80 FR 22635 - Airworthiness Directives; Dassault Aviation Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 78 (April 23, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 78 (April 23, 2015)
| Page Range | 22635-22638 | |
| FR Document | 2015-09290 |
[Federal Register Volume 80, Number 78 (Thursday, April 23, 2015)] [Rules and Regulations] [Pages 22635-22638] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-09290] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0830; Directorate Identifier 2015-NM-024-AD; Amendment 39-18141; AD 2015-08-05] RIN 2120-AA64 Airworthiness Directives; Dassault Aviation Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are superseding Airworthiness Directive (AD) 2013-26-05 for all Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. AD 2013-26-05 required repetitive weighing of fire extinguisher bottles having a certain part number, and eventual replacement of those bottles to terminate the repetitive weighing. This new AD continues to require repetitive weighing of fire extinguisher bottles having a certain part number, and eventual replacement of those bottles to terminate the repetitive weighing. This AD was prompted by our determination that certain text in the method of compliance language specified in AD 2013- 26-05 incorrectly refers to Airbus, instead of ``Dassault Aviation.'' We are issuing this AD to detect and correct a dormant failure in the fire suppression system, which could result in the inability to put out a fire in an engine, auxiliary power unit (APU), or rear compartment. DATES: This AD becomes effective May 8, 2015. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of October 20, 2014 (79 FR 54897, dated September 15, 2014). We must receive comments on this AD by June 8, 2015. 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, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this AD, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201- 440-6700; Internet http://www.dassaultfalcon.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 0830; or in person at the Docket Operations office 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 Operations 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: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. SUPPLEMENTARY INFORMATION: Discussion On August 29, 2014, we issued AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), which applied to all Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes. AD 2013-26-05 was prompted by reports of a manufacturing defect in the charge indicator on fire extinguisher bottles. AD 2013-26-05 required repetitive weighing of fire extinguisher bottles having a certain part number, and eventual replacement of those bottles to terminate the repetitive weighing. We issued AD 2013-26-05 to detect and correct a dormant failure in the fire suppression system, which could result in the inability to put out a fire in an engine, APU, or rear compartment. AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), corresponds to Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) AD 2012-0189, dated September 24, 2012. You may examine the MCAI on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 0830. Since we issued AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), we have determined that there is an error in the manufacturer's name in the method of compliance language in certain text in the ``Explanation of Change Made to This AD'' section and in certain paragraphs of the regulatory text of AD 2013-26-05. AD 2013-26- 05 refers to Airbus's EASA Design Organization Approval (DOA), instead of Dassault Aviation's EASA DOA. In order to refer to the appropriate EASA DOA, this AD replaces ``Airbus's'' with ``Dassault Aviation's'' in paragraphs (h)(2), (h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), (i), (i)(1), (i)(2), (i)(3), (i)(4), (j)(1), (j)(2), (j)(3), (j)(4), and (l)(2) of this AD. The ``Explanation of Change Made to This AD'' section of AD 2013-26-05 is not restated in this AD. [[Page 22636]] FAA's Determination and Requirements of This AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of these same type designs. FAA's Determination of the Effective Date We are superseding AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), to correct certain erroneous manufacturer information in the ``Explanation of Changes to This AD'' section and in certain paragraphs of the regulatory text. No other changes have been made to AD 2013-26-05. Therefore, we determined that notice and opportunity for prior public comment are unnecessary. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2015-0830; Directorate Identifier 2015-NM-024-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 personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance We estimate that this AD affects 185 airplanes of U.S. registry. The actions required by AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), and retained in this AD take about 4 work- hours per product, at an average labor rate of $85 per work-hour. Required parts cost about $6,400 per product. Based on these figures, the estimated cost of the actions that were required by AD 2013-26-05 is $1,246,900, or $6,740 per product. The new requirements of this AD add no additional economic burden. 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 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 this AD: 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); 3. Will not affect intrastate aviation in Alaska; and 4. 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. 