Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005

Agriculture Department See Agricultural Marketing Service See Commodity Credit Corporation See Forest Service NOTICES Committees; establishment, renewal, termination, etc.: National Sheep Industry Improvement Center Board of Directors, 2376 Architectural and Transportation Barriers Compliance Board NOTICES Meetings: Courthouse Access Advisory Committee, 2389–2390 Army Department NOTICES Patent licenses; non-exclusive, exclusive, or partially exclusive: Identification of small molecules of inhibitors anthrax factor, 2396 Centers for Disease Control and Prevention NOTICES Grants and cooperative agreements; availability, etc.: National Cancer Prevention and Control Program, 2407– 2410 Children and Families Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 2410–2411 Coast Guard RULES Anchorage regulations: Massachusetts, 2353–2355 Drawbridge operations: Louisiana, 2355 Ports and waterways safety: Bering Sea, Aleutian Islands, and Unalaska Island, AK; safety zone, 2355–2357 Puget Sound, WA, Captain of Port Zone; security zone, 2357 Commerce Department See Industry and Security Bureau See International Trade Administration See National Oceanic and Atmospheric Administration Commodity Credit Corporation NOTICES Grants and cooperative agreements; availability, etc.: Emerging Markets Program, 2376–2380 Foreign Market Development Cooperator Program, 2380– 2382 Market Access Program, 2382–2384 Quality Samples Program, 2384–2386 Technical Assistance for Specialty Crops Program, 2386– 2388 Commodity Futures Trading Commission RULES National Futures Association; review of disciplinary, membership denial, registration, and member responsibility actions decisions; amendments, 2350– 2352 Consumer Product Safety Commission PROPOSED RULES Flammable Fabrics Act: Bedclothes; flammability (open flame ignition) standard, 2513–2517 Mattresses and mattress and foundation sets; flammability (open flame) standard, 2469–2514 Defense Department See Army Department RULES Acquisition regulations: Australia and Morocco; free trade agreements, 2361–2366 Competition requirements; correction, 2361 NOTICES Meetings: Defense Acquisition University Board of Visitors, 2395 Servicemembers Civil Relief Act: Housing price inflation adjustment, 2395–2396 Education Department NOTICES Agency information collection activities; proposals, submissions, and approvals, 2396 Grants and cooperative agreements; availability, etc.: Advanced Placement Test Fee Program, 2397 Arts in Education Model Development and Dissemination Program; proposed priority, requirements, and definitions, 2397–2399 Professional Development for Arts Educators Program, 2399–2401 Meetings: Special Education and Rehabilitative Services Office, 2401–2402 Energy Department NOTICES Natural gas exportation and importation: Amerada Hess Corp. et al., 2402–2403 Environmental Protection Agency RULES Air quality implementation plans; approval and promulgation; various States: New York, 2358–2360 NOTICES Toxic and hazardous substances control: Neurotoxicity test guideline development and harmonized test guideline; revocation and withdrawal requests; agency response, 2403–2404 VerDate jul<14>2003 20:15 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00001 Fmt 4748 Sfmt 4748 E:\FR\FM\13JACN.SGM 13JACN IV Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Contents Farm Credit System Insurance Corporation NOTICES Meetings, 2404 Federal Aviation Administration RULES Aircraft products and parts; certification procedures: Armed Forces surplus aircraft; large reciprocating-engine powered airplanes; type certification; correction, 2325 Airworthiness directives: Boeing, 2330–2333, 2339–2342 Rolls-Royce plc, 2333–2339 Airworthiness standards: Special conditions— Boeing Model 767-300 airplane, 2325–2330 Class E airspace, 2342–2348 PROPOSED RULES Airworthiness directives: Cirrus Design Corp., 2370–2372 NOTICES Airport noise compatibility program: Noise exposure maps— Missoula International Airport, MT, 2451–2452 Exemption petitions; summary and disposition, 2453–2454 Meetings: Aviation Rulemaking Advisory Committee, 2454 Federal Communications Commission RULES Common carrier services: Individuals with hearing and speech disabilities; telecommunications relay and speech-to-speech services; three-way calling requirement; waiver expiration, 2360–2361 NOTICES Agency information collection activities; proposals, submissions, and approvals, 2404–2405 Common carrier services: Enhanced 911 capabilities for multi-line telephone systems; States deployment actions, 2405–2406 Federal Election Commission NOTICES Meetings; Sunshine Act, 2406 Federal Motor Carrier Safety Administration NOTICES Motor carrier safety standards: Commercial Driver’s License Information System; information availability policy, 2454–2455 Federal Railroad Administration NOTICES Safety advisories, bulletins, and directives: Position of switches in non-signaled territory, 2455–2456 Federal Reserve System NOTICES Banks and bank holding companies: Permissible nonbanking activities, 2406–2407 Food and Drug Administration RULES Animal drugs, feeds, and related products: Levamisole powder for oral solution, 2352–2353 Sponsor name and address changes— Alstoe, Ltd., 2352 NOTICES Agency information collection activities; proposals, submissions, and approvals, 2411–2415 Food additive petitions: Alltech, Inc., 2415 Reports and guidance documents; availability, etc.: Labeling over-the-counter human drug products-questions and answers, 2415–2416 Forest Service NOTICES Appealable decisions; legal notice: Northern Region, 2388 Meetings: Resource Advisory Committees— Madison-Beaverhead, 2389 North Central Idaho, 2388–2389 Siskiyou County, 2389 Shasta-Trinity National Forest, CA; collaborative off- highway vehicle route designation process, 2389 Government Ethics Office NOTICES Intelligence Reform and Terrorism Prevention Act: Executive branch employees; financial disclosure process; recommendations and evaluation study, 2407 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 Health Resources and Services Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 2416–2417 Meetings: Interdisciplinary, Community-Based Linkages Advisory Committee, 2417 Homeland Security Department See Coast Guard See Transportation Security Administration Indian Affairs Bureau NOTICES Committees; establishment, renewal, termination, etc.: Exceptional Education Advisory Board, 2417–2421 Indian Reservation Roads Program Coordinating Committee, 2422–2423 Land acquisitions into trust: White Earth Chippewa Reservation of Minnesota, 2423– 2425 Industry and Security Bureau RULES Export administration regulations: Commerce Control List— Australia Group understandings and intersessional decision; clarifications, corrections, and Chemical Weapons Convention membership additions; correction, 2348–2350 Interior Department See Indian Affairs Bureau See Land Management Bureau VerDate jul<14>2003 20:15 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00002 Fmt 4748 Sfmt 4748 E:\FR\FM\13JACN.SGM 13JACN V Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Contents Internal Revenue Service NOTICES Meetings: Taxpayer Advocacy Panels, 2465 Privacy Act: Systems of records, 2465–2466 International Trade Administration NOTICES North American Free Trade Agreement (NAFTA); binational panel reviews: Carbon and alloy steel wire rod from— Canada; correction, 2390 International Trade Commission NOTICES Import investigations: Potassium permanganate from— China, 2428 U.S.-Central America Free Trade Agreement; potential economywide and selected sectoral effects; investigation terminated, 2429 Land Management Bureau NOTICES Meetings: McInnis Canyons National Conservation Area Advisory Council, 2425 Pinedale Anticline Working Group task groups, 2425– 2426 Resource Advisory Councils— Southeast Oregon, 2426 Oil and gas leases: Wyoming, 2426–2427 Recreation management restrictions, etc.: La Paz County, AZ; temporary closure of selected public lands during operation of Parker 425 Desert Race, 2427–2428 Maritime Administration NOTICES Agency information collection activities; proposals, submissions, and approvals, 2457 National Highway Traffic Safety Administration NOTICES Grants and cooperative agreements; availability, etc.: Crash Injury Research and Engineering Network; Level One Trauma Centers; responses to questions, 2457– 2462 Motor vehicle safety standards; exemption petitions, etc.: Morgan Motor Co. Ltd., 2462–2464 National Oceanic and Atmospheric Administration RULES Marine mammals: Commercial fishing authorizations— Atlantic Large Whale Take Reduction Plan, 2367–2369 NOTICES Endangered and threatened species: Andromous fish take— Washington County, OR; Routine Road Maintenance Program; availability, 2390–2391 Meetings: Gray’s Reef National Marine Sanctuary Advisory Council, 2391–2392 Marine Protected Areas Federal Advisory Committee, 2392 Mid-Atlantic Fishery Management Council; correction, 2392 New England Fishery Management Council, 2392–2393 Western Pacific Fishery Management Council, 2393–2394 Permits: Marine mammals, 2394–2395 Scientific research, 2395 National Science Foundation NOTICES Meetings; Sunshine Act, 2429 Nuclear Regulatory Commission NOTICES Applications, hearings, determinations, etc.: Louisiana Energy Services, L.P., 2429–2430 Safety Light Corp., 2430–2431 Research and Special Programs Administration RULES Hazardous materials: Transportation— Primary lithium batteries and cells; prohibition aboard passenger aircraft; public meeting, 2367 Securities and Exchange Commission NOTICES Options Price Reporting Authority: Consolidated Options Last Sale Reports and Quotation Information; Reporting Plan; amendments, 2432 Self-regulatory organizations; proposed rule changes: American Stock Exchange LLC, 2432–2435 