On December 14, 2007, the FAA issued Emergency AD 2007-26-51 for Eurocopter Model EC135 helicopters, which requires, within 5 hours TIS, inspecting the control rod and adjoining ball pivot and replacing any unairworthy parts before further flight. That action was prompted by a report of a fatal accident involving the failure of a control rod. This condition, if not corrected, could result in the failure of a control rod and subsequent loss of control of the helicopter. \n\n\tThe European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, notified us that an unsafe condition may exist on Eurocopter EC135 and EC635 helicopters. EASA advises that an accident recently occurred with an EC135 helicopter in Japan. Preliminary investigation results indicate that the helicopter loss of control was due to the failure of the control rod. \n\n\tEurocopter has issued Alert Service Bulletin No. EC135-67A-017, dated December 13, 2007 (ASB), which specifies procedures for checking the attachment hardware on the control rod for a tight fit, checking the ball pivot for damage and freedom of movement, and replacing any damaged part before the next flight. EASA classified this ASB as mandatory and issued EASA AD No. 2007-0301-E, dated December 13, 2007, to ensure the continued airworthiness of these helicopters in the Federal Republic of Germany. \n\n\tThese helicopter models are manufactured in the Federal Republic of Germany and are type certificated for operation in the United States under the provisions of 14 CFR 21.29 and the applicable bilateral agreement. Pursuant to the applicable bilateral agreement, EASA has kept the FAA informed of the situation. The FAA has examined the findings of EASA, reviewed all available information, and determined that AD action is necessary for products of this type design that are certificated for operation in the United States. \n\n\tSince the unsafe condition described is likely to exist or develop on other Eurocopter Model EC135 helicopters of the same type design, the FAA issued Emergency AD 2007-26-51 to prevent failure of a control rod and subsequent loss of control of the helicopter. The AD requires, within 5 hours TIS, inspecting the control rod and adjoining ball pivot and replacing any unairworthy parts before further flight. The short compliance time involved is required because the previously described critical unsafe condition can adversely affect the controllability of the helicopter. Therefore, within 5 hours TIS, inspecting the control rod and adjoining ball pivot and replacing any unairworthy parts before further flight are required, and this AD must be issued immediately. \n\n\tSince it was found that immediate corrective action was required, notice and opportunity for prior public comment thereon were impracticable and contrary to the public interest, and good cause existed to make the AD effective immediately by individual lettersissued on December 14, 2007, to all known U.S. owners and operators of Eurocopter Model EC135 helicopters. These conditions still exist, and the AD is hereby published in the Federal Register as an amendment to 14 CFR 39.13 to make it effective to all persons. \n\n\tThe FAA estimates that this AD will affect 163 helicopters of U.S. registry. We estimate 1 work hour to inspect the control rod and ball pivot and 3 work hours to replace a control rod or ball pivot, if necessary, at an average labor rate of $80 per work hour. Required parts will cost $400 for the control rod and $675 for the ball pivot, per helicopter. Based on these figures, we estimate the total cost impact of the AD on U.S. operators to be $32,765, assuming 15 helicopters require a control rod and ball pivot to be replaced. \n\nComments Invited \n\n\tThis AD is a final rule that involves requirements that affect flight safety and was not preceded by notice and an opportunity for public comment; however, we invite you tosubmit any written data, views, or arguments regarding this AD. Send your comments to an address listed under ADDRESSES. Include "Docket No. FAA-2008-0101; Directorate Identifier 2007-SW-76-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the AD. We will consider all comments received by the closing date and may amend the AD in light of those comments. \n\n\tWe will post all comments we receive, without change, to http://www.regulations.gov , including any personal information you provide. We will also post a report summarizing each substantive verbal contact with FAA personnel concerning this AD. Using the search function of our docket web site, you can find and read the comments to any of our dockets, including the name of the individual who sent the comment. You may review the DOT's complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477-78), or youmay visit http://www.regulations.gov for the Federal government privacy notice. \n\nRegulatory Findings \n\n\tWe have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. \n\n\tFor the reasons discussed above, I certify that the regulation: \n\n\t1. Is not a "significant regulatory action'' under Executive Order 12866; \n\t2. Is not a "significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and \n\t3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. \n\n\tWe prepared an economic evaluation of the estimated costs to comply with this AD. See the AD docket to examine the economic evaluation. \n\nAuthority for This Rulemaking \n\n\tTitle 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. \n\n\tWe are issuing this rulemaking under the authority described in subtitle VII, part A, subpart III, section 44701, "General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. \n\nList of Subjects in 14 CFR Part 39 \n\n\tAir transportation, Aircraft, Aviation safety, Safety. \n\nAdoption of theAmendment \n\nAccordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n1. The authority citation for part 39 continues to read as follows: \n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\nSec. 39.13 (Amended) \n\n2. Section 39.13 is amended by adding a new airworthiness directive to read as follows: