80 FR 52955 - Airworthiness Directives; Bombardier, Inc. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 170 (September 2, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 170 (September 2, 2015)
| Page Range | 52955-52959 | |
| FR Document | 2015-21472 |
[Federal Register Volume 80, Number 170 (Wednesday, September 2, 2015)] [Rules and Regulations] [Pages 52955-52959] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-21472] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2014-0583; Directorate Identifier 2013-NM-130-AD; Amendment 39-18258; AD 2015-17-25] RIN 2120-AA64 Airworthiness Directives; Bombardier, Inc. Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400 series airplanes. This AD was prompted by reports of chafing of the fuel lines due to contact with the surrounding structures in the fuel tank. This AD requires replacing and modifying fuel lines, revising the maintenance or inspection program, as applicable, to include critical design configuration control limitations (CDCCL) and airworthiness limitation (AWL) items, and, for certain airplanes, removing certain clamps and mounting hardware. We are issuing this AD to prevent chafing of the fuel lines in the fuel tank, which could result in potential ignition sources in the fuel tank in the event of a lightning strike and consequent fire or explosion. DATES: This AD becomes effective October 7, 2015. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of October 7, 2015. ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0583 or in person at the Docket Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC. For service information identified in this AD, contact Bombardier, Inc., Q-Series Technical Help Desk, 123 Garratt Boulevard, Toronto, Ontario M3K 1Y5, Canada; telephone 416-375-4000; fax 416-375-4539; email [email protected]; Internet http://www.bombardier.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 [[Page 52956]] FAA, call 425-227-1221. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014- 0583. FOR FURTHER INFORMATION CONTACT: Kent Fredrickson, Aerospace Engineer, Propulsion and Services Branch, ANE-173, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7364; fax 516-794-5531. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Bombardier, Inc. Model DHC-8-400 series airplanes. The NPRM published in the Federal Register on August 26, 2014 (79 FR 50860). Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian Airworthiness Directive CF- 2013-09R1, dated May 28, 2013 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Bombardier, Inc. Model DHC-8-400 series airplanes. The MCAI states: Reports from operators have revealed a number of instances of chafing of the fuel lines due to contact with the surrounding structures in the fuel tank. An internal audit conducted by Bombardier revealed a number of locations in the fuel tank where low clearances were noted between fuel lines and the surrounding structure. Low clearances between fuel lines and the surrounding structures may result in ignition sources in the fuel tank in the event of a lightning strike, creating an unacceptable level of safety. Bombardier had issued Service Bulletin (SB) 84-28-09 to introduce new fuel line assemblies that include new fuel lines and Teflon protective sleeves, and SBs 84-28-10 and 84-28-13 to remove unnecessary hardware in the wing fuel tanks, in order to eliminate potential fouling conditions on the affected fuel lines. Upon an operator's incorporation of SB 84-28-09, an additional fouling condition was identified on the post-modification fuel lines. In order to address this concern on the aeroplane, Bombardier has issued SBs 84-28-14 and 84-28-15, along with ModSum IS4Q2800012 to rectify this problem. This [Canadian] AD mandates the replacement of fuel lines and the installation of fuel line Teflon protective sleeves. In addition, the fuel line Teflon protective sleeves have been added to the Critical Design Configuration Control Limitations (CDCCL) along with the introduction of associated Fuel System Limitations tasks, to ensure integrity of the new assembly. Since the original issue of this [Canadian] AD, it was found that there were editorial errors in Parts IB and II A of this [Canadian] AD. In addition, the Temporary Revisions (TR) Airworthiness Limitation Items (ALI)-111/-112 ``referenced'' in Parts III and IV of this AD had been superseded by later revisions. This [Canadian] AD is revised to correct the editorial errors and accept the later TR approved by Transport Canada. You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0583-0002. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM (79 FR 50860, August 26, 2014) and the FAA's response to each comment. Request To Refer to Revised Service Information All Nippon Airways (ANA) and Horizon Air requested that we revise paragraph (g) of the proposed AD (79 FR 50860, August 26, 2014) to refer to the following service information:Bombardier Service Bulletin 84-28-14, Revision A, dated June 9, 2014 Bombardier Service Bulletin 84-28-09, Revision D, January 29, 2013 Bombardier Service Bulletin 84-28-15, dated August 17, 2012 Horizon also requested that we revise paragraph (n) of the proposed AD (79 FR 50860, August 26, 2014) to provide credit for the prior accomplishment of the actions specified in Bombardier Service Bulletin 84-28-14, dated August 17, 2012. We agree with the requests and have revised paragraphs (g)(1), (g)(2)(i), (g)(2)(ii), and (m) of this AD accordingly. We have also redesignated paragraph (n) of the proposed AD (79 FR 50860, August 26, 2014) as paragraph (n)(1) of this AD, and added new paragraph (n)(2) to this AD to indicate the new credit service information. Request To Clarify Certain Affected Airplanes ANA requested that we correct the identity of the affected airplanes in paragraph (g)(2) of the proposed AD (79 FR 50860, August 26, 2014). Although paragraph (g)(2) of the NPRM specified airplanes on which ModSum 4-113643 ``was incorporated'' in production, ANA noted that this requirement should apply to airplanes on which ModSum 4- 113643 ``was not incorporated'' in production. ANA noted that ModSum 4- 113643 is equivalent to the Bombardier Service Bulletin 84-28-09. We agree with the request. The intent of the NPRM (79 FR 50860, August 26, 2014) was to include only airplanes on which neither the ModSum nor the corresponding service bulletin was done. We have revised paragraph (g)(2) of this AD accordingly. Request To Exclude Specific Access and Close Requirements Horizon Air requested that we revise paragraphs (g) and (i) of the proposed AD (79 FR 50860, August 26, 2014) to exclude the Job Set-up and the Close Out sections in certain service information, because these actions do not directly correct the unsafe condition. Horizon Air stated that requiring the actions in these sections restricts an operator's ability to do other maintenance actions concurrently with the actions required by this AD. We agree to revise paragraphs (g) and (i) of this AD to specify only the actions in paragraph B., ``Procedures,'' which correct the unsafe condition. Request To Allow Use of Later Revisions of Service Information