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 2013_register executive 2013-06-28 article Rules and Regulations D09002ee1c7fb4dc1 D09002ee1c7fb4e4a 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 publishing a new airworthiness directive (AD) for various model helicopters with certain part-numbered and serial- numbered Goodrich externally-mounted hoists installed. This AD requires performing a cable conditioning lift and a load inspection test, deactivating or replacing any hoist that fails the load inspection test, and recording the results of the load inspection test. This AD is prompted by a report of a failure of the overload clutch resulting in an in-flight failure of a hoist containing a dummy load during a maintenance flight. These actions are intended to detect conditions that may result in failure of the hoist and injury to persons being lifted. 78 FR 38826 https://www.govinfo.gov/app/details/FR-2013-06-28/2013-14842 2013-14842 fr28jn13-5 RIN 2120-AA64 4910-13-P Docket No. FAA-2013-0521 Directorate Identifier 2013-SW-010-AD Amendment 39-17486 AD 2013-06-51 https://www.govinfo.gov/app/details/FR-2013-06-28/2013-14842 https://www.govinfo.gov/content/pkg/FR-2013-06-28/html/2013-14842.htm https://www.govinfo.gov/content/pkg/FR-2013-06-28/pdf/2013-14842.pdf Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety 3 p. 38826 38828 78 FR 38826 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; Various Helicopter Models; Federal Register Vol. 78, Issue RULE 2013-14842 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 2013-07-15 Docket No. FAA-2013-0521 Directorate Identifier 2013-SW-010-AD Amendment 39-17486 AD 2013-06-51 4910-13-P 2013-14842 Final rule; request for comments.

We are publishing a new airworthiness directive (AD) for various model helicopters with certain part-numbered and serial- numbered Goodrich externally-mounted hoists installed. This AD requires performing a cable conditioning lift and a load inspection test, deactivating or replacing any hoist that fails the load inspection test, and recording the results of the load inspection test. This AD is prompted by a report of a failure of the overload clutch resulting in an in-flight failure of a hoist containing a dummy load during a maintenance flight. These actions are intended to detect conditions that may result in failure of the hoist and injury to persons being lifted.

This AD becomes effective July 15, 2013 to all persons except those persons to whom it was made immediately effective by Emergency AD (EAD) No. 2013-06-51, issued on March 25, 2013, which contained the requirements of this AD. Matt Wilbanks, Aviation Safety Engineer, Regulations and Policy Group, Rotorcraft Directorate, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone (817) 222-5110; email matt.wilbanks@faa.gov. Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety Airworthiness Directives: Various Helicopter Models , matt.wilbanks@faa.gov http://www.archives.gov/federal-register/cfr/ibr-locations.html http://www.goodrich.com/Goodrich http://www.regulations.gov Vol. 78, no. 125 Office of the Federal Register, National Archives and Records Administration 2013-06-28 continuing daily deposited born digital 362 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-2013-06-28 P0b002ee185091ead 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr28jn13 https://www.govinfo.gov/app/details/FR-2013-06-28 https://www.govinfo.gov/content/pkg/FR-2013-06-28/pdf/FR-2013-06-28.pdf https://www.govinfo.gov/content/pkg/FR-2013-06-28/xml/FR-2013-06-28.xml fdlp 38811 39161 DGPO 2013-06-28 2024-06-03 FR-2013-06-28 machine generated eng FR FR-2013-06-28 78 125