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 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by removing airworthiness directive (AD) 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), and adding the following new AD: 2015-08-05 Dassault Aviation: Amendment 39-18141. Docket No. FAA- 2015-0830; Directorate Identifier 2015-NM-024-AD. (a) Effective Date This AD becomes effective May 8, 2015. (b) Affected ADs This AD replaces AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014). (c) Applicability This AD applies to Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; Model MYSTERE-FALCON 200 airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20- F5 airplanes, certificated in any category; all serial numbers. (d) Subject Air Transport Association (ATA) of America Code 26, Fire Protection. (e) Reason This AD was prompted by reports of a manufacturing defect in the charge indicator on fire extinguisher bottles and also our determination that certain text in the method of compliance language specified in AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), incorrectly refers to ``Airbus'' instead of ``Dassault Aviation.'' We are issuing this AD to detect and correct a dormant failure in the fire suppression system, which could result in the inability to put out a fire in an engine, auxiliary power unit (APU), or rear compartment. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Definitions, With No Changes This paragraph restates the requirements of paragraph (g) of AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), with no changes. For the purposes of this AD, the following definitions apply. (1) An affected fire extinguisher bottle is any fire extinguisher bottle having a part number included in table 1 to the introductory text of paragraph (h) of this AD and having a manufacturing batch number 168 through 200 inclusive on the data plate of the charge indicator. [[Page 22637]] (2) A serviceable fire extinguisher bottle is any fire extinguisher bottle having a manufacturing batch number lower than 168 or higher than 200 on the data plate of the charge indicator. (h) Retained Determining Charge Indicator Batch Number, With Revised Method of Compliance Language This paragraph restates the requirements of paragraph (h) of AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), with revised method of compliance language in paragraphs (h)(2), (h)(2)(i), (h)(2)(ii), (h)(2)(iii) and (h)(2)(iv) of this AD. Within 30 days or 100 flight hours after October 20, 2014 (the effective date of AD 2013-26-05), whichever occurs first: Determine the manufacturing batch number for the charge indicator installed on each engine and APU fire extinguisher bottle having a part number included in table 1 to the introductory text of paragraph (h) of this AD, in accordance with the Accomplishment Instructions of Dassault Service Bulletin F20-785, also referred to as 785, dated June 11, 2012 (for Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes); or Dassault Service Bulletin F200-131, also referred to as 131, dated June 11, 2012 (for Model MYSTERE-FALCON 200 airplanes). Table 1 to the Introductory Text of Paragraph (h) of This AD--Part Numbers of Affected Fire Extinguisher Bottles ------------------------------------------------------------------------ Type of bottle-- Part No.-- ------------------------------------------------------------------------ Engine Fire Extinguisher Bottle...... 111-1555-324-12A Engine Fire Extinguisher Bottle...... 811456 Engine Fire Extinguisher Bottle...... 111-355-32142A APU Fire Extinguisher Bottle......... 111-011-324-12A APU Fire Extinguisher Bottle......... 811475 ------------------------------------------------------------------------ (1) For fire extinguisher bottles with part numbers that are not included in table 1 to the introductory text of paragraph (h) of this AD, no further action is required by paragraph (h) of this AD. (2) For any affected charge indicator, as identified in paragraph (g)(1) of this AD: Before further flight, weigh each affected fire extinguisher bottle, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Dassault Aviation's EASA Design Organization Approval (DOA). Weigh the fire extinguishers thereafter at intervals not to exceed 12 months until the replacement specified in paragraph (h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), or (j) of this AD is accomplished. If it is determined that the fire extinguisher weighs less than the lowest weight limit indicated on the fire extinguisher's data plate, before further flight, replace any affected fire extinguisher bottle and charge indicator cartridge with a serviceable part, in accordance with the applicable method specified in paragraph (h)(2)(i), (h)(2)(ii), (h)(2)(iii), or (h)(2)(iv) of this AD. Note 1 to paragraph (h)(2) of this AD: The instructions specified in Dassault Maintenance Procedure, ``Weighing of Engine Freon Fire Extinguishers,'' (page 601, ``Inspection/Check'') of Subject 26-20-2, ``Extinguishing System--Description and Operation, of Chapter 26, ``Fire Protection,'' in Book 2 of the Dassault Falcon 20 Maintenance Manual, Phase 50, dated October 2011 (for Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes); or Procedure 2, ``Engine and Rear Compartment Extinguisher (14W1-14W2): Weighing'' of Falcon 200 Maintenance Requirement Card 171.0, Revised December 2011, of Chapter 26, ``Fire Protection,'' in Book 1, ``Work Cards,'' of the Dassault Falcon 200 Maintenance Manual, Revision 30, dated December 2011 (for Model MYSTERE-FALCON 200 airplanes); provide additional guidance for weighing affected fire extinguisher bottles. This service information is not incorporated by reference in this AD. (i) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or EASA; or Dassault Aviation's EASA DOA. Note 2 to paragraphs (h)(2)(i), (i), (i)(1), and (j)(1) of this AD: The instructions specified in Dassault Maintenance Procedure, ``Removal of Pyrotechnical Cartridge for Check/Replacement'' (pages 401-403, ``Removal/Installation''), of Subject 26-20-2 ``Extinguishing System--Description and Operation,'' of Chapter 26, ``Fire Protection,'' in Book 2 of the Dassault Falcon 20 Maintenance Manual, Phase 50, dated October 2011, are a source of guidance for the actions specified in paragraphs (h)(2)(i), (i), (i)(1), and (j)(1) of this AD. This service information is not incorporated by reference in this AD. (ii) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes: Replace the fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (iii) For Model MYSTERE-FALCON 200 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. Note 3 to paragraphs (h)(2)(iii), (i), (i)(3), and (j)(3) of this AD: Procedure 3, ``Engine and Rear Compartment Extinguisher (14W1-14W2): Check/Replacement of Percussion Cartridge,'' of