ANA requested that we allow use of ``later revisions'' of the service information, as done in the MCAI. We disagree with the request. We cannot use the phrase ``or later revisions'' in an AD when referring to service documents because doing so violates Office of the Federal Register (OFR) regulations for approval of materials ``incorporated by reference'' in rules. See 1 CFR 51.1(f). In general terms, we are required by these OFR regulations to either publish the service document contents as part of the actual AD language; or submit the service document to the OFR for approval as ``referenced'' material, in which case we may refer to such material in the text of an AD. The AD may refer to service documents only if the OFR has approved them for incorporation by reference. See 1 CFR part 51. To allow operators to use later revisions of the referenced document (issued after publication of the AD), either we must revise the AD to refer to specific later revisions, or operators must request approval to use later revisions as an alternative method of compliance with this AD under the provisions of paragraph (o)(1) of this AD. We have not changed this AD regarding this issue. Conclusion We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting this AD with the changes described previously and minor editorial changes. We have determined that these minor changes: [[Page 52957]] Are consistent with the intent that was proposed in the NPRM (79 FR 50860, August 26, 2014) for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM (79 FR 50860, August 26, 2014). We also determined that these changes will not increase the economic burden on any operator or increase the scope of this AD. Related Service Information Under 1 CFR Part 51 Bombardier has issued the following service information: Service Bulletin 84-28-09, Revision D, dated January 29, 2013, which describes procedures for replacing fuel lines, adding Teflon tubing to certain fuel lines in the fuel tank, and contacting the manufacturer for certain corrective actions. Service Bulletin 84-28-10, Revision B, dated March 19, 2013, which describes procedures for inspecting for the presence of certain clamps and hardware and, if those are present, removing those certain clamps and mounting hardware. Service Bulletin 84-28-13, dated August 17, 2012, which describes procedures for removing certain clamps and mounting hardware. Service Bulletin 84-28-14, Revision A, dated June 9, 2014, which describes procedures for replacing a tube assembly. Service Bulletin 84-28-15, dated August 17, 2012, which describes procedures for replacing fuel lines, adding Teflon tubing to certain fuel lines in the fuel tank, and contacting the manufacturer for certain corrective actions. Temporary Revision ALI-111, dated January 11, 2011, to Section 4-1, ``Fuel System Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7, which describes updates to the fuel system limitations for inspections of the Teflon sleeve on the fuel tank vent lines. Temporary Revision ALI-112, dated January 11, 2011, to Section 5-1, ``Critical Design Configuration Control Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7, which describes updates to the critical design configuration control limitations on Teflon protective sleeves on fuel vent lines inside the fuel tanks. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section of this NPRM. Costs of Compliance We estimate that this AD affects 72 airplanes of U.S. registry. We also estimate that it will take about 80 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $2,845 per product. Based on these figures, we estimate the cost of this AD on U.S. operators to be $694,440, or $9,645 per product. 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. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0583; 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 Operations office (telephone 800-647- 5527) is in the ADDRESSES section. 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 adding the following new airworthiness directive (AD): 2015-17-25 Bombardier, Inc.: Amendment 39-18258. Docket No. FAA- 2014-0583; Directorate Identifier 2013-NM-130-AD. (a) Effective Date This AD becomes effective October 7, 2015 (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and - 402 airplanes, certificated in any category, serial numbers 4001, and 4003 through 4417 inclusive. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Reason This AD was prompted by reports of chafing of the fuel lines due to contact with the surrounding structures in the fuel tank. We are issuing this AD to prevent chafing of the fuel lines in the fuel tank, which could result in potential ignition sources in the fuel tank in the event of a lightning strike and consequent fire or explosion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. [[Page 52958]] (g) Installation of New Fuel Tube Assemblies For airplanes having serial numbers 4001, 4003, 4004, 4006, and 4008 through 4417 inclusive: Within 6,000 flight hours or 3 years after the effective date of this AD, whichever occurs first, install new, improved fuel tube assemblies, in accordance with paragraph B., ``Procedure,'' of the Accomplishment Instructions of the applicable service information identified in paragraphs (g)(1) and (g)(2) of this AD. (1) For airplanes on which Bombardier Service Bulletin 84-28-09 was incorporated prior to the effective date of this AD, or on which Bombardier Modification Summary (ModSum) 4-113643 was incorporated in production: Bombardier Service Bulletin 84-28-14, Revision A, dated June 9, 2014. (2) For airplanes on which Bombardier Service Bulletin 84-28-09 was not incorporated prior to the effective date of this AD, or on which Bombardier ModSum 4-113643 was not incorporated in production, use the service information identified in paragraph (g)(2)(i) or (g)(2)(ii) of this AD. (i) Bombardier Service Bulletin 84-28-09, Revision D, dated January 29, 2013; and Bombardier Service Bulletin 84-28-14, Revision A, dated June 9, 2014. (ii) Bombardier Service Bulletin 84-28-15, dated August 17, 2012. (h) Prior Incorporation of Bombardier ModSum IS4Q2800012 For airplanes on which Bombardier Service Bulletin 84-28-09, and Bombardier ModSum IS4Q2800012 were incorporated before the effective date of this AD; and for airplanes on which Bombardier ModSum 4- 113643 was incorporated in production, and Bombardier ModSum IS4Q2800012 was incorporated prior to the effective date of this AD: The requirements of paragraph (g) are not required. (i) Removal of Clamps and Mounting Hardware For airplanes having serial numbers 4003 through 4151 inclusive, and 4332 through 4417 inclusive: Within 6,000 flight hours or 3 years after the effective date of this AD, whichever occurs first, do the actions required by paragraphs (i)(1) and (i)(2) of this AD, as applicable. (1) For airplanes having serial numbers 4003 through 4151 inclusive, on which Bombardier ModSum IS4Q2800010 was incorporated: Inspect for the presence of certain clamps and hardware, and, if present, remove certain clamps and mounting hardware, in accordance with paragraph B., ``Procedure,'' of the Accomplishment