82 FR 39344 - Airworthiness Directives; The Boeing Company Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 159 (August 18, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 159 (August 18, 2017)
| Page Range | 39344-39347 | |
| FR Document | 2017-16354 |
[Federal Register Volume 82, Number 159 (Friday, August 18, 2017)] [Rules and Regulations] [Pages 39344-39347] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-16354] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9112; Product Identifier 2016-NM-091-AD; Amendment 39-18982; AD 2017-16-05] RIN 2120-AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by a report of a Krueger flap bullnose departing an airplane during taxi, which caused damage to the wing structure and thrust reverser. This AD requires a one-time detailed visual inspection for discrepancies in the Krueger flap bullnose attachment hardware, and related investigative and corrective actions, if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective September 22, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of September 22, 2017. ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; Internet https://www.myboeingfleet.com. You may view this referenced service information at the FAA, Transport Standards Staff, 1601 Lind Avenue SW., Renton, WA. 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-2016- 9112. 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-2016- 9112; 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: Alan Pohl, Aerospace Engineer, Airframe Section, FAA, Seattle Aircraft Certification Office (ACO) Branch, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6450; fax: 425-917-6590; email: alan.pohl@faa.gov. 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 The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. The NPRM published in the Federal Register on September 29, 2016 (81 FR 66874) (``the NPRM''). The NPRM was prompted by a report of a Krueger flap bullnose departing an airplane during taxi, which caused damage to the wing [[Page 39345]] structure and thrust reverser. The NPRM proposed to require a one-time detailed visual inspection for discrepancies in the Krueger flap bullnose attachment hardware, and related investigative and corrective actions, if necessary. We are issuing this AD to detect and correct missing Krueger flap bullnose hardware. Such missing hardware could result in the Krueger flap bullnose departing the airplane during flight, which could damage empennage structure and lead to the inability to maintain continued safe flight and landing. 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. Support for the NPRM Vincent Romano, a private citizen, and United Airlines (UAL), stated their support for the NPRM. Effect of Winglets on Accomplishment of the Proposed Actions Aviation Partners Boeing stated that accomplishing the Supplemental Type Certificate (STC) ST00830SE does not affect the actions specified in the NPRM. We concur with the commenter. We have redesignated paragraph (c) of the NPRM as paragraph (c)(1) and added paragraph (c)(2) to this AD to state that installation of STC ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a ``change in product'' alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17. Request To Reference the Latest Service Information All Nippon Airways (ANA), American Airlines (AAL), Boeing, Jet2.com, TUIfly GmbH (HAP), UAL, and Kennedy Juma, requested revising the NPRM to reference Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016. Some commenters pointed out that the original issue had some errors in the illustrations and needed certain clarifications. ANA and Boeing also requested that we provide credit for accomplishing the original issue of the service information. We agree that this final rule should reference the latest service information. Since we issued the NPRM, Boeing issued Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016. We have revised paragraphs (c)(1) (paragraph (c) of the proposed AD) and (g) of this AD to reference Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016, for accomplishment of the required actions. We have also revised this AD to provide credit for using Boeing Alert Service Bulletin 737-57A1327, dated May 20, 2016, to accomplish the required actions before the effective date of this AD. Request To Correct the Latest Service Information AAL requested that Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016, be corrected to address errors in Figures 1, 2, 3, and 4. AAL stated that these errors affect the depiction of how the clevis assembly, clevis, and bullnose hinge lug are attached to each other, and suggested that revising the figures to correct the errors would clarify which parts must be subject to the detailed inspection. We acknowledge that Figures 1, 2, 3, and 4 of Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016, contain errors in the labeling of parts in the illustrations. However, the instructions in the tables in the figures correctly identify the parts and actions to be accomplished. Since the instructions are correct, the service bulletin adequately addresses the unsafe condition. We do not revise manufacturers' service information. However, Boeing might decide to revise Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016, to correct the errors. We have not changed the AD in this regard. Request To Allow Alternate Replacement Procedure AAL and Southwest Airlines (SWA) requested that we revise the NPRM to provide an option to replace cracked or deformed bullnose hinge lugs or clevis assemblies with bullnose hinge lugs or clevis assemblies instead of replacement with a Krueger flap assembly, as specified in paragraph 3.B.2.a.