81 FR 34864 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 105 (June 1, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 105 (June 1, 2016)
| Page Range | 34864-34867 | |
| FR Document | 2016-12331 |
[Federal Register Volume 81, Number 105 (Wednesday, June 1, 2016)] [Rules and Regulations] [Pages 34864-34867] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-12331] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0496; Directorate Identifier 2014-NM-101-AD; Amendment 39-18533; AD 2016-11-06] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are superseding Airworthiness Directive (AD) 2005-18-18 for certain The Boeing Company Model 757 airplanes. AD 2005-18-18 required inspections of certain wire bundles in the left and right engine-to- wing aft fairings for discrepancies; installation of back-to-back p- clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and associated re-routing of the wire bundles, if necessary. This new AD also requires an installation of spiral cable wrap on fuel shutoff valve (FSV) wires at the aft end of the strut, for both left and right engines, and related investigative and corrective actions. This AD was prompted by a determination that the service information referenced in AD 2005-18-18 did not adequately address FSV wires at the aft end of the struts. We are issuing this AD to prevent chafing between the wire bundle and the structure of the aft fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and a possible uncontrollable fire. DATES: This AD is effective July 6, 2016. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of July 6, 2016. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of October 14, 2005 (70 FR 53554, September 9, 2005). ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA 98057. For information on the availability of this material at the 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-2015-0496. 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- 0496; 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 address for the Docket Office (phone: 800-647- 5527) is 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 20590. FOR FURTHER INFORMATION CONTACT: William Bond, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5253; fax: 562-627-5210; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2005-18-18, Amendment 39-14258 (70 FR 53554, September 9, 2005) (``AD 2005-18-18''). AD 2005-18-18 applied to certain The Boeing Company Model 757-200, -200PF, -200CB, and -300 series airplanes. The NPRM published in the Federal Register on March 27, 2015 (80 FR 16318) (``the NPRM''). The NPRM was prompted by a report that the service information referenced in AD 2005-18-18 did not adequately address FSV wires at the aft end of the strut, for both left and right engine struts. The NPRM proposed to continue to require inspections of certain wire bundles in the left and right engine-to- wing aft fairings for discrepancies; installation of back-to-back p- clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and associated re-routing of the wire bundles, if necessary. The NPRM also proposed to require installation of tetrafluoroethylene spiral cable wrap on the FSV wires at the aft end of the strut that would provide additional wiring protection. We are issuing this AD to prevent chafing between the wire bundle and the structure of the aft [[Page 34865]] fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and a possible uncontrollable fire. Comments We gave the public the opportunity to participate in developing this AD. The following presents the comments received on the NPRM and the FAA's response to each comment. Request To Clarify Certain Requirements Boeing requested clarification of the actions required by paragraph (g) of the proposed AD. Boeing suggested that paragraph (g) of the proposed AD be revised to add a statement to clarify that no further work would be required if the requirements of AD 2005-18-18 have already been accomplished. We agree to provide clarification. In paragraph (g) of this AD, we restated the requirements of paragraph (f) of AD 2005-18-18. Paragraph (f) of this AD states, ``Comply with this AD within the compliance times specified, unless already done.'' If operators have already done the actions required by paragraph (f) of AD 2005-18-18, they have already done the actions required by paragraph (g) of this AD. If operators have not already done the actions required by paragraph (g) of this AD before the effective date of the AD, then they must use the most recent revision of the service information. We have not changed this AD in this regard. Request To Clarify Certain Compliance Time Requirements Boeing requested clarification of the compliance times stated in paragraph (h) of the proposed AD. Boeing stated that there is confusion between ``Within 60 months after the effective date of this AD . . . ,'' as stated in the first sentence of the paragraph for the spiral cable wrap installation, and ``. . . before further flight,'' as stated in the second sentence for the related investigative and corrective actions. Boeing suggested that the second sentence be deleted from paragraph (h) of the proposed AD. We do not agree to revise paragraph (h) of this AD. The installation of the spiral cable wrap includes related investigative and corrective actions, i.e., doing inspections for damaged wire bundles, repairing