Instructions of Bombardier Service Bulletin 84-28-10, Revision B, dated March 19, 2013. (2) For airplanes having serial numbers 4332 through 4417 inclusive: Remove certain clamps and mounting hardware, in accordance with paragraph B., ``Procedure,'' of the Accomplishment Instructions of Bombardier Service Bulletin 84-28-13, dated August 17, 2012. (j) Incorporation of Fuel System Limitations (FSL) Tasks Within 60 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the information in FSL Task Numbers 284000-406 and 284000-418 as specified in Bombardier Temporary Revision ALI-111, dated January 11, 2011, to Section 4-1, ``Fuel System Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. The initial compliance time for Task 284000-418 is within 108 months or 18,000 flight hours after accomplishing the requirements of paragraph (g) of this AD, whichever occurs first, for airplanes identified in paragraphs (g)(1) and (g)(2) of this AD; or, for those airplanes identified in paragraph (h) of this AD, within 108 months or 18,000 flight hours after the incorporation of Bombardier ModSum IS4Q2800012. The maintenance program revision required by this paragraph may be done by inserting a copy of Bombardier Temporary Revision ALI-111, dated January 11, 2011, into the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. When Bombardier Temporary Revision ALI-111, dated January 11, 2011, has been included in the general revisions of the manual, the general revisions may be inserted into the manual, and this temporary revision may be removed, provided the relevant information in the general revision is identical to that in Bombardier Temporary Revision ALI-111. (k) Incorporation of Critical Design Configuration Control Limitations (CDCCL) Items Within 60 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the CDCCL items specified in Bombardier Temporary Revision ALI-112, dated January 11, 2011, to Section 5-1, ``Critical Design Configuration Control Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. The maintenance program revision required by this paragraph may be done by inserting a copy of Bombardier Temporary Revision ALI-112, dated January 11, 2011, into the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. When Bombardier Temporary Revision ALI-112, dated January 11, 2011, has been included in the general revisions of the manual, the general revisions may be inserted into the manual, and this temporary revision may be removed, provided the relevant information in the general revision is identical to that in Bombardier Temporary Revision ALI-112. (l) No Alternative Actions, Intervals, and CDCCLs After the maintenance or inspection program, as applicable, has been revised as required by paragraphs (j) and (k) of this AD, no alternative actions (e.g., inspections), intervals, or CDCCLs may be used unless the actions, intervals, or CDCCL are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (o)(1) of this AD. (m) Exception to Service Information Specifications Where Bombardier Service Bulletin 84-28-09, Revision D, dated January 29, 2013; and Bombardier Service Bulletin 84-28-15, dated August 17, 2012; specify contacting the manufacturer for corrective action during accomplishment of the actions in those service bulletins: Before further flight, repair the discrepancy using a method approved by the Manager, New York Aircraft Certification Office (ACO), FAA; or Transport Canada Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval Organization (DAO). (n) Credit for Previous Actions (1) This paragraph provides credit for actions required by paragraph (i)(1) of this AD, if those actions were performed before the effective date of this AD using Bombardier Service Bulletin 84- 28-10, dated December 6, 2011; or Bombardier Service Bulletin 84-28- 10, Revision A, dated May 15, 2012. This service information is not incorporated by reference in this AD. (2) This paragraph provides credit for actions required by paragraph (g) of this AD, if the corresponding actions were performed before the effective date of this AD using Bombardier Service Bulletin 84-28-14, dated August 15, 2012, which is not incorporated by reference in this AD. (o) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York ACO, ANE-170, 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 ACO, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228- 7300; fax 516-794-5531. 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: 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, New York ACO, ANE-170, FAA; or TCCA; or Bombardier, Inc.'s TCCA DAO. If approved by the DAO, the approval must include the DAO-authorized signature. (p) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian Airworthiness Directive CF-2013-09R1, dated May 28, 2013, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0583-0002. [[Page 52959]] (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (q)(3) and (q)(4) of this AD. (q) 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. (i) Bombardier Service Bulletin 84-28-09, Revision D, dated January 29, 2013. (ii) Bombardier Service Bulletin 84-28-10, Revision B, dated March 19, 2013. (iii) Bombardier Service Bulletin 84-28-13, dated August 17, 2012. (iv) Bombardier Service Bulletin 84-28-14, Revision A, dated June 9, 2014. (v) Bombardier Service Bulletin 84-28-15, dated August 17, 2012. (vi) Bombardier Temporary Revision ALI-111, dated January 11, 2011, to Section 4-1, ``Fuel System Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. (vii) Bombardier Temporary Revision ALI-112, dated January 11, 2011, to Section 5-1, ``Critical Design Configuration Control Limitations,'' of Part 2, ``Airworthiness Limitation Items,'' of the Airworthiness Limitation Items section of Bombardier Q400 Dash 8 Maintenance Requirements Manual PSM 1-84-7. (3) For service information identified in this AD, contact Bombardier, Inc., Q-Series Technical Help Desk, 123 Garratt Boulevard, Toronto, Ontario M3K 1Y5, Canada; telephone 416-375-4000; fax 416-375-4539; email [email protected]; Internet http://www.bombardier.com. (4) 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. (5) 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 August 21, 2015. Kevin Hull, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-21472 Filed 9-1-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations 52955
(A) Before the accumulation of 20,000 total (k) Related Information DEPARTMENT OF TRANSPORTATION
flight hours or within 96 months since the Refer to Mandatory Continuing
date of issuance of the original Brazilian Federal Aviation Administration
Airworthiness Information (MCAI) Brazilian
standard airworthiness certificate or date of
Airworthiness Directive 2013–12–02,
issuance of the original Brazilian export 14 CFR Part 39
certificate of airworthiness, whichever occurs effective December 27, 2013, for related
first. information. This MCAI may be found in the [Docket No. FAA–2014–0583; Directorate
(B) Within 60 months after the effective AD docket on the Internet at http:// Identifier 2013–NM–130–AD; Amendment
date of this AD. www.regulations.gov/ 39–18258; AD 2015–17–25]
#!documentDetail;D=FAA-2014-0586-0003.