American Stock Exchange LLC; correction, 2467 Boston Stock Exchange, Inc.; correction, 2467 Chicago Board Options Exchange, Inc., 2435–2439 International Securities Exchange LLC, 2439–2440 National Association of Securities Dealers, Inc., 2440– 2441 Options Clearing Corp., 2442 Pacific Exchange, Inc., 2443–2444 Philadelphia Stock Exchange, Inc., 2444–2447 Applications, hearings, determinations, etc.: Premier Farnell Plc, 2431 Social Security Administration NOTICES Social Security Protection Act; implementation: Direct payment to non-attorney representatives; demonstration project, 2447–2450 State Department NOTICES Art objects; importation for exhibition: Kingdom of Siam: Art of Central Thailand (1350-1800), 2450 Meetings: International Telecommunication Advisory Committee, 2450 Shipping Coordinating Committee, 2450–2451 Surface Transportation Board NOTICES Motor carriers: Control applications— Pacific Coast Sightseeing Tours & Charters, 2464–2465 Transportation Department See Federal Aviation Administration VerDate jul<14>2003 20:15 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00003 Fmt 4748 Sfmt 4748 E:\FR\FM\13JACN.SGM 13JACN VI Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Contents See Federal Motor Carrier Safety Administration See Federal Railroad Administration See Maritime Administration See National Highway Traffic Safety Administration See Research and Special Programs Administration See Surface Transportation Board PROPOSED RULES Aviation economic regulations: Print advertisements of scheduled passenger services; code-sharing arrangements and long-term wet leases; disclosure, 2372–2375 Transportation Security Administration RULES Maritime and land transportation security: Hazardous materials drivers; security threat assessments; fees, 2541–2560 Treasury Department See Internal Revenue Service Separate Parts In This Issue Part II Consumer Product Safety Commission, 2469–2517 Part III Agriculture Department, Agricultural Marketing Service, 2519–2540 Part IV Homeland Security Department, Transportation Security Administration, 2541–2560 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. VerDate jul<14>2003 20:15 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00004 Fmt 4748 Sfmt 4748 E:\FR\FM\13JACN.SGM 13JACN CFR PARTS AFFECTED IN THIS ISSUE A cumulative list of the parts affected this month can be found in the Reader Aids section at the end of this issue. VII Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Contents 7 CFR Proposed Rules: 927.....................................2520 14 CFR 21.......................................2325 25.......................................2325 39 (4 documents) ...2330, 2333, 2336, 2339 71 (7 documents) ...2342, 2343, 2344, 2345, 2346, 2347, 2348 Proposed Rules: 39.......................................2370 257.....................................2372 15 CFR 742.....................................2348 774.....................................2348 16 CFR Proposed Rules: 1633...................................2470 1634...................................2514 17 CFR 171.....................................2350 21 CFR 510.....................................2352 520.....................................2352 33 CFR 110.....................................2353 117.....................................2355 165 (2 documents) ...........2355, 2357 40 CFR 52.......................................2358 47 CFR 64.......................................2360 48 CFR 206.....................................2361 225.....................................2361 252.....................................2361 49 CFR 171.....................................2367 172.....................................2367 173.....................................2367 175.....................................2367 1572...................................2542 50 CFR 229.....................................2367 VerDate jul 14 2003 20:15 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00001 Fmt 4711 Sfmt 4711 E:\FR\FM\13JALS.LOC 13JALS This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. Rules and Regulations Federal Register 2325 Vol. 70, No. 9 Thursday, January 13, 2005 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 21 Certification Procedures for Products and Parts: Type Certificates; Issue of Type Certificate: Surplus Aircraft of the Armed Forces; Correction AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Correcting amendment. SUMMARY : This document corrects an error that appears in the Code of Federal Regulations (CFR), title 14, as of January 1, 2004. The regulation relates to type certification of large reciprocating- engine powered airplanes that are surplus from the Armed Forces of the United States. DATES : Effective on January 13, 2005. FOR FURTHER INFORMATION CONTACT : Brian Yanez, phone (202) 267–5864. SUPPLEMENTARY INFORMATION : Need for Correction As published in the CFR, this regulation contains an error in which the date ‘‘Aug. 25, 1959’’ was incorrectly substituted for the date ‘‘Aug. 25, 1955’’. List of Subjects in 14 CFR Part 21, Subpart B Type certificates.
Accordingly, 14 CFR part 21 is corrected by making the following correcting amendments: PART 21—CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS
(1) The authority citation for part 21 continues to read as follows: Authority: 42 U.S.C. 7572; 49 U.S.C. 106(g), 40105, 40113, 44701–44702, 44707, 44709, 44711, 44713, 44715, 45303.
(2) In § 21.27, amend paragraph (f) by revising the dates in the table for the entry ‘‘Large reciprocating-engine powered airplanes’’ to read as follows: § 21.27 Issue of type certificate: surplus aircraft of the Armed Forces. * * * * * (b) * * * * * * Large reciprocating-engine powered airplanes: Before Aug. 26, 1955. After Aug. 25, 1955. * * * * * Issued in Washington, DC, on January 7, 2005. Anthony F. Fazio, Director, Office of Rulemaking. [FR Doc. 05–754 Filed 1–12–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. NM299; Special Conditions No. 25–283–SC] Special Conditions: Boeing Model 767– 300 Airplane; Forward Lower Deck Service/Cargo Compartment AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final special conditions; request for comments. SUMMARY : These special conditions are issued for a Boeing Model 767–300 airplane modified by Jet Aviation Engineering Services (JAES), Spring Branch, Texas. This modified airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The modification is associated with a forward lower deck compartment that will serve as both a service compartment and a Class C cargo compartment. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES : The effective date of these special conditions is February 14, 2005. Comments must be received on or before February 28, 2005. ADDRESSES : Comments on these special conditions may be mailed in duplicate to: Federal Aviation Administration, Transport Airplane Directorate, Attention: Rules Docket (ANM–113), Docket No. NM299, 1601 Lind Avenue SW., Renton, Washington 98055–4056; or delivered in duplicate to the Transport Airplane Directorate at the above address. All comments must be marked: Docket No. NM299. FOR FURTHER INFORMATION CONTACT : Gerald Lakin, FAA, Standardization, ANM–113, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington, 98055–4056; telephone (425) 227–1187; facsimile (425) 227–1149. SUPPLEMENTARY INFORMATION : The FAA has determined that notice and opportunity for prior public comment hereon are impracticable, because those procedures would significantly delay issuance of the approval design and thus delivery of the affected aircraft. The FAA, therefore, finds that good cause exists for making these special conditions effective upon issuance. Comments Invited Interested persons are invited to submit such written data, views, or arguments as they may desire. Comments should identify the rules docket number and be submitted in duplicate to the address specified above. The Administrator will consider all comments received on or before the closing date for comments. The special conditions may be changed in light of the comments received. All comments received will be available in the Rules Docket for examination by interested persons, both before and after the closing date for comments. A report summarizing each substantive public contact with FAA personnel concerning this rulemaking will be filed in the docket. Persons wishing the FAA to acknowledge receipt of their comments submitted in response to these special conditions must include with those comments a self-addressed postcard on which the following statement is made: ‘‘Comments to Docket No. NM299. The postcard will be date stamped and returned to the commenter. VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2326 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations Background On December 4, 2003, Jet Aviation Engineering Services (JAES) applied for a supplemental type certificate that would allow modification of a Boeing Model 767–300 airplane interior to an executive jet interior configuration. Boeing Model 767–300 series airplanes, currently approved under Type Certificate A1NM, are large transport category airplanes with a main passenger deck limited to 290 passengers or fewer, depending on the interior configuration. As part of the type design, certified Class C cargo compartments are installed below the main deck. Jet Aviation Engineering Services proposes to include as part of the interior STC modification, access to the forward lower deck Class C cargo compartment and to convert that compartment for use as a combined service compartment and Class C cargo compartment (service/cargo compartment). Access will be provided by two hatches installed in the cabin floor, a primary hatch in the galley and a secondary hatch located in the crew rest area. A ladder will be installed