Falcon 200 Maintenance Requirement Card 171.0, Revised December 2011, of Chapter 26, ``Fire Protection'', in Book 1, ``Work Cards,'' of the Dassault Falcon 200 Maintenance Manual, Revision 30, dated December 2011, is a source of guidance for paragraphs (h)(2)(iii), (i), (i)(3), and (j)(3) of this AD. This service information is not incorporated by reference in this AD. (iv) For Model MYSTERE-FALCON 200 airplanes: Replace the fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. Note 4 to paragraphs (h)(2)(iv), (i)(4), and (j)(4) of this AD: Procedure 1, ``Removal/Installation,'' of Falcon 200 Maintenance Requirement Card 171.0, Revised December 2011, of Chapter 26, ``Fire Protection'', in Book 1, ``Work Cards,'' of the Dassault Falcon 200 Maintenance Manual, Revision 30, dated December 2011, is a source of guidance for replacing the fire extinguisher bottle. This service information is not incorporated by reference in this AD. (i) Retained Repetitive Inspections To Determine if Charge Indicator Cartridge Was Fired, With Revised Method of Compliance Language This paragraph restates the requirements of paragraph (i) of AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), with revised method of compliance language in paragraphs (i), (i)(1), (i)(2), (i)(3) and (i)(4) of this AD. Within 6 months after October 20, 2014 (the effective date of AD 2013-26-05): Do an inspection to determine if the charge indicator cartridge installed on each engine and APU fire extinguisher bottle, as identified in table 1 to the introductory text of paragraph (h) of this AD, was fired, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. Repeat the inspection thereafter at intervals not to exceed 6 months until the replacement specified in paragraph (i)(1), (i)(2), (i)(3), (i)(4), or (j) of this AD is accomplished. If it is determined that any charge indicator cartridge was fired, before further flight, replace the affected fire extinguisher bottle and charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (1) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 2-D5, 20-E5, and 20-F5 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (2) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes: Replace the [[Page 22638]] fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (3) For Model MYSTERE-FALCON 200 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (4) For Model MYSTERE-FALCON 200 airplanes: Replace the fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (j) Retained Replacement of Fire Extinguisher Bottle and Charge Indicator Cartridge, With Revised Method of Compliance Language This paragraph restates the requirements of paragraph (j) of AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), with revised method of compliance language specified in paragraphs (j)(1), (j)(2), (j)(3), and (j)(4) of this AD. Unless previously accomplished as specified in paragraph (h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), (i)(1), (i)(2), (i)(3), or (i)(4) of this AD: Within 60 months after October 20, 2014 (the effective date of AD 2013-26-05), replace any affected fire extinguisher bottle and charge indicator cartridge, as specified in paragraph (g)(1) of this AD, with a serviceable part, in accordance with the method specified in paragraph (j)(1), (j)(2), (j)(3), or (j)(4) of this AD, as applicable. Replacement of any affected fire extinguisher bottle and charge indicator cartridge with a serviceable part terminates the repetitive actions specified in paragraphs (h) and (i) of this AD. (1) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (2) For Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E, F, and G airplanes; and Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 airplanes: Replace the fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (3) For Model MYSTERE-FALCON 200 airplanes: Replace the charge indicator cartridge with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (4) For Model MYSTERE-FALCON 200 airplanes: Replace the fire extinguisher bottle with a serviceable part, in accordance with a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. (k) Retained Parts Installation Prohibition, With No Changes This paragraph restates the requirements of paragraph (k) of AD 2013-26-05, Amendment 39-17714 (79 FR 54897, September 15, 2014), with no changes. As of October 20, 2014 (the effective date of AD 2013-26-05), no person may install, on any airplane, a fire extinguisher bottle having a part number included in table 1 to the introductory text of paragraph (h) of this AD, fitted with a charge indicator having a manufacturing batch number on the data plate of 168 through 200 inclusive. (l) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD. (2) Contacting the Manufacturer: As of the effective date of this AD, for any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA DOA. If approved by the DOA, the approval must include the DOA- authorized signature. (m) Related Information Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2012-0189, dated September 24, 2012, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-0830. (n) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (3) The following service information was approved for IBR on October 20, 2014, (79 FR 54897, September 15, 2014). (i) Dassault Service Bulletin F20-785, also referred to as 785, dated June 11, 2012. (ii) Dassault Service Bulletin F200-131, also referred to as 131, dated June 11, 2012. (4) For service information identified in this AD, contact Dassault Falcon Jet, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. (5) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (6) You may view this 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 to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Renton, Washington, on April 9, 2015. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-09290 Filed 4-22-15; 8:45 am] BILLING CODE 4910-13-P
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(d) Shipping requirements. Sealed require repetitive weighing of fire section. Comments will be available in
containers of apples destined for export extinguisher bottles having a certain the AD docket shortly after receipt.
