AD 2009-03-01

7554 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations 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 adding the following new airworthiness directive (AD): 2009–04–04 Cessna Aircraft Company: Amendment 39–15810; Docket No. FAA–2009–0118; Directorate Identifier 2008–CE–073–AD. Effective Date (a) This AD becomes effective on March 2, 2009. Affected ADs (b) None. Applicability (c) This AD applies to the following airplane models and serial numbers that are certificated in any category: Models Serial Nos. 401 ........................................................ 655 and 401–0001 through 401–0322. 401A ..................................................... 655 and 401A0001 through 401A0132. 401B ..................................................... 401B0001 through 401B0221. 402 ........................................................ 402–0001 through 402–0322. 402A ..................................................... 402A0001 through 402A0129. 402B ..................................................... 402B0001 through 402B0122, 402B0201 through 402B0249, 402B0301 through 402B0455, 402B0501 through 402B0640, 402B0801 through 402B0935, 402B1001 through 402B1100, 402B1201 through 402B1250, and 402B1301 through 402B1384. Unsafe Condition (d) This AD is the result of several reports of fatigue cracking on the affected airplanes in the auxiliary wing spar. We are issuing this AD to detect and correct such cracks, which, if not corrected, could result in failure of the wing auxiliary spar web and cause landing gear collapse during normal landing. This could lead to loss of control and passenger injury. Compliance (e) To address this problem, you must do the actions below using Cessna Service Bulletin MEB08–8, dated December 23, 2008, at the following compliance time, unless already done: Note 1: Cessna Service Bulletin MEB08–8, dated December 23, 2008, provides detailed instructions on measuring, inspecting, and replacing cracked parts, including how to handle two or more cracks in the same hole. (1) Within the next 10 hours time-in- service (TIS) after March 2, 2009 (the effective date of this AD) and, in addition, before further flight anytime the airplane experiences a ‘‘hard landing,’’ visually inspect the auxiliary wing spar near the location where the main landing gear trunnion is mounted for cracks. (2) If any crack is found during any inspection required by this AD that is 0.5 inch or more, before further flight after any such crack is found, replace the cracked parts. (3) If cracks are found during any inspection required by this AD that are less than 0.5 inch, do the following: (i) Repetitively thereafter inspect the cracks for length at intervals not to exceed 50 hours TIS and, before further flight, replace any part that has a crack length of 0.5 inch or more; and (ii) Replace the cracked part within 200 hours TIS after the original crack was found or within 12 months after the original crack was found, whichever occurs first. (4) If you find any cracks as a result of any inspection required by this AD, report the results to Cessna using the form in the service bulletin. Send a copy of this report to the FAA at the address specified in paragraph (f) of this AD. For the reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120–0056. Do the reporting requirement at whichever of the following that occurs later: (i) Within 10 days after the inspection; or (ii) Within the next 10 days after March 2, 2009 (the effective date of this AD). Note 2: The FAA considers this interim action. We will work with Cessna and evaluate the crack reports and all other information. Based on this information, we may initiate additional rulemaking action. Alternative Methods of Compliance (AMOCs) (f) The Manager, Wichita Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Adam Neubauer, Wichita ACO, Aerospace Engineer, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946– 4156; fax: (316) 946–4107. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. Material Incorporated by Reference (g) You must use Cessna Service Bulletin MEB08–8, dated December 23, 2008, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Cessna Aircraft Company, P.O. Box 7704, Wichita, Kansas 67277; telephone: (800) 423–7762 or (316) 517–6056; Internet: http://www.cessna.com . (3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329–3768. (4) You may also review copies of the service information incorporated by reference for this AD at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741–6030, or go to: http://www.archives.gov/federal _ register/ code _ of _ federal _ regulations/ibr _ locations.html . Issued in Kansas City, Missouri, on February 6, 2009. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E9–3016 Filed 2–17–09; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2009–0054; Directorate Identifier 2008–NM–222–AD; Amendment 39–15802; AD 2009–03–01] RIN 2120–AA64 Airworthiness Directives; Learjet Model 55, 55B, and 55C Airplanes AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : We are adopting a new airworthiness directive (AD) for certain Learjet Model 55, 55B, and 55C airplanes. This AD requires inspecting the installation of the forward light VerDate Nov<24>2008 11:38 Feb 17, 2009 Jkt 217001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 cprice-sewell on PRODPC61 with RULES