damaged wires, and testing certain fuel shutoff wires. These related investigative and corrective actions must be done before further flight after damage is found. We have not changed the AD in this regard. Request To Provide Credit for Required Service Information FedEx requested that the proposed AD be revised to add a paragraph granting credit for accomplishing Boeing Service Bulletin 757-28A0073 or 757-28A0074, both Revision 2, both dated June 4, 2009, before the effective date of the AD. FedEx stated that they had already accomplished the requirements on airplanes in their fleet. We agree to clarify. The intent of paragraph (f) of this AD is to provide relief for accomplishing the requirements of this AD before the effective date of this AD. Therefore, this AD already includes the credit requested by the commenter. We have not changed this AD in this regard. Request To Allow Credit for Previous AMOC Approvals United Airlines (UAL) requested that a paragraph be added to the proposed AD to allow credit for all previously approved AMOC letters that affect Boeing Service Bulletin 757-28A0073 or 757-28A0074. We do not agree to add a new paragraph to this AD. Credit is already provided in paragraph (i)(4) of this AD, which specifies that AMOCs approved for AD 2005-18-18 are also acceptable as AMOCs for the corresponding provisions of paragraph (g) of this AD. (Paragraph (g) of this AD restates the requirements of paragraph (f) of AD 2005-18-18.) Paragraph (h) of this AD is a new requirement and AMOCs cannot be approved for that paragraph until this AD is published. We have not changed this AD in this regard. Request To Provide Relief for Model 757-300 Airplanes Similar to Relief Provided to Model 757-200 Airplanes UAL requested relief for Model 757-300 airplanes that is similar to that provided to the Model 757-200 airplanes in FAA AMOC letter 757- 28A0073-AMOC-01. We agree. The issue that the AMOC letter addresses (for Boeing Service Bulletin 757-28A0073, Revision 2, dated June 4, 2009) also exists in Boeing Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009. We have revised paragraphs (g) and (h) of this AD to include a statement that where Boeing Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009, states ``SWPM 20-10-11, Table IX,'' this AD instead requires ``SWPM 20-10-11, `Minimum Clearance' Table.'' Request To Incorporate Proposed AD Requirements Into the Maintenance Planning Data (MPD) Document UAL requested that the proposed AD be revised to require incorporation of a required repetitive inspection of the modification into the MPD requirements for Model 757 Heavy Check intervals, preferably at intervals of 3,000 flight cycles or 20 months. UAL suggested that this addition to the MPD could ensure the long-term integrity of the modification. We do not agree to require a revision to the MPD. We infer that the term ``modification'' used by UAL is intended to refer to the corrective actions required by paragraph (g) of this AD, and the cable wrap installation and related investigative and corrective actions required by paragraph (h) of this AD. These actions required by paragraphs (g) and (h) of this AD are considered to provide long-term integrity of the ``modification'' and maintain an acceptable level of safety. However, we encourage operators to proactively revise their maintenance programs in accordance with FAA regulations to address problems or issues as they arise. We have not changed this AD in this regard. Effect of Winglets on Accomplishment of the Proposed Actions Aviation Partners Boeing (APB) stated that the installation of winglets per Supplemental Type Certificate (STC) ST01518SE (http:// rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/ 312bc296830a925c86257c85006d1b1f/$FILE/ST01518SE.pdf) does not affect accomplishment of the manufacturer's service instructions. We agree with the commenter that STC ST01518SE (http://rgl.faa.gov/ Regulatory_and_Guidance_Library/rgstc.nsf/0/ 312bc296830a925c86257c85006d1b1f/$FILE/ST01518SE.pdf) does not affect the accomplishment of the manufacturer's service instructions. Therefore, the installation of STC ST01518SE does not affect the ability to accomplish the actions required by this AD. We have not changed this AD in this regard. Change Made to the Format of Paragraph (g) of This AD We have revised the format of paragraph (g) of this AD by converting Table 1 to paragraph (g)(1) to text in paragraph (g). This change to the format does not affect the requirements of paragraphs (g), (g)(1), or (g)(2) of this AD. [[Page 34866]] 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:Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. 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 We reviewed Boeing Alert Service Bulletins 757-28A0073 and 757- 28A0074, both Revision 2, both dated June 4, 2009. The service information describes procedures for inspecting certain wire bundles in the left and right engine-to-wing aft fairings for discrepancies; installing back-to-back p-clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; associated re-routing of the wire bundles, if necessary; and installing spiral cable wrap on FSV wires on the aft ends of the left and right engine struts, and related investigative and corrective actions. 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. Costs of Compliance We estimate that this AD affects 346 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Parts cost Cost per product Cost on U.S. operators ---------------------------------------------------------------------------------------------------------------- Inspection of certain wire Between 16 and 44 $600 Between $1,960 Between $678,160 and bundles, and p-clamp work-hours x $85 and $4,340. $1,501,640 installation [retained actions per hour = from AD 2005-18-18]. Between $1,360 and $3,740. Installation of spiral cable 10 work-hours x $10 $860............. $297,560 wrap [new action]. $85 per hour = $850. ---------------------------------------------------------------------------------------------------------------- Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, Section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701, ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We have determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (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) 2005-18-18, Amendment 39-14258 (70 FR 53554, September 9, 2005), and adding the following new AD: 2016-11-06 The Boeing Company: Amendment 39-18533; Docket No. FAA- 2015-0496; Directorate Identifier 2014-NM-101-AD. (a) Effective Date This AD is effective July 6, 2016. (b) Affected ADs This AD replaces AD 2005-18-18, Amendment 39-14258 (70 FR 53554, September 9, 2005) (``AD 2005-18-18''). (c) Applicability This AD applies to The Boeing Company Model 757-200, -200PF, - 200CB, and -300 series airplanes; certificated in any category; equipped with Rolls-Royce engines; as identified in Boeing Alert Service Bulletins 757-28A0073 and 757-28A0074, both Revision 2, both dated June 4, 2009. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. (e) Unsafe Condition This AD was prompted by a report that the service information referenced in AD 2005-18-18, did not adequately address fuel shutoff valve (FSV) wires at the aft end of the strut, for both left and right engine struts. We are issuing this AD to prevent chafing between the wire bundle and the structure of the aft fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and a possible uncontrollable fire. (f) Compliance Comply with this AD within the compliance times specified, unless already done. [[Page 34867]] (g) Retained One-Time Inspections/Related Investigative and Corrective Actions, With New Service Information and an Exception to Certain Service Information This paragraph restates the requirements of paragraph (f) of AD 2005-18-18, with new service information and an exception to certain service information. Within 60 months after October 14, 2005 (the effective date of AD 2005-18-18), do the actions required by paragraphs (g)(1) and (g)(2) of this AD. Where Boeing Alert Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009, states ``SWPM 20-10-11, Table IX,'' the correct phrase is ``SWPM 20-10-11, `Minimum Clearance' Table.'' (1) Accomplish the detailed inspections for discrepancies of the wire bundles in the left and right engine-to-wing aft fairings, and applicable and related investigative and corrective actions if necessary, as applicable, by doing all the actions specified in the Accomplishment Instructions of the applicable service bulletins listed in paragraphs (g)(1)(i) and (g)(1)(ii) of this AD. As of the effective date of this AD, use only Boeing Alert Service Bulletin 757-28A0073 or 757-28A0074, both Revision 2, both dated June 4, 2009, as applicable. Accomplish any related investigative and corrective actions before further flight, in accordance with the applicable service bulletin. For the purposes of this AD, a detailed inspection is: ``An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.'' (i) For Boeing Model 757-200, -200CB, and -200PF series airplanes, use the service information identified in paragraphs (g)(1)(i)(A), (g)(1)(i)(B), and (g)(1)(i)(C) of this AD. (A) Boeing Alert Service Bulletin 757-28A0073, dated November 20, 2003; (B) Boeing Alert Service Bulletin 757-28A0073, Revision 1, dated February 24, 2005. (C) Boeing Alert Service Bulletin 757-28A0073, Revision 2, dated June 4, 2009. (ii) For Boeing Model 757-300 series airplanes, use the service information identified in paragraphs (g)(1)(ii)(A), (g)(1)(ii)(B), and (g)(1)(ii)(C) of this AD. (A) Boeing Alert Service Bulletin 757-28A0074, dated November 20, 2003. (B) Boeing Alert Service Bulletin 757-28A0074, Revision 1, dated February 24, 2005. (C) Boeing Alert Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009. (2) Install back-to-back p-clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and re- route the wire bundles, if necessary; by doing all the applicable actions specified in the Accomplishment Instructions of the applicable service information identified in paragraphs (g)(2)(i) through (g)(2)(iv) of this AD. As of the effective date of this AD, use only the service information identified in paragraphs (g)(2)(ii) and (g)(2)(iv) of this AD, as applicable. (i) Boeing Alert Service Bulletin 757-28A0073, Revision 1, dated February 24, 2005. (ii) Boeing Alert Service Bulletin 757-28A0073, Revision 2, dated June 4, 2009. (iii) Boeing Alert Service Bulletin 757-28A0074, Revision 1, dated February 24, 2005. (iv) Boeing Alert Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009. (h) New Spiral Cable Wrap Installation Within 60 months after the effective date of this AD, install spiral cable wrap on FSV wires at the aft end of the strut, for both left and right engines, and do all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 757-28A0073 (for Model 757-200, -200CB, and -200PF series airplanes) or 757-28A0074 (for Model 757-300 series airplanes), both Revision 2, both dated June 4, 2009. Where Boeing Alert Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009, states ``SWPM 20-10-11, Table IX,'' the correct phrase is ``SWPM 20-10-11, `Minimum Clearance' Table.'' Do all applicable related investigative and corrective actions before further flight. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Los Angeles Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 manager of the ACO, send it to the attention of the person identified in paragraph (j) of this AD. Information may be emailed to: [email protected]. (2) 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. (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Los Angeles ACO, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (4) AMOCs approved for AD 2005-18-18 are approved as AMOCs for the corresponding provisions of paragraph (g) of this AD. (j) Related Information For more information about this AD, contact William Bond, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles ACO, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562- 627-5253; fax: 562-627-5210; email: [email protected]. (k) 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 the AD specifies otherwise. (3) The following service information was approved for IBR on July 6, 2016. (i) Boeing Alert Service Bulletin 757-28A0073, Revision 2, dated June 4, 2009. (ii) Boeing Alert Service Bulletin 757-28A0074, Revision 2, dated June 4, 2009. (4) The following service information was approved for IBR on October 14, 2005 (70 FR 53554, September 9, 2005). (i) Boeing Alert Service Bulletin 757-28A0073, dated November 20, 2003. (ii) Boeing Alert Service Bulletin 757-28A0073, Revision 1, dated February 24, 2005. (iii) Boeing Alert Service Bulletin 757-28A0074, dated November 20, 2003. (iv) Boeing Alert Service Bulletin 757-28A0074, Revision 1, dated February 24, 2005. (5) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544- 5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet.com. (6) 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. (7) 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 May 17, 2016. Dionne Palermo, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-12331 Filed 5-31-16; 8:45 am] BILLING CODE 4910-13-P
![34864 Federal Register / Vol. 81, No. 105 / Wednesday, June 1, 2016 / Rules and Regulations
adding in its place ‘‘paragraph (c) of this DEPARTMENT OF TRANSPORTATION material at the FAA, call 425–227–1221.
section’’. It is also available on the Internet at
Federal Aviation Administration http://www.regulations.gov by searching
PART 114—CORPORATE AND LABOR for and locating Docket No. FAA–2015–
ORGANIZATION ACTIVITY 14 CFR Part 39 0496.
[Docket No. FAA–2015–0496; Directorate Examining the AD Docket
■ 18. The authority citation for part 114 Identifier 2014–NM–101–AD; Amendment
continues to read as follows: 39–18533; AD 2016–11–06] You may examine the AD docket on
the Internet at http://
Authority: 52 U.S.C. 30101(8), 30101(9), RIN 2120–AA64 www.regulations.gov by searching for
30102, 30104, 30107(a)(8), 30111(a)(8),
and locating Docket No. FAA–2015–
30118. Airworthiness Directives; The Boeing
0496; or in person at the Docket
Company Airplanes
§ 114.2 [Amended] Management Facility between 9 a.m.
AGENCY: Federal Aviation and 5 p.m., Monday through Friday,
■ 19. Amend the note to paragraph (b) Administration (FAA), DOT. except Federal holidays. The AD docket
of § 114.2 by removing all references to ACTION: Final rule. contains this AD, the regulatory
‘‘non-connected’’ and adding in their evaluation, any comments received, and
place ‘‘nonconnected’’. SUMMARY: We are superseding other information. The address for the
Airworthiness Directive (AD) 2005–18– Docket Office (phone: 800–647–5527) is
§ 114.10 [Amended] 18 for certain The Boeing Company Docket Management Facility, U.S.
Model 757 airplanes. AD 2005–18–18 Department of Transportation, Docket
■ 20. Amend the note to paragraph (a)
required inspections of certain wire Operations, M–30, West Building
of § 114.10 by removing all references to bundles in the left and right engine-to- Ground Floor, Room W12–140, 1200
‘‘non-connected’’ and adding in their wing aft fairings for discrepancies; New Jersey Avenue SE., Washington,
place ‘‘nonconnected’’. installation of back-to-back p-clamps DC 20590.
between the wire and hydraulic supply FOR FURTHER INFORMATION CONTACT:
PART 9004—ENTITLEMENT OF
tube at the aft end of the right-hand strut William Bond, Aerospace Engineer,
ELIGIBLE CANDIDATES TO only; and associated re-routing of the
PAYMENTS; USE OF PAYMENTS Propulsion Branch, ANM–140L, FAA,
wire bundles, if necessary. This new AD Los Angeles Aircraft Certification Office
also requires an installation of spiral (ACO), 3960 Paramount Boulevard,
■ 21. The authority citation for part cable wrap on fuel shutoff valve (FSV) Lakewood, CA 90712–4137; phone:
9004 continues to read as follows: wires at the aft end of the strut, for both 562–627–5253; fax: 562–627–5210;
Authority: 26 U.S.C. 9004 and 9009(b). left and right engines, and related email: william.bond@faa.gov.
investigative and corrective actions.
SUPPLEMENTARY INFORMATION:
§ 9004.6 [Amended] This AD was prompted by a
determination that the service Discussion
■ 22. Amend the subject heading to information referenced in AD 2005–18–
paragraph (c) introductory text of We issued a notice of proposed
18 did not adequately address FSV rulemaking (NPRM) to amend 14 CFR
§ 9004.6 by removing ‘‘Deducation’’ and wires at the aft end of the struts. We are
adding in its place ‘‘Deduction’’. part 39 to supersede AD 2005–18–18,
issuing this AD to prevent chafing Amendment 39–14258 (70 FR 53554,
between the wire bundle and the September 9, 2005) (‘‘AD 2005–18–18’’).
PART 9034—ENTITLEMENTS structure of the aft fairing, which could AD 2005–18–18 applied to certain The
result in electrical arcing and Boeing Company Model 757–200,
■ 23. The authority citation for part subsequent ignition of flammable vapors
9034 continues to read as follows: –200PF, –200CB, and –300 series
and a possible uncontrollable fire. airplanes. The NPRM published in the
Authority: 26 U.S.C. 9034 and 9039(b). DATES: This AD is effective July 6, 2016. Federal Register on March 27, 2015 (80
The Director of the Federal Register FR 16318) (‘‘the NPRM’’). The NPRM
§ 9034.2 [Amended] approved the incorporation by reference was prompted by a report that the
■ 24. Amend paragraph (c)(1)(iii) of of certain publications listed in this AD service information referenced in AD
§ 9034.2 by removing ‘‘11 CFR 110.1 (1), as of July 6, 2016. 2005–18–18 did not adequately address
(3), (5), and (6)’’ and adding in its place The Director of the Federal Register FSV wires at the aft end of the strut, for
approved the incorporation by reference both left and right engine struts. The
‘‘11 CFR 110.1(l)(3), (5), and (6)’’.
of certain other publications listed in NPRM proposed to continue to require
On behalf of the Commission, this AD as of October 14, 2005 (70 FR inspections of certain wire bundles in
Dated: May 23, 2016. 53554, September 9, 2005). the left and right engine-to-wing aft
Matthew S. Petersen, ADDRESSES: For service information fairings for discrepancies; installation of
Chairman, Federal Election Commission. identified in this final rule, contact back-to-back p-clamps between the wire
[FR Doc. 2016–12661 Filed 5–31–16; 8:45 am] Boeing Commercial Airplanes, and hydraulic supply tube at the aft end
Attention: Data & Services Management, of the right-hand strut only; and
BILLING CODE 6715–01–P
P.O. Box 3707, MC 2H–65, Seattle, WA associated re-routing of the wire
98124–2207; telephone 206–544–5000, bundles, if necessary. The NPRM also
sradovich on DSK3TPTVN1PROD with RULES
extension 1; fax 206–766–5680; Internet proposed to require installation of
https://www.myboeingfleet.com. You tetrafluoroethylene spiral cable wrap on
may view this referenced service the FSV wires at the aft end of the strut
information at the FAA, Transport that would provide additional wiring
Airplane Directorate, 1601 Lind Avenue protection. We are issuing this AD to
SW., Renton, WA 98057. For prevent chafing between the wire
information on the availability of this bundle and the structure of the aft
VerDate Sep<11>2014 16:11 May 31, 2016 Jkt 238001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\01JNR1.SGM 01JNR1](https://thefederalregister.org/doc/81_FR_34969/page/1.svg)
![34866 Federal Register / Vol. 81, No. 105 / Wednesday, June 1, 2016 / Rules and Regulations
Conclusion burden on any operator or increase the the wire bundles, if necessary; and
We reviewed the relevant data, scope of this AD. installing spiral cable wrap on FSV
considered the comments received, and wires on the aft ends of the left and right
Related Service Information Under 1
determined that air safety and the engine struts, and related investigative
CFR Part 51
public interest require adopting this AD and corrective actions. This service
with the changes described previously We reviewed Boeing Alert Service information is reasonably available
and minor editorial changes. We have Bulletins 757–28A0073 and 757– because the interested parties have
determined that these minor changes: 28A0074, both Revision 2, both dated access to it through their normal course
• Are consistent with the intent that June 4, 2009. The service information of business or by the means identified
was proposed in the NPRM for describes procedures for inspecting in the ADDRESSES section.
correcting the unsafe condition; and certain wire bundles in the left and right Costs of Compliance
• Do not add any additional burden engine-to-wing aft fairings for
upon the public than was already discrepancies; installing back-to-back p- We estimate that this AD affects 346
proposed in the NPRM. clamps between the wire and hydraulic airplanes of U.S. registry.
