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 2012_register executive 2012-08-02 article Proposed Rules D09002ee1c7fca48e D09002ee1c7fca50e 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 propose to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft Inc.) PA-28, PA-32, PA-34, and PA-44 airplanes. This proposed AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stabilator control system and could result in loss of pitch control. This proposed AD would require inspections of the stabilator control system and replacement of parts as necessary. We are proposing this AD to correct the unsafe condition on these products. 77 FR 45979 https://www.govinfo.gov/app/details/FR-2012-08-02/2012-18618 2012-18618 fr02au12-18 RIN 2120-AA64 4910-13-P Docket No. FAA-2012-0731 Directorate Identifier 2012-CE-020-AD https://www.govinfo.gov/app/details/FR-2012-08-02/2012-18618 https://www.govinfo.gov/content/pkg/FR-2012-08-02/html/2012-18618.htm https://www.govinfo.gov/content/pkg/FR-2012-08-02/pdf/2012-18618.pdf Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety 3 p. 45979 45981 77 FR 45979 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; Piper Aircraft, Inc. Airplanes; Federal Register Vol. 77, Issue PRORULE 2012-18618 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 2012-09-17 Docket No. FAA-2012-0731 Directorate Identifier 2012-CE-020-AD 4910-13-P 2012-18618 Notice of proposed rulemaking (NPRM).

We propose to adopt a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (type certificate previously held by The New Piper Aircraft Inc.) PA-28, PA-32, PA-34, and PA-44 airplanes. This proposed AD was prompted by reports of control cable assembly failures that may lead to failure of the horizontal stabilator control system and could result in loss of pitch control. This proposed AD would require inspections of the stabilator control system and replacement of parts as necessary. We are proposing this AD to correct the unsafe condition on these products.

We must receive comments on this proposed AD by September 17, 2012. Hector Hernandez, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone: (404) 474-5587; fax: (404) 474- 5606; email: hector.hernandez@faa.gov. Air Transportation Aircraft Aviation Safety Incorporation by Reference Safety Airworthiness Directives: Piper Aircraft, Inc. Airplanes , hector.hernandez@faa.gov http://registry.faa.gov/aircraftinquiry/Serial_Inquiry.aspx http://www.regulations.gov www.piper.com Vol. 77, no. 149 Office of the Federal Register, National Archives and Records Administration 2012-08-02 continuing daily deposited born digital 369 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-2012-08-02 P0b002ee1833628e2 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr02au12 https://www.govinfo.gov/app/details/FR-2012-08-02 https://www.govinfo.gov/content/pkg/FR-2012-08-02/pdf/FR-2012-08-02.pdf https://www.govinfo.gov/content/pkg/FR-2012-08-02/xml/FR-2012-08-02.xml fdlp 45895 46255 DGPO 2012-08-02 2024-06-03 FR-2012-08-02 machine generated eng FR FR-2012-08-02 77 149