7555 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations assembly in the aft lavatory to determine the location of the terminal connector; inspecting for damage of the light assembly terminals, wires, and oxygen lines; inspecting to determine if the cable nipple is installed over the light assembly terminal; and doing corrective actions if necessary. This AD also requires installing a clamp to the forward side of the frame to maintain a positive distance between the light assembly and oxygen line. This AD results from a report of a cabin fire in the left-hand upper cabin fuselage above the aft cabin window at frame 23. We are issuing this AD to detect and correct improper installation of the lavatory light assembly, which could result in contact between the electrical terminals of the light assembly and an adjacent oxygen supply line, and consequent short circuit or fire hazard. DATES : This AD is effective March 5, 2009. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 5, 2009. We must receive comments on this AD by April 20, 2009. ADDRESSES : You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to http://www.regulations.gov . Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. • Hand Delivery: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this AD, contact Learjet, Inc., One Learjet Way, Wichita, Kansas 67209– 2942; telephone 316–946–2000; fax 316–946–2220; e-mail ac.ict@aero.bombardier.com ; Internet http://www.bombardier.com . Examining the AD Docket You may examine the AD docket on the Internet at http:// www.regulations.gov ; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone 800–647– 5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT : Daniel Hilton, Aerospace Engineer, Electrical Systems and Avionics Branch, ACE–119W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946–4173; fax (316) 946–4107. SUPPLEMENTARY INFORMATION : Discussion We received a report of a cabin fire in the left-hand upper cabin fuselage above the aft cabin window at frame 23 on a Learjet Model 55 airplane. If installed incorrectly, the power lead terminals of the lavatory light assembly have the potential to chafe against the oxygen line, causing deterioration of the insulation on the light assembly wiring. This condition, if not corrected, could result in contact between the electrical terminals of the light assembly and an adjacent oxygen supply line, and consequent short circuit or fire hazard. Relevant Service Information We reviewed Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008. The alert service bulletin describes procedures for an inspection of the installation of the forward light assembly in the aft lavatory to determine the location of the terminal connector (as shown in Figure 1, detail A of the alert service bulletin); an inspection for damage of the light assembly terminals, wires, and oxygen line; an inspection to determine if the cable nipple is installed over the light assembly terminal; and corrective actions if necessary. The corrective actions include turning the light assembly to locate the terminal connector in the forward position; replacing damaged light assembly terminals, wires, and oxygen line; and installing a new cable nipple. The alert service bulletin also describes procedures for installing a clamp to the forward side of the frame to maintain a positive distance between the light assembly and oxygen line. FAA’s Determination and Requirements of This AD We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the(se) same type design(s). This AD requires accomplishing the actions specified in the service information described previously, except as discussed under ‘‘Differences Between the AD and the Service Information.’’ Differences Between the AD and the Service Information Operators should note that, although the Accomplishment Instructions of the Bombardier Alert Service Bulletin A55– 25–7, dated December 17, 2008, describes procedures for submitting information to the manufacturer, this AD does not require that action. Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008, refers only to doing ‘‘inspections.’’ We have determined that the procedures in the alert service bulletin should be described as ‘‘general visual inspections.’’ Note 1 has been included in this AD to define this type of inspection. FAA’s Justification and Determination of the Effective Date This condition has the potential to compromise the integrity of the oxygen line due to the chafing between the light assembly terminals and oxygen line and has the potential to become an oxygen- fueled ignition source. Because of our requirement to promote safe flight of civil aircraft and thus the critical need to ensure the risk of fire is mitigated by proper installation of the forward light assembly in the aft lavatory and proper positive distance maintained between the oxygen line and light assembly, and the short compliance time involved with this action, this AD must be issued immediately. Because an unsafe condition exists that requires the immediate adoption of this AD, we find that notice and opportunity for prior public comment hereon are impracticable and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA– 2009–0054; Directorate Identifier 2008– NM–222–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. We will post all comments we receive, without change, to http:// www.regulations.gov , including any VerDate Nov<24>2008 11:38 Feb 17, 2009 Jkt 217001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 cprice-sewell on PRODPC61 with RULES