We also determined that these supply tube at the aft end of the right- We estimate the following costs to
changes will not increase the economic hand strut only; associated re-routing of comply with this AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Inspection of certain wire bundles, and p-clamp in- Between 16 and 44 $600 Between $1,960 and Between $678,160
stallation [retained actions from AD 2005–18–18]. work-hours × $85 per $4,340. and $1,501,640
hour = Between
$1,360 and $3,740.
Installation of spiral cable wrap [new action] .......... 10 work-hours × $85 per $10 $860 ............................... $297,560
hour = $850.
Authority for This Rulemaking (2) Is not a ‘‘significant rule’’ under (a) Effective Date
Title 49 of the United States Code DOT Regulatory Policies and Procedures This AD is effective July 6, 2016.
specifies the FAA’s authority to issue (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation (b) Affected ADs
rules on aviation safety. Subtitle I,
in Alaska, and This AD replaces AD 2005–18–18,
Section 106, describes the authority of
(4) Will not have a significant Amendment 39–14258 (70 FR 53554,
the FAA Administrator. Subtitle VII,
economic impact, positive or negative, September 9, 2005) (‘‘AD 2005–18–18’’).
Aviation Programs, describes in more
detail the scope of the Agency’s on a substantial number of small entities (c) Applicability
authority. under the criteria of the Regulatory
This AD applies to The Boeing Company
We are issuing this rulemaking under Flexibility Act.
Model 757–200, –200PF, –200CB, and –300
the authority described in Subtitle VII, List of Subjects in 14 CFR Part 39 series airplanes; certificated in any category;
Part A, Subpart III, Section 44701, equipped with Rolls-Royce engines; as
‘‘General requirements.’’ Under that Air transportation, Aircraft, Aviation
identified in Boeing Alert Service Bulletins
section, Congress charges the FAA with safety, Incorporation by reference,
757–28A0073 and 757–28A0074, both
promoting safe flight of civil aircraft in Safety.
Revision 2, both dated June 4, 2009.
air commerce by prescribing regulations Adoption of the Amendment
for practices, methods, and procedures (d) Subject
the Administrator finds necessary for Accordingly, under the authority Air Transport Association (ATA) of
safety in air commerce. This regulation delegated to me by the Administrator, America Code 28, Fuel.
is within the scope of that authority the FAA amends 14 CFR part 39 as
follows: (e) Unsafe Condition
because it addresses an unsafe condition
that is likely to exist or develop on This AD was prompted by a report that the
PART 39—AIRWORTHINESS service information referenced in AD 2005–
products identified in this rulemaking
DIRECTIVES 18–18, did not adequately address fuel
action.
shutoff valve (FSV) wires at the aft end of the
Regulatory Findings ■ 1. The authority citation for part 39 strut, for both left and right engine struts. We
We have determined that this AD will continues to read as follows: are issuing this AD to prevent chafing
not have federalism implications under Authority: 49 U.S.C. 106(g), 40113, 44701. between the wire bundle and the structure of
Executive Order 13132. This AD will the aft fairing, which could result in
§ 39.13 [Amended] electrical arcing and subsequent ignition of
not have a substantial direct effect on
the States, on the relationship between ■ 2. The FAA amends § 39.13 by flammable vapors and a possible
the national government and the States, removing Airworthiness Directive (AD) uncontrollable fire.
sradovich on DSK3TPTVN1PROD with RULES
or on the distribution of power and 2005–18–18, Amendment 39–14258 (70 (f) Compliance
responsibilities among the various FR 53554, September 9, 2005), and
Comply with this AD within the
levels of government. adding the following new AD:
compliance times specified, unless already
For the reasons discussed above, I 2016–11–06 The Boeing Company: done.
certify that this AD: Amendment 39–18533; Docket No.
(1) Is not a ‘‘significant regulatory FAA–2015–0496; Directorate Identifier
action’’ under Executive Order 12866, 2014–NM–101–AD.