to the continental United States must be part number, and eventual replacement FOR FURTHER INFORMATION CONTACT: Tom
held in a cold storage facility while of those bottles to terminate the Rodriguez, Aerospace Engineer,
awaiting export. repetitive weighing. This AD was International Branch, ANM–116,
(e) Phytosanitary certificate. Each prompted by our determination that Transport Airplane Directorate, FAA,
consignment of apples imported from certain text in the method of compliance 1601 Lind Avenue SW., Renton, WA
China into the continental United States language specified in AD 2013–26–05 98057–3356; telephone 425–227–1137;
must be accompanied by a incorrectly refers to Airbus, instead of fax 425–227–1149.
phytosanitary certificate issued by the ‘‘Dassault Aviation.’’ We are issuing this SUPPLEMENTARY INFORMATION:
NPPO of China with an additional AD to detect and correct a dormant
declaration stating that the requirements failure in the fire suppression system, Discussion
of this section have been met and the which could result in the inability to On August 29, 2014, we issued AD
consignment has been inspected by the put out a fire in an engine, auxiliary 2013–26–05, Amendment 39–17714 (79
NPPO and found free of quarantine power unit (APU), or rear compartment. FR 54897, September 15, 2014), which
pests. DATES: This AD becomes effective May applied to all Dassault Aviation Model
(f) Additional conditions for apples 8, 2015. FAN JET FALCON, FAN JET FALCON
from areas of China south of the 33rd The Director of the Federal Register SERIES C, D, E, F, and G airplanes;
parallel. In addition to the conditions in approved the incorporation by reference Model MYSTERE–FALCON 200
paragraphs (a) through (e) of this of certain other publications listed in airplanes; and Model MYSTERE–
section, apples from areas of China this AD as of October 20, 2014 (79 FR FALCON 20–C5, 20–D5, 20–E5, and 20–
south of the 33rd parallel apples must 54897, dated September 15, 2014). F5 airplanes. AD 2013–26–05 was
be treated in accordance with 7 CFR We must receive comments on this prompted by reports of a manufacturing
part 305. (Approved by the Office of AD by June 8, 2015. defect in the charge indicator on fire
Management and Budget under control ADDRESSES: You may send comments by extinguisher bottles. AD 2013–26–05
number 0579–0423) any of the following methods: required repetitive weighing of fire
Done in Washington, DC, this 20th day of • Federal eRulemaking Portal: Go to extinguisher bottles having a certain
April 2015. http://www.regulations.gov. Follow the part number, and eventual replacement
Kevin Shea, instructions for submitting comments. of those bottles to terminate the
Administrator, Animal and Plant Health • Fax: 202–493–2251. repetitive weighing. We issued AD
Inspection Service. • Mail: U.S. Department of 2013–26–05 to detect and correct a
[FR Doc. 2015–09508 Filed 4–22–15; 8:45 am] Transportation, Docket Operations, M– dormant failure in the fire suppression
BILLING CODE 3410–34–P 30, West Building Ground Floor, Room system, which could result in the
W12–140, 1200 New Jersey Avenue SE., inability to put out a fire in an engine,
Washington, DC 20590. APU, or rear compartment.
