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 1995_register executive 2010-09-25 article Rules and Regulations D09002ee1be0637b8 D09002ee1be063821 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 This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-07-01 that was sent previously to all known U.S. owners and operators of Textron Lycoming O-360, LO- 360, HO-360, HIO-360, TIO-360, LIO-360, AEIO-360, O-540, IO-540, TIO- 540, LTIO-540, IVO-540, AEIO-540, TIO-541, and IO-720 series reciprocating engines by individual letters. This AD requires removal prior to further flight of suspect unapproved connecting rod bolts and replacement with serviceable connecting rod bolts. This amendment is prompted by reports of connecting rod bolt failures. The actions specified by this AD are intended to prevent engine failure due to connecting rod bolt failure, which could result in damage to or loss of the aircraft. 60 FR 15864 https://www.govinfo.gov/app/details/FR-1995-03-28/95-7683 95-7683 fr28mr95-6 4910-13-U Docket No. 95-ANE-14 Amendment 39-9183 AD 95-07-01 https://www.govinfo.gov/app/details/FR-1995-03-28/95-7683 https://www.govinfo.gov/content/pkg/FR-1995-03-28/html/95-7683.htm https://www.govinfo.gov/content/pkg/FR-1995-03-28/pdf/95-7683.pdf 4 p. 15864 15867 60 FR 15864 Title 14 Part 39 14 CFR Part 39 Airworthiness Directives; Textron Lycoming O-360, LO-360, HO-360, HIO-360, TIO-360, LIO-360, AEIO-360, O-540, IO-540, TIO-540, LTIO-540, IVO-540, AEIO-540, TIO-541, and IO-720 Series Reciprocating Engines; Federal Register Vol. 60, Issue RULE 95-7683 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 1995-04-12 Docket No. 95-ANE-14 Amendment 39-9183 AD 95-07-01 4910-13-U 95-7683 Final rule, request for comments.

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 95-07-01 that was sent previously to all known U.S. owners and operators of Textron Lycoming O-360, LO- 360, HO-360, HIO-360, TIO-360, LIO-360, AEIO-360, O-540, IO-540, TIO- 540, LTIO-540, IVO-540, AEIO-540, TIO-541, and IO-720 series reciprocating engines by individual letters. This AD requires removal prior to further flight of suspect unapproved connecting rod bolts and replacement with serviceable connecting rod bolts. This amendment is prompted by reports of connecting rod bolt failures. The actions specified by this AD are intended to prevent engine failure due to connecting rod bolt failure, which could result in damage to or loss of the aircraft.

Effective April 12, 1995, to all persons except those persons to whom it was made immediately effective by priority letter AD 95-07-01, issued on March 17, 1995, which contained the requirements of this amendment. Richard D. Karanian, Aerospace Engineer, Special Certification Office, FAA, Rotorcraft Directorate, 2601 Meacham Blvd., Fort Worth, TX 76137-4298; telephone (817) 222- 5195, fax (817) 222-5959; or Locke Easton, Aerospace Engineer, Engine and Propeller Standards Staff, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA [[Page 15865]] 01803- 5299; telephone (617) 238-7113, fax (617) 238-7199. Vol. 60, no. 59 Office of the Federal Register, National Archives and Records Administration 1995-03-28 continuing daily deposited born digital 190 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-1995-03-28 P0b002ee180a8f4ec 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr28mr95 https://www.govinfo.gov/app/details/FR-1995-03-28 https://www.govinfo.gov/content/pkg/FR-1995-03-28/pdf/FR-1995-03-28.pdf fdlp 15855 16034 DGPO 2010-09-25 2023-05-07 FR-1995-03-28 machine generated eng FR FR-1995-03-28 60 59