VerDate Sep<11>2014 16:11 May 31, 2016 Jkt 238001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\01JNR1.SGM 01JNR1](https://thefederalregister.org/doc/81_FR_34969/page/3.svg)
![Federal Register / Vol. 81, No. 105 / Wednesday, June 1, 2016 / Rules and Regulations 34867
(g) Retained One-Time Inspections/Related (i) Boeing Alert Service Bulletin 757– (k) Material Incorporated by Reference
Investigative and Corrective Actions, With 28A0073, Revision 1, dated February 24, (1) The Director of the Federal Register
New Service Information and an Exception 2005. approved the incorporation by reference
to Certain Service Information (ii) Boeing Alert Service Bulletin 757– (IBR) of the service information listed in this
This paragraph restates the requirements of 28A0073, Revision 2, dated June 4, 2009. paragraph under 5 U.S.C. 552(a) and 1 CFR
paragraph (f) of AD 2005–18–18, with new (iii) Boeing Alert Service Bulletin 757– part 51.
service information and an exception to 28A0074, Revision 1, dated February 24, (2) You must use this service information
certain service information. Within 60 2005. as applicable to do the actions required by
months after October 14, 2005 (the effective (iv) Boeing Alert Service Bulletin 757– this AD, unless the AD specifies otherwise.
date of AD 2005–18–18), do the actions 28A0074, Revision 2, dated June 4, 2009. (3) The following service information was
required by paragraphs (g)(1) and (g)(2) of approved for IBR on July 6, 2016.
this AD. Where Boeing Alert Service Bulletin (h) New Spiral Cable Wrap Installation (i) Boeing Alert Service Bulletin 757–
757–28A0074, Revision 2, dated June 4, Within 60 months after the effective date 28A0073, Revision 2, dated June 4, 2009.
2009, states ‘‘SWPM 20–10–11, Table IX,’’ of this AD, install spiral cable wrap on FSV (ii) Boeing Alert Service Bulletin 757–
the correct phrase is ‘‘SWPM 20–10–11, wires at the aft end of the strut, for both left 28A0074, Revision 2, dated June 4, 2009.
‘Minimum Clearance’ Table.’’ and right engines, and do all applicable (4) The following service information was
(1) Accomplish the detailed inspections for related investigative and corrective actions, approved for IBR on October 14, 2005 (70 FR
discrepancies of the wire bundles in the left in accordance with the Accomplishment 53554, September 9, 2005).
and right engine-to-wing aft fairings, and Instructions of Boeing Alert Service Bulletin (i) Boeing Alert Service Bulletin 757–
applicable and related investigative and 757–28A0073 (for Model 757–200, –200CB, 28A0073, dated November 20, 2003.
corrective actions if necessary, as applicable, and –200PF series airplanes) or 757–28A0074 (ii) Boeing Alert Service Bulletin 757–
by doing all the actions specified in the 28A0073, Revision 1, dated February 24,
(for Model 757–300 series airplanes), both
Accomplishment Instructions of the 2005.
Revision 2, both dated June 4, 2009. Where
applicable service bulletins listed in (iii) Boeing Alert Service Bulletin 757–
Boeing Alert Service Bulletin 757–28A0074, 28A0074, dated November 20, 2003.
paragraphs (g)(1)(i) and (g)(1)(ii) of this AD.
Revision 2, dated June 4, 2009, states ‘‘SWPM (iv) Boeing Alert Service Bulletin 757–
As of the effective date of this AD, use only
Boeing Alert Service Bulletin 757–28A0073 20–10–11, Table IX,’’ the correct phrase is 28A0074, Revision 1, dated February 24,
or 757–28A0074, both Revision 2, both dated ‘‘SWPM 20–10–11, ‘Minimum Clearance’ 2005.
June 4, 2009, as applicable. Accomplish any Table.’’ Do all applicable related investigative (5) For service information identified in
related investigative and corrective actions and corrective actions before further flight. this AD, contact Boeing Commercial
before further flight, in accordance with the (i) Alternative Methods of Compliance Airplanes, Attention: Data & Services
applicable service bulletin. For the purposes (AMOCs) Management, P.O. Box 3707, MC 2H–65,
of this AD, a detailed inspection is: ‘‘An Seattle, WA 98124–2207; telephone 206–
intensive examination of a specific item, (1) The Manager, Los Angeles Aircraft 544–5000, extension 1; fax 206–766–5680;
installation, or assembly to detect damage, Certification Office (ACO), FAA, has the Internet https://www.myboeingfleet.com.
failure, or irregularity. Available lighting is authority to approve AMOCs for this AD, if (6) You may view this service information
normally supplemented with a direct source requested using the procedures found in 14 at the FAA, Transport Airplane Directorate,
of good lighting at an intensity deemed CFR 39.19. In accordance with 14 CFR 39.19, 1601 Lind Avenue SW., Renton WA. For
appropriate. Inspection aids such as mirror, send your request to your principal inspector information on the availability of this
magnifying lenses, etc., may be necessary. or local Flight Standards District Office, as material at the FAA, call 425–227–1221.