at each hatch to provide access from the hatch to the forward lower deck service compartment floor. Access would be limited to one trained crewmember and would be allowed during level flight, but would not be allowed during taxi, takeoff and landing or during a fire. As part of the safety enhancement necessary to allow occupancy of the forward lower deck service/cargo compartment by a crewmember, JAES proposes the installation of warning and emergency equipment, as defined for a lower lobe service compartment in 14 CFR 25.819. Speakers, warning lights, and buzzers will be installed in the forward lower deck service/cargo compartment to warn an occupant of turbulent conditions, the presence of smoke or fire, or the need to leave the area. A crew interphone will be provided for communications with the flightdeck. Jet Aviation Engineering Services indicates that the forward lower deck service/cargo compartment will meet the Class C cargo requirements of §§ 25.855 and 25.857. The compartment will be built using materials meeting the flammability standards for Class C cargo compartments and will have a smoke detection system. The compartment will be equipped with an approved built-in fire suppression system, which is controllable from the cockpit to eliminate the need to send someone into the compartment to fight a fire. In the event of a fire, the forward lower deck service/cargo compartment will be evacuated, and the pilot will activate the built-in fire suppression system. A means will be provided to prevent inadvertent access to the compartment when the fire suppression system has been activated. Current regulations specify the requirements for a forward lower deck service compartment (§ 25.819) and a Class C cargo compartment (§§ 25.855 and 25.857) but the regulations did not envision a dual-purpose compartment. Currently, § 25.819 specifies that a service compartment may be occupied and does not need to be evacuated under certain normal conditions or under certain unsafe conditions (e.g., in the case of fire, the occupant could function as a firefighter). The fire control system of a service compartment, however, would not utilize a flood-type fire suppressant, since the compartment might be occupied. Section 25.857, however, specifies that a Class C cargo compartment have a fire detection system and a built-in fire suppression system, i.e., a total flood system. The applicant intends to use the compartment as a dual-purpose service/ cargo compartment and intends for the operator to use the built-in systems to fight fires in every instance. The concept of a multi-use compartment, which JAES proposes, would be acceptable if the FAA could be assured that whether the compartment is used as a service compartment or as a Class C cargo compartment, the level of safety would be equivalent to that of a separate service compartment or a separate Class C cargo compartment. Therefore, special conditions that provide an equivalent level of safety are being required. These special conditions pertain to visible and audible warnings, placards and limitations, equipment, evacuation routes, training, and the use of ladders between the main deck and the forward lower deck service/cargo compartment. Type Certification Basis Under the provisions of 14 CFR 21.101, Jet Aviation Engineering Services must show that the Boeing Model 767–300 airplane, as modified, continues to meet the applicable provisions of the regulations incorporated by reference in Type Certificate A1NM or the applicable regulations in effect on the date of application for the change. The regulations incorporated by reference in the type certificate are commonly referred to as the ‘‘original type certification basis.’’ The regulations incorporated by reference in Type Certificate A1NM for the Boeing Model 767–300 series airplanes include 14 CFR part 25, as amended by Amendments 25–1 through 25–37 with certain additions and special conditions as listed in the type certificate data sheet. The U.S. type certification basis for the Boeing Model 767–300 series airplane is established in accordance with §§ 21.17 and 21.21 and the type certification application date. The type certification basis listed in Type Certificate Data Sheet No. A1NM, for the Boeing Model 767–300 does not include § 25.819, which was introduced in Amendment 25–53. In this case, § 25.819 does provide appropriate safety standards for that portion of this STC’s design considered a service compartment. Therefore, in lieu of applying the requirements of § 25.819 as a special condition, § 25.819 (Amendment 25–110) will be added as a requirement to this STC’s certification basis. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for a Boeing Model 767–300 series airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16. In addition to the applicable airworthiness regulations and special conditions, the Boeing Model 767–300 must comply with the fuel vent and exhaust emission requirements of 14 CFR part 34 and the noise certification requirements of 14 CFR part 36. Special conditions, as defined in 14 CFR 11.19, are issued in accordance with § 11.38 and become part of the type certification basis in accordance with § 21.101. Special conditions are initially applicable to the model for which they are issued. Should the applicant apply for a supplemental type certificate to modify any other model included on the same type certificate to incorporate the same novel or unusual design feature, the special conditions would also apply to the other model under the provisions of § 21.101. Novel or Unusual Design Features The Boeing Model 767–300 airplane will incorporate a novel or unusual design feature; specifically, the forward lower deck compartment will be used as a combined service compartment and Class C cargo compartment. Discussion To allow the use of a dual-purposed service/cargo compartment, these VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2327 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations special conditions require certain visible and audible warnings, placards and limitations, equipment, and training. The applicant has not proposed a means of satisfying regulatory requirements governing occupancy of the forward lower deck service/cargo compartment during taxi, takeoff, and landing. Therefore, the FAA will specify appropriate limitations for such occupancy. A discussion of each specific special condition follows but is limited where the specific special condition is self-explanatory: Special Condition 1—Visible and Audible Warnings To maintain the advantages of both a service compartment and a Class C cargo compartment, certain warnings need to be provided. Special Condition 1a requires a visible advisory in the cockpit to notify the flightcrew when the forward lower deck service/cargo compartment is occupied. The potential exists that the forward lower deck service/cargo compartment may inadvertently be occupied when it should not be, such as during taxi, takeoff or landing or during certain emergencies. Special Condition 1a also ensures that the flightcrew is aware that the forward lower deck service/cargo compartment is occupied in order that the flightcrew can take appropriate action to evacuate the compartment before flooding it with fire suppressant. There must be a placard or sign adjacent to the warning light which indicates that the light means that the compartment is occupied. Special Condition 1b requires an ‘‘on/ off’’ visible warning placard stating ‘‘Do Not Enter’’ (or similar words) placard to be located on or near each hatch. The location should be on the main deck side of the hatch. The warning is to be controlled from the flightdeck to prevent someone from entering the forward lower deck service/cargo compartment when it should not be occupied; such as during taxi, takeoff or landing, or when smoke or fire has been detected. Opening the door during a fire would degrade the effectiveness of the fire suppressant and allow smoke, flame, and/or fire suppressant into the cabin. Special Condition 1c requires a visible and audible warning in the forward lower deck service/cargo compartment to notify an occupant that he or she must leave the compartment. This warning must be one which can be seen and heard from any part of the compartment. The visible and audible warning is to be controlled from the flightdeck. Because the forward lower deck service/cargo compartment may be occupied on the ground or in the air, a warning must be provided to notify an occupant to leave the compartment prior to taxi, takeoff or landing or during certain emergencies (other than fire, which is dealt with under Special Condition 1e). A visible warning is required, in case the audible warning becomes masked or distorted by engine, equipment, or ground noises. Special condition 1d requires a visible and audible warning in the forward lower deck service/cargo compartment to notify an occupant of the need to use a portable oxygen bottle in the event of decompression. This warning must be one which can be seen and heard from any part of the compartment and must be distinct from other warnings in the compartment to prevent confusion and to elicit correct action. The decompression warning must be automatic (i.e., not require separate crew action) to ensure that an occupant of the forward lower deck service/cargo compartment does not delay putting on the mask attached to the portable oxygen bottle. This section of the special conditions is partially in lieu of the visible effect provided by the automatic presentation feature required by § 25.1447. Special Condition 1e requires a visible and audible warning in the forward lower deck service/cargo compartment when a fire is detected to notify an occupant that he or she must evacuate the compartment. The warning must be