DEPARTMENT OF TRANSPORTATION • Hand Delivery: U.S. Department of AD 2013–26–05, Amendment 39–
Transportation, Docket Operations, M– 17714 (79 FR 54897, September 15,
Federal Aviation Administration 30, West Building Ground Floor, Room 2014), corresponds to Mandatory
W12–140, 1200 New Jersey Avenue SE., Continuing Airworthiness Information
14 CFR Part 39 Washington, DC, between 9 a.m. and 5 (MCAI) European Aviation Safety
p.m., Monday through Friday, except Agency (EASA) AD 2012–0189, dated
[Docket No. FAA–2015–0830; Directorate
Identifier 2015–NM–024–AD; Amendment Federal holidays. September 24, 2012. You may examine
39–18141; AD 2015–08–05] For service information identified in the MCAI on the Internet at http://
this AD, contact Dassault Falcon Jet, www.regulations.gov by searching for
RIN 2120–AA64 P.O. Box 2000, South Hackensack, NJ and locating Docket No. FAA–2015–
07606; telephone 201–440–6700; 0830.
Airworthiness Directives; Dassault Since we issued AD 2013–26–05,
Internet http://www.dassaultfalcon.com.
Aviation Airplanes Amendment 39–17714 (79 FR 54897,
You may view this referenced service
AGENCY: Federal Aviation information at the FAA, Transport September 15, 2014), we have
Administration (FAA), Department of Airplane Directorate, 1601 Lind Avenue determined that there is an error in the
Transportation (DOT). SW., Renton, WA. For information on manufacturer’s name in the method of
ACTION: Final rule; request for the availability of this material at the compliance language in certain text in
comments. FAA, call 425–227–1221. the ‘‘Explanation of Change Made to
This AD’’ section and in certain
SUMMARY: We are superseding Examining the AD Docket paragraphs of the regulatory text of AD
Airworthiness Directive (AD) 2013–26– You may examine the AD docket on 2013–26–05. AD 2013–26–05 refers to
05 for all Dassault Aviation Model FAN the Internet at http:// Airbus’s EASA Design Organization
JET FALCON, FAN JET FALCON www.regulations.gov by searching for Approval (DOA), instead of Dassault
SERIES C, D, E, F, and G airplanes; and locating Docket No. FAA–2015– Aviation’s EASA DOA. In order to refer
Model MYSTERE–FALCON 200 0830; or in person at the Docket to the appropriate EASA DOA, this AD
airplanes; and Model MYSTERE– Operations office between 9 a.m. and 5 replaces ‘‘Airbus’s’’ with ‘‘Dassault
rljohnson on DSK7TPTVN1PROD with RULES
FALCON 20–C5, 20–D5, 20–E5, and 20– p.m., Monday through Friday, except Aviation’s’’ in paragraphs (h)(2),
F5 airplanes. AD 2013–26–05 required Federal holidays. The AD docket (h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv),
repetitive weighing of fire extinguisher contains this AD, the regulatory (i), (i)(1), (i)(2), (i)(3), (i)(4), (j)(1), (j)(2),
bottles having a certain part number, evaluation, any comments received, and (j)(3), (j)(4), and (l)(2) of this AD. The
and eventual replacement of those other information. The street address for ‘‘Explanation of Change Made to This
bottles to terminate the repetitive the Docket Operations office (telephone AD’’ section of AD 2013–26–05 is not
weighing. This new AD continues to 800–647–5527) is in the ADDRESSES restated in this AD.
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![22636 Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations
FAA’s Determination and Requirements cost of the actions that were required by PART 39—AIRWORTHINESS
of This AD AD 2013–26–05 is $1,246,900, or $6,740 DIRECTIVES
This product has been approved by per product.
the aviation authority of another The new requirements of this AD add ■ 1. The authority citation for part 39
country, and is approved for operation no additional economic burden. continues to read as follows:
in the United States. Pursuant to our Authority: 49 U.S.C. 106(g), 40113, 44701.
Authority for This Rulemaking
bilateral agreement with the State of
Design Authority, we have been notified Title 49 of the United States Code § 39.13 [Amended]
of the unsafe condition described in the specifies the FAA’s authority to issue ■ 2. The FAA amends § 39.13 by
MCAI and service information rules on aviation safety. Subtitle I, removing airworthiness directive (AD)
referenced above. We are issuing this section 106, describes the authority of 2013–26–05, Amendment 39–17714 (79
AD because we evaluated all pertinent the FAA Administrator. ‘‘Subtitle VII: FR 54897, September 15, 2014), and
information and determined the unsafe Aviation Programs,’’ describes in more adding the following new AD:
condition exists and is likely to exist or detail the scope of the Agency’s
develop on other products of these same 2015–08–05 Dassault Aviation:
authority. Amendment 39–18141. Docket No.
type designs. We are issuing this rulemaking under FAA–2015–0830; Directorate Identifier
FAA’s Determination of the Effective the authority described in ‘‘Subtitle VII, 2015–NM–024–AD.