7556 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. 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 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 this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Is not a ‘‘significant rule’’ under 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. You can find our regulatory evaluation and the estimated costs of compliance in the AD Docket. 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 adding the following new AD: 2009–03–01 Learjet: Amendment 39–15802. Docket No. FAA–2009–0054; Directorate Identifier 2008–NM–222–AD. Effective Date (a) This airworthiness directive (AD) is effective March 5, 2009. Affected ADs (b) None. Applicability (c) This AD applies to Learjet Model 55, 55B, and 55C airplanes, certificated in any category; serial numbers 002 through 147 inclusive. Subject (d) Air Transport Association (ATA) of America Code 25: Equipment/Furnishings. Unsafe Condition (e) This AD results from a report of a cabin fire in the left-hand upper cabin fuselage above the aft cabin window at frame 23. We are issuing this AD to detect and correct improper installation of the lavatory light assembly, which could result in contact between the electrical terminals of the light assembly and an adjacent oxygen supply line, and consequent short circuit or fire hazard. Compliance (f) Comply with this AD within the compliance times specified, unless already done. Inspections, Corrective Actions, and Installation (g) Within 30 days or 25 flight hours after the effective date of this AD, whichever occurs first, do the actions specified in paragraphs (g)(1) and (g)(2) of this AD. Do the actions in accordance with the Accomplishment Instructions of Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008. (1) Do a general visual inspection of the installation of the forward light assembly in the aft lavatory to determine the location of the terminal connector; do a general visual inspection for damage of the light assembly terminals, wires, and oxygen lines; do a general visual inspection to determine if the cable nipple is installed over the light assembly terminal; and do all applicable corrective actions. Do all applicable corrective actions before further flight. Note 1: For the purposes of this AD, a general visual inspection is: ‘‘A visual examination of an interior or exterior area, installation, or assembly to detect obvious damage, failure, or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to ensure visual access to all surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked.’’ (2) Install a clamp and hardware to the forward side of the frame to maintain the distance specified in Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008, between the light assembly and oxygen line. No Reporting (h) Although Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008, specifies to submit certain information to the manufacturer, this AD does not include that requirement. Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, Wichita Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Daniel Hilton, Aerospace Engineer, Electrical Systems and Avionics Branch, ACE–119W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946– 4173; fax (316) 946–4107. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office (FSDO). The AMOC approval letter must specifically reference this AD. Material Incorporated by Reference (j) You must use Bombardier Alert Service Bulletin A55–25–7, dated December 17, 2008, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Learjet, Inc., One Learjet Way, Wichita, Kansas 67209–2942; telephone 316–946–2000; fax 316–946–2220; e-mail ac.ict@aero.bombardier.com ; Internet http:// www.bombardier.com . (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425–227–1221 or 425–227–1152. (4) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go VerDate Nov<24>2008 11:38 Feb 17, 2009 Jkt 217001 PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 cprice-sewell on PRODPC61 with RULES

7557 Federal Register / Vol. 74, No. 31 / Wednesday, February 18, 2009 / Rules and Regulations to: http://www.archives.gov/federal _ register/ code _ of _ federal _ regulations/ ibr _ locations.html . Issued in Renton, Washington, on January 21, 2009. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E9–3023 Filed 2–17–09; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2008–1105; Airspace Docket No. 08–AGL–10] Amendment of Class E Airspace; Atlantic, IA AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : This action amends Class E airspace at Atlantic, IA. Additional controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Atlantic Municipal Airport, Atlantic, IA. The FAA is taking this action to enhance the safety and management of Instrument Flight Rule (IFR) operations at Atlantic Municipal Airport. DATES : Effective Date: 0901 UTC, May 7, 2009. The Director of the Federal Register approves this incorporation by reference action under 1 CFR Part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. FOR FURTHER INFORMATION CONTACT : Scott Enander, Central Service Center, Operations Support Group, Federal Aviation Administration, Southwest Region, 2601 Meacham Blvd., Ft. Worth, TX 76193–0530; telephone (817) 321– 7716. SUPPLEMENTARY INFORMATION : History On December 8, 2008, the FAA published in the Federal Register a notice of proposed rulemaking to amend Class E airspace at Atlantic, IA, adding additional controlled airspace at Atlantic Municipal Airport, Atlantic, IA. (73 FR 74376, Docket No. FAA–2008– 1105). Interested parties were invited to participate in this rulemaking effort by submitting written comments on the proposal to the FAA. No comments were received. Class E airspace designations are published in paragraph 6005 of FAA Order 7400.9S signed October 3, 2008, and effective October 31, 2008, which is incorporated by reference in 14 CFR Part 71.1. The Class E airspace designations listed in this document will be published subsequently in that Order. The Rule This action amends Title 14 Code of Federal Regulations (14 CFR) Part 71 by amending Class E airspace at Atlantic, IA, adding additional controlled airspace at Atlantic Municipal Airport, Atlantic, IA. The FAA has determined that this regulation only involves an established body of technical regulations for which frequent and routine amendments are necessary to keep them operationally current. Therefore, this regulation: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866; (2) is not a ‘‘significant rule’’ under DOT Regulatory Policies and Procedures (44 FR 11034; February 26, 1979); and (3) does not warrant preparation of a regulatory evaluation as the anticipated impact is so minimal. Since this is a routine matter that will only affect air traffic procedures and air navigation, it is certified that this rule, when promulgated, will not have a significant economic impact on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. The FAA’s authority to issue rules regarding aviation safety is found in Title 49 of the U.S. Code. Subtitle 1, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the agency’s authority. This rulemaking is promulgated under the authority described in Subtitle VII, Part A, Subpart I, Section 40103. Under that section, the FAA is charged with prescribing regulations to assign the use of airspace necessary to ensure the safety of aircraft and the efficient use of airspace. This regulation is within the scope of that authority as it adds additional controlled airspace at Atlantic Municipal Airport, Atlantic, IA. List of Subjects in 14 CFR Part 71 Airspace, Incorporation by reference, Navigation (air). Adoption of the Amendment ■ In consideration of the foregoing, the Federal Aviation Administration amends 14 CFR Part 71 as follows: PART 71—DESIGNATION OF CLASS A, B, C, D, AND E AIRSPACE AREAS; AIR TRAFFIC SERVICE ROUTES; AND REPORTING POINTS ■ 1. The authority citation for 14 CFR Part 71 continues to read as follows: Authority: 49 U.S.C. 106(g), 40103, 40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR, 1959– 1963 Comp., p. 389. § 71.1 [Amended] ■ 2. The incorporation by reference in 14 CFR Part 71.1 of the Federal Aviation Administration Order 7400.9S, Airspace Designations and Reporting Points, signed October 3, 2008, and effective October 31, 2008, is amended as follows: Paragraph 6005 Class E airspace areas extending upward from 700 feet or more above the surface. * * * * * ACE IA E5 Atlantic, IA [Amended] Atlantic Municipal Airport, IA (Lat. 41 ° 24 ′ 26 ″ N., long. 95 ° 02 ′ 49 ″ W.) That airspace extending upward from 700 feet above the surface within a 6.8-mile radius of Atlantic Municipal Airport and within 3.4 miles each side of the 022 ° bearing from the airport extending from the 6.8-mile radius to 9.9 miles northeast of the airport. * * * * * Issued in Fort Worth, TX, on February 5, 2009. Anthony D. Roetzel, Manager, Operations Support Group, ATO Central Service Center. [FR Doc. E9–3007 Filed 2–17–09; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2008–0987; Airspace Docket No. 08–ASW–19] Amendment of Class E Airspace; Corpus Christi, TX AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : This action amends Class E airspace at Corpus Christi, TX. Controlled airspace is necessary to accommodate Area Navigation (RNAV) Standard Instrument Approach Procedures (SIAP) at Mustang Beach Airport, Port Aransas, TX; and T.P. McCampbell Airport, Ingleside, TX. Also, Class E airspace around Aransas County Airport, Rockport, TX, and San Jose Island Airport, Rockport, TX, will VerDate Nov<24>2008 11:38 Feb 17, 2009 Jkt 217001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\18FER1.SGM 18FER1 cprice-sewell on PRODPC61 with RULES