(1)(a)1) of Boeing Alert Service Bulletin 737- 57A1327, Revision 1, dated September 28, 2016. AAL suggested that the replacement option could be done using certain sections of a component maintenance manual (CMM). SWA suggested the use of Boeing production installation drawings. Both AAL and SWA also stated that replacing only the affected bullnose hinge lugs or clevis assemblies would also reduce the cost of repair or replacement. SWA also stated that there is a limited inventory of Krueger flap assemblies and that limited inventory, combined with a 6-month compliance time could significantly impair operators. We understand that the suggested replacement option might reduce the burden on operators. However, we do not agree to revise this AD to include the suggested changes. The repairs provided by the suggested sections of the CMM address normal wear-and-tear, and these repairs may not be appropriate for addressing damage that might result from an improperly attached Krueger flap. Boeing informed us that there is no procedure in the CMM that would provide step-by-step instructions to remove only the bullnose other than by use of the drawing system. Engineering instructions would be needed to ensure that the remainder of the flap assembly is serviceable and not damaged in addition to the damaged bullnose hinge lugs or clevis assembly, and that level of instruction would be too much detail for an AD. However, once we issue this AD, any person may request approval of an AMOC under the provisions of paragraph (i) of this AD. We have not changed the AD in this regard. 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. [[Page 39346]] 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 Bulletin 737-57A1327, Revision 1, dated September 28, 2016. The service information describes procedures for a one-time detailed visual inspection for discrepancies in the Krueger flap bullnose attachment hardware, 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 1,495 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspection of the Krueger flap 3 work-hours x $85 per None................ $255 $381,225 bullnose hardware. hour = $255. ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all available costs in our cost estimate. 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. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (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 adding the following new airworthiness directive (AD): 2017-16-05 The Boeing Company: Amendment 39-18982; Docket No. FAA- 2016-9112; Product Identifier 2016-NM-091-AD. (a) Effective Date This AD is effective September 22, 2017. (b) Affected ADs None. (c) Applicability (1) This AD applies to The Boeing Company Model 737-600, -700, - 700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737- 57A1327, Revision 1, dated September 28, 2016. (2) Installation of Supplemental Type Certificate (STC) ST00830SE (http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/354588EE63741A068625807D006726F6?OpenDocument&Highlight=st00830se) does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a ``change in product'' alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Unsafe Condition This AD was prompted by a report of a Krueger flap bullnose departing an airplane during taxi, which caused damage to the wing structure and thrust reverser. We are issuing this AD to detect and correct missing Krueger flap bullnose hardware. Such missing hardware could result in the Krueger flap bullnose departing the airplane during flight, which could damage empennage structure and lead to the inability to maintain continued safe flight and landing. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection of the Krueger Flap Bullnose Within 6 months after the effective date of this AD, do a detailed inspection for discrepancies of the Krueger flap bullnose attachment hardware, and do all applicable related investigative and corrective actions, [[Page 39347]] in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016. Do all applicable related investigative and corrective actions before further flight. (h) Credit for Previous Actions This paragraph provides credit for the actions specified in paragraph (g) of this AD, if those actions were performed before the effective date of this AD using Boeing Alert Service Bulletin 737- 57A1327, dated May 20, 2016. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle Aircraft Certification Office (ACO) Branch, 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 certification office, send it to the attention of the person identified in paragraph (j)(1) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov. (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, Seattle ACO Branch, 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) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (i)(4)(i) and (i)(4)(ii) of this AD apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or sub-step is labeled ``RC Exempt,'' then the RC requirement is removed from that step or sub-step. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (j) Related Information (1) For more information about this AD, contact Alan Pohl, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917-6450; fax: 425-917-6590; email: alan.pohl@faa.gov. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (k)(3) and (k)(4) of this AD. (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. (i) Boeing Alert Service Bulletin 737-57A1327, Revision 1, dated September 28, 2016. (ii) Reserved. (3) For Boeing service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; Internet https://www.myboeingfleet.com. (4) You may view this service information at FAA, Transport Standards Branch, 1601 Lind Ave 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 July 26, 2017. Jeffrey E. Duven, Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2017-16354 Filed 8-17-17; 8:45 am] BILLING CODE 4910-13-P
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Bulletin 670BA–36–022, dated May 30, 2016; (iv) Bombardier CRJ Series Regional Jet AD to address the unsafe condition on
or Bombardier Service Bulletin 670BA–36– Airworthiness Limitations Temporary these products.
