United States Government Publishing Office publisher pbl distributor dst United States National Archives and Records Administration Office of the Federal Register author aut Government Organization text government publication eng FR Regulatory Information 2008_register executive 2010-09-23 article Rules and Regulations D09002ee1c80886a3 D09002ee1c8088731 United States Department of Transportation originator org United States Government Agency or Subagency United States Federal Aviation Administration originator org United States Government Agency or Subagency We are adopting a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 helicopters. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Canada, with which we have a bilateral agreement, states in the MCAI: "It has been determined that some helicopters have been fitted with a CRES steel fitting, part number (P/N) 407-030-750-103, and the installation of the tailboom attachment bolt does not meet the design criteria." We are issuing this AD to require actions that are intended to address the unsafe condition that results from an improper installation of the tailboom attachment bolt in the upper left-hand tailboom attachment CRES steel fitting. 73 FR 39577 https://www.govinfo.gov/app/details/FR-2008-07-10/E8-14736 E8-14736 fr10jy08-5 RIN 2120-AA64 4910-13-P Docket No. FAA-2008-0040 Directorate Identifier 2007-SW-13-AD Amendment 39-15598 AD 2008-14-03 https://www.govinfo.gov/app/details/FR-2008-07-10/E8-14736 https://www.govinfo.gov/content/pkg/FR-2008-07-10/html/E8-14736.htm https://www.govinfo.gov/content/pkg/FR-2008-07-10/pdf/E8-14736.pdf Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety 2 p. 39577 39578 73 FR 39577 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 Helicopters; Federal Register Vol. 73, Issue RULE E8-14736 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 2008-08-14 Docket No. FAA-2008-0040 Directorate Identifier 2007-SW-13-AD Amendment 39-15598 AD 2008-14-03 4910-13-P E8-14736 Final rule.

We are adopting a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 helicopters. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Canada, with which we have a bilateral agreement, states in the MCAI: "It has been determined that some helicopters have been fitted with a CRES steel fitting, part number (P/N) 407-030-750-103, and the installation of the tailboom attachment bolt does not meet the design criteria." We are issuing this AD to require actions that are intended to address the unsafe condition that results from an improper installation of the tailboom attachment bolt in the upper left-hand tailboom attachment CRES steel fitting.

This AD becomes effective on August 14, 2008. Sharon Miles, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Regulations and Policy Group, Fort Worth, Texas 76193-0111, telephone (817) 222-5122, fax (817) 222- 5961. Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety Airworthiness Directives: Bell Helicopter Textron Canada Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-4 Helicopters, http://regulations.gov http://www.archives.gov/federal-register/cfr/ibr-locations.html Vol. 73, no. 133 Office of the Federal Register, National Archives and Records Administration 2008-07-10 continuing daily deposited born digital 298 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-2008-07-10 P0b002ee1809b7fd7 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr10jy08 https://www.govinfo.gov/app/details/FR-2008-07-10 https://www.govinfo.gov/content/pkg/FR-2008-07-10/pdf/FR-2008-07-10.pdf https://www.govinfo.gov/content/pkg/FR-2008-07-10/xml/FR-2008-07-10.xml fdlp 39569 39855 DGPO 2010-09-23 2024-06-05 FR-2008-07-10 machine generated eng FR FR-2008-07-10 73 133