83 FR 28553 - Airworthiness Directives; Bombardier, Inc., Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 119 (June 20, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 119 (June 20, 2018)
| Page Range | 28553-28555 | |
| FR Document | 2018-13126 |
[Federal Register Volume 83, Number 119 (Wednesday, June 20, 2018)] [Proposed Rules] [Pages 28553-28555] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-13126] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0546; Product Identifier 2017-NM-171-AD] RIN 2120-AA64 Airworthiness Directives; Bombardier, Inc., Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This proposed AD was prompted by reports of multiple in-flight departures of the aft belly fairing access panels. This proposed AD would require modification of the aft belly fairing access panels. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by August 6, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-7401; email thd.crj@aero.bombardier.com; internet http://www.bombardier.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. 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-2018- 0546; 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 NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Andrea Jimenez, Aerospace Engineer, [[Page 28554]] Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7330; fax 516-794-5531. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2018-0546; Product Identifier 2017-NM-171-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM based on those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this NPRM. Discussion Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian AD CF-2017-31, dated September 22, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Bombardier, Inc., Model BD-700-1A10 and BD-700- 1A11 airplanes. The MCAI states: There have been multiple in-service occurrences where operators reported in-flight departure of the aft belly fairing access panels, 185CL and/or 186CR. There has been no damage reported to the affected aircraft to date, however departure of the panels in any phase of flight could create runway hazards or a hazard to persons and property on the ground. Bombardier Inc. has issued Service Bulletins (SBs) to incorporate new self-locking nutplates with associated hardware (retaining rings and studs) to improve fastener engagement. A bracket has also been added to provide two additional panel attachment points. This [Canadian] AD requires the incorporation of these design changes to prevent departure of the two aft belly fairing access panels in flight and the associated risk on the ground. You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0546. Related Service Information Under 1 CFR Part 51 Bombardier has issued the following service information: Service Bulletin 700-1A11-53-025, Revision 01, dated December 16, 2016; Service Bulletin 700-53-050, Revision 01, dated December 16, 2016; Service Bulletin 700-53-5009, Revision 01, dated December 16, 2016; and Service Bulletin 700-53-6008, Revision 01, dated December 16, 2016. The service information describes actions to modify the aft belly fairing access panels by replacing the attachments. These documents are distinct since they apply to different airplane models in different configurations. 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. FAA's Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design. Costs of Compliance We estimate that this proposed AD affects 110 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- 4 work-hours x $85 per hour = $340........................... $2,640 $2,980 $327,800 ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some of the costs of this proposed 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 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 proposed 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 We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation: 1. Is not a ``significant regulatory action'' under Executive Order 12866; [[Page 28555]] 2. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 3. Will not affect intrastate aviation in Alaska; and 4. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): Bombardier, Inc.: Docket No. FAA-2018-0546; Product Identifier 2017- NM-171-AD. (a) Comments Due Date We must receive comments by August 6, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc., Model BD-700-1A10 and BD- 700-1A11 airplanes, certificated in any category, serial numbers 9002 through 9770 inclusive, 9772 through 9781 inclusive, and 9998. (d) Subject Air Transport Association (ATA) of America Code 53, Fuselage. (e) Reason This AD was prompted by reports of multiple in-flight departures of the aft belly fairing access panels. We are issuing this AD to prevent in-flight departures of the aft belly fairing access panels, which could result in runway hazards or hazards to people on the ground. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Access Panel Modification Within 15 months after the effective date of this AD, modify the aft belly fairing access panels by replacing the attachments, in accordance with the Accomplishment Instructions of the applicable service information identified in paragraphs (g)(1) and (g)(2) of this AD. (1) For Model BD-700-1A10 airplanes: Bombardier Service Bulletin 700-53-050, or 700-53-6008, both Revision 01, both dated December 16, 2016. (2) For Model BD-700-1A11 airplanes: Bombardier Service Bulletin 700-1A11-53-025, or 700-53-5009, both Revision 01, both dated December 16, 2016. (h) Credit for Previous Actions This paragraph provides credit for actions required by paragraph (g) of this AD, if those actions were performed before the effective date of this AD using the applicable service information identified in paragraphs (h)(1) through (h)(4) of this AD. (1) Bombardier Service Bulletin 700-1A11-53-025, dated July 14, 2016. (2) Bombardier Service Bulletin 700-53-050, dated July 14, 2016. (3) Bombardier Service Bulletin 700-53-5009, dated July 14, 2016. (4) Bombardier Service Bulletin 700-53-6008, dated July 14, 2016. (i) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York 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 ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO Branch, 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. (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 Branch, FAA; or Transport Canada Civil Aviation (TCCA); or Bombardier Inc.'s TCCA Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (j) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian Airworthiness Directive CF-2017-31, dated September 22, 2017, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0546. (2) For more information about this AD, contact Andrea Jimenez, Aerospace Engineer, Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7330; fax 516-794-5531. (3) For service information identified in this AD, contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855- 7401; email thd.crj@aero.bombardier.com; internet http://www.bombardier.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. Issued in Des Moines, Washington, on June 8, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-13126 Filed 6-19-18; 8:45 am] BILLING CODE 4910-13-P
![28554 Federal Register / Vol. 83, No. 119 / Wednesday, June 20, 2018 / Proposed Rules
Airframe and Mechanical Systems Model BD–700–1A10 and BD–700– • Service Bulletin 700–53–6008,
Section, FAA, New York ACO Branch, 1A11 airplanes. The MCAI states: Revision 01, dated December 16, 2016.
1600 Stewart Avenue, Suite 410, There have been multiple in-service The service information describes
Westbury, NY 11590; telephone 516– occurrences where operators reported in- actions to modify the aft belly fairing
228–7330; fax 516–794–5531. flight departure of the aft belly fairing access access panels by replacing the
SUPPLEMENTARY INFORMATION: panels, 185CL and/or 186CR. There has been attachments. These documents are
no damage reported to the affected aircraft to
Comments Invited date, however departure of the panels in any distinct since they apply to different
We invite you to send any written phase of flight could create runway hazards airplane models in different
relevant data, views, or arguments about or a hazard to persons and property on the configurations. This service information
this proposal. Send your comments to ground. is reasonably available because the
Bombardier Inc. has issued Service interested parties have access to it
an address listed under the ADDRESSES
Bulletins (SBs) to incorporate new through their normal course of business
section. Include ‘‘Docket No. FAA– self¥locking nutplates with associated
2018–0546; Product Identifier 2017– or by the means identified in the
hardware (retaining rings and studs) to
NM–171–AD’’ at the beginning of your ADDRESSES section.
improve fastener engagement. A bracket has
comments. We specifically invite also been added to provide two additional FAA’s Determination and Requirements
comments on the overall regulatory, panel attachment points. of This Proposed AD
economic, environmental, and energy This [Canadian] AD requires the
aspects of this NPRM. We will consider incorporation of these design changes to This product has been approved by
all comments received by the closing prevent departure of the two aft belly fairing the aviation authority of another
date and may amend this NPRM based access panels in flight and the associated risk
on the ground. country, and is approved for operation
on those comments. in the United States. Pursuant to our
We will post all comments we You may examine the MCAI in the bilateral agreement with the State of
receive, without change, to http:// AD docket on the internet at http:// Design Authority, we have been notified
www.regulations.gov, including any www.regulations.gov by searching for of the unsafe condition described in the
personal information you provide. We and locating Docket No. FAA–2018– MCAI and service information
will also post a report summarizing each 0546. referenced above. We are proposing this
substantive verbal contact we receive AD because we evaluated all pertinent
about this NPRM. Related Service Information Under 1
CFR Part 51 information and determined an unsafe
Discussion condition exists and is likely to exist or
Bombardier has issued the following
Transport Canada Civil Aviation develop on other products of the same
service information:
(TCCA), which is the aviation authority • Service Bulletin 700–1A11–53–025, type design.
for Canada, has issued Canadian AD Revision 01, dated December 16, 2016; Costs of Compliance
CF–2017–31, dated September 22, 2017 • Service Bulletin 700–53–050,
(referred to after this as the Mandatory Revision 01, dated December 16, 2016; We estimate that this proposed AD
Continuing Airworthiness Information, • Service Bulletin 700–53–5009, affects 110 airplanes of U.S. registry. We
or ‘‘the MCAI’’), to correct an unsafe Revision 01, dated December 16, 2016; estimate the following costs to comply
condition for certain Bombardier, Inc., and with this proposed AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Labor cost Parts cost product operators
4 work-hours × $85 per hour = $340 .......................................................................................... $2,640 $2,980 $327,800
According to the manufacturer, some General requirements.’’ Under that Director has delegated the authority to
of the costs of this proposed AD may be section, Congress charges the FAA with issue ADs applicable to transport
covered under warranty, thereby promoting safe flight of civil aircraft in category airplanes to the Director of the
reducing the cost impact on affected air commerce by prescribing regulations System Oversight Division.
individuals. We do not control warranty for practices, methods, and procedures
coverage for affected individuals. As a the Administrator finds necessary for Regulatory Findings
result, we have included all costs in our safety in air commerce. This regulation We determined that this proposed AD
cost estimate. is within the scope of that authority would not have federalism implications
because it addresses an unsafe condition under Executive Order 13132. This
Authority for This Rulemaking
that is likely to exist or develop on
proposed AD would not have a
Title 49 of the United States Code products identified in this rulemaking
substantial direct effect on the States, on
specifies the FAA’s authority to issue action.
the relationship between the national
rules on aviation safety. Subtitle I, This proposed AD is issued in
sradovich on DSK3GMQ082PROD with PROPOSALS
Government and the States, or on the
section 106, describes the authority of accordance with authority delegated by distribution of power and
the FAA Administrator. ‘‘Subtitle VII: the Executive Director, Aircraft responsibilities among the various
Aviation Programs,’’ describes in more Certification Service, as authorized by levels of government.
detail the scope of the Agency’s FAA Order 8000.51C. In accordance
authority. with that order, issuance of ADs is For the reasons discussed above, I
We are issuing this rulemaking under normally a function of the Compliance certify this proposed regulation:
the authority described in ‘‘Subtitle VII, and Airworthiness Division, but during 1. Is not a ‘‘significant regulatory
Part A, Subpart III, Section 44701: this transition period, the Executive action’’ under Executive Order 12866;
VerDate Sep<11>2014 16:51 Jun 19, 2018 Jkt 244001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 E:\FR\FM\20JNP1.SGM 20JNP1](https://thefederalregister.org/doc/83_FR_28672/page/2.svg)
![Federal Register / Vol. 83, No. 119 / Wednesday, June 20, 2018 / Proposed Rules 28555
2. Is not a ‘‘significant rule’’ under the accordance with the Accomplishment Avenue, Suite 410, Westbury, NY 11590;
DOT Regulatory Policies and Procedures Instructions of the applicable service telephone 516–228–7330; fax 516–794–5531.
(44 FR 11034, February 26, 1979); information identified in paragraphs (g)(1) (3) For service information identified in
and (g)(2) of this AD. this AD, contact Bombardier, Inc., 400 Côte-
3. Will not affect intrastate aviation in Vertu Road West, Dorval, Québec H4S 1Y9,
(1) For Model BD–700–1A10 airplanes:
Alaska; and Bombardier Service Bulletin 700–53–050, or Canada; telephone 514–855–5000; fax 514–
4. Will not have a significant 700–53–6008, both Revision 01, both dated 855–7401; email thd.crj@
economic impact, positive or negative, December 16, 2016. aero.bombardier.com; internet http://
on a substantial number of small entities (2) For Model BD–700–1A11 airplanes: www.bombardier.com. You may view this
under the criteria of the Regulatory Bombardier Service Bulletin 700–1A11–53– service information at the FAA, Transport
Flexibility Act. 025, or 700–53–5009, both Revision 01, both Standards Branch, 2200 South 216th St., Des
dated December 16, 2016. Moines, WA. For information on the
List of Subjects in 14 CFR Part 39 availability of this material at the FAA, call
(h) Credit for Previous Actions 206–231–3195.
Air transportation, Aircraft, Aviation
This paragraph provides credit for actions Issued in Des Moines, Washington, on June
safety, Incorporation by reference,
required by paragraph (g) of this AD, if those 8, 2018.
Safety. actions were performed before the effective Michael Kaszycki,
The Proposed Amendment date of this AD using the applicable service
Acting Director, System Oversight Division,
information identified in paragraphs (h)(1)
Accordingly, under the authority Aircraft Certification Service.
through (h)(4) of this AD.
delegated to me by the Administrator, (1) Bombardier Service Bulletin 700– [FR Doc. 2018–13126 Filed 6–19–18; 8:45 am]
the FAA proposes to amend 14 CFR part 1A11