Date Part A, Subpart III, Section 44701: (a) Effective Date
We are superseding AD 2013–26–05, General requirements.’’ Under that
This AD becomes effective May 8, 2015.
Amendment 39–17714 (79 FR 54897, section, Congress charges the FAA with
September 15, 2014), to correct certain promoting safe flight of civil aircraft in (b) Affected ADs
erroneous manufacturer information in air commerce by prescribing regulations This AD replaces AD 2013–26–05,
the ‘‘Explanation of Changes to This for practices, methods, and procedures Amendment 39–17714 (79 FR 54897,
AD’’ section and in certain paragraphs the Administrator finds necessary for September 15, 2014).
of the regulatory text. No other changes safety in air commerce. This regulation (c) Applicability
have been made to AD 2013–26–05. is within the scope of that authority
This AD applies to Dassault Aviation
Therefore, we determined that notice because it addresses an unsafe condition
Model FAN JET FALCON, FAN JET FALCON
and opportunity for prior public that is likely to exist or develop on SERIES C, D, E, F, and G airplanes; Model
comment are unnecessary. products identified in this rulemaking MYSTERE–FALCON 200 airplanes; and
action. Model MYSTERE–FALCON 20–C5, 20–D5,
Comments Invited 20–E5, and 20–F5 airplanes, certificated in
Regulatory Findings
This AD is a final rule that involves any category; all serial numbers.
requirements affecting flight safety, and We determined that this AD will not (d) Subject
we did not precede it by notice and have federalism implications under Air Transport Association (ATA) of
opportunity for public comment. We Executive Order 13132. This AD will America Code 26, Fire Protection.
invite you to send any written relevant not have a substantial direct effect on
data, views, or arguments about this AD. the States, on the relationship between (e) Reason
Send your comments to an address the national government and the States, This AD was prompted by reports of a
listed under the ADDRESSES section. or on the distribution of power and manufacturing defect in the charge indicator
Include ‘‘Docket No. FAA–2015–0830; responsibilities among the various on fire extinguisher bottles and also our
Directorate Identifier 2015–NM–024– levels of government. determination that certain text in the method
AD’’ at the beginning of your comments. of compliance language specified in AD
For the reasons discussed above, I 2013–26–05, Amendment 39–17714 (79 FR
We specifically invite comments on the certify that this AD: 54897, September 15, 2014), incorrectly
overall regulatory, economic, refers to ‘‘Airbus’’ instead of ‘‘Dassault
environmental, and energy aspects of 1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866; Aviation.’’ We are issuing this AD to detect
this AD. We will consider all comments and correct a dormant failure in the fire
received by the closing date and may 2. Is not a ‘‘significant rule’’ under the suppression system, which could result in
amend this AD because of those DOT Regulatory Policies and Procedures the inability to put out a fire in an engine,
comments. (44 FR 11034, February 26, 1979); auxiliary power unit (APU), or rear
We will post all comments we 3. Will not affect intrastate aviation in compartment.
receive, without change, to http:// Alaska; and (f) Compliance
www.regulations.gov, including any
4. Will not have a significant Comply with this AD within the
personal information you provide. We
economic impact, positive or negative, compliance times specified, unless already
will also post a report summarizing each done.
on a substantial number of small entities
substantive verbal contact we receive
under the criteria of the Regulatory (g) Retained Definitions, With No Changes
about this AD.
Flexibility Act.
This paragraph restates the requirements of
Costs of Compliance paragraph (g) of AD 2013–26–05,
List of Subjects in 14 CFR Part 39
We estimate that this AD affects 185 Amendment 39–17714 (79 FR 54897,
airplanes of U.S. registry. Air transportation, Aircraft, Aviation September 15, 2014), with no changes. For
The actions required by AD 2013–26– safety, Incorporation by reference, the purposes of this AD, the following
definitions apply.
rljohnson on DSK7TPTVN1PROD with RULES
05, Amendment 39–17714 (79 FR Safety.