022, Revision A, dated September 16, 2016. Revision ALI–0555, dated August 19, 2016.
DATES: This AD is effective September
(v) Bombardier CRJ Series Regional Jet
(k) Other FAA AD Provisions Airworthiness Limitations Temporary 22, 2017.
The following provisions also apply to this Revision ALI–0556, dated August 19, 2016. The Director of the Federal Register
AD: (vi) Bombardier CRJ Series Regional Jet approved the incorporation by reference
(1) Alternative Methods of Compliance Airworthiness Limitations Temporary of a certain publication listed in this AD
(AMOCs): The Manager, New York Aircraft Revision ALI–0557, dated August 19, 2016. as of September 22, 2017.
Certification Office (ACO), ANE–170, FAA, (3) For service information identified in ADDRESSES: For service information
has the authority to approve AMOCs for this this AD, contact Bombardier, Inc., 400 Côte- identified in this final rule, contact
AD, if requested using the procedures found Vertu Road West, Dorval, Québec H4S 1Y9,
Boeing Commercial Airplanes,
in 14 CFR 39.19. In accordance with 14 CFR Canada; Widebody Customer Response
Center North America toll-free telephone 1– Attention: Contractual & Data Services
39.19, send your request to your principal
inspector or local Flight Standards District 866–538–1247 or direct-dial telephone 1– (C&DS), 2600 Westminster Blvd., MC
Office, as appropriate. If sending information 514–855–2999; fax 514–855–7401; email 110–SK57, Seal Beach, CA 90740–5600;
directly to the manager of the ACO, send it ac.yul@aero.bombardier.com; Internet http:// telephone 562–797–1717; Internet
to ATTN: Program Manager, Continuing www.bombardier.com. https://www.myboeingfleet.com. You
Operational Safety, FAA, New York ACO, (4) You may view this service information may view this referenced service
1600 Stewart Avenue, Suite 410, Westbury, at the FAA, Transport Airplane Directorate, information at the FAA, Transport
NY 11590; telephone 516–228–7300; fax 1601 Lind Avenue SW., Renton, WA. For Standards Staff, 1601 Lind Avenue SW.,
516–794–5531. Before using any approved information on the availability of this
Renton, WA. For information on the
AMOC, notify your appropriate principal material at the FAA, call 425–227–1221.
(5) You may view this service information availability of this material at the FAA,
inspector, or lacking a principal inspector, call 425–227–1221. It is also available
the manager of the local flight standards that is incorporated by reference at the
National Archives and Records on the Internet at http://
district office/certificate holding district
Administration (NARA). For information on www.regulations.gov by searching for
office.
(2) Contacting the Manufacturer: For any
the availability of this material at NARA, call and locating Docket No. FAA–2016–
202–741–6030, or go to: http:// 9112.
requirement in this AD to obtain corrective
www.archives.gov/federal-register/cfr/ibr-
actions from a manufacturer, the action must Examining the AD Docket
locations.html.
be accomplished using a method approved
by the Manager, New York ACO, ANE–170, Issued in Renton, Washington, on July 13, You may examine the AD docket on
FAA; or Transport Canada Civil Aviation 2017. the Internet at http://
(TCCA); or Bombardier, Inc.’s TCCA Design Dionne Palermo, www.regulations.gov by searching for
Approval Organization (DAO). If approved by Acting Manager, Transport Airplane and locating Docket No. FAA–2016–
the DAO, the approval must include the Directorate, Aircraft Certification Service. 9112; or in person at the Docket
DAO-authorized signature. Management Facility between 9 a.m.
[FR Doc. 2017–15484 Filed 8–17–17; 8:45 am]
(l) Related Information BILLING CODE 4910–13–P
and 5 p.m., Monday through Friday,
(1) Refer to Mandatory Continuing except Federal holidays. The AD docket
Airworthiness Information (MCAI) Canadian contains this AD, the regulatory
Airworthiness Directive CF–2016–35, dated DEPARTMENT OF TRANSPORTATION evaluation, any comments received, and
November 16, 2016, for related information. other information. The address for the
You may examine the MCAI on the Internet Federal Aviation Administration Docket Office (phone: 800–647–5527) is
at http://www.regulations.gov by searching Docket Management Facility, U.S.
for and locating Docket No. FAA–2017–0699. 14 CFR Part 39 Department of Transportation, Docket
(2) For more information about this AD, Operations, M–30, West Building
contact Joseph Catanzaro, Aerospace [Docket No. FAA–2016–9112; Product
Identifier 2016–NM–091–AD; Amendment Ground Floor, Room W12–140, 1200
Engineer, Propulsion and Services Branch,
39–18982; AD 2017–16–05] New Jersey Avenue SE., Washington,
ANE–173, FAA, New York ACO, 1600
Stewart Avenue, Suite 410, Westbury, NY
DC 20590.
RIN 2120–AA64 FOR FURTHER INFORMATION CONTACT:
11590; telephone 516–228–7366; fax 516–
794–5531. Alan Pohl, Aerospace Engineer,
Airworthiness Directives; The Boeing
(3) Service information identified in this Airframe Section, FAA, Seattle Aircraft
AD that is not incorporated by reference is
Company Airplanes
Certification Office (ACO) Branch, 1601
available at the addresses specified in AGENCY: Federal Aviation Lind Avenue SW., Renton, WA 98057–
paragraphs (m)(3) and (m)(4) of this AD. Administration (FAA), DOT. 3356; phone: 425–917–6450; fax: 425–
(m) Material Incorporated by Reference ACTION: Final rule. 917–6590; email: alan.pohl@faa.gov.
(1) The Director of the Federal Register SUPPLEMENTARY INFORMATION:
approved the incorporation by reference SUMMARY: We are adopting a new
airworthiness directive (AD) for certain Discussion
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR The Boeing Company Model 737–600, We issued a notice of proposed
part 51. –700, –700C, –800, –900, and –900ER rulemaking (NPRM) to amend 14 CFR
(2) You must use this service information series airplanes. This AD was prompted part 39 by adding an AD that would
as applicable to do the actions required by by a report of a Krueger flap bullnose apply to certain The Boeing Company
this AD, unless this AD specifies otherwise. departing an airplane during taxi, which Model 737–600, –700, –700C, –800,
(i) Bombardier Service Bulletin 670BA–36–
mstockstill on DSK30JT082PROD with RULES
caused damage to the wing structure –900, and –900ER series airplanes. The
022, Revision B, dated December 20, 2016.
(ii) Bombardier CRJ Series Regional Jet
and thrust reverser. This AD requires a NPRM published in the Federal
Airworthiness Limitations Temporary one-time detailed visual inspection for Register on September 29, 2016 (81 FR
Revision ALI–0553, dated August 19, 2016. discrepancies in the Krueger flap 66874) (‘‘the NPRM’’). The NPRM was
(iii) Bombardier CRJ Series Regional Jet bullnose attachment hardware, and prompted by a report of a Krueger flap
Airworthiness Limitations Temporary related investigative and corrective bullnose departing an airplane during
Revision ALI–0554, dated August 19, 2016. actions, if necessary. We are issuing this taxi, which caused damage to the wing
VerDate Sep<11>2014 15:59 Aug 17, 2017 Jkt 241001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\18AUR1.SGM 18AUR1](https://thefederalregister.org/doc/82_FR_39503/page/1.svg)
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We also determined that these dated September 28, 2016. The service through their normal course of business
changes will not increase the economic information describes procedures for a or by the means identified in the
burden on any operator or increase the one-time detailed visual inspection for ADDRESSES section.
scope of this AD. discrepancies in the Krueger flap
Costs of Compliance
bullnose attachment hardware, and
Related Service Information Under 1
related investigative and corrective We estimate that this AD affects 1,495
CFR Part 51
actions. This service information is airplanes of U.S. registry. We estimate
We reviewed Boeing Alert Service reasonably available because the the following costs to comply with this
Bulletin 737–57A1327, Revision 1, interested parties have access to it AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Inspection of the Krueger flap bullnose hard- 3 work-hours × $85 per hour = $255 ......... None .................. $255 $381,225
ware.
We have received no definitive data Regulatory Findings FAA–2016–9112; Product Identifier
that would enable us to provide cost 2016–NM–091–AD.
This AD will not have federalism
estimates for the on-condition actions implications under Executive Order (a) Effective Date
specified in this AD. 13132. This AD will not have a This AD is effective September 22, 2017.
According to the manufacturer, some
substantial direct effect on the States, on (b) Affected ADs
of the costs of this AD may be covered
the relationship between the national
under warranty, thereby reducing the None.
government and the States, or on the
cost impact on affected individuals. We (c) Applicability
distribution of power and
do not control warranty coverage for
responsibilities among the various (1) This AD applies to The Boeing
affected individuals. As a result, we Company Model 737–600, –700, –700C,
levels of government.
have included all available costs in our –800, –900, and –900ER series airplanes,
For the reasons discussed above, I
cost estimate. certificated in any category, as identified in
certify that this AD:
Boeing Alert Service Bulletin 737–57A1327,
Authority for This Rulemaking (1) Is not a ‘‘significant regulatory Revision 1, dated September 28, 2016.
Title 49 of the United States Code action’’ under Executive Order 12866, (2) Installation of Supplemental Type
specifies the FAA’s authority to issue (2) Is not a ‘‘significant rule’’ under Certificate (STC) ST00830SE (http://rgl.faa.
rules on aviation safety. Subtitle I, DOT Regulatory Policies and Procedures gov/Regulatory_and_Guidance_Library/rgstc.
(44 FR 11034, February 26, 1979), nsf/0/354588EE63741A068625807D006
section 106, describes the authority of 726F6?OpenDocument&Highlight=st00830se)
the FAA Administrator. Subtitle VII: (3) Will not affect intrastate aviation
does not affect the ability to accomplish the
Aviation Programs, describes in more in Alaska, and actions required by this AD. Therefore, for
detail the scope of the Agency’s (4) Will not have a significant airplanes on which STC ST00830SE is
authority. economic impact, positive or negative, installed, a ‘‘change in product’’ alternative
We are issuing this rulemaking under on a substantial number of small entities method of compliance (AMOC) approval
the authority described in Subtitle VII, under the criteria of the Regulatory request is not necessary to comply with the
Part A, Subpart III, Section 44701: Flexibility Act. requirements of 14 CFR 39.17.
‘‘General requirements.’’ Under that List of Subjects in 14 CFR Part 39 (d) Subject
section, Congress charges the FAA with Air Transport Association (ATA) of
promoting safe flight of civil aircraft in Air transportation, Aircraft, Aviation America Code 57, Wings.
air commerce by prescribing regulations safety, Incorporation by reference,
(e) Unsafe Condition
for practices, methods, and procedures Safety.
the Administrator finds necessary for This AD was prompted by a report of a
Adoption of the Amendment Krueger flap bullnose departing an airplane
safety in air commerce. This regulation during taxi, which caused damage to the
is within the scope of that authority Accordingly, under the authority
wing structure and thrust reverser. We are
because it addresses an unsafe condition delegated to me by the Administrator, issuing this AD to detect and correct missing
that is likely to exist or develop on the FAA amends 14 CFR part 39 as Krueger flap bullnose hardware. Such
products identified in this rulemaking follows: missing hardware could result in the Krueger
action. flap bullnose departing the airplane during
This AD is issued in accordance with PART 39—AIRWORTHINESS flight, which could damage empennage
authority delegated by the Executive DIRECTIVES structure and lead to the inability to maintain
continued safe flight and landing.
Director, Aircraft Certification Service,
■ 1. The authority citation for part 39 (f) Compliance
as authorized by FAA Order 8000.51C.
continues to read as follows:
In accordance with that order, issuance Comply with this AD within the
of ADs is normally a function of the Authority: 49 U.S.C. 106(g), 40113, 44701. compliance times specified, unless already
mstockstill on DSK30JT082PROD with RULES
Compliance and Airworthiness done.
§ 39.13 [Amended]
Division, but during this transition (g) Inspection of the Krueger Flap Bullnose
period, the Executive Director has ■ 2. The FAA amends § 39.13 by adding
the following new airworthiness Within 6 months after the effective date of
delegated the authority to issue ADs this AD, do a detailed inspection for
applicable to transport category directive (AD): discrepancies of the Krueger flap bullnose
airplanes to the Director of the System 2017–16–05 The Boeing Company: attachment hardware, and do all applicable
Oversight Division. Amendment 39–18982; Docket No. related investigative and corrective actions,
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![Federal Register / Vol. 82, No. 159 / Friday, August 18, 2017 / Rules and Regulations 39347
in accordance with the Accomplishment (2) Service information identified in this manual (AFM) to provide procedures
Instructions of Boeing Alert Service Bulletin AD that is not incorporated by reference is that address latent failures in the spoiler
737–57A1327, Revision 1, dated September available at the addresses specified in and elevator computer (SEC). This AD
28, 2016. Do all applicable related paragraphs (k)(3) and (k)(4) of this AD.
investigative and corrective actions before
requires installing new updated SEC
further flight. (k) Material Incorporated by Reference software. This AD was prompted by
(1) The Director of the Federal Register reports that certain maintenance
(h) Credit for Previous Actions approved the incorporation by reference messages indicated the loss of elevator
This paragraph provides credit for the (IBR) of the service information listed in this servo control monitoring performed by
actions specified in paragraph (g) of this AD, paragraph under 5 U.S.C. 552(a) and 1 CFR SEC 1, SEC 2, or both, during the engine
if those actions were performed before the part 51. start. We are issuing this AD to address
effective date of this AD using Boeing Alert (2) You must use this service information
Service Bulletin 737–57A1327, dated May
the unsafe condition on these products.
as applicable to do the actions required by
20, 2016. this AD, unless the AD specifies otherwise. DATES: This AD is effective September
(i) Boeing Alert Service Bulletin 737– 22, 2017.
(i) Alternative Methods of Compliance The Director of the Federal Register
(AMOCs) 57A1327, Revision 1, dated September 28,
2016. approved the incorporation by reference
(1) The Manager, Seattle Aircraft (ii) Reserved. of certain publications listed in this AD
Certification Office (ACO) Branch, FAA, has (3) For Boeing service information as of September 22, 2017.
the authority to approve AMOCs for this AD, identified in this AD, contact Boeing The Director of the Federal Register
if requested using the procedures found in 14 Commercial Airplanes, Attention:
CFR 39.19. In accordance with 14 CFR 39.19, approved the incorporation by reference
Contractual & Data Services (C&DS), 2600 of a certain other publication listed in
send your request to your principal inspector Westminster Blvd., MC 110–SK57, Seal
or local Flight Standards District Office, as this AD as of November 20, 2015 (80 FR
Beach, CA 90740–5600; telephone 562–797–
appropriate. If sending information directly 1717; Internet https:// 68429, November 5, 2015).
to the manager of the certification office, www.myboeingfleet.com. ADDRESSES: For service information
send it to the attention of the person (4) You may view this service information identified in this final rule, contact
identified in paragraph (j)(1) of this AD.
at FAA, Transport Standards Branch, 1601 Airbus, Airworthiness Office–EIAS, 1
Information may be emailed to: 9-ANM-
Lind Ave SW., Renton, WA. For information Rond Point Maurice Bellonte, 31707
Seattle-ACO-AMOC-Requests@faa.gov.
on the availability of this material at the Blagnac Cedex, France; telephone +33 5
(2) Before using any approved AMOC,
FAA, call 425–227–1221. 61 93 36 96; fax +33 5 61 93 44 51; email
notify your appropriate principal inspector,
(5) You may view this service information
or lacking a principal inspector, the manager account.airworth-eas@airbus.com;
that is incorporated by reference at the
of the local flight standards district office/ Internet http://www.airbus.com. You
National Archives and Records
certificate holding district office. may view this referenced service
Administration (NARA). For information on
(3) An AMOC that provides an acceptable information at the FAA, Transport
the availability of this material at NARA, call
level of safety may be used for any repair,
202–741–6030, or go to: http://www.archives. Airplane Directorate, 1601 Lind Avenue
modification, or alteration required by this
AD if it is approved by the Boeing gov/federal-register/cfr/ibr-locations.html. SW., Renton, WA. For information on
Commercial Airplanes Organization Issued in Renton, Washington, on July 26, the availability of this material at the
Designation Authorization (ODA) that has 2017. FAA, call 425 227–1221. It is also
been authorized by the Manager, Seattle ACO Jeffrey E. Duven, available on the Internet at http://
Branch, to make those findings. To be www.regulations.gov by searching for
Director, System Oversight Division, Aircraft
approved, the repair method, modification and locating Docket No. FAA–2016–
Certification Service.
deviation, or alteration deviation must meet 9508.
the certification basis of the airplane, and the [FR Doc. 2017–16354 Filed 8–17–17; 8:45 am]
approval must specifically refer to this AD. BILLING CODE 4910–13–P Examining the AD Docket
(4) For service information that contains
steps that are labeled as Required for
You may examine the AD docket on
Compliance (RC), the provisions of the Internet at http://
DEPARTMENT OF TRANSPORTATION
paragraphs (i)(4)(i) and (i)(4)(ii) of this AD www.regulations.gov by searching for
apply. Federal Aviation Administration and locating Docket No. FAA–2016–
(i) The steps labeled as RC, including 9508; or in person at the Docket
substeps under an RC step and any figures Management Facility between 9 a.m.
14 CFR Part 39
identified in an RC step, must be done to and 5 p.m., Monday through Friday,
comply with the AD. If a step or sub-step is [Docket No. FAA–2016–9508; Directorate except Federal holidays. The AD docket
labeled ‘‘RC Exempt,’’ then the RC Identifier 2016–NM–065–AD; Amendment
requirement is removed from that step or
contains this AD, the regulatory
39–18956; AD 2017–14–12]
sub-step. An AMOC is required for any evaluation, any comments received, and
deviations to RC steps, including substeps RIN 2120–AA64 other information. The address for the
and identified figures. Docket Office (telephone 800–647–5527)
(ii) Steps not labeled as RC may be Airworthiness Directives; Airbus is Docket Management Facility, U.S.
deviated from using accepted methods in Airplanes Department of Transportation, Docket
accordance with the operator’s maintenance Operations, M–30, West Building
or inspection program without obtaining AGENCY: Federal Aviation
Administration (FAA), Department of Ground Floor, Room W12–140, 1200
approval of an AMOC, provided the RC steps,
including substeps and identified figures, can Transportation (DOT). New Jersey Avenue SE., Washington,
still be done as specified, and the airplane DC 20590.
ACTION: Final rule.
can be put back in an airworthy condition. FOR FURTHER INFORMATION CONTACT:
mstockstill on DSK30JT082PROD with RULES
SUMMARY: We are superseding Sanjay Ralhan, Aerospace Engineer,
(j) Related Information
Airworthiness Directive (AD) 2015–22– International Branch, ANM–116,
(1) For more information about this AD, Transport Airplane Directorate, FAA,
contact Alan Pohl, Aerospace Engineer,
06 which applied to all Airbus Model
Airframe Section, FAA, Seattle ACO Branch, A318, A319, A320, and A321 series 1601 Lind Avenue SW., Renton, WA
1601 Lind Avenue SW., Renton, WA 98057– airplanes. AD 2015–22–06 required 98057–3356; telephone 425–227–1405;
3356; phone: 425–917–6450; fax: 425–917– revising the After Start Normal fax 425–227–1149.
6590; email: alan.pohl@faa.gov. Procedures section of the airplane flight SUPPLEMENTARY INFORMATION:
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Document Created: 2017-08-18 07:40:37
Document Modified: 2017-08-18 07:40:37
| 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 September 22, 2017. | |
| Contact | Alan Pohl, Aerospace Engineer, Airframe Section, FAA, Seattle Aircraft Certification Office (ACO) Branch, 1601 Lind Avenue SW., Renton, WA 98057-3356; phone: 425-917- 6450; fax: 425-917-6590; email: [email protected] | |
| FR Citation | 82 FR 39344 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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