360-B1F6 or AIO-360-B1G6 engine installed. AD 79-20-08 currently requires you to inspect the engine induction system and the alternate air door for any signs of damage and repairing or replacing any damaged components. AD 79-20-08 also requires you to inspect the induction system for the presence of a drain fitting. If the drain fitting is blocked, restricted, or does not exist, AD 79-20-08 requires you to clear the fitting or drill a hole in the elbow at the fitting location. This AD is the result of the FAA inadvertently omitting Lycoming engine AEIO- 360-B1G6 from the applicability section of AD 79-20-08. Consequently, this AD retains the actions required in AD 79-20-08 and adds Lycoming engine AEIO-360-B1G6 to the applicability section. We are issuing this AD to prevent the aircraft induction system from becoming blocked or restricted, which could result in engine failure. This failure could lead to loss of control of the airplane.
69 FR 75236
https://www.govinfo.gov/app/details/FR-2004-12-16/04-27521
04-27521
fr16de04-7
RIN 2120-AA64
4910-13-P
Docket No. FAA-2004-18744
Directorate Identifier 2004-CE-24-AD
Amendment 39-13910
AD 2004-25-22
https://www.govinfo.gov/app/details/FR-2004-12-16/04-27521
https://www.govinfo.gov/content/pkg/FR-2004-12-16/html/04-27521.htm
https://www.govinfo.gov/content/pkg/FR-2004-12-16/pdf/04-27521.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
8 p.
75236
75243
69 FR 75236
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Great Lakes Aircraft Company, LLC, Models 2T-1A-1 and 2T-1A-2 Airplanes; Federal Register Vol. 69, Issue
RULE
04-27521
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-01-28
Docket No. FAA-2004-18744
Directorate Identifier 2004-CE-24-AD
Amendment 39-13910
AD 2004-25-22
4910-13-P
04-27521
Final rule.
The FAA supersedes Airworthiness Directive (AD) 79-20-08, which applies to all Great Lakes Aircraft Company, LLC, (Great Lakes) Models 2T-1A-1 and 2T-1A-2 airplanes with a Lycoming IO-360-B1F6 or AIO-360-B1G6 engine installed. AD 79-20-08 currently requires you to inspect the engine induction system and the alternate air door for any signs of damage and repairing or replacing any damaged components. AD 79-20-08 also requires you to inspect the induction system for the presence of a drain fitting. If the drain fitting is blocked, restricted, or does not exist, AD 79-20-08 requires you to clear the fitting or drill a hole in the elbow at the fitting location. This AD is the result of the FAA inadvertently omitting Lycoming engine AEIO- 360-B1G6 from the applicability section of AD 79-20-08. Consequently, this AD retains the actions required in AD 79-20-08 and adds Lycoming engine AEIO-360-B1G6 to the applicability section. We are issuing this AD to prevent the aircraft induction system from becoming blocked or restricted, which could result in engine failure. This failure could lead to loss of control of the airplane.
This AD becomes effective on January 28, 2005.
Roger Caldwell, Aerospace Engineer, Denver Aircraft Certification Office (ACO), Federal Aviation Administration (FAA), 26805 E. 68th Ave., Rm 214 Denver, CO 80249-6361; telephone: (303) 342-1086; facsimile: (303) 342-1088.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Great Lakes Aircraft Co., LLC,
http://dms.dot.gov
Federal Register
Vol. 69, no. 241
Office of the Federal Register, National Archives and Records Administration
2004-12-16
continuing
daily
deposited
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240 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-12-16
P0b002ee180977e00
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr16de04
https://www.govinfo.gov/app/details/FR-2004-12-16
https://www.govinfo.gov/content/pkg/FR-2004-12-16/pdf/FR-2004-12-16.pdf
https://www.govinfo.gov/content/pkg/FR-2004-12-16/xml/FR-2004-12-16.xml
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FR-2004-12-16
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