one which can be seen and heard from any part of the compartment and must be distinct from other warnings in the compartment in order to prevent confusion and to elicit the correct actions. The fire or smoke detection warning must be automatic (i.e., not require or depend on separate crew action) to ensure that an occupant of the forward lower deck service/cargo compartment leaves before the flightdeck crew releases fire suppressant in the compartment. Special Condition 2—Placards and Limitations The forward lower deck service/cargo compartment must be evacuated if a fire occurs. In addition, there must be a way to prevent access into the compartment during taxi, takeoff or landing or in the event of a fire. Placards and limitations are specified for these situations. Special Condition 2a requires a placard to be located outside each hatch to the forward lower deck service/cargo compartment, indicating that access is limited to one crewmember trained in evacuation procedures. Special Condition 2b requires placards to be located inside and outside each hatch of the forward lower deck service/cargo compartment, indicating that the compartment hatch must remain closed, except when someone is entering or leaving the compartment. The hatches should remain closed except for entering or leaving the compartment so as to not degrade the fire detection and suppression systems, which are tested and certified with the compartment hatches closed. Further, with this limitation there is less chance someone will accidentally step through an open hatch. Special Condition 2c requires a limitation to be placed in the airplane flight manual (AFM) and placards to be posted inside and outside the hatches of the forward lower deck service/cargo compartment, all stating that (1) the compartment may not be occupied during taxi, takeoff, or landing or during a fire and (2) only authorized personnel are permitted access. These placards are being required, because the compartment is not being certified for occupancy during taxi, takeoff, or landing and because the compartment must not be occupied during a fire so that an occupant is not exposed to fire or to fire suppressant. These placards are somewhat redundant, given the warning required under Special Conditions 1b and 1c but would provide information to an occupant, if the flightcrew failed to activate the warnings of Special Conditions 1b and 1c. Special Condition 2d requires in the AFM (or AFM supplement) instructions for the flightcrew to follow regarding— (1) Permissible access and occupancy; (2) The need to exit (or evacuate in the event of an incapacitated person) and discharge (flood) extinguishing agent in the compartment; and (3) The need, after decompression warning, to immediately don the oxygen mask and exit the compartment. These requirements are to ensure that a single member of the crew could access the cargo compartment safely during flight and exit safely during failure conditions. Special Condition 2e. Because access is being provided to the forward lower deck service/cargo compartment, there is concern that during flight, passengers may retrieve hazardous materials or weapons stored in luggage. Access could be prevented by locking the forward lower deck service/cargo compartment, and that is being specified as one solution (in Special Condition 2e(1)). However, this airplane is being designed for use by a head-of- state, it will have limited access, and it will have placards limiting access. VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2328 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations Furthermore, there will be notification to the flightcrew when the forward lower deck service/cargo compartment is occupied (in Special Condition 1a). Special Condition 2e(2), therefore, would prohibit the airplane from being operated for hire or offered for common carriage. Special Condition 3—Equipment In addition to that required by § 25.819, Special Condition 3 requires the following equipment: Special Condition 3a requires that two portable oxygen bottles be readily available at all times and that each be sufficient to supply a member of the crew who is occupying the forward lower deck service/cargo compartment (except during taxi, takeoff, or landing, or during a fire). The supply of oxygen must be compatible with the emergency descent profile following a decompression. Because it would not be advisable to provide drop-down masks in a cargo compartment or to store a portable oxygen bottle in the compartment, the FAA is requiring that a portable oxygen bottles be mounted outside and near the main deck entrance of the forward lower deck service/cargo compartment. A member of the crew must carry the portable oxygen bottle, when he or she enters the compartment. The second bottle is for a second crewmember’s use who must evacuate an incapacitated crewmember. Special Condition 3b requires supplemental handheld lighting (with locator light) when an occupant enters the forward lower deck service/cargo compartment and any of the following three conditions exist: (1) Power to the compartment is off, (2) the emergency escape path lighting is off or lost, or (3) visibility is poor. At least two flashlights are required. One flashlight would be located adjacent to each emergency exit in the forward lower deck service/cargo compartment at the foot of the stairs in the compartment. Note that this requirement is in addition to the automatic emergency lighting system required by § 25.819(a). Special Condition 4—Evacuation Routes To allow the forward lower deck service/cargo compartment to be utilized as a service compartment, Special Condition 4 requires a limitation to keep the two evacuation routes required under § 25.819(a) clear for evacuation. The cargo in the compartment must be restrained to ensure that the crewmember’s paths to the exits are clear. Further, all entrances and exits (hatches) from the forward lower deck service/cargo compartment must be capable of being opened and closed, without obstruction. This allows exiting under emergency conditions. Further, the hatches must be able to be closed to maintain the integrity of the compartment with respect to fire detection and with respect to smoke, fire and extinguishing agent containment requirements applicable to the Class C cargo compartment, including §§ 25.855, 25.857, and 25.858. Also see Special Condition 2b. Special Condition 5—Training Because the design features required by these special conditions can fulfill their safety objectives only if crewmembers are properly trained in their use, these special conditions require the applicant to develop the following training materials: Special Condition 5a requires training materials about use of the forward lower deck service/cargo compartment and actions associated with the warnings and placards required by these special conditions. Special Condition 5b requires training materials about entering and exiting the forward lower deck service/cargo compartment, including emergency exiting, (associated with Special Conditions 1b, 1c, 1d, 1e, 2a, 2b, 2c, 2d, and 3a). Special Condition 5c requires training materials about checking the pressure of the portable oxygen bottle prior to entering the forward lower deck service/ cargo compartment (associated with Special Condition 3a). Special Condition 5d requires training materials about carrying a portable oxygen bottle when entering the forward lower deck service/cargo compartment (associated with Special Condition 3a). Special Condition 5e requires training materials about maintaining an exit aisle and access to the evacuation routes from the lower lobe service/cargo compartment (associated with Special Condition 2f and 4). Special Condition 5f requires a limitation in the AFM (or AFM supplement) stating all personnel accessing the forward lower deck service/cargo compartment must be trained in the procedures specified above. Special Condition 5f also states there should be at least two crewmembers (not the pilot or co-pilot) trained in emergency evacuation procedures. The second person is to aid the evacuation of an incapacitated crewmember should that occur. Special Condition 6—Ladders The ladders between the forward lower deck service/cargo compartment and the main deck must meet the following requirements: Special Condition 6a requires that each ladder consist of a single segment (to minimize potential errors of use). Special Condition 6b requires that the ladders have essentially rectangular treads (to reduce the potential to slip). Special Condition 6c requires that general illumination of at least 0.05 foot- candle, when measured along the centerlines of each tread, be provided, when the ladders are to be used (to facilitate evacuation and reduce miss- steps). Applicability As discussed above, these special conditions are applicable to the Boeing Model 767–300 airplane. Should JAES apply at a later date for a supplemental type certificate to modify any other model included on Type Certificate A1NM to incorporate the same novel or unusual design feature, the special conditions would apply to that model as well under the provisions of § 21.101. Conclusion This action affects only certain novel or unusual design features on one model of airplane. It is not a rule of general applicability, and it affects only the applicant which applied to the FAA for approval of these features on the airplane. Under standard practice, the effective date of final special conditions would be 30 days after the date of publication in the Federal Register. However, as the certification date for the Boeing Model 767–300, as modified by JAES, is imminent, the FAA finds, that good cause exists to make these special conditions effective upon issuance. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements.
