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 2009_register executive 2009-05-13 article Rules and Regulations D09002ee1c8069e68 D09002ee1c8069ee8 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 The FAA is adopting a new airworthiness directive (AD) for Cessna Aircraft Company (Cessna) 150 and 152 series airplanes. This AD requires you to either install a placard prohibiting spins and other acrobatic maneuvers in the airplane or to replace the rudder stop, rudder stop bumper, and attachment hardware with a new rudder stop modification kit and replace the safety wire with jamnuts. This AD results from follow-on investigations of two accidents where the rudder was found in the over-travel position with the stop plate hooked over the stop bolt heads. While neither of the accident aircraft met type design, investigations revealed that aircraft in full conformity with type design can exceed the travel limits set by the rudder stops. We are issuing this AD to prevent the rudder from traveling past the normal travel limit. Operation in this non-certificated control position is unacceptable and could cause undesirable consequences, such as contact between the rudder and the elevator. 74 FR 22429 https://www.govinfo.gov/app/details/FR-2009-05-13/E9-11029 E9-11029 FR13MY09-5 RIN 2120-AA64 4910-13-P Docket No. FAA-2007-27747 Directorate Identifier 2007-CE-030-AD Amendment 39-15904 AD 2009-10-09 https://www.govinfo.gov/app/details/FR-2009-05-13/E9-11029 https://www.govinfo.gov/content/pkg/FR-2009-05-13/html/E9-11029.htm https://www.govinfo.gov/content/pkg/FR-2009-05-13/pdf/E9-11029.pdf Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety 4 p. 22429 22432 74 FR 22429 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; Cessna Aircraft Company 150 and 152 Series Airplanes; Federal Register Vol. 74, Issue RULE E9-11029 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 2009-06-17 Docket No. FAA-2007-27747 Directorate Identifier 2007-CE-030-AD Amendment 39-15904 AD 2009-10-09 4910-13-P E9-11029 Final rule.

The FAA is adopting a new airworthiness directive (AD) for Cessna Aircraft Company (Cessna) 150 and 152 series airplanes. This AD requires you to either install a placard prohibiting spins and other acrobatic maneuvers in the airplane or to replace the rudder stop, rudder stop bumper, and attachment hardware with a new rudder stop modification kit and replace the safety wire with jamnuts. This AD results from follow-on investigations of two accidents where the rudder was found in the over-travel position with the stop plate hooked over the stop bolt heads. While neither of the accident aircraft met type design, investigations revealed that aircraft in full conformity with type design can exceed the travel limits set by the rudder stops. We are issuing this AD to prevent the rudder from traveling past the normal travel limit. Operation in this non-certificated control position is unacceptable and could cause undesirable consequences, such as contact between the rudder and the elevator.

This AD becomes effective on June 17, 2009. Ann Johnson, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4105; fax: (316) 946-4107. Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety Airworthiness Directives: Cessna Aircraft Co. 150 and 152 Series Airplanes , http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html http://www.cessna.com http://www.regulations.gov Vol. 74, no. 91 Office of the Federal Register, National Archives and Records Administration 2009-05-13 continuing daily deposited born digital 229 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-2009-05-13 P0b002ee18001ca17 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:FR13MY09 https://www.govinfo.gov/app/details/FR-2009-05-13 https://www.govinfo.gov/content/pkg/FR-2009-05-13/pdf/FR-2009-05-13.pdf https://www.govinfo.gov/content/pkg/FR-2009-05-13/xml/FR-2009-05-13.xml fdlp 22417 22635 DGPO 2009-05-13 2024-06-04 FR-2009-05-13 machine generated eng FR FR-2009-05-13 74 91