96-18-05 R1: Tailboom

96-18-05 R1 Bell Helicopter Textron Canada: Amendment 39-16511. Docket No. FAA-2008-1242; Directorate Identifier 96-SW-13-AD. Revises AD 96-18-05, Amendment 39-9729. Applicability: Model 206L, 206L-1, and 206L-3 helicopters, with tailboom, part number (P/N) 206-033-004-003, -011, -45, -045, or - 103, installed, certificated in any category. Compliance: Required as indicated. To prevent failure of the tailboom and subsequent loss of control of the helicopter, accomplish the following: (a) Before further flight, unless accomplished previously, using a 10-power or higher magnifying glass, inspect the tailboom for cracks or corrosion in accordance with the Accomplishment Instructions, Part II, steps (1) through (7), of Bell Helicopter Textron Alert Service Bulletin No. 206L-87-47, Revision C, dated October 23, 1989 (ASB). (b) For a tailboom that has not been modified in accordance with the Accomplishment Instructions, Part I of the ASB, using a 10-power or highermagnifying glass, inspect the tailboom for a crack at intervals not to exceed 50 hours time-in-service (TIS) in accordance with the Accomplishment Instructions, Part II, steps (1) through (7), of the ASB. (c) For a tailboom that has been modified in accordance with the Accomplishment Instructions, Part I of the ASB, using a 10-power or higher magnifying glass, inspect the tailboom for a crack or corrosion at intervals not to exceed 100 hours TIS in accordance with the Accomplishment Instructions, Part II and Part III of the ASB, except you are not required to contact the manufacturer. (d) If a crack or corrosion is detected that is beyond the repairable limits stated in the applicable maintenance manual, remove the tailboom and replace it with an airworthy tailboom. (e) Replacing the tailboom with a tailboom, P/N 206-033-004-143 or -177, or an airworthy part-numbered tailboom that is not listed in the Applicability section of this AD, constitutes a terminating action for the requirements of this AD. (f) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Contact the Manager, Safety Management Group, FAA, ATTN: DOT/FAA Southwest Region, Sharon Miles, Aviation Safety Engineer, ASW-111, Rotorcraft Directorate, Regulations and Policy Group, 2601 Meacham Blvd., Fort Worth, Texas 76137, telephone (817) 222-5122, fax (817) 222-5961, for information about previously approved alternative methods of compliance. (g) Special flight permits will not be issued. (h) You must use Bell Helicopter Textron Inc. Alert Service Bulletin 206L-87-47, Revision C, dated October 23, 1989, to do the actions required by this AD, unless the AD specifies otherwise. (1) On September 16, 1996 (61 FR 45876, August 30, 1996), the Director of the Federal Register previously approved the incorporation by reference of Bell Helicopter Textron Inc. Alert Service Bulletin 206L-87-47, Revision C, dated October 23, 1989. (2) For service information identified in this AD, contact Bell Helicopter Textron Canada, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4, telephone (450) 437-2862 or (800) 363-8023, fax (450) 433- 0272, or at http://www.bellcustomer.com/files/. (3) You may review copies of the service information incorporated by reference for this AD at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas. (4) You may also review copies of the service information incorporated by reference for this AD at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http:// www.archives.gov/federal_register/code_of_federal_regulations/ ibr_locations.html. (i) This amendment becomes effective on December 21, 2010.