The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. The Special Conditions
Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for the Boeing Model 767–300 airplane, modified by Jet Aviation Engineering Services, to include a forward lower deck compartment configured for use as both a service compartment and a Class C cargo compartment. 1. Visible and Audible Warnings In addition to the audible warnings (fire/smoke detection and VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2329 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations decompression) required by § 25.819(c), the following warnings are required: a. A visible advisory in the cockpit to notify the flightcrew when the forward lower deck service/cargo compartment is occupied. The advisory light must be accompanied by a placard or message indicating that the compartment is occupied. b. A (on/off) visible warning placard stating ‘‘Do Not Enter’’ (or similar words) to be located on or near each hatch. The location should be on the main deck side of the hatch. The warning is to be controlled from the flightdeck. c. A visible and audible warning in the forward lower deck service/cargo compartment to notify an occupant when he or she must evacuate the compartment. The warning must be one which can be seen and heard from any part of the compartment. The warning is to be controlled from the flightdeck. d. A visible and audible warning in the forward lower deck service/cargo compartment, which in the event of decompression, warns an occupant of the need to use a portable oxygen bottle. This warning must be one which can be seen and heard from any part of the compartment and must be distinct from other warnings in the compartment. The decompression warning must be automatic (i.e., not require separate crew action), to ensure that an occupant of the forward lower deck service/cargo compartment does not delay using a portable oxygen bottle. This section of the special conditions is partially in lieu of the visible effect provided by the automatic presentation feature required by § 25.1447. e. A visible and audible warning in the forward lower deck service/cargo compartment, which in the event of a fire, warns an occupant of the need to evacuate the compartment. This warning must be one which can be seen and heard from any part of the compartment and should be distinct from other warnings in the compartment. The fire or smoke detection warning must be automatic (i.e., not require a separate crew action) to ensure that an occupant of the forward lower deck service/cargo compartment leaves before the flightdeck crew releases fire suppressant. 2. Placards and Limitations In addition to those required in part 25, the following placards and limitations are required: a. A placard located outside each hatch to the forward lower deck service/ cargo compartment, indicating that access to the compartment is limited to one crewmember trained in evacuation procedures. b. A placard located inside and outside each hatch to the forward lower deck service/cargo compartment, indicating that the compartment hatches must remain closed, except when someone is entering or leaving the compartment. c. A limitation in the AFM and a placard located inside and outside each hatch to the forward lower deck service/ cargo compartment, all stating that (1) the forward lower deck service/cargo compartment must not be occupied during taxi, takeoff, or landing or during a fire, and (2) only authorized personnel are permitted access. d. Instructions in the AFM (or AFM supplement) for the flightcrew to follow regarding— (1) Permissible access and occupancy of the forward lower deck service/cargo compartment; (2) The need to exit (or evacuate in the event of an incapacitated person) and discharge (flood) extinguishing agent in the compartment; and (3) The need, after decompression warning, to immediately don the oxygen mask and exit the compartment. e. A Limitation in the AFM supplement stating that: ‘‘Carriage of hazardous material and/ or weapons in the forward lower deck service/cargo compartment is prohibited unless the following conditions are met: (1) The forward lower deck service compartment is locked during flight, and the key remains with the flightcrew, or (2) The airplane is not operated for hire or offered for common carriage. This provision does not preclude the operator from receiving remuneration to the extent consistent with 14 CFR part 125, and 14 CFR part 91, and subpart F, as applicable.’’ 3. Equipment In addition to that required by §§ 25.819, the following equipment is required: a. Two portable oxygen bottles with masks must be readily available outside and near the primary main deck entrance (hatch) of the forward lower deck service/cargo compartment. Either portable oxygen bottle must be sufficient to supply a member of the crew who is occupying the forward lower deck service/cargo compartment and a bottle with mask attached must be carried by the crewmember when in the compartment. The second bottle is for the crewmember’s use who must evacuate an incapacitated crewmember. b. Flashlights or other supplemental handheld lighting, in addition to the emergency illumination required by § 25.819(a). At least two flashlights, each equipped with a locator light, must be provided. A flashlight must be located adjacent to each emergency exit (hatch) at the foot of the ladder in the forward lower deck service/cargo compartment. 4. Evacuation Routes A limitation must be placed in the AFM (or AFM supplement) stating that: When the forward lower deck service/ cargo compartment is operated as a service compartment, the two evacuation routes must be kept clear, the special storage pallets/containers must be installed, no loose storage is permitted, and all items stored in the compartment must be stored in appropriate pallets/containers (or similar words). Similar loading restrictions should be placed in the weight and balance manual. 5. Training Training manuals must be provided for authorized crewmembers that may enter the forward lower deck service/ cargo compartment and the manuals and training shall include: a. Use of the forward lower deck service/service compartment and actions indicated by the warnings and placards specified herein. b. Entering and exiting the forward lower deck service/cargo compartment, including emergency exiting. c. Checking the pressure of the portable oxygen bottle prior to entering the forward lower deck service/cargo compartment. d. Carrying a portable oxygen bottle when entering the forward lower deck service/ cargo compartment. e. Maintaining an exit aisle and access to evacuation routes from the forward lower deck service/cargo compartment. Training must address how to keep the evacuation routes clear, i.e., how to restrain cargo in the compartment to ensure that the paths to the exits (hatches) are clear. f. A limitation in the AFM supplement stating that all personnel accessing the forward lower deck service/cargo compartment must be trained in the procedures listed above. To facilitate the evacuation of an incapacitated person, there should be at least two crewmembers (not the pilot or co-pilot) trained in the emergency procedures for the forward lower deck service/cargo compartment. 6. Ladders The following requirements must be met for ladders installed between the VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2330 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations main deck and the forward lower deck service/cargo compartment: a. Each ladder must consist of a single segment. b. The ladders must have essentially rectangular treads. c. General illumination of at least 0.05 foot-candle, when measured along the centerlines of each ladder tread, must be provided when the ladders are to be used. Issued in Renton, Washington, on January 5, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–660 Filed 1–12–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–20009; Directorate Identifier 2003–NM–220–AD; Amendment 39–13937; AD 94–01–10 R2] RIN 2120–AA64 Airworthiness Directives; Boeing Model 757–200 and –200PF Series Airplanes AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : The FAA is revising an existing airworthiness directive (AD) for certain Boeing Model 757–200 and –200PF series airplanes. That AD currently requires inspections, adjustments, and functional checks of the engine thrust reverser system; and modification of the engine thrust reverser directional control valve. That AD also requires installation of an additional thrust reverser locking feature and periodic functional tests of the locking feature following installation. This new AD retains the requirements of the existing AD, but removes certain tests and inspections for certain airplanes. This AD is prompted by a determination of an error in the existing AD. We are issuing this AD to prevent deployment of a thrust reverser in flight and subsequent reduced controllability of the airplane. DATES : Effective January 28, 2005. The incorporation by reference of certain publications, as listed in the regulations, was approved by the Director of the Federal Register as of March 3, 1994 (59 FR 4558, February 1, 1994). The incorporation by reference of certain other publications, as listed in the regulations, was approved previously by the Director of the Federal Register as of September 16, 1991 (56 FR 46725, September 16, 1991). We must receive comments on this AD by March 14, 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. • 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. For service information identified in this AD, contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124–2207. You can 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. You can examine the contents of this AD docket on the Internet at http:// dms.dot.gov, or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL–401, on the plaza level of the Nassif Building, Washington, DC. This docket number is FAA–2005– 20009; the directorate identifier for this docket is 2003–NM–220–AD. Examining the Docket You can examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647–5227) is located on the plaza level of the Nassif Building at the DOT 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 : Thomas S. Thorson, Aerospace Engineer, Propulsion Branch, ANM– 140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 917–6508; fax (425) 917–6590. SUPPLEMENTARY INFORMATION : On August 7, 2003, we issued AD 94–01–10 R1, amendment 39–13247 (68 FR 48546, August 14, 2003). That AD applies to certain Boeing Model 757–200 and –200PF series airplanes. That AD requires inspections, adjustments, and functional checks of the engine thrust reverser system; and modification of the engine thrust reverser directional control valve. That AD also requires installation