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 2011_register executive 2011-03-10 article Rules and Regulations D09002ee1c80038b5 D09002ee1c800394c 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 superseding an existing airworthiness directive (AD) for the products listed above. That AD currently requires you to incorporate operating limitations of maximum operating altitude of 37,000 feet into Section 2, Limitations, of the airplane flight manual (AFM). This AD requires you to incorporate operating limitations of maximum operating altitude of 30,000 feet into Section 2, Limitations, of the AFM. This AD was prompted by several incidents of engine surge. We are issuing this AD to prevent hard carbon buildup on the static vane, which could result in engine surges. Engine surges may result in a necessary reduction in thrust and decreased power for the affected engine. In some cases, this could result in flight and landing under single-engine conditions. It is also possible this could affect both engines at the same time, requiring dual-engine shutdown. 76 FR 13078 https://www.govinfo.gov/app/details/FR-2011-03-10/2011-5296 2011-5296 fr10mr11-10 RIN 2120-AA64 4910-13-P Docket No. FAA-2011-0199 Directorate Identifier 2011-CE-005-AD Amendment 39-16631 AD 2011-06-06 https://www.govinfo.gov/app/details/FR-2011-03-10/2011-5296 https://www.govinfo.gov/content/pkg/FR-2011-03-10/html/2011-5296.htm https://www.govinfo.gov/content/pkg/FR-2011-03-10/pdf/2011-5296.pdf Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety 3 p. 13078 13080 76 FR 13078 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; Eclipse Aerospace, Inc. Model EA500 Airplanes Equipped With a Pratt and Whitney Canada, Corp. (PWC) PW610F-A Engine; Federal Register Vol. 76, Issue RULE 2011-5296 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 2011-03-21 Docket No. FAA-2011-0199 Directorate Identifier 2011-CE-005-AD Amendment 39-16631 AD 2011-06-06 4910-13-P 2011-5296 Final rule; request for comments.

We are superseding an existing airworthiness directive (AD) for the products listed above. That AD currently requires you to incorporate operating limitations of maximum operating altitude of 37,000 feet into Section 2, Limitations, of the airplane flight manual (AFM). This AD requires you to incorporate operating limitations of maximum operating altitude of 30,000 feet into Section 2, Limitations, of the AFM. This AD was prompted by several incidents of engine surge. We are issuing this AD to prevent hard carbon buildup on the static vane, which could result in engine surges. Engine surges may result in a necessary reduction in thrust and decreased power for the affected engine. In some cases, this could result in flight and landing under single-engine conditions. It is also possible this could affect both engines at the same time, requiring dual-engine shutdown.

This AD is effective March 21, 2011. Eric Kinney, Aerospace Engineer, Ft. Worth Aircraft Certification Office, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone: (817) 222-5459; fax: (817) 222-5960; e- mail: eric.kinney@faa.gov. Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety Airworthiness Directives: Eclipse Aerospace, Inc. Model EA500 Airplanes Equipped With a Pratt and Whitney Canada, Corp. PW610FA Engine , eric.kinney@faa.gov http://www.regulations.gov Vol. 76, no. 47 Office of the Federal Register, National Archives and Records Administration 2011-03-10 continuing daily deposited born digital 233 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-2011-03-10 P0b002ee180c20eda 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr10mr11 https://www.govinfo.gov/app/details/FR-2011-03-10 https://www.govinfo.gov/content/pkg/FR-2011-03-10/pdf/FR-2011-03-10.pdf https://www.govinfo.gov/content/pkg/FR-2011-03-10/xml/FR-2011-03-10.xml fdlp 13059 13283 DGPO 2011-03-10 2024-06-04 FR-2011-03-10 machine generated eng FR FR-2011-03-10 76 47