54897, September 15, 2014), and (1) An affected fire extinguisher bottle is
Adoption of the Amendment any fire extinguisher bottle having a part
retained in this AD take about 4 work- number included in table 1 to the
hours per product, at an average labor Accordingly, under the authority introductory text of paragraph (h) of this AD
rate of $85 per work-hour. Required delegated to me by the Administrator, and having a manufacturing batch number
parts cost about $6,400 per product. the FAA amends 14 CFR part 39 as 168 through 200 inclusive on the data plate
Based on these figures, the estimated follows: of the charge indicator.
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![22638 Federal Register / Vol. 80, No. 78 / Thursday, April 23, 2015 / Rules and Regulations
fire extinguisher bottle with a serviceable a method approved by the Manager, (3) The following service information was
part, in accordance with a method approved International Branch, ANM–116, Transport approved for IBR on October 20, 2014, (79 FR
by the Manager, International Branch, ANM– Airplane Directorate, FAA; or the EASA; or 54897, September 15, 2014).
116, Transport Airplane Directorate, FAA; or Dassault Aviation’s EASA DOA. (i) Dassault Service Bulletin F20–785, also
the EASA; or Dassault Aviation’s EASA referred to as 785, dated June 11, 2012.
DOA. (k) Retained Parts Installation Prohibition, (ii) Dassault Service Bulletin F200–131,
(3) For Model MYSTERE–FALCON 200 With No Changes also referred to as 131, dated June 11, 2012.
airplanes: Replace the charge indicator This paragraph restates the requirements of (4) For service information identified in
cartridge with a serviceable part, in paragraph (k) of AD 2013–26–05, this AD, contact Dassault Falcon Jet, P.O. Box
accordance with a method approved by the Amendment 39–17714 (79 FR 54897, 2000, South Hackensack, NJ 07606;
Manager, International Branch, ANM–116, September 15, 2014), with no changes. As of telephone 201–440–6700; Internet http://
Transport Airplane Directorate, FAA; or the October 20, 2014 (the effective date of AD www.dassaultfalcon.com.
EASA; or Dassault Aviation’s EASA DOA. 2013–26–05), no person may install, on any (5) You may view this service information
(4) For Model MYSTERE–FALCON 200 airplane, a fire extinguisher bottle having a at the FAA, Transport Airplane Directorate,
airplanes: Replace the fire extinguisher bottle part number included in table 1 to the 1601 Lind Avenue SW., Renton, WA. For
with a serviceable part, in accordance with introductory text of paragraph (h) of this AD, information on the availability of this
a method approved by the Manager, fitted with a charge indicator having a material at the FAA, call 425–227–1221.
International Branch, ANM–116, Transport manufacturing batch number on the data (6) You may view this service information
Airplane Directorate, FAA; or the EASA; or plate of 168 through 200 inclusive. that is incorporated by reference at the
Dassault Aviation’s EASA DOA. National Archives and Records
(l) Other FAA AD Provisions Administration (NARA). For information on
(j) Retained Replacement of Fire The following provisions also apply to this the availability of this material at NARA, call
Extinguisher Bottle and Charge Indicator AD: 202–741–6030, or go to: http://
Cartridge, With Revised Method of (1) Alternative Methods of Compliance www.archives.gov/federal-register/cfr/ibr-
Compliance Language (AMOCs): The Manager, International locations.html.
This paragraph restates the requirements of Branch, ANM–116, Transport Airplane Issued in Renton, Washington, on April 9,
paragraph (j) of AD 2013–26–05, Amendment Directorate, FAA, has the authority to 2015.
39–17714 (79 FR 54897, September 15, 2014), approve AMOCs for this AD, if requested
Jeffrey E. Duven,
with revised method of compliance language using the procedures found in 14 CFR 39.19.
In accordance with 14 CFR 39.19, send your Manager, Transport Airplane Directorate,
specified in paragraphs (j)(1), (j)(2), (j)(3), and
request to your principal inspector or local Aircraft Certification Service.
(j)(4) of this AD. Unless previously
accomplished as specified in paragraph Flight Standards District Office, as [FR Doc. 2015–09290 Filed 4–22–15; 8:45 am]
(h)(2)(i), (h)(2)(ii), (h)(2)(iii), (h)(2)(iv), (i)(1), appropriate. If sending information directly BILLING CODE 4910–13–P
(i)(2), (i)(3), or (i)(4) of this AD: Within 60 to the International Branch, send it to ATTN:
months after October 20, 2014 (the effective Tom Rodriguez, Aerospace Engineer,
date of AD 2013–26–05), replace any affected International Branch, ANM–116, Transport
Airplane Directorate, FAA, 1601 Lind DEPARTMENT OF COMMERCE
fire extinguisher bottle and charge indicator
cartridge, as specified in paragraph (g)(1) of Avenue SW., Renton, WA 98057–3356;
telephone 425–227–1137; fax 425–227–1149. Bureau of Industry and Security
this AD, with a serviceable part, in
accordance with the method specified in Information may be emailed to: 9-ANM-116-
AMOC-REQUESTS@faa.gov. Before using 15 CFR Part 744
paragraph (j)(1), (j)(2), (j)(3), or (j)(4) of this
AD, as applicable. Replacement of any any approved AMOC, notify your appropriate
[Docket No. 150318286–5286–01]
principal inspector, or lacking a principal
affected fire extinguisher bottle and charge
inspector, the manager of the local flight RIN 0694–AG58
indicator cartridge with a serviceable part
standards district office/certificate holding
terminates the repetitive actions specified in
district office. The AMOC approval letter Addition of Certain Persons to the
paragraphs (h) and (i) of this AD.
must specifically reference this AD. Entity List
(1) For Model FAN JET FALCON, FAN JET
(2) Contacting the Manufacturer: As of the
FALCON SERIES C, D, E, F, and G airplanes;
effective date of this AD, for any requirement AGENCY: Bureau of Industry and
and Model MYSTERE–FALCON 20–C5, 20–
in this AD to obtain corrective actions from Security, Commerce.
D5, 20–E5, and 20–F5 airplanes: Replace the
a manufacturer, the action must be ACTION: Final rule.
charge indicator cartridge with a serviceable
accomplished using a method approved by
part, in accordance with a method approved the Manager, International Branch, ANM–
by the Manager, International Branch, ANM– SUMMARY: This rule amends the Export
116, Transport Airplane Directorate, FAA; or Administration Regulations (EAR) by
116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation’s EASA
the EASA; or Dassault Aviation’s EASA adding eight persons under nine entries
DOA. If approved by the DOA, the approval
DOA. must include the DOA-authorized signature.
to the Entity List. The eight persons who
(2) For Model FAN JET FALCON, FAN JET are added to the Entity List have been
FALCON SERIES C, D, E, F, and G airplanes; (m) Related Information determined by the U.S. Government to
and Model MYSTERE–FALCON 20–C5, 20– Refer to Mandatory Continuing be acting contrary to the national
D5, 20–E5, and 20–F5 airplanes: Replace the Airworthiness Information (MCAI) EASA security or foreign policy interests of the
fire extinguisher bottle with a serviceable Airworthiness Directive 2012–0189, dated United States. These eight persons will
part, in accordance with a method approved September 24, 2012, for related information.
by the Manager, International Branch, ANM–
be listed on the Entity List under the
This MCAI may be found in the AD docket destinations of China, Iran, Taiwan, and
116, Transport Airplane Directorate, FAA; or on the Internet at http://www.regulations.gov
the EASA; or Dassault Aviation’s EASA by searching for and locating Docket No.
Turkey. There are nine entries for the
DOA. FAA–2015–0830. eight persons because one person is
(3) For Model MYSTERE–FALCON 200 listed in two locations, resulting in an
airplanes: Replace the charge indicator (n) Material Incorporated by Reference additional entry. Specifically, the
cartridge with a serviceable part, in (1) The Director of the Federal Register additional entry covers one person that
rljohnson on DSK7TPTVN1PROD with RULES
accordance with a method approved by the approved the incorporation by reference will be listed on the Entity List under
Manager, International Branch, ANM–116, (IBR) of the service information listed in this the destination of Iran and Turkey.
Transport Airplane Directorate, FAA; or the paragraph under 5 U.S.C. 552(a) and 1 CFR
DATE: Effective Date: This rule is
EASA; or Dassault Aviation’s EASA DOA. part 51.
(4) For Model MYSTERE–FALCON 200 (2) You must use this service information effective April 23, 2015.
airplanes: Replace the fire extinguisher bottle as applicable to do the actions required by FOR FURTHER INFORMATION CONTACT:
with a serviceable part, in accordance with this AD, unless this AD specifies otherwise. Chair, End-User Review Committee,
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Document Created: 2015-12-16 08:41:08
Document Modified: 2015-12-16 08:41:08
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD becomes effective May 8, 2015. | |
| Contact | Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. | |
| FR Citation | 80 FR 22635 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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