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 1997_register executive 2010-09-24 article Proposed Rules D09002ee1be00808d D09002ee1be0080f9 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 proposes to adopt a new airworthiness directive (AD) that would apply to certain SOCATA-Groupe AEROSPATIALE (Socata) Models TB10 and TB200 airplanes. The proposed AD would require inspecting the wing rear attachment fittings for cracks, replacing any cracked fitting, and incorporating wing rear attachment fitting reinforcement kits. The proposed AD is the result of mandatory continued airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by the proposed AD are intended to prevent structural failure of the wing rear attachment fittings caused by cracks in this area, which could result in a wing separating from the airplane with consequent loss of control of the airplane. 62 FR 65768 https://www.govinfo.gov/app/details/FR-1997-12-16/97-32727 97-32727 fr16de97-14 RIN 2120-AA64 4910-13-U Docket No. 95-CE-71-AD https://www.govinfo.gov/app/details/FR-1997-12-16/97-32727 https://www.govinfo.gov/content/pkg/FR-1997-12-16/html/97-32727.htm https://www.govinfo.gov/content/pkg/FR-1997-12-16/pdf/97-32727.pdf 3 p. 65768 65770 62 FR 65768 Title 14 Part 39 14 CFR Part 39 RIN 2120-AA64 Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models TB10 and TB200 Airplanes; Federal Register Vol. 62, Issue PRORULE 97-32727 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 1998-01-11 Docket No. 95-CE-71-AD 4910-13-U 97-32727 Notice of proposed rulemaking (NPRM).

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain SOCATA-Groupe AEROSPATIALE (Socata) Models TB10 and TB200 airplanes. The proposed AD would require inspecting the wing rear attachment fittings for cracks, replacing any cracked fitting, and incorporating wing rear attachment fitting reinforcement kits. The proposed AD is the result of mandatory continued airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by the proposed AD are intended to prevent structural failure of the wing rear attachment fittings caused by cracks in this area, which could result in a wing separating from the airplane with consequent loss of control of the airplane.

Comments must be received on or before January 11, 1998. Mr. Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 1201 Walnut Street, suite 900, Kansas City, Missouri 64106; telephone (816) 426-6934; facsimile (816) 426-2169. Vol. 62, no. 241 Office of the Federal Register, National Archives and Records Administration 1997-12-16 continuing daily deposited born digital 262 p. Table of Contents: AE 2.7: GS 4.107: AE 2.106: KF70.A2 https://www.govinfo.gov/app/details/FR-1997-12-16 P0b002ee180a3eece 0097-6326 0042-1219 0364-1406 769-004-00000-9 000582072 f:fr16de97 https://www.govinfo.gov/app/details/FR-1997-12-16 https://www.govinfo.gov/content/pkg/FR-1997-12-16/pdf/FR-1997-12-16.pdf fdlp 65741 65990 DGPO 2010-09-24 2023-05-06 FR-1997-12-16 machine generated eng FR FR-1997-12-16 62 241