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Code · REGISTER · 2005-02-17 · PROPOSED RULES · Unknown

Unknown. Final rule; request for comments

4,109 words·~19 min read·/register/2005/02/17/05-3049·

A research copy — for the controlling text, always check the official state or federal source. Not legal advice.

--- schema: federal-register doc_type: fedreg source_file: FR-2005-02-17.xml --- 70 32 Thursday, February 17, 2005 Contents AID Agency for International Development NOTICES Agency information collection activities; proposals, submissions, and approvals, 8056 05-3078 Agricultural Agricultural Marketing Service PROPOSED RULES Agricultural Marketing Act; miscellaneous marketing practices: USDA farmers market; operating procedures, 8040-8043 05-3072 Milk marketing orders: Mideast, 8043-8048 05-3070 NOTICES Beef promotion and research:
Cattlemen's Beef Promotion and Research Board; certification and nomination, 8056-8057 05-3071 Agriculture Agriculture Department See Agricultural Marketing Service See Animal and Plant Health Inspection Service See Food Safety and Inspection Service See Forest Service Animal Animal and Plant Health Inspection Service NOTICES Agency information collection activities; proposals, submissions, and approvals, 8057-8058 05-3056 Census Census Bureau PROPOSED RULES Foreign trade statistics:
Automated Export System; shipper's export declaration information; mandatory filing requirement, 8199-8227 05-2926 Centers Centers for Disease Control and Prevention NOTICES Meetings: Public Health Service Activities and Research at DOE Sites Citizens Advisory Committee, 8092-8093 05-3051 Children Children and Families Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8093 05-3087 Grants and cooperative agreements; availability, etc.:
Child support enforcement special improvement projects, 8093-8102 05-3090 State median income estimates for four-person families (2006 FY), 8102-8104 05-3088 Coast Guard Coast Guard NOTICES Meetings: National Offshore Safety Advisory Committee, 8106-8107 05-3019 Commerce Commerce Department See Census Bureau See Economic Development Administration See International Trade Administration See National Oceanic and Atmospheric Administration See Patent and Trademark Office NOTICES Agency information collection activities; proposals, submissions, and approvals, 8069-8070 05-3039 Defense Defense Department See Navy Department NOTICES Federal Acquisition Regulation (FAR):
Agency information collection activities; proposals, submissions, and approvals, 8085 05-3058 Drug Drug Enforcement Administration NOTICES *Applications, hearings, determinations, etc.:* Cody Laboratories, Inc., 8112 05-3028 Economic Economic Development Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 05-3034 8070-8071 05-3036 Education Education Department NOTICES Grants and cooperative agreements; availability, etc.: Elementary and secondary education— William F.
Goodling Even Start Family Literacy Programs, 8085-8089 E5-657 Energy Energy Department NOTICES Agency information collection activities; proposals, submissions, and approvals, 8090 05-3067 EPA Environmental Protection Agency NOTICES Agency information collection activities; proposals, submissions, and approvals, 8090-8091 05-3061 FAA Federal Aviation Administration RULES Airworthiness directives: Bell Helicopter Textron Canada, 8021-8025 05-3049 Bombardier, 8025-8028 05-2964 Empresa Brasileira de Aeronautica, S.A.
(EMBRAER), 8028-8032 05-2842 NOTICES Agency information collection activities; proposals, submissions, and approvals, 8132-8133 05-3017 Meetings: RTCA, Inc., 8133-8134 05-3016 Reports and guidance documents; availability, etc.: Type validation and post-type validation procedures for imported and exported products; comment request, 8134 05-3021 FCC Federal Communications Commission RULES Common carrier services: Individuals with hearing and speech disabilities; telecommunications relay service marketing and call handling and video relay procedures; clarification, 8034-8037 05-3066 PROPOSED RULES Radio stations; table of assignments:
Various States, 8054-8055 05-3063 Federal Highway Federal Highway Administration NOTICES Environmental statements; notice of intent: Loudoun County et al., VA; withdrawn, 8134-8135 05-3079 Federal Railroad Federal Railroad Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8135 05-3015 Exemption petitions, etc.: Uniontown Central Railroad, 8135-8136 05-3018 Fish Fish and Wildlife Service RULES Endangered and threatened species:
Critical habitat designations— Santa Ana sucker; correction, 8037 05-3047 NOTICES Comprehensive conservation plans; availability, etc.: Kern and Pixley National Wildlife Refuges, CA, 8108-8109 05-3073 Food Food and Drug Administration RULES Food additives: Direct food additives— Acacia (gum arabic), 8032-8034 05-3026 NOTICES GRAS or prior-sanctioned ingredients: Kerry, Inc.; petition withdrawn, 8104 05-3024 Meetings: Dermatologic and Ophthalmic Drugs Advisory Committee and Nonprescription Drugs Advisory Committee, 8104 05-3055 Food Food Safety and Inspection Service NOTICES Reports and guidance documents; availability, etc.:
Generic E. coli and salmonella standards; baseline studies results, 8058-8060 05-3030 Forest Forest Service NOTICES Reports and guidance documents; availability, etc.: Forest Service Outdoor Recreation Accessibility Guidelines; compliance and Forest Service Manual integration, 8060-8066 05-3069 Forest Service Trail Accessibility Guidelines; compliance and Forest Service Manual integration, 8066-8069 05-3068 GSA General Services Administration NOTICES Federal Acquisition Regulation (FAR):
Agency information collection activities; proposals, submissions, and approvals, 8085 05-3058 Health Health and Human Services Department See Centers for Disease Control and Prevention See Children and Families Administration See Food and Drug Administration See Health Resources and Services Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8091 05-3042 Grants and cooperative agreements; availability, etc.: Family planning— Services projects; correction, 8091-8092 05-3059 Health Health Resources and Services Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8104-8106 05-3022 05-3023 05-3054 Homeland Homeland Security Department See Coast Guard Housing Housing and Urban Development Department NOTICES Agency information collection activities; proposals, submissions, and approvals, 8107-8108 05-3007 Interior Interior Department See Fish and Wildlife Service See Land Management Bureau International International Trade Administration NOTICES Antidumping:
Circular welded carbon quality line pipe from— Mexico and Korea, 8071-8072 05-3081 Polyethylene terephthalate film, sheet and strip from— India, 8072-8074 E5-658 International International Trade Commission NOTICES Meetings; Sunshine Act, 8109 05-3145 Justice Justice Department See Drug Enforcement Administration NOTICES Pollution control; consent judgments: Arvanitis, Demetra, et al., 8109-8110 05-3014 Bello, Ralph, et al., 8110 05-3008 Bernstein, Frederic M., et al., 8110 05-3032 Formica Corp., et al., 8110-8111 05-3009 International Paper Co., et al., 8111 05-3010 Polaroid Corp. et al., 8111-8112 05-3013 Thomasville Furniture Industries, Inc., et al., 8112 05-3011 Labor Labor Department NOTICES Agency information collection activities; proposals, submissions, and approvals, 05-3075 8113-8116 05-3076 05-3077 Land Land Management Bureau NOTICES Public land orders:
New Mexico, 8109 05-3053 NASA National Aeronautics and Space Administration NOTICES Federal Acquisition Regulation (FAR): Agency information collection activities; proposals, submissions, and approvals, 8085 05-3058 Meetings: Summit Industry Panel, 8116 05-3006 National Archives National Archives and Records Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8116 05-3012 National Crime National Crime Prevention and Privacy Compact Council PROPOSED RULES Interstate Identification Index
(III)System; compliant conduct and responsible use for noncriminal justice purposes; Compact Council procedures, 8050-8054 05-3045 State criminal history record screening standards, 8048-8050 05-3041 National Highway National Highway Traffic Safety Administration NOTICES Motor vehicle safety standards: Exemption petitions, etc.— Nissan North America, Inc., 8136-8137 05-3020 NOAA National Oceanic and Atmospheric Administration RULES Fishery conservation and management: Caribbean, Gulf, and South Atlantic fisheries— Gulf of Mexico deep-water and shallow-water grouper, 8037-8039 05-3092 NOTICES Agency information collection activities; proposals, submissions, and approvals, 05-3033 8074-8076 05-3037 05-3038 Permits: Marine mammals, 8076-8078 05-3093 Navy Navy Department NOTICES Patent licenses; non-exclusive, exclusive, or partially exclusive: Vector Test Systems, Inc., 8085 05-3043 Nuclear Nuclear Regulatory Commission NOTICES Agency information collection activities; proposals, submissions, and approvals, 8116-8117 05-3050 Overseas Overseas Private Investment Corporation NOTICES Agency information collection activities; proposals, submissions, and approvals, 8117 05-3082 Patent Patent and Trademark Office NOTICES Agency information collection activities; proposals, submissions, and approvals, 8078-8085 05-3048 SEC Securities and Exchange Commission NOTICES Public Utility Holding Company Act of 1935 filings, 8117-8119 05-3057 Self-regulatory organizations; proposed rule changes: Chicago Board Options Exchange, Inc., 8119-8121 E5-656 National Securities Clearing Corp., 8121-8123 E5-655 New York Stock Exchange, Inc., 8123 E5-653 Pacific Exchange, Inc., 8123-8125 E5-654 Social Social Security Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 8125-8128 05-3029 State State Department NOTICES Grants and cooperative agreements; availability, etc.: Junior Faculty Development Program, 8128-8132 05-3083 Transportation Transportation Department See Federal Aviation Administration See Federal Highway Administration See Federal Railroad Administration See National Highway Traffic Safety Administration PROPOSED RULES Economic regulations: Aviation traffic data; collection, processing, and reporting requirements, 8139-8198 05-2861 Veterans Veterans Affairs Department NOTICES Inventions, Government-owned; availability for licensing, 8137 05-3085 Separate Parts In This Issue Part II Transportation Department, 8139-8198 05-2861 Part III Commerce Department, Census Bureau, 8199-8227 05-2926 Reader Aids Consult the Reader Aids section at the end of this issue for phone numbers, online resources, finding aids, reminders, and notice of recently enacted public laws. To subscribe to the Federal Register Table of Contents LISTSERV electronic mailing list, go to http://listserv.access.gpo.gov and select Online mailing list archives, FEDREGTOC-L, Join or leave the list (or change settings); then follow the instructions. 70 32 Thursday, February 17, 2005 Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20107; Directorate Identifier 2005-SW-02-AD; Amendment 39-13981; AD 2005-04-09] RIN 2120-AA64 Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; request for comments. SUMMARY: This amendment supersedes an existing airworthiness directive
(AD)for the specified Bell Helicopter Textron Canada
(BHTC)model helicopters that currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This amendment requires the same checks and inspections as the existing AD, but expands the applicability with the addition of two BHTC Model 430 helicopter serial numbers. This amendment is prompted by the manufacturer issuing revised service information that includes the additional two serial numbers. The actions specified by this AD are intended to detect a crack in the blade, and to prevent loss of a blade and subsequent loss of control of the helicopter. DATES: Effective March 4, 2005. Comments for inclusion in the Rules Docket must be received on or before April 18, 2005. ADDRESSES: Use one of the following addresses to submit comments on this AD: • DOT Docket Web site: Go to *http://dms.dot.gov* and follow the instructions for sending your comments electronically; • Government-wide rulemaking Web site: Go to *http://www.regulations.gov* and follow the instructions for sending your comments electronically; • *Mail:* Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street SW., Nassif Building, Room PL-401, Washington, DC 20590; • *Fax:*
(202)493-2251; or • *Hand Delivery:* Room PL-401 on the plaza level of the Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. You may get the service information identified in this AD from 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. You may examine this information 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.* Examining the Docket: You may examine the docket that contains the AD, any comments, and other information on the Internet at *http://dms.dot.gov,* or in person at the Docket Management System
(DMS)Docket Offices between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Office (telephone
(800)647-5227) is located on the plaza level of the Department of Transportation Nassif Building at the street address stated in the ADDRESSES section. Comments will be available in the AD docket shortly after the DMS receives them. FOR FURTHER INFORMATION CONTACT: Sharon Miles, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Regulations and Policy Group, Fort Worth, Texas 76193-0111, telephone
(817)222-5122, fax
(817)222-5961. SUPPLEMENTARY INFORMATION: On December 23, 2004, the FAA issued AD 2004-26-11, Amendment 39-13923 (70 FR 7; January 3, 2005), to require certain checks and inspections of the blades. If a crack is found, that AD requires replacing the blade with an airworthy blade before further flight. That action was prompted by three reports of cracked blades that were found during scheduled inspections. That condition, if not corrected, could result in loss of a blade and subsequent loss of control of the helicopter. Since issuing that AD, the alert service bulletin
(ASB)that is applicable to BHTC Model 430 helicopters has been revised by the manufacturer to include two additional helicopter serial numbers. Further, we discovered two typographical errors in the AD—the word “Canada” is inadvertently omitted from the manufacturer's name in the Summary section, and in Note 1 of the AD, the number for the Model 430 helicopter ASB is incorrectly stated as 430-04-32 instead of 430-04-31—as well as some minor editorial errors, which have been corrected in this AD. Transport Canada, the airworthiness authority for Canada, notified the FAA that an unsafe condition may exist on the specified BHTC model helicopters. Transport Canada advises of the discovery of cracked blades during scheduled inspections on three occasions. Two cracks originated from the outboard feathering bearing bore underneath the flanged sleeves. The third crack started from the inboard feathering bearing bore. Investigation found that the cracks originated from either a machining burr or a corrosion site in the bearing bore underneath the flanged sleeves. BHTC has issued ASB No. 222-04-100 for Model 222 and 222B helicopters; ASB No. 222U-04-71 for Model 222U helicopters; and ASB No. 230-04-31 for Model 230 helicopters, all dated August 27, 2004; and, ASB No. 430-04-31, Revision A, dated November 29, 2004, for Model 430 helicopters. The ASBs specify a visual inspection of the blade root end around the feather bearings for a crack, not later than at the next scheduled inspection, and thereafter at intervals not to exceed 3 flight hours. Further, they describe a visual inspection for a crack, to include removing the blade from the helicopter, within 50 flight hours, and thereafter at intervals not to exceed 50 flight hours. Transport Canada classified these ASBs as mandatory and issued AD CF-2004-21R1, dated December 9, 2004, to ensure the continued airworthiness of these helicopters in Canada. This AD differs from those ASBs in that it requires an initial visual check, which may be performed by a pilot, within 3 hours time-in-service
(TIS)rather than a visual inspection not later than at the next scheduled inspection and every 3 flight hours maximum thereafter as stated in the ASBs. These helicopter models are manufactured in Canada 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, Transport Canada has kept the FAA informed of the situation described above. The FAA has examined the findings of Transport Canada, reviewed all available information, and determined that AD action is necessary for products of these type designs that are certificated for operation in the United States. This previously described unsafe condition is likely to exist or develop on other helicopters of the same type design. Therefore, this AD supersedes AD 2004-26-11 to require the following: • Within 3 hours TIS, and thereafter at intervals not to exceed 3 hours TIS, clean and visually check both sides of each blade for a crack in the area around the tail rotor feathering bearing. An owner/operator (pilot) may perform this check. Pilots may perform the checks required by paragraph
(a)of this AD because they require no tools, can be done by observation, and can be done equally well by a pilot or a mechanic. However, the pilot must enter compliance with these requirements into the helicopter maintenance records by following 14 CFR 43.11 and 91.417(a)(2)(v). • Within 50 hours TIS, and thereafter at intervals not to exceed 50 hours TIS, clean and inspect both sides of each blade for a crack using a 10X or higher magnifying glass. • If a crack is found in the blade paint during a visual check or inspection, further inspect the blade as follows, before further flight: • Remove the blade. Remove the paint to the bare metal in the area of the suspected crack by using plastic metal blasting
(PMB)or a nylon web abrasive pad and abrading the blade surface in a span-wise direction only. • Using a 10X or higher power magnifying glass, inspect the blade for a crack. • If a crack is found, replace the blade with an airworthy blade before further flight. • If no crack is found in the blade surface, refinish the blade by applying one coat of epoxy polyamide primer, MIL-P-23377 or MIL-P-85582, so that the primer overlaps the existing coats just beyond the abraded area. Let the area dry for 30 minutes to 1 hour. Then, apply one sealer coat of polyurethane, MILC85285 TYI CL2, color number 27925 (semi-gloss white), per Fed. Std. 595, and reinstall the blade. This AD is an interim action, pending release of additional service information from the manufacturer concerning instructions for inspecting and reworking the affected blades. We expect that service information to eliminate the recurring inspections required by this AD. The short compliance time involved is required because the previously described critical unsafe condition can adversely affect the controllability and structural integrity of the helicopter. Therefore, checking the blade for a crack within 3 hours TIS, and thereafter at intervals not to exceed 3 hours TIS, is required, and this AD must be issued immediately. Since a situation exists that requires the immediate adoption of this regulation, it is found that notice and opportunity for prior public comment hereon are impracticable, and that good cause exists for making this amendment effective in less than 30 days. We estimate that this AD will affect 156 helicopters and will require: • 0.25 work hour for a pilot check, and 2 work hours for a maintenance inspection, at an average labor rate of $65 per work hour; and • Parts, which will cost an estimated $13,410 per helicopter. Based on these figures, the estimated total cost impact of the AD on U.S. operators is $2,842,320 per year, assuming each helicopter will require 200 pilot checks, 12 maintenance inspections, and one blade replacement per year. Comments Invited This 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 to submit any written data, views, or arguments regarding this AD. Send or deliver your comments to an address listed under ADDRESSES. Include “Docket No. FAA-2005-20107; Directorate Identifier 2005-SW-02-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. We will post all comments we receive, without change, to *http://dms.dot.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 you may visit *http://dms.dot.gov.* Regulatory Findings We 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. For the reasons discussed above, I certify that the regulation: 1. Is not a “significant regulatory action” under Executive Order 12866; 2. Is not a “significant rule” under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and 3. 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. We prepared an economic evaluation of the estimated costs to comply with this AD. See the DMS to examine the economic evaluation. Authority for This Rulemaking Title 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. We 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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety. Adoption of the Amendment Accordingly, 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: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. Section 39.13 is amended by removing Amendment 39-13923 (70 FR 7, January 3, 2005), and by adding a new airworthiness directive (AD), Amendment 39-13981, to read as follows: **2005-04-09 Bell Helicopter Textron Canada:** Amendment 39-13981. Docket No. FAA-2005-20107; Directorate Identifier 2005-SW-02-AD. Supersedes AD 2004-26-11, Amendment 39-13923, Docket No. FAA-2004-19969, Directorate Identifier 2004-SW-43-AD. *Applicability:* The following helicopter models, identified by serial number, with one of the following part numbered tail rotor blades installed, certificated in any category. Model Serial No. Tail rotor blade (blade) part no. 222 47006 through 47089 222-016-001-123, -127, -131, and -135. 222B 47131 through 47156 222-016-001-123, -127, -131, and -135. 222U 47501 through 47574 222-016-001-123, and -131. 230 23001 through 23038 222-016-001-123, and -131. 430 49001 through 49107 222-016-001-123, and -131. *Compliance:* Required as indicated. To detect a crack in the blade and to prevent loss of the blade and subsequent loss of control of the helicopter, accomplish the following:
(a)Within 3 hours time-in-service (TIS), and thereafter at intervals not to exceed 3 hours TIS, clean and visually check both sides of each blade for a crack in the paint in the areas shown in Figure 1 of this AD. An owner/operator (pilot), holding at least a private pilot certificate, may perform this visual check and must enter compliance with this paragraph into the helicopter maintenance records by following 14 CFR 43.11 and 91.417(a)(2)(v). BILLING CODE 4910-13-P ER17FE05.002 BILLING CODE 4910-13-C Note 1: Bell Helicopter Textron Alert Service Bulletin
(ASB)No. 222-04-100, No. 222U-04-71, and No. 230-04-31, all dated August 27, 2004, and ASB No. 430-04-31, Revision A, dated November 29, 2004, pertain to the subject of this AD.
(b)If the visual check required by paragraph
(a)reveals a crack in the paint, before further flight, remove the blade and follow the requirements in paragraphs (c)(2) through (c)(3)(ii) of this AD.
(c)Within the next 50 hours TIS, unless accomplished previously, and thereafter at intervals not to exceed 50 hours TIS, clean the blade by wiping down both surfaces of each blade in the inspection area depicted in Figure 1 of this AD using aliphatic naphtha (C-305) or detergent (C-318) or an equivalent. Using a 10X or higher power magnifying glass, visually inspect both sides of the blade in the areas depicted in Figure 1 of this AD.
(1)If a crack is found, even if only in the paint, before further flight, remove the blade from the helicopter and proceed with the following:
(2)Remove the paint on the blade down to the bare metal in the area of the suspected crack by using plastic metal blasting
(PMB)or a nylon web abrasive pad. Abrade the blade surface in a span-wise direction only. Note 2: PMB may cause damage to helicopter parts if untrained personnel perform the paint removal. BHT-ALL-SPM, chapter 3, paragraph 3-24, pertains to the subject of this AD.
(3)Using a 10X or higher power magnifying glass, inspect the blade for a crack.
(i)If a crack is found, replace the blade with an airworthy blade before further flight.
(ii)If no crack is found in the blade surface, refinish the blade by applying one coat of epoxy polyamide primer, MIL-P-23377 or MIL-P-85582, so that the primer overlaps the existing coats just beyond the abraded area. Let the area dry for 30 minutes to 1 hour. Then, apply one sealer coat of polyurethane, MILC85285 TYI CL2, color number 27925 (semi-gloss white), per Fed. Std. 595. Reinstall the blade. Note 3: BHT-ALL-SPM, chapter 4, pertains to painting the blade.
(d)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 Safety Management Group, FAA, for information about previously approved alternative methods of compliance.
(e)Special flight permits may be issued by following 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the requirements of this AD can be accomplished provided you do not find a crack in the blade paint during a check or inspection.
(f)This amendment becomes effective March 4, 2005. Note 4: The subject of this AD is addressed in Transport Canada (Canada) Airworthiness Directive CF-2004-21R1, dated December 9, 2004. Issued in Fort Worth, Texas, on February 10, 2005. Kim Smith, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 05-3049 Filed 2-16-05; 8:45 am]
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