of an additional thrust reverser locking feature and periodic functional tests of the locking feature following installation. That AD was prompted by a determination that the applicability of AD 94–01–10, amendment 39–8792 (59 FR 4558, February 1, 1994), should be limited to Boeing Model 757–200 and –200PF series airplanes equipped with Pratt and Whitney PW2000 series engines. The actions specified in the AD are intended to prevent deployment of a thrust reverser in flight and subsequent reduced controllability of the airplane. Actions Since AD Was Issued We have since determined that paragraph (c) of AD 94–01–10 R1 should be revised to apply only to airplanes with line numbers 441 and lower. That AD applies to Boeing Model 757 series airplanes with Pratt & Whitney PW2000 series engines. The airplanes in that AD are divided into two groups: • Airplanes without a thrust reverser sync lock (airplane line numbers 1 through 441 inclusive); and • Airplanes with changes to the sync lock installation done in production (airplane line numbers 442 and subsequent). When we issued that AD, we made changes as a result of comments we received. One of the changes was to change paragraph (d) to apply only to airplanes without a thrust reverser sync lock installed in production. The action in paragraph (d) (installing the thrust reverser sync lock) is terminating action for paragraphs (a) through (c). We intended for the repetitive tests and inspections in paragraph (c) to apply only to airplanes without a thrust reverser sync lock installed during production. Unlike paragraph (d), however, paragraph (c) of that AD incorrectly applies to all line numbers of airplanes, including those with changes to the sync lock installation done in production. Therefore, we have changed paragraph (c) of this final rule to clarify VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2331 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations that the paragraph applies to all airplanes affected by paragraph (d). For the same reasons, we have changed paragraph (e) to clarify that its requirements apply to all airplanes. We have also changed the paragraph identifiers in this final rule to the new identifiers that are discussed under ‘‘Changes to the Existing AD.’’ FAA’s Determination and Requirements of This AD The unsafe condition described previously is likely to exist or develop on other airplanes of the same type design that may be registered in the U.S. at some time in the future. For this reason, we are issuing this AD to revise AD 94–01–10 R1. This new AD retains the requirements of AD 94–01–10 R1 but removes certain test and inspection requirements for certain airplanes. Changes to the Existing AD This AD retains certain requirements of AD 94–01–10 R1. Since that AD was issued, the AD format has been revised, and certain paragraphs have been rearranged. As a result, the corresponding paragraph identifiers have changed in this AD, as listed in the following table: REVISED PARAGRAPH IDENTIFIERS Requirement in AD 94–01–10 R1 Corresponding requirement in this new AD Paragraph (a) .................... Paragraph (f). Paragraph (b) .................... Paragraph (g). Paragraph (c) ..................... Paragraph (h). Paragraph (d) .................... Paragraph (i). Paragraph (e) .................... Paragraph (j). Paragraph (f) ..................... Paragraph (k). Paragraph (g) .................... Paragraph (l). After AD 94–01–10 R1 was issued, we reviewed the figures we have used over the past several years to calculate AD costs to operators. To account for various inflationary costs in the airline industry, we find it necessary to increase the labor rate used in these calculations from $60 per work hour to $65 per work hour. The cost impact information, below, reflects this increase in the specified hourly labor rate. Costs of Compliance The following table provides the estimated costs for U.S. operators to comply with this AD for any affected airplane that might be imported and placed on the U.S. Register in the future. ESTIMATED COSTS Action Work hours Average hourly labor rate Parts cost Cost per airplane Number of U.S.- registered airplanes Fleet cost Modification ........................ 624 $65 Provided at no cost to op- erators. $40,560 ............................. 270 $10,951,200. Functional test .................... 1 65 None required ................... $65, per test ...................... 270 $17,550, per test. The airplanes that are added to the applicability of this new AD are not on the U.S. Register and are currently operated by non-U.S. operators under foreign registry; therefore, they are not directly affected by this AD. However, we consider this AD necessary to ensure that the unsafe condition is addressed if a newly affected airplane is imported and placed on the U.S. Register in the future; in that case, the costs identified in the Estimated Costs table above would apply. FAA’s Determination of the Effective Date The newly added airplanes affected by this AD are currently not on the U.S. Register. Therefore, providing notice and opportunity for public comment is unnecessary before this AD is issued, and this AD may be made effective in less than 30 days after it is published in the Federal Register. Comments Invited Although this is a final rule that was not preceded by notice and an opportunity for public comment, we invite you to submit any relevant written data, views, or arguments regarding this AD. Send your comments to an address listed under ADDRESSES . Include ‘‘Docket No. FAA–2005–20009; Directorate Identifier 2003–NM–220– 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, anyone can find and read the comments in any of our dockets, including the name of the individual who sent the comment (or signed the comment on behalf of an association, business, labor union, etc.). You can review the DOT’s complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477–78), or you can visit http://dms.dot.gov. 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. 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; VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2332 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations 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 a regulatory evaluation of the estimated costs to comply with this AD. See the ADDRESSES section for a location to examine the regulatory evaluation. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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. The FAA amends § 39.13 by removing amendment 39–13247 (68 FR 48546, August 14, 2003) and adding the following new AD: 94–01–10 R2 Boeing: Amendment 39– 13937. Docket No. FAA–2005–20009; Directorate Identifier 2003–NM–220–AD. Effective Date (a) This airworthiness directive (AD) becomes effective January 28, 2005. Affected ADs (b) This AD revises AD 94–01–10 R1, amendment 39–13247 (68 FR 48546, August 14, 2003). Applicability (c) This AD applies to Boeing Model 757– 200 and –200PF series airplanes, certificated in any category, equipped with Pratt and Whitney PW2000 series engines. Unsafe Condition (d) This AD was prompted by a determination of an error in the existing AD. The Federal Aviation Administration is issuing this AD to prevent deployment of a thrust reverser in flight and subsequent reduced controllability of the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Inspections/Adjustments/Functional Checks/ Modification (f) For airplanes having line numbers prior to 442: Within 14 days after September 16, 1991 (the effective date of AD 91–20–09, amendment 39–8043), accomplish either paragraph (f)(1) or (f)(2) of this AD. (1) Accomplish both paragraphs (f)(1)(i) and (f)(1)(ii) of this AD: (i) Inspect the thrust reverser directional control valve (DCV) assemblies of both engines to determine the solenoid-driven pilot valve’s part number, in accordance with Boeing Alert Service Bulletin 757–78A0027, dated September 9, 1991. (A) If any DCV has a suspect pilot valve as specified in the service bulletin, prior to further flight, replace the DCV with a DCV that has a part number of a non-suspect solenoid-driven pilot valve, in accordance with the service bulletin. (B) If a DCV has a non-suspect solenoid- driven pilot valve as specified in the service bulletin, that pilot valve does not need to be replaced. (ii) Perform all tests and inspections of the engine thrust reverser control and indication system on both engines in accordance with Boeing Service Bulletin 757–78–0025, dated September 9, 1991. Prior to further flight, correct any discrepancy found in accordance with the service bulletin. (2) Accomplish paragraph (f)(1) of this AD on one engine’s thrust reverser and deactivate the other engine’s thrust reverser, in accordance with section 78–31–1 of Boeing Document D630N002, ‘‘Boeing 757 Dispatch Deviation Guide,’’ Revision 8, dated January 15, 1991. (g) For airplanes having line numbers prior to 442: Within 24 days after September 16, 1991, the requirements of paragraph (f)(1) of this AD must be accomplished on both engines’ thrust reverser systems. (h) For airplanes having line numbers prior to 442: Repeat the tests and inspections specified in paragraph (f)(1)(ii) of this AD at intervals not to exceed 3,000 flight hours, and before further flight following any maintenance that disturbs the thrust reverser control system. Correct any discrepancy before further flight in accordance with Boeing Service Bulletin 757–78–0025, dated September 9, 1991. Installation/Functional Test (i) For airplanes having line numbers prior to 442: Within 5 years after March 3, 1994 (the effective date of AD 94–01–10, amendment 39–8792), install an additional thrust reverser system locking feature (sync lock installation), in accordance with Boeing Service Bulletin 757–78–0028, Revision 1, dated October 29, 1992; or Revision 2, dated January 14, 1993. (j) For all airplanes: Within 1,000 hours’ time-in-service after installing the sync lock required by paragraph (i) of this AD (either in production or by retrofit), or within 1,000 hours’ time-in-service after March 3, 1994, whichever occurs later; and thereafter at intervals not to exceed 1,000 hours’ time-in- service: Perform functional tests of the sync lock in accordance with the ‘‘Thrust Reverser Sync Lock Integrity Test’’ procedures specified below. If any discrepancy is found during any test, correct it before further flight in accordance with a method approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA; the corrective action in the Boeing 757 Maintenance Manual is one approved method. Thrust Reverser Sync Lock Integrity Test 1. General A. Use this procedure to test the integrity of the thrust reverser sync locks. 2. Thrust Reverser Sync Lock Test A. Prepare for the Thrust Reverser Sync Lock Test. (1) Open the auto speedbrake circuit breaker on the overhead circuit breaker panel, P11. (2) Do the steps that follow to supply power to the thrust reverser system: (a) Make sure the thrust levers are in the idle position. Caution: Do not extend the thrust reverser while the core cowl panels are open. Damage to the thrust reverser and core cowl panels can occur. (b) Make sure the thrust reverser halves are closed. (c) Make sure the core cowl panels are closed. (d) Put the EEC Maint Power switch or the EEC Power L and EEC Power R switches to the Altn position. (e) For the left engine: (1) Put the EEC Maint Channel Sel L switch to the Auto position. (2) Put the L Eng fire switch to the Norm position. (f) For the right engine: (1) Put the EEC Maint Channel Sel R switch to the Auto position. (2) Put the R Eng fire switch to the Norm position. (g) Make sure the EICAS circuit breakers (6 locations) are closed. Warning: The Thrust Reverser will automatically retract if the electrical power to the EEC/Thrust Reverser Control System is turned off or if the EEC Maint Power switch is moved to the Norm position. The accidental operation of the Thrust Reverser can cause injury to persons or damage to equipment can occur. (h) Make sure these circuit breakers on the main power distribution panel, P6, are closed: (1) Fuel Cond Cont L (2) Fuel Cond Cont R (3) T/L Interlock L (4) T/L Interlock R (5) Left T/R Sync Lock (6) Right T/R Sync Lock (7) L Eng Electronic Engine Control Altn Pwr (if installed) (8) R Eng Electronic Engine Control Altn Pwr (if installed) (i) Make sure these circuit breakers on the overhead circuit breaker panel, P11, are closed: (1) Air/Gnd Sys 1 (2) Air/Gnd Sys 2 (3) Landing Gear Pos Sys 1 (4) Landing Gear Pos Sys 2 (j) For the left engine, make sure these circuit breakers on the P11 panel are closed: VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2333 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations (1) Left Engine PDIU (2) Left Engine Thrust Reverser Cont/Scav Press (3) Left Engine Electronic Engine Control Altn Pwr (if installed) (4) Left Engine Thrust Reverser PRI Cont (5) Left Engine Thrust Reverser Sec Cont (k) For the right engine, make sure these circuit breakers on the P11 panel are closed: (1) Right Engine PDIU (2) Right Engine Thrust Reverser Cont/Scav Press (3) Right Engine Electronic Engine Control Altn Pwr (if installed) (4) Right Engine Thrust Reverser PRI Cont (5) Right Engine Thrust Reverser Sec Cont (l) Supply electrical power. (m) Remove the pressure from the left (right) hydraulic system. B. Do the Thrust Reverser Sync Lock Test. (1) Move and hold the manual unlock lever on the center actuator on both thrust reverser sleeves to the unlock position. (2) Make sure the thrust reverser sleeves did not move. (3) Move the left (right) reverser thrust lever up and rearward to the idle detent position. (4) Make sure both thrust reverser sleeves move aft (approximately 0.15 to 0.25 inch). (5) Release the manual unlock lever on the center actuators. Warning: Make sure all persons and equipment are clear of the area around the Thrust Reverser. When you apply hydraulic pressure the Thrust Reverser will extend and can cause injuries to persons or damage to equipment. (6) Pressurize the left (right) hydraulic system. (7) Make sure the thrust reverser extends. (8) Move the left (right) reverser thrust lever to the fully forward and down position to retract the thrust reverser. C. Put the Airplane Back to its Usual Condition. (1) Remove hydraulic pressure. (2) Close the left and right fan cowls. (3) Close the Auto Speedbrake circuit breaker on the P11 panel. (4) Remove electrical power if it is not necessary. (5) Return the EEC Maint Power switch or the EEC Power L and EEC Power R switches to the Normal position. D. Repeat the Thrust Reverser Sync Lock Test on the other engine.’’ (k) Installation of the sync lock, as required by paragraph (i) of this AD, constitutes terminating action for the requirements of paragraphs (f) through (h) of this AD. Alternative Methods of Compliance (AMOCs) (l)(1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) We approve the following for the corresponding requirements of this AD: AMOCs approved previously in accordance with AD 91–20–09, amendment 39–8043; AD 94–01–10, amendment 39–8792; and AD 94– 01–10 R1, amendment 39–13247. Material Incorporated by Reference (m) Except as otherwise specified in this AD, the actions must be done in accordance with Boeing Alert Service Bulletin 757– 78A0027, dated September 9, 1991; Boeing Service Bulletin 757–78–0025, dated September 9, 1991; Boeing Document D630N002, ‘‘Boeing 757 Dispatch Deviation Guide,’’ Revision 8, dated January 15, 1991; and Boeing Service Bulletin 757–78–0028, Revision 1, dated October 29, 1992, or Boeing Service Bulletin 757–78–0028, Revision 2, dated January 14, 1993; as applicable. (1) The incorporation by reference of Boeing Service Bulletin 757–78–0028, Revision 1, dated October 29, 1992; and Boeing Service Bulletin 757–78–0028, Revision 2, dated January 14, 1993; was approved previously by the Director of the Federal Register as of March 3, 1994 (59 FR 4558, February 1, 1994). (2) The incorporation by reference of Boeing Alert Service Bulletin 757–78A0027, dated September 9, 1991; Boeing Service Bulletin 757–78–0025, dated September 9, 1991; and Boeing Document D630N002, ‘‘Boeing 757 Dispatch Deviation Guide,’’ Revision 8, dated January 15, 1991; was approved previously by the Director of the Federal Register as of September 16, 1991 (56 FR 46725, September 16, 1991). (The document number of Boeing Alert Service Bulletin 757–78A0027, dated September 9, 1991, was cited erroneously in the September 16, 1991, issue of the Federal Register as ‘‘757–78H0027.’’ The document number of Boeing Service Bulletin 757–78–0025, dated September 9, 1991, was also cited erroneously in the September 16, 1991, issue of the Federal Register as ‘‘757–0025.’’) (3) Contact Boeing Commercial Airplanes, PO Box 3707, Seattle, Washington 98124– 2207, for copies of the service documents. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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. Issued in Renton, Washington, on December 29, 2004. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05–536 Filed 1–12–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2000–NE–05–AD; Amendment 39–13941; AD 2005–01–16] RIN 2120–AA64 Airworthiness Directives; Rolls-Royce plc RB211 Trent 700 Series Turbofan Engines AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 768– 60, Trent 772–60, and Trent 772B–60 turbofan engines with low pressure compressor (LPC) fan blade part numbers FK22580, FK23411, FK25441, and FK25968 installed. That AD currently requires initial ultrasonic inspections of the fan blade root with blades removed, repetitive ultrasonic inspections of the fan blade root with blades removed or installed, and ultrasonic inspection of the fan blade root to be done with the fan blades removed at least every third inspection. This AD requires the same inspections but at lower thresholds and intervals, and eliminates the requirement for ultrasonic inspection with the fan blades removed at least every third inspection. This AD results from analysis of flight data returned to RR, that shows a need for consistent inspection thresholds for all engine models. We are issuing this AD to prevent possible multiple LPC fan blade failures, which could result in an uncontained engine failure and damage to the airplane. DATES : Effective January 28, 2005. The Director of the Federal Register approved the incorporation by reference of certain publications listed in the regulations as of January 28, 2005. We must receive any comments on this AD by March 14, 2005. ADDRESSES : Use one of the following addresses to submit comments on this AD: • By mail: Federal Aviation Administration (FAA), New England Region, Office of the Regional Counsel, Attention: Rules Docket No. 2000–NE– 05–AD, 12 New England Executive Park, Burlington, MA 01803–5299. • By fax: (781) 238–7055. • By e-mail: 9-ane- adcomment@faa.gov. You can get the service information referenced in this AD from Rolls-Royce VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2334 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations plc, PO Box 31, Derby, England; telephone: 011–44–1332–249428; fax: 011–44–1332–249223. You may review copies at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA; or 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. You may examine the AD docket at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA. FOR FURTHER INFORMATION CONTACT : Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803–5299; telephone (781) 238–7175; fax (781) 238–7199. SUPPLEMENTARY INFORMATION : On August 1, 2001, we issued AD 2001–16–05, Amendment 39–12373 (66 FR 42105, August 10, 2001). That AD requires initial ultrasonic inspections of the fan blade root with blades removed, repetitive ultrasonic inspections of the fan blade root with blades removed or installed, and ultrasonic inspections to be done with the fan blades removed at least every third inspection. That AD resulted from reports of fan blade failures due to dovetail root cracks. That condition, if not corrected, could result in possible multiple LPC fan blade failures, uncontained engine failure, and damage to the airplane. Actions Since AD 2001–16–05 Was Issued Since that AD was issued, analysis of flight data returned to RR shows a need for consistent inspection thresholds for all engine models. The actions specified in this AD are intended to prevent possible multiple LPC fan blade failures, which could result in an uncontained engine failure and damage to the airplane. Special Flight Permits Paragraph Removed Paragraph (g) of the current AD, AD 2001–16–05, contains a paragraph pertaining to special flight permits. Even though this final rule does not contain a similar paragraph, we have made no changes with regard to the use of special flight permits to operate the airplane to a repair facility to do the work required by this AD. In July 2002, we published a new Part 39 that contains a general authority regarding special flight permits and airworthiness directives; see Docket No. FAA–2004– 8460, Amendment 39–9474 (69 FR 47998, July 22, 2002). Thus, when we now supersede ADs we will not include a specific paragraph on special flight permits unless we want to limit the use of that general authority granted in section 39.23. Relevant Service Information We have reviewed and approved the technical contents of RR Mandatory Service Bulletin (MSB) No. RB.211–72– C878, Revision 7, dated December 5, 2003, that: • Removes LPC fan blades and performs initial and repetitive ultrasonic inspections for cracks in LPC fan blade dovetail roots, at earlier initial thresholds than the inspections required by the current AD, and, at adjusted repetitive inspection intervals from the current AD. • Provides a procedure that does not require blade removal from the engine in order to perform repetitive ultrasonic inspections for cracks in LPC fan blade dovetail roots. Bilateral Airworthiness Agreement This engine model is manufactured in the United Kingdom and is type certificated for operation in the United States under the provisions of section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, the Civil Aviation Authority (CAA) has kept the FAA informed of the situation described above. The FAA has examined the findings of the CAA, 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. FAA’s Determination of an Unsafe Condition and Proposed Actions Although none of these affected engine models are used on any airplanes that are registered in the United States, the possibility exists that the engine models could be used on airplanes that are registered in the United States in the future. Since an unsafe condition has been identified that is likely to exist or develop on other RR RB211 Trent 768– 60, Trent 772–60, and Trent 772B–60 turbofan engine models of the same type design, this AD is being issued to prevent possible multiple LPC fan blade failures, which could result in an uncontained engine failure and damage to the airplane. This AD requires: • Initial ultrasonic inspections of the fan blade root with blades removed; at or before accumulating 1,100 cycles- since-new (CSN) on the fan blades after the effective date of the AD; and • For blades with more than 1,100 CSN that have not been previously inspected, initial ultrasonic inspections of the fan blade root with blades removed; within 300 cycles-in-service (CIS) from the effective date of the AD or within 2,000 CSN, whichever occurs first; and • Repetitive ultrasonic inspections of the fan blade root, with blades removed within 300 CIS intervals, or with blades not removed within 250 CIS intervals. The actions are required to be done using the service bulletin described previously. Immediate Adoption of This AD Since there are currently no domestic operators of these engine models, notice and opportunity for prior public comment are unnecessary. Therefore, a situation exists that allows the immediate adoption of this regulation. Comments Invited This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment; however, we invite you to submit any written relevant data, views, or arguments regarding this AD. Send your comments to an address listed under ADDRESSES . Include ‘‘AD Docket No. 2000–NE–05–AD’’ in the subject line of your comments. If you want us to acknowledge receipt of your mailed comments, send us a self-addressed, stamped postcard with the docket number written on it; we will date- stamp your postcard and mail it back to you. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify it. If a person contacts us verbally, and that contact relates to a substantive part of this AD, we will summarize the contact and place the summary in the docket. We will consider all comments received by the closing date and may amend the AD in light of those comments. Examining the AD Docket You may examine the AD Docket (including any comments and service information), by appointment, between 8 a.m. and 4:30 p.m., Monday through Friday, except Federal holidays. See ADDRESSES for the location. VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2335 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations 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. 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 a summary of the costs to satisfy the initial requirements of this AD and placed it in the AD Docket. You may get a copy of this summary by sending a request to us at the address listed under ADDRESSES . Include ‘‘AD Docket No. 2000–NE–05–AD’’ in your request. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA 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. The Federal Aviation Administration (FAA) amends § 39.13 by removing Amendment 39–12373 (66 FR 42105, August 10, 2001), and by adding a new airworthiness directive (AD), Amendment 39–13941, to read as follows: 2005–01–16 Rolls-Royce plc: Amendment 39–13941. Docket No. 2000–NE–05–AD. Supersedes AD 2001–16–05, Amendment 39–12373. Effective Date (a) This AD becomes effective January 28, 2005. Affected ADs (b) This AD supersedes AD 2001–16–05, Amendment 39–12373. Applicability (c) This AD applies to Rolls-Royce plc (RR) RB211 Trent 768–60, Trent 772–60, and Trent 772B–60 turbofan engines with low pressure compressor (LPC) fan blade part numbers FK22580, FK23411, FK25441, and FK25968 installed. These engines are installed on, but not limited to, Airbus A330 series airplanes. Unsafe Condition (d) This AD supersedure results from analysis of flight data returned to RR, that shows a need for consistent inspection thresholds for all engine models. We are issuing this AD to prevent possible multiple LPC fan blade failures, which could result in an uncontained engine failure and damage to the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Initial Ultrasonic Inspection (f) Perform an initial ultrasonic inspection of the LPC fan blade dovetail roots using Method A (paragraphs 3.A.(1) through 3.A.(8); blades removed from engine) of Accomplishment Instructions of RR Mandatory Service Bulletin (MSB) No. RB.211–72–C878, Revision 7, dated December 5, 2003, as follows: (1) Inspect before accumulating 1,100 cycles-since-new (CSN) on the fan blades; or (2) For fan blades that have accumulated more than 800 CSN on the effective date of this AD that have not been previously inspected, inspect within 300 cycles-in- service (CIS) from the effective date of this AD or within 2,000 CSN, whichever occurs first. Repetitive Ultrasonic Inspections (g) Perform repetitive inspections of the LPC fan blades using Method A, or Method B (paragraphs 3.B.(1) through 3.B.(5); blades not removed from the engine) of the Accomplishment Instructions of RR MSB No. RB.211–72–C878, Revision 7, dated December 5, 2003, as follows: (1) Inspect within 300 CIS since-last- inspected with Method A of the SB; or (2) Inspect within 250 CIS since-last- inspected with Method B of the SB. Alternative Methods of Compliance (h) The Manager, Engine Certification Office, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Material Incorporated by Reference (i) You must use the Rolls-Royce plc service information specified in Table 1 of this AD to perform the blade inspections and replacements required by this AD. The Director of the Federal Register approved the incorporation by reference of the documents listed in Table 1 of this AD in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You can get a copy from Rolls-Royce plc, PO Box 31, Derby DE24 6BJ, UK; telephone 44 (0) 1332 242424; fax 44 (0) 1332 249936. You may review copies at the FAA, New England Region, Office of the Regional Counsel, Attention: Rules Docket No. 2000–NE–05– AD, 12 New England Executive Park, Burlington, MA; or 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. Table 1 follows: TABLE 1.—INCORPORATION BY REFERENCE Mandatory service bulletin No. Page Revision Date RB.211–72–C878 ................................................................................... All ................................................... 7 December 5, 2003. Total Pages: 9 RB.211–72–C878, Appendix 1 ............................................................... All ................................................... 7 December 5, 2003. Total Pages: 4 RB.211–72–C878, Appendix 2 ............................................................... All ................................................... 7 December 5, 2003. VerDate jul<14>2003 14:42 Jan 12, 2005 Jkt 205001 PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 E:\FR\FM\13JAR1.SGM 13JAR1 2336 Federal Register / Vol. 70, No. 9 / Thursday, January 13, 2005 / Rules and Regulations TABLE 1.—INCORPORATION BY REFERENCE—Continued Mandatory service bulletin No. Page Revision Date Total Pages: 5 Related Information (j) United Kingdom Civil Aviation Authority airworthiness directive 003–11–99 also addresses the subject of this AD. Issued in Burlington, Massachusetts, on January 4, 2005. Francis A. Favara, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 05–484 Filed 1–12–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001–NE–17–AD; Amendment 39–13940; AD 2005–01–15] RIN 2120–AA64 Airworthiness Directives; Rolls-Royce plc RB211 Trent 875, 877, 884, 884B, 892, 892B, and 895 Series Turbofan Engines AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : The FAA is superseding an existing airworthiness directive (AD) for Rolls-Royce plc (RR) RB211 Trent 875, 877, 884, 892, 892B, and 895 series turbofan engines with certain part number (P/N) low pressure compressor (LPC) fan blades installed. That AD currently requires initial and repetitive ultrasonic inspections of the fan blade dovetail roots. This AD requires the same actions except at reduced compliance times for certain blades, defines a specific terminating action to the repetitive blade inspection requirements, and adds the 884B series to the applicability. This AD results from a report of a cracked fan blade found before the blade reached the initial inspection threshold of AD 2002– 11–08. This AD also results from the need to reduce a repetitive inspection compliance time due to potential breakdown of blade coating and lubrication on certain blades. We are issuing this AD to prevent multiple LPC fan blade failures due to cracks, which could result in uncontained engine failure and possible damage to the airplane. DATES : Effective January 28, 2005. The Director of the Federal Register approved the incorporation by reference of certain publications listed in the regulations as of January 28, 2005. We must receive any comments on this AD by March 14, 2005. ADDRESSES : Use one of the following addresses to submit comments on this AD: • By mail: Federal Aviation Administration (FAA), New England Region, Office of the Regional Counsel, Attention: Rules Docket No. 2001–NE– 17–AD, 12 New England Executive Park, Burlington, MA 01803–5299. • By fax: (781) 238–7055. • By e-mail: 9-ane- adcomment@faa.gov. You can get the service information referenced in this AD from Rolls-Royce plc, P.O. Box 31, Derby DE24 6BJ, UK; telephone 44 (0) 1332 242424; fax 44 (0) 1332 249936. You may examine the AD docket, by appointment, at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA. FOR FURTHER INFORMATION CONTACT : Christopher Spinney, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803–5299; telephone (781) 238–7175; fax (781) 238–7199. SUPPLEMENTARY INFORMATION : On May 27, 2002, the FAA issued AD 2002–11– 08, Amendment