Surface cleaning and elaborate procedures appropriate. If sending information directly (7) You may view this service information
may be required.’’ to the manager of the ACO, send it to the that is incorporated by reference at the
(i) For Boeing Model 757–200, –200CB, attention of the person identified in National Archives and Records
and –200PF series airplanes, use the service paragraph (j) of this AD. Information may be Administration (NARA). For information on
information identified in paragraphs emailed to: 9-ANM-LAACO-AMOC- the availability of this material at NARA, call
(g)(1)(i)(A), (g)(1)(i)(B), and (g)(1)(i)(C) of this Requests@faa.gov. 202–741–6030, or go to: http://
AD. (2) Before using any approved AMOC, www.archives.gov/federal-register/cfr/ibr-
(A) Boeing Alert Service Bulletin 757– notify your appropriate principal inspector, locations.html.
28A0073, dated November 20, 2003; or lacking a principal inspector, the manager Issued in Renton, Washington, on May 17,
(B) Boeing Alert Service Bulletin 757– of the local flight standards district office/ 2016.
28A0073, Revision 1, dated February 24, certificate holding district office.
2005. Dionne Palermo,
(3) An AMOC that provides an acceptable
(C) Boeing Alert Service Bulletin 757– Acting Manager, Transport Airplane
level of safety may be used for any repair,
28A0073, Revision 2, dated June 4, 2009. Directorate, Aircraft Certification Service.
modification, or alteration required by this
(ii) For Boeing Model 757–300 series [FR Doc. 2016–12331 Filed 5–31–16; 8:45 am]
AD if it is approved by the Boeing
airplanes, use the service information
Commercial Airplanes Organization BILLING CODE 4910–13–P
identified in paragraphs (g)(1)(ii)(A),
Designation Authorization (ODA) that has
(g)(1)(ii)(B), and (g)(1)(ii)(C) of this AD.
(A) Boeing Alert Service Bulletin 757– been authorized by the Manager, Los Angeles
28A0074, dated November 20, 2003. ACO, to make those findings. To be DEPARTMENT OF TRANSPORTATION
(B) Boeing Alert Service Bulletin 757– approved, the repair method, modification
28A0074, Revision 1, dated February 24, deviation, or alteration deviation must meet Federal Aviation Administration
2005. the certification basis of the airplane, and the
(C) Boeing Alert Service Bulletin 757– approval must specifically refer to this AD. 14 CFR Part 39
28A0074, Revision 2, dated June 4, 2009. (4) AMOCs approved for AD 2005–18–18
are approved as AMOCs for the [Docket No. FAA–2015–1273; Directorate
(2) Install back-to-back p-clamps between
corresponding provisions of paragraph (g) of Identifier 2014–NM–194–AD; Amendment
the wire and hydraulic supply tube at the aft
this AD. 39–18530; AD 2016–11–03]
end of the right-hand strut only; and re-route
the wire bundles, if necessary; by doing all RIN 2120–AA64
(j) Related Information
sradovich on DSK3TPTVN1PROD with RULES
the applicable actions specified in the
Accomplishment Instructions of the For more information about this AD, Airworthiness Directives; The Boeing
applicable service information identified in contact William Bond, Aerospace Engineer,
Company Airplanes
paragraphs (g)(2)(i) through (g)(2)(iv) of this Propulsion Branch, ANM–140L, FAA, Los
AD. As of the effective date of this AD, use Angeles ACO, 3960 Paramount Boulevard, AGENCY: Federal Aviation
only the service information identified in Lakewood, CA 90712–4137; phone: 562–627– Administration (FAA), DOT.
paragraphs (g)(2)(ii) and (g)(2)(iv) of this AD, 5253; fax: 562–627–5210; email:
ACTION: Final rule.
as applicable. william.bond@faa.gov.
VerDate Sep<11>2014 16:11 May 31, 2016 Jkt 238001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\01JNR1.SGM 01JNR1](https://thefederalregister.org/doc/81_FR_34969/page/4.svg)
Document Created: 2018-02-08 07:27:29
Document Modified: 2018-02-08 07:27:29
| 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 is effective July 6, 2016. | |
| Contact | William Bond, Aerospace Engineer, Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification Office (ACO), 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627-5253; fax: 562-627-5210; email: [email protected] | |
| FR Citation | 81 FR 34864 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR