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applicable Gulfstream alert customer bulletin Supplement CE51 628M001, Revision A, (4) Gulfstream V Alert Customer Bulletin identified in table 1 of this AD: Do the dated December 20, 2010, (for Model GV–SP 30A, dated December 20, 2010, including actions required by paragraph (g)(3)(i) or (G500) airplanes). Gulfstream GV/GV–SP AFM Supplement (g)(3)(ii) of this AD. (3) Alert Customer CE51 628M001, Revision A, dated December (i) Before further flight, remove the bottle, Bulletin 10A, dated December 20, 2010, 20, 2010, approved for IBR January 3, 2012. in accordance with the Accomplishment including Gulfstream GV/GV–SP AFM (5) For service information identified in Instructions of the applicable Gulfstream Supplement CE51 628M001, Revision A, this AD, contact alert customer bulletin identified in table 1 dated December 20, 2010, (for Model GV–SP Corporation, Technical Publications Dept., of this AD. (G550) airplanes). P.O. Box 2206, Savannah, Georgia 31402– (ii) Before further flight, revise the 2206; telephone (800) 810–4853; fax (912) limitations section of the applicable (k) Special Flight Permit 965–3520; e-mail [email protected]; Gulfstream AFM specified in table 1 of this Special flight permits, as described in Internet http://www.gulfstream.com/ AD to include the information in Gulfstream Section 21.197 and Section 21.199 of the product_support/technical_pubs/pubs/ GV/GV–SP AFM Supplement CE51 Federal Aviation Regulations (14 CFR 21.197 index.htm. You may review copies of the 628M001, Revision A, dated December 20, and 21.199), may be issued to operate the referenced service information at the FAA. 2010. This AFM supplement adds airplane to a location where the requirements (6) You may review copies of the service restrictions for APU usage. Operate the of this AD can be accomplished, provided the information at the FAA, Transport Airplane airplane thereafter according to the following conditions are met: Directorate, 1601 Lind Avenue SW., Renton, limitations in that AFM supplement. (1) If an airplane is grounded due to a Washington. For information on the Note 2: This may be done by inserting a single generator failure, the APU may be availability of this material at the FAA, call copy of Gulfstream GV/GV–SP AFM operated during a ferry flight, provided no (425) 227–1221. Supplement CE51 628M001, Revision A, passengers are carried. (7) You may also review copies of the dated December 20, 2010, in the applicable (2) Only the minimum required flight-crew service information that is incorporated by AFM. When information in this AFM is allowed on any ferry flight. reference at the National Archives and supplement has been included in general Records Administration (NARA). For revisions of the applicable AFM, the general (l) Alternative Methods of Compliance information on the availability of this revisions may be inserted in the applicable (AMOCs) material at an NARA facility, call (202) 741– AFM, provided the relevant information in (1) The Manager, Atlanta Aircraft 6030, or go to http://www.archives.gov/ the general revision is identical to that in Certification Office (ACO), FAA, has the federal_register/code_of_federal_regulations/ Gulfstream GV/GV–SP AFM Supplement authority to approve AMOCs for this AD, if ibr_locations.html. CE51 628M001, Revision A, dated December requested using the procedures found in 14 Issued in Renton, Washington, on 20, 2010, and that AFM supplement may be CFR 39.19. In accordance with 14 CFR 39.19, November 8, 2011. removed. send your request to your principal inspector or local Flight Standards District Office, as Kalene C. Yanamura, (h) Credit for Actions Accomplished in appropriate. If sending information directly Acting Manager, Transport Airplane Accordance With Previous Service to the manager of the ACO, send it to the Directorate, Aircraft Certification Service. Information attention of the person identified in the [FR Doc. 2011–29806 Filed 11–28–11; 8:45 am] Actions accomplished before the effective Related Information section of this AD. BILLING CODE 4910–13–P date of this AD in accordance with (2) Before using any approved AMOC, Gulfstream V Alert Customer Bulletin 30, notify your appropriate principal inspector, dated December 6, 2010, including or lacking a principal inspector, the manager DEPARTMENT OF TRANSPORTATION Gulfstream GV/GV–SP AFM Supplement of the local flight standards district office/ CE51 628M001, dated November 18, 2010 certificate holding district office. Federal Aviation Administration (for Model GV airplanes); Gulfstream G550 (m) Related Information Alert Customer Bulletin 10, dated December 6, 2010, including Gulfstream GV/GV–SP For more information about this AD, 14 CFR Part 39 AFM Supplement CE51 628M001, dated contact Sanford Proveaux, Aerospace [Docket No. FAA–2011–1232; Directorate November 18, 2010 (for Model GV airplanes); Engineer, Continued Operational Safety and Identifier 2011–NM–039–AD; Amendment or G500 Alert Customer Bulletin 10, dated Certificate Management Branch, ACE–102A, 39–16873; AD 2011–24–09] December 6, 2010, including Gulfstream GV/ FAA, Atlanta Aircraft Certification Office GV–SP AFM Supplement CE51 628M001, (ACO), 1701 Columbia Avenue, College Park, RIN 2120–AA64 dated November 18, 2010 (for Model GV Georgia 30337; telephone (404) 474–5566; fax airplanes), are acceptable for compliance (404) 474–5606; email: Airworthiness Directives; Airbus with the corresponding actions required by [email protected]. Airplanes paragraph (g) of this AD. (n) Material Incorporated by Reference AGENCY: Federal Aviation (i) Parts Installation (1) You must use the following service Administration (FAA), Department of As of the effective date of this AD, no information to do the actions required by this Transportation (DOT). person may install a third fire extinguisher AD, unless the AD specifies otherwise. The ACTION: Final rule; request for bottle in the APU fragment impact zone Director of the Federal Register approved the (rotor fragment impact zone) of any airplane. incorporation by reference (IBR) under comments. 5 U.S.C. 552(a) and 1 CFR part 51 of the (j) No Reporting following service information on the date SUMMARY: We are adopting a new Although the service information specified specified: airworthiness directive (AD) for certain in paragraphs (j)(1), (j)(2), and (j)(3) of this (2) Gulfstream G500 Alert Customer Airbus Model A340–200 and -300 series AD specify to submit certain information to Bulletin 10A, dated December 20, 2010, airplanes. This AD results from the manufacturer, this AD does not include including Gulfstream GV/GV–SP airplane mandatory continuing airworthiness that requirement. flight manual (AFM) Supplement CE51 information (MCAI) originated by an (1) Gulfstream V Alert Customer Bulletin 628M001, Revision A, dated December 20, aviation authority of another country to 30A, dated December 20, 2010, including 2010, approved for IBR January 3, 2012. identify and correct an unsafe condition Gulfstream GV/GV–SP AFM Supplement (3) Gulfstream G550 Alert Customer on an aviation product. The MCAI CE51 628M001, Revision A, dated December Bulletin 10A, dated December 20, 2010, 20, 2010, (for Model GV airplanes). including Gulfstream GV/GV–SP AFM describes the unsafe condition as: (2) Gulfstream G500 Alert Customer Supplement CE51 628M001, Revision A, [T]he FAA published SFAR 88 (Special Bulletin 10A, dated December 20, 2010, dated December 20, 2010, approved for IBR Federal Aviation Regulation 88) [(66 FR including Gulfstream GV/GV–SP AFM January 3, 2012. 23086, May 7, 2001)].

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By mail referenced 04/00/02/07/01–L296 Discussion systems. As a result of those findings, of March 4th, 2002 and 04/00/02/07/03–L024 The European Aviation Safety Agency we issued a regulation titled ‘‘Transport of February 3rd, 2003 the JAA [Joint Aviation Airplane Fuel Tank System Design Authorities] recommended to the National (EASA), which is the Technical Agent for the Member States of the European Review, Flammability Reduction and Aviation Authorities (NAA) the application Maintenance and Inspection of a similar regulation. Community, has issued EASA The aim of this [EASA] regulation is to Airworthiness Directive 2010–0232, Requirements’’ (66 FR 23086, May 7, require * * * a definition review against dated November 12, 2010 (referred to 2001). In addition to new airworthiness explosion hazards. after this as ‘‘the MCAI’’), to correct an standards for transport airplanes and * * * * * unsafe condition for the specified new maintenance requirements, this This AD requires inspections to verify products. The MCAI states: rule included Special Federal Aviation electrical bonding to prevent the Regulation No. 88 (‘‘SFAR 88,’’ [T]he FAA published SFAR 88 (Special Amendment 21–78, and subsequent potential of ignition sources inside fuel Federal Aviation Regulation 88) [(66 FR tanks, which, in combination with Amendments 21–82 and 21–83). 23086, May 7, 2001)]. Among other actions, SFAR 88 (66 FR flammable fuel vapors, could result in By mail referenced 04/00/02/07/01–L296 23086, May 7, 2001) requires certain fuel tank explosions and consequent of March 4th, 2002 and 04/00/02/07/03–L024 of February 3rd, 2003 the JAA [Joint Aviation type design (i.e., type certificate (TC) loss of the airplane. This AD requires and supplemental type certificate (STC)) actions that are intended to address the Authorities] recommended to the National Aviation Authorities (NAA) the application holders to substantiate that their fuel unsafe condition described in the MCAI. of a similar regulation. tank systems can prevent ignition DATES: This AD becomes effective The aim of this regulation is to require all sources in the fuel tanks. This December 14, 2011. holders of type certificates for transport requirement applies to type design The Director of the Federal Register aircraft certified after 01 January 1958 with holders for large turbine-powered approved the incorporation by reference a capacity of 30 passengers or more, or a payload of 3,402 kg or more, to carry out a transport airplanes and for subsequent of a certain publication listed in the AD definition review against explosion hazards. modifications to those airplanes. It as of December 14, 2011. To be compliant with SFAR88/JAA INT/ requires them to perform design reviews We must receive comments on this POL 25/12 requirements, this [EASA] AD and to develop design changes and AD by January 13, 2012. requires, for operators who have already maintenance procedures if their designs ADDRESSES: You may send comments by embodied the Revision 03 or any previous do not meet the new fuel tank safety revision of Airbus SB A340–28–4097 on any of the following methods: standards. As explained in the preamble • aeroplanes which were previously in SB to the rule, we intended to adopt Federal eRulemaking Portal: Go to Configurations 02 or 03 [required by FAA AD http://www.regulations.gov. Follow the 2008–25–02, Amendment 39–15760 (73 FR airworthiness directives to mandate any instructions for submitting comments. 75307, December 11, 2008)], an inspection to changes found necessary to address • Fax: (202) 493–2251. verify if the electrical bonding of the water unsafe conditions identified as a result • Mail: U.S. Department of drain system (Trim Tank) and the electrical of these reviews. Transportation, Docket Operations, bonding of the ventilation intake system were In evaluating these design reviews, we M–30, West Building Ground Floor, correctly accomplished or need additional have established four criteria intended work associated to the aeroplane to define the unsafe conditions Room W12–140, 1200 New Jersey configuration. Avenue SE., Washington, DC 20590. associated with fuel tank systems that • * * * * * require corrective actions. The Hand Delivery: U.S. Department of Additional work could involve Transportation, Docket Operations, percentage of operating time during modifying or installing certain bonding which fuel tanks are exposed to M–30, West Building Ground Floor, points (such as pipe clamps, screws, Room W12–140, 1200 New Jersey flammable conditions is one of these attachment fittings, restrictor valves, criteria. The other three criteria address Avenue SE., Washington, DC, between 9 flame arrestors, and pipes); doing a.m. and 5 p.m., Monday through the failure types under evaluation: electrical bonding of the wing fuel Single failures, single failures in Friday, except Federal holidays. pumps, the water drain system between combination with a latent condition(s), Examining the AD Docket certain ribs, a water drain system and and in-service failure experience. For all the ventilation intake system; You may examine the AD docket on four criteria, the evaluations included depending on configuration. The the Internet at http:// consideration of previous actions taken additional work required by this AD is www.regulations.gov; or in person at the that may mitigate the need for further in addition to the requirements of AD Docket Operations office between 9 a.m. action. 2008–25–02, Amendment 39–15760 (73 The Joint Aviation Authorities (JAA) and 5 p.m., Monday through Friday, FR 75307, December 11, 2008). The has issued a regulation that is similar to except Federal holidays. The AD docket unsafe condition is the potential of SFAR 88 (66 FR 23086, May 7, 2001). contains this AD, the regulatory ignition sources inside fuel tanks, (The JAA is an associated body of the evaluation, any comments received, and which, in combination with flammable European Civil Aviation Conference other information. The street address for fuel vapors, could result in fuel tank (ECAC) representing the civil aviation the Docket Operations office (telephone explosions and consequent loss of the regulatory authorities of a number of (800) 647–5527) is in the ADDRESSES airplane. You may obtain further European States who have agreed to co- section. Comments will be available in information by examining the MCAI in operate in developing and the AD docket shortly after receipt. the AD docket. implementing common safety regulatory FOR FURTHER INFORMATION CONTACT: The FAA has examined the standards and procedures.) Under this Vladimir Ulyanov, Aerospace Engineer, underlying safety issues involved in fuel regulation, the JAA stated that all International Branch, ANM–116, tank explosions on several large members of the ECAC that hold type Transport Airplane Directorate, FAA, transport airplanes, including the certificates for transport category 1601 Lind Avenue SW., Renton, adequacy of existing regulations, the airplanes are required to conduct a Washington 98057–3356; telephone service history of airplanes subject to design review against explosion risks. (425) 227–1138; fax (425) 227–1149. those regulations, and existing We have determined that the actions SUPPLEMENTARY INFORMATION: maintenance practices for fuel tank identified in this AD are necessary to

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reduce the potential of ignition sources opportunity for public comment. We on a substantial number of small entities inside fuel tanks, which, in combination invite you to send any written relevant under the criteria of the Regulatory with flammable fuel vapors, could result data, views, or arguments about this AD. Flexibility Act. in fuel tank explosions and consequent Send your comments to an address List of Subjects in 14 CFR Part 39 loss of the airplane. listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2011–1232; Air transportation, Aircraft, Aviation Relevant Service Information Directorate Identifier 2011–NM–039– safety, Incorporation by reference, Airbus has issued Mandatory Service AD’’ at the beginning of your comments. Safety. Bulletin A340–28–4097, Revision 05, We specifically invite comments on the Adoption of the Amendment including Appendix 1, dated June 3, overall regulatory, economic, 2010. The actions described in this environmental, and energy aspects of Accordingly, under the authority service information are intended to this AD. We will consider all comments delegated to me by the Administrator, correct the unsafe condition identified received by the closing date and may the FAA amends 14 CFR part 39 as in the MCAI. amend this AD because of those follows: FAA’s Determination and Requirements comments. PART 39—AIRWORTHINESS of This AD We will post all comments we DIRECTIVES receive, without change, to http:// This product has been approved by www.regulations.gov, including any ■ 1. The authority citation for part 39 the aviation authority of another personal information you provide. We continues to read as follows: country, and is approved for operation will also post a report summarizing each Authority: 49 U.S.C. 106(g), 40113, 44701. in the . Pursuant to our substantive verbal contact we receive bilateral agreement with the State of about this AD. § 39.13 [Amended] Design Authority, we have been notified Authority for This Rulemaking ■ 2. The FAA amends § 39.13 by adding of the unsafe condition described in the the following new AD: MCAI and service information Title 49 of the United States Code referenced above. We are issuing this specifies the FAA’s authority to issue 2011–24–09 Airbus: Amendment 39–16873. AD because we evaluated all pertinent rules on aviation safety. Subtitle I, Docket No. FAA–2011–1232; Directorate Identifier 2011–NM–039–AD. information and determined the unsafe section 106, describes the authority of condition exists and is likely to exist or the FAA Administrator. ‘‘Subtitle VII: Effective Date develop on other products of the same Aviation Programs,’’ describes in more (a) This airworthiness directive (AD) type design. detail the scope of the Agency’s becomes effective December 14, 2011. There are no products of this type authority. Affected ADs currently registered in the United States. We are issuing this rulemaking under However, this rule is necessary to the authority described in ‘‘Subtitle VII, (b) None. ensure that the described unsafe Part A, Subpart III, Section 44701: Applicability condition is addressed if any of these General requirements.’’ Under that (c) This AD applies to Airbus Model A340– products are placed on the U.S. Register section, Congress charges the FAA with 211, –212, –213, –311, –312 and –313 in the future. promoting safe flight of civil aircraft in airplanes, certificated in any category, all air commerce by prescribing regulations manufacturer serial numbers, on which Differences Between the AD and the for practices, methods, and procedures Airbus modification 41600 has been MCAI or Service Information the Administrator finds necessary for embodied in production and Airbus Service Bulletin A340–28–4097, dated June 14, 2004; We have reviewed the MCAI and safety in air commerce. This regulation related service information and, in Revision 01, dated March 3, 2005; Revision is within the scope of that authority 02, dated August 16, 2006; or Revision 03, general, agree with their substance. But because it addresses an unsafe condition dated July 3, 2007; has been embodied in we might have found it necessary to use that is likely to exist or develop on service, except airplanes on which Airbus different words from those in the MCAI products identified in this rulemaking modification 49135 has been embodied in to ensure the AD is clear for U.S. action. production. operators and is enforceable. In making Subject these changes, we do not intend to differ Regulatory Findings substantively from the information This AD will not have federalism (d) Air Transport Association (ATA) of America Code 28: Fuel. provided in the MCAI and related implications under Executive Order service information. 13132. This AD will not have a Reason We might also have required different substantial direct effect on the States, on (e) The mandatory continued airworthiness actions in this AD from those in the the relationship between the national information (MCAI) states: MCAI in order to follow FAA policies. government and the States, or on the [T]he FAA published SFAR 88 (Special Any such differences are highlighted in distribution of power and Federal Aviation Regulation 88) [(66 FR a NOTE within the AD. responsibilities among the various 23086, May 7, 2001)]. levels of government. By mail referenced 04/00/02/07/01–L296 FAA’s Determination of the Effective of March 4th, 2002 and 04/00/02/07/03–L024 For the reasons discussed above, I Date of February 3rd, 2003 the JAA [Joint Aviation certify that this AD: Authorities] recommended to the National Since there are currently no domestic (1) Is not a ‘‘significant regulatory Aviation Authorities (NAA) the application operators of this product, notice and action’’ under Executive Order 12866, of a similar regulation. opportunity for public comment before (2) Is not a ‘‘significant rule’’ under The aim of this [EASA] regulation is to issuing this AD are unnecessary. DOT Regulatory Policies and Procedures require * * * a definition review against (44 FR 11034, February 26, 1979), explosion hazards. Comments Invited (3) Will not affect intrastate aviation * * * * * This AD is a final rule that involves in Alaska, and This AD requires inspections to verify requirements affecting flight safety, and (4) Will not have a significant electrical bonding to prevent the potential of we did not precede it by notice and economic impact, positive or negative, ignition sources inside fuel tanks, which, in

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combination with flammable fuel vapors, Before using any approved AMOC, notify DEPARTMENT OF TRANSPORTATION could result in fuel tank explosions and your appropriate principal inspector, or consequent loss of the airplane. lacking a principal inspector, the manager of Federal Aviation Administration Compliance the local flight standards district office/ certificate holding district office. The AMOC (f) You are responsible for having the 14 CFR Part 39 approval letter must specifically reference actions required by this AD performed within [Docket No. FAA–2011–1261; Directorate this AD. the compliance times specified, unless the Identifier 2011–NE–38–AD; Amendment 39– actions have already been done. (2) Airworthy Product: For any requirement 16875; AD 2011–24–11] in this AD to obtain corrective actions from Actions a manufacturer or other source, use these RIN 2120–AA64 (g) Within 24 months after the effective actions if they are FAA-approved. Corrective date of this AD, do a detailed inspection of actions are considered FAA-approved if they Airworthiness Directives; Honeywell the electrical bonding for the water drain are approved by the State of Design Authority International Inc. Engines system (trim tank) and the ventilation intake (or their delegated agent). You are required system to verify whether it is equivalent to AGENCY: Federal Aviation the electrical bonding done in accordance to assure the product is airworthy before it Administration (FAA), DOT. is returned to service. with the Accomplishment Instructions of ACTION: Final rule; request for Airbus Mandatory Service Bulletin A340–28– Related Information comments. 4097, Revision 05, including Appendix 1, (k) Refer to Mandatory Continuing dated June 3, 2010. SUMMARY: We are adopting a new Airworthiness Information (MCAI) European (h) If, during the inspection required by airworthiness directive (AD) for certain paragraph (g) of this AD, the electrical Aviation Safety Agency (EASA) Honeywell International Inc. ALF502L– bonding of the water drain system and the Airworthiness Directive 2010–0232, dated 2C, ALF502R–3, ALF502R–3A, ventilation intake system is found to be not November 12, 2010; and Airbus Mandatory ALF502R–5, LF507–1F, and LF507–IH equivalent to the electrical bonding done in Service Bulletin A340–28–4097, Revision 05, accordance with the Accomplishment including Appendix 1, dated June 3, 2010; turbofan engines. This AD requires Instructions of Airbus Mandatory Service for related information. removing from service certain second Bulletin A340–28–4097, Revision 05, stage high pressure compressor (HPC2) including Appendix 1, dated June 3, 2010: Material Incorporated by Reference discs. This AD was prompted by a Within 24 months after the effective date of (l) You must use Airbus Mandatory Service report of cracks found in an HPC2 disc this AD, modify the electrical bonding during routine inspection. We are associated with the airplane configuration in Bulletin A340–28–4097, Revision 05, accordance with paragraph 3.B.(11) or including Appendix 1, dated June 3, 2010, to issuing this AD to prevent the affected 3.B.(12), as applicable, of the do the actions required by this AD, unless the discs from fracturing before reaching the Accomplishment Instructions of Airbus AD specifies otherwise. currently published life limit. A disc Mandatory Service Bulletin A340–28–4097, (1) The Director of the Federal Register fracture could result in an uncontained Revision 05, including Appendix 1, dated approved the incorporation by reference of failure of the disc and damage to the June 3, 2010. this service information under 5 U.S.C. airplane. (i) A review of the airplane maintenance 552(a) and 1 CFR part 51. records is acceptable in lieu of the inspection DATES: This AD is effective December (2) For service information identified in 14, 2011. required by paragraph (g) of this AD provided this AD, contact Airbus SAS—Airworthiness that the accomplishment of the electrical The Director of the Federal Register Office—EAL, 1 Rond Point Maurice Bellonte, bonding for the water drain system (trim approved the incorporation by reference tank) and the ventilation intake system can 31707 Blagnac Cedex, France; telephone +33 of a certain publication listed in the AD be conclusively identified as performed in 5 61 93 36 96; fax +33 5 61 93 45 80; email as of December 14, 2011. accordance with Airbus Mandatory Service [email protected]; We must receive comments on this Bulletin A340–28–4097, Revision 05, Internet http://www.airbus.com. AD by January 13, 2012. including Appendix 1, dated June 3, 2010. (3) You may review copies of the service information at the FAA, Transport Airplane ADDRESSES: You may send comments, FAA AD Differences Directorate, 1601 Lind Avenue SW., Renton, using the procedures found in 14 CFR Note 1: This AD differs from the MCAI Washington. For information on the 11.43 and 11.45, by any of the following and/or service information as follows: No availability of this material at the FAA, call methods: • differences. (425) 227–1221. Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the Other FAA AD Provisions (4) You may also review copies of the service information that is incorporated by instructions for submitting comments. (j) The following provisions also apply to • reference at the National Archives and Fax: (202) 493–2251. this AD: • Records Administration (NARA). For Mail: U.S. Department of (1) Alternative Methods of Compliance information on the availability of this Transportation, Docket Operations, (AMOCs): The Manager, International M–30, West Building Ground Floor, Branch, ANM–116, Transport Airplane material at NARA, call (202) 741–6030, or go Directorate, FAA, has the authority to to: http://www.archives.gov/federal_register/ Room W12–140, 1200 New Jersey approve AMOCs for this AD, if requested code_of_federal_regulations/ Avenue SE., Washington, DC 20590. using the procedures found in 14 CFR 39.19. ibr_locations.html. • Hand Delivery: U.S. Department of In accordance with 14 CFR 39.19, send your Transportation, Docket Operations, Issued in Renton, Washington, on request to your principal inspector or local M–30, West Building Ground Floor, November 14, 2011. Flight Standards District Office, as Room W12–140, 1200 New Jersey appropriate. If sending information directly Ali Bahrami, Avenue SE., Washington, DC 20590, to the International Branch, send it to ATTN: Manager, Transport Airplane Directorate, between 9 a.m. and 5 p.m., Monday Vladimir Ulyanov, Aerospace Engineer, Aircraft Certification Service. through Friday, except Federal holidays. International Branch, ANM–116, Transport [FR Doc. 2011–30229 Filed 11–28–11; 8:45 am] Airplane Directorate, FAA, 1601 Lind For service information identified in Avenue SW., Renton, Washington 98057– BILLING CODE 4910–13–P this AD, contact Honeywell 3356; telephone (425) 227–1138; fax (425) International Inc., P.O. Box 52181, 227–1149. Information may be emailed to: 9- Phoenix, AZ 85072–2181, phone: (800) [email protected]. 601–3099; Web site: http://

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