(h) Incorporation of TRs Into General RIN 2120–AA64
Revisions (l) Material Incorporated by Reference
When the information from Embraer TR 8– (1) The Director of the Federal Register
Airworthiness Directives; Bombardier,
1, dated October 26, 2012; TR 8–2, dated approved the incorporation by reference Inc. Airplanes
December 5, 2012; and TR 8–3, dated April (IBR) of the service information listed in this
8, 2013; to the Embraer Legacy BJ MPG,
AGENCY: Federal Aviation
paragraph under 5 U.S.C. 552(a) and 1 CFR Administration (FAA), Department of
MPG–1483, has been included in the general
part 51. Transportation (DOT).
revisions of Embraer Legacy BJ MPG, MPG–
(2) You must use this service information
1483, the general revisions may be inserted ACTION: Final rule.
in the MPG, provided that the relevant as applicable to do the actions required by
information in the general revision is this AD, unless this AD specifies otherwise. SUMMARY: We are adopting a new
identical to that in Embraer TR 8–1, dated (i) Embraer Temporary Revision 8–1, dated airworthiness directive (AD) for certain
October 26, 2012; TR 8–2, dated December 5, October 26, 2012, to the Embraer Legacy BJ Bombardier, Inc. Model DHC–8–400
2012; and TR 8–3, dated April 8, 2013; and Maintenance Planning Guide (MPG), MPG– series airplanes. This AD was prompted
the TRs may be removed. 1483. by reports of chafing of the fuel lines
(i) No Alternative Actions, Intervals, and/or (ii) Embraer Temporary Revision 8–2, due to contact with the surrounding
Critical Design Configuration Control dated December 5, 2012, to the Embraer structures in the fuel tank. This AD
Limitations (CDCCLs) Legacy BJ MPG, MPG–1483. requires replacing and modifying fuel
After accomplishing the revision required (iii) Embraer Temporary Revision 8–3, lines, revising the maintenance or
by paragraph (g) of this AD, no alternative dated April 8, 2013, to the Embraer Legacy inspection program, as applicable, to
actions (e.g., inspections), intervals, and/or BJ MPG, MPG–1483. include critical design configuration
CDCCLs may be used unless the actions, (3) For service information identified in
control limitations (CDCCL) and
intervals, and/or CDCCLs are approved as an this AD, contact Empresa Brasileira de
airworthiness limitation (AWL) items,
alternative method of compliance (AMOC) in Aeronautica S.A. (Embraer), Technical
accordance with the procedures specified in
and, for certain airplanes, removing
Publications Section (PC 060), Av. Brigadeiro
paragraph (j)(1) of this AD. certain clamps and mounting hardware.
Faria Lima, 2170—Putim—12227–901 São
We are issuing this AD to prevent
(j) Other FAA AD Provisions Jose dos Campos—SP—Brasil; telephone +55
chafing of the fuel lines in the fuel tank,
12 3927–5852 or +55 12 3309–0732; fax +55
The following provisions also apply to this
12 3927–7546; email distrib@embraer.com.br;
which could result in potential ignition
AD: sources in the fuel tank in the event of
(1) Alternative Methods of Compliance Internet http://www.flyembraer.com.
(4) You may view this service information
a lightning strike and consequent fire or
(AMOCs): The Manager, International explosion.
Branch, ANM–116, Transport Airplane at the FAA, Transport Airplane Directorate,
Directorate, FAA, has the authority to 1601 Lind Avenue SW., Renton, WA. For DATES: This AD becomes effective
approve AMOCs for this AD, if requested information on the availability of this October 7, 2015.
using the procedures found in 14 CFR 39.19. material at the FAA, call 425–227–1221. The Director of the Federal Register
In accordance with 14 CFR 39.19, send your (5) You may view this service information approved the incorporation by reference
request to your principal inspector or local that is incorporated by reference at the of certain publications listed in this AD
Flight Standards District Office, as National Archives and Records as of October 7, 2015.
appropriate. If sending information directly
Administration (NARA). For information on ADDRESSES: You may examine the AD
to the International Branch, send it to ATTN:
the availability of this material at NARA, call docket on the Internet at http://
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, Transport 202–741–6030, or go to: http:// www.regulations.gov/
Airplane Directorate, FAA, 1601 Lind www.archives.gov/federal-register/cfr/ibr- #!docketDetail;D=FAA-2014-0583 or in
Avenue SW., Renton, WA 98057–3356; locations.html. person at the Docket Management
telephone 425–227–1175; fax 425–227–1149. Issued in Renton, Washington, on August Facility, U.S. Department of
Information may be emailed to: 9-ANM-116- 21, 2015. Transportation, Docket Operations, M–
AMOC-REQUESTS@faa.gov. Before using 30, West Building Ground Floor, Room
any approved AMOC, notify your appropriate Kevin Hull,
W12–140, 1200 New Jersey Avenue SE.,
principal inspector, or lacking a principal Acting Manager, Transport Airplane
inspector, the manager of the local flight Washington, DC.
Directorate, Aircraft Certification Service.
standards district office/certificate holding For service information identified in
[FR Doc. 2015–21473 Filed 9–1–15; 8:45 am]
district office. The AMOC approval letter this AD, contact Bombardier, Inc., Q-
BILLING CODE 4910–13–P Series Technical Help Desk, 123 Garratt
must specifically reference this AD.
(2) Contacting the Manufacturer: For any Boulevard, Toronto, Ontario M3K 1Y5,
requirement in this AD to obtain corrective Canada; telephone 416–375–4000; fax
asabaliauskas on DSK5VPTVN1PROD with RULES
actions from a manufacturer, the action must 416–375–4539; email
be accomplished using a method approved thd.qseries@aero.bombardier.com;
by the Manager, International Branch, ANM–
Internet http://www.bombardier.com.
116, Transport Airplane Directorate, FAA; or
the Agência Nacional de Aviação Civil You may view this referenced service
(ANAC); or ANAC’s authorized Designee. If information at the FAA, Transport
approved by the ANAC Designee, the Airplane Directorate, 1601 Lind Avenue
approval must include the Designee’s SW., Renton, WA. For information on
authorized signature. the availability of this material at the
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![52956 Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations
FAA, call 425–227–1221. It is also errors in Parts IB and II A of this [Canadian] 2014) was to include only airplanes on
available on the Internet at http:// AD. In addition, the Temporary Revisions which neither the ModSum nor the
www.regulations.gov by searching for (TR) Airworthiness Limitation Items (ALI)– corresponding service bulletin was
111/–112 ‘‘referenced’’ in Parts III and IV of
and locating Docket No. FAA–2014– done. We have revised paragraph (g)(2)
this AD had been superseded by later
0583. revisions. This [Canadian] AD is revised to of this AD accordingly.
FOR FURTHER INFORMATION CONTACT: Kent correct the editorial errors and accept the Request To Exclude Specific Access and
Fredrickson, Aerospace Engineer, later TR approved by Transport Canada. Close Requirements
Propulsion and Services Branch, ANE– You may examine the MCAI in the Horizon Air requested that we revise
173, FAA, New York Aircraft AD docket on the Internet at http:// paragraphs (g) and (i) of the proposed
Certification Office, 1600 Stewart www.regulations.gov/ AD (79 FR 50860, August 26, 2014) to
Avenue, Suite 410, Westbury, NY #!documentDetail;D=FAA-2014-0583- exclude the Job Set-up and the Close
11590; telephone 516–228–7364; fax 0002. Out sections in certain service
516–794–5531.
Comments information, because these actions do
SUPPLEMENTARY INFORMATION: not directly correct the unsafe
We gave the public the opportunity to condition. Horizon Air stated that
Discussion
participate in developing this AD. The requiring the actions in these sections
We issued a notice of proposed following presents the comments
rulemaking (NPRM) to amend 14 CFR restricts an operator’s ability to do other
received on the NPRM (79 FR 50860, maintenance actions concurrently with
part 39 by adding an AD that would August 26, 2014) and the FAA’s
apply to certain Bombardier, Inc. Model the actions required by this AD.
response to each comment. We agree to revise paragraphs (g) and
DHC–8–400 series airplanes. The NPRM
Request To Refer to Revised Service (i) of this AD to specify only the actions
published in the Federal Register on
Information in paragraph B., ‘‘Procedures,’’ which
August 26, 2014 (79 FR 50860).
Transport Canada Civil Aviation correct the unsafe condition.
All Nippon Airways (ANA) and
(TCCA), which is the aviation authority Horizon Air requested that we revise Request To Allow Use of Later
for Canada, has issued Canadian paragraph (g) of the proposed AD (79 FR Revisions of Service Information
Airworthiness Directive CF–2013–09R1, 50860, August 26, 2014) to refer to the ANA requested that we allow use of
dated May 28, 2013 (referred to after following service information: ‘‘later revisions’’ of the service
this as the Mandatory Continuing • Bombardier Service Bulletin 84–28– information, as done in the MCAI.
Airworthiness Information, or ‘‘the 14, Revision A, dated June 9, 2014 We disagree with the request. We
MCAI’’), to correct an unsafe condition • Bombardier Service Bulletin 84–28– cannot use the phrase ‘‘or later
for certain Bombardier, Inc. Model 09, Revision D, January 29, 2013 revisions’’ in an AD when referring to
DHC–8–400 series airplanes. The MCAI • Bombardier Service Bulletin 84–28– service documents because doing so
states: 15, dated August 17, 2012 violates Office of the Federal Register
Reports from operators have revealed a Horizon also requested that we revise (OFR) regulations for approval of
number of instances of chafing of the fuel paragraph (n) of the proposed AD (79 FR materials ‘‘incorporated by reference’’ in
lines due to contact with the surrounding 50860, August 26, 2014) to provide rules. See 1 CFR 51.1(f). In general
structures in the fuel tank. An internal audit credit for the prior accomplishment of terms, we are required by these OFR
conducted by Bombardier revealed a number
of locations in the fuel tank where low the actions specified in Bombardier regulations to either publish the service
clearances were noted between fuel lines and Service Bulletin 84–28–14, dated document contents as part of the actual
the surrounding structure. Low clearances August 17, 2012. AD language; or submit the service
between fuel lines and the surrounding We agree with the requests and have document to the OFR for approval as
structures may result in ignition sources in revised paragraphs (g)(1), (g)(2)(i), ‘‘referenced’’ material, in which case we
the fuel tank in the event of a lightning strike, (g)(2)(ii), and (m) of this AD may refer to such material in the text of
creating an unacceptable level of safety. accordingly. We have also redesignated an AD. The AD may refer to service
Bombardier had issued Service Bulletin paragraph (n) of the proposed AD (79 FR
(SB) 84–28–09 to introduce new fuel line
documents only if the OFR has
assemblies that include new fuel lines and 50860, August 26, 2014) as paragraph approved them for incorporation by
Teflon protective sleeves, and SBs 84–28–10 (n)(1) of this AD, and added new reference. See 1 CFR part 51.
and 84–28–13 to remove unnecessary paragraph (n)(2) to this AD to indicate To allow operators to use later
hardware in the wing fuel tanks, in order to the new credit service information. revisions of the referenced document
eliminate potential fouling conditions on the (issued after publication of the AD),
affected fuel lines. Request To Clarify Certain Affected
either we must revise the AD to refer to
Upon an operator’s incorporation of SB 84– Airplanes
specific later revisions, or operators
28–09, an additional fouling condition was ANA requested that we correct the must request approval to use later
identified on the post-modification fuel lines.
identity of the affected airplanes in revisions as an alternative method of
In order to address this concern on the
aeroplane, Bombardier has issued SBs 84– paragraph (g)(2) of the proposed AD (79 compliance with this AD under the
28–14 and 84–28–15, along with ModSum FR 50860, August 26, 2014). Although provisions of paragraph (o)(1) of this
IS4Q2800012 to rectify this problem. paragraph (g)(2) of the NPRM specified AD. We have not changed this AD
This [Canadian] AD mandates the airplanes on which ModSum 4–113643 regarding this issue.
replacement of fuel lines and the installation ‘‘was incorporated’’ in production, ANA
asabaliauskas on DSK5VPTVN1PROD with RULES
of fuel line Teflon protective sleeves. In noted that this requirement should Conclusion
addition, the fuel line Teflon protective apply to airplanes on which ModSum We reviewed the relevant data,
sleeves have been added to the Critical 4–113643 ‘‘was not incorporated’’ in considered the comments received, and
Design Configuration Control Limitations
(CDCCL) along with the introduction of production. ANA noted that ModSum determined that air safety and the
associated Fuel System Limitations tasks, to 4–113643 is equivalent to the public interest require adopting this AD
ensure integrity of the new assembly. Bombardier Service Bulletin 84–28–09. with the changes described previously
Since the original issue of this [Canadian] We agree with the request. The intent and minor editorial changes. We have
AD, it was found that there were editorial of the NPRM (79 FR 50860, August 26, determined that these minor changes:
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![Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations 52957
• Are consistent with the intent that This service information is reasonably Examining the AD Docket
was proposed in the NPRM (79 FR available because the interested parties
You may examine the AD docket on
50860, August 26, 2014) for correcting have access to it through their normal
the Internet at http://
the unsafe condition; and course of business or by the means
• Do not add any additional burden www.regulations.gov/#!docketDetail;
identified in the ADDRESSES section of
upon the public than was already D=FAA-2014-0583; or in person at the
this NPRM.
proposed in the NPRM (79 FR 50860, Docket Management Facility between 9
August 26, 2014). Costs of Compliance a.m. and 5 p.m., Monday through
We also determined that these We estimate that this AD affects 72 Friday, except Federal holidays. The AD
changes will not increase the economic airplanes of U.S. registry. We also docket contains this AD, the regulatory
burden on any operator or increase the estimate that it will take about 80 work- evaluation, any comments received, and
scope of this AD. hours per product to comply with the other information. The street address for
basic requirements of this AD. The the Docket Operations office (telephone
Related Service Information Under 1 800–647–5527) is in the ADDRESSES
average labor rate is $85 per work-hour.
CFR Part 51 section.
Required parts will cost about $2,845
Bombardier has issued the following per product. Based on these figures, we List of Subjects in 14 CFR Part 39
service information: estimate the cost of this AD on U.S.
• Service Bulletin 84–28–09, Revision operators to be $694,440, or $9,645 per Air transportation, Aircraft, Aviation
D, dated January 29, 2013, which product. safety, Incorporation by reference,
describes procedures for replacing fuel Safety.
lines, adding Teflon tubing to certain Authority for This Rulemaking
Adoption of the Amendment
fuel lines in the fuel tank, and Title 49 of the United States Code
contacting the manufacturer for certain specifies the FAA’s authority to issue Accordingly, under the authority
corrective actions. rules on aviation safety. Subtitle I, delegated to me by the Administrator,
• Service Bulletin 84–28–10, Revision section 106, describes the authority of the FAA amends 14 CFR part 39 as
B, dated March 19, 2013, which the FAA Administrator. ‘‘Subtitle VII: follows:
describes procedures for inspecting for Aviation Programs,’’ describes in more
the presence of certain clamps and detail the scope of the Agency’s PART 39—AIRWORTHINESS
hardware and, if those are present, authority. DIRECTIVES
removing those certain clamps and We are issuing this rulemaking under
mounting hardware. the authority described in ‘‘Subtitle VII, ■ 1. The authority citation for part 39
• Service Bulletin 84–28–13, dated Part A, Subpart III, Section 44701: continues to read as follows:
August 17, 2012, which describes General requirements.’’ Under that Authority: 49 U.S.C. 106(g), 40113, 44701.
procedures for removing certain clamps section, Congress charges the FAA with
and mounting hardware. promoting safe flight of civil aircraft in § 39.13 [Amended]
• Service Bulletin 84–28–14, Revision air commerce by prescribing regulations ■ 2. The FAA amends § 39.13 by adding
A, dated June 9, 2014, which describes for practices, methods, and procedures the following new airworthiness
procedures for replacing a tube the Administrator finds necessary for directive (AD):
assembly. safety in air commerce. This regulation
• Service Bulletin 84–28–15, dated is within the scope of that authority
2015–17–25 Bombardier, Inc.: Amendment
August 17, 2012, which describes 39–18258. Docket No. FAA–2014–0583;
because it addresses an unsafe condition Directorate Identifier 2013–NM–130–AD.
procedures for replacing fuel lines, that is likely to exist or develop on
adding Teflon tubing to certain fuel products identified in this rulemaking (a) Effective Date
lines in the fuel tank, and contacting the action. This AD becomes effective October 7, 2015
manufacturer for certain corrective
Regulatory Findings (b) Affected ADs
actions.
• Temporary Revision ALI–111, dated We determined that this AD will not None.
January 11, 2011, to Section 4–1, ‘‘Fuel have federalism implications under (c) Applicability
System Limitations,’’ of Part 2, Executive Order 13132. This AD will This AD applies to Bombardier, Inc. Model
‘‘Airworthiness Limitation Items,’’ of not have a substantial direct effect on DHC–8–400, -401, and -402 airplanes,
the Airworthiness Limitation Items the States, on the relationship between certificated in any category, serial numbers
section of Bombardier Q400 Dash 8 the national government and the States, 4001, and 4003 through 4417 inclusive.
Maintenance Requirements Manual or on the distribution of power and (d) Subject
PSM 1–84–7, which describes updates responsibilities among the various
to the fuel system limitations for Air Transport Association (ATA) of
levels of government. America Code 28, Fuel.
inspections of the Teflon sleeve on the For the reasons discussed above, I
fuel tank vent lines. certify that this AD: (e) Reason
• Temporary Revision ALI–112, dated 1. Is not a ‘‘significant regulatory This AD was prompted by reports of
January 11, 2011, to Section 5–1, action’’ under Executive Order 12866; chafing of the fuel lines due to contact with
‘‘Critical Design Configuration Control 2. Is not a ‘‘significant rule’’ under the the surrounding structures in the fuel tank.
Limitations,’’ of Part 2, ‘‘Airworthiness DOT Regulatory Policies and Procedures We are issuing this AD to prevent chafing of
asabaliauskas on DSK5VPTVN1PROD with RULES
Limitation Items,’’ of the Airworthiness (44 FR 11034, February 26, 1979); the fuel lines in the fuel tank, which could
Limitation Items section of Bombardier 3. Will not affect intrastate aviation in result in potential ignition sources in the fuel
Q400 Dash 8 Maintenance Requirements Alaska; and tank in the event of a lightning strike and
Manual PSM 1–84–7, which describes 4. Will not have a significant consequent fire or explosion.
updates to the critical design economic impact, positive or negative, (f) Compliance
configuration control limitations on on a substantial number of small entities Comply with this AD within the
Teflon protective sleeves on fuel vent under the criteria of the Regulatory compliance times specified, unless already
lines inside the fuel tanks. Flexibility Act. done.
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![Federal Register / Vol. 80, No. 170 / Wednesday, September 2, 2015 / Rules and Regulations 52959
(2) Service information identified in this DEPARTMENT OF COMMERCE benefits of available regulatory
AD that is not incorporated by reference is alternatives and, if regulation is
available at the addresses specified in Bureau of Industry and Security necessary, to select regulatory
paragraphs (q)(3) and (q)(4) of this AD. approaches that maximize net benefits
(q) Material Incorporated by Reference
15 CFR Parts 730, 732, 734, 736, 738, (including potential economic,
740, 742, 743, 744, 746, 747, 748, 750, environmental, public health and safety
(1) The Director of the Federal Register 752, 754, 756, 758, 760, 762, 764, 766, effects, distributive impacts, and
approved the incorporation by reference 768, 770, 772, and 774 equity). This rule does not impose any
(IBR) of the service information listed in this
[Docket No. 150813713–5713–01 ] regulatory burden on the public and is
paragraph under 5 U.S.C. 552(a) and 1 CFR
consistent with the goals of Executive
part 51. RIN 0694–AG71 Order 13563. This rule has been
(2) You must use this service information
determined to be not significant for
as applicable to do the actions required by Updated Statements of Legal Authority purposes of Executive Order 12866.
this AD, unless this AD specifies otherwise. for the Export Administration
(i) Bombardier Service Bulletin 84–28–09, Regulations To Include August 7, 2015 2. Notwithstanding any other
Revision D, dated January 29, 2013. Extension of Emergency Declared in provision of law, no person is required
(ii) Bombardier Service Bulletin 84–28–10, Executive Order 13222 to respond to, nor shall any person be
Revision B, dated March 19, 2013. subject to a penalty for failure to comply
(iii) Bombardier Service Bulletin 84–28–13, AGENCY: Bureau of Industry and with, a collection of information subject
dated August 17, 2012. Security, Commerce. to the requirements of the Paperwork
(iv) Bombardier Service Bulletin 84–28–14, ACTION: Final rule. Reduction Act of 1995 (44 U.S.C. 3501
Revision A, dated June 9, 2014. et seq.) (PRA), unless that collection of
(v) Bombardier Service Bulletin 84–28–15, SUMMARY: This rule updates the Code of information displays a currently valid
dated August 17, 2012. Federal Regulations (CFR) legal Office of Management and Budget
(vi) Bombardier Temporary Revision ALI– authority paragraphs in the Export (OMB) Control Number. This rule does
111, dated January 11, 2011, to Section 4–1, Administration Regulations (EAR) to not involve any collection of
‘‘Fuel System Limitations,’’ of Part 2, cite the most recent Presidential notice information.
‘‘Airworthiness Limitation Items,’’ of the extending an emergency declared 3. This rule does not contain policies
Airworthiness Limitation Items section of pursuant to the International Emergency with Federalism implications as that
Bombardier Q400 Dash 8 Maintenance Economic Powers Act. This is a term is defined under Executive Order
Requirements Manual PSM 1–84–7. procedural rule that only updates 13132.
(vii) Bombardier Temporary Revision ALI– authority paragraphs of the EAR. It does
not alter any right, obligation or 4. The Department finds that there is
112, dated January 11, 2011, to Section 5–1,
prohibition that applies to any person good cause under 5 U.S.C. 553(b)(B) to
‘‘Critical Design Configuration Control
Limitations,’’ of Part 2, ‘‘Airworthiness under the EAR. waive the provisions of the
Limitation Items,’’ of the Airworthiness
Administrative Procedure Act requiring
DATES: The rule is effective September
Limitation Items section of Bombardier Q400
prior notice and the opportunity for
2, 2015. public comment because they are
Dash 8 Maintenance Requirements Manual FOR FURTHER INFORMATION CONTACT:
PSM 1–84–7. unnecessary. This rule only updates
William Arvin, Regulatory Policy legal authority citations. It clarifies
(3) For service information identified in Division, Bureau of Industry and
this AD, contact Bombardier, Inc., Q-Series information and is non-discretionary.
Security, Telephone: (202) 482–2440. This rule does not alter any right,
Technical Help Desk, 123 Garratt Boulevard,
SUPPLEMENTARY INFORMATION: obligation or prohibition that applies to
Toronto, Ontario M3K 1Y5, Canada;
telephone 416–375–4000; fax 416–375–4539; Background any person under the EAR. Because
email thd.qseries@aero.bombardier.com; these revisions are not substantive
Authority for all parts of the EAR changes, it is unnecessary to provide
Internet http://www.bombardier.com.
(4) You may view this service information
other than part 745 rests, in part, on notice and opportunity for public
at the FAA, Transport Airplane Directorate,
Executive Order 13222 of August 17, comment. In addition, the 30-day delay
1601 Lind Avenue SW., Renton, WA. For
2001—National Emergency with in effectiveness otherwise required by 5
information on the availability of this Respect to Export Control Regulations, U.S.C. 553(d) is not applicable because
material at the FAA, call 425–227–1221. 66 FR 44025, 3 CFR, 2001 Comp., p. 783 this rule is not a substantive rule.
(5) You may view this service information and on annual notices extending the Because neither the Administrative
that is incorporated by reference at the emergency declared in that executive Procedure Act nor any other law
National Archives and Records order. This rule revises the authority requires that notice of proposed
Administration (NARA). For information on paragraphs for the affected parts to cite rulemaking and an opportunity for
the availability of this material at NARA, call the most recent such notice, which the public comment be given for this rule,
202–741–6030, or go to http:// President signed on August 7, 2015. the analytical requirements of the
www.archives.gov/federal-register/cfr/ibr- This rule is purely procedural, and Regulatory Flexibility Act (5 U.S.C. 601
locations.html. makes no changes other than to revise et seq.) are not applicable. Accordingly,
CFR authority paragraphs for the no Final Regulatory Flexibility Analysis
Issued in Renton, Washington, on August purpose of making the authority
21, 2015. is required and none has been prepared.
citations current. It does not change the
asabaliauskas on DSK5VPTVN1PROD with RULES
Kevin Hull, text of any section of the EAR, nor does List of Subjects
Acting Manager, Transport Airplane it alter any right, obligation or 15 CFR Part 730
Directorate, Aircraft Certification Service. prohibition that applies to any person
[FR Doc. 2015–21472 Filed 9–1–15; 8:45 am] under the EAR. Administrative practice and
BILLING CODE 4910–13–P
procedure, Advisory committees,
Rulemaking Requirements Exports, Reporting and recordkeeping
1. Executive Orders 13563 and 12866 requirements, Strategic and critical
direct agencies to assess all costs and materials.
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Document Created: 2018-02-26 10:10:32
Document Modified: 2018-02-26 10:10:32
| 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. | |
| Dates | This AD becomes effective October 7, 2015. | |
| Contact | Kent Fredrickson, Aerospace Engineer, Propulsion and Services Branch, ANE-173, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7364; fax 516-794-5531. | |
| FR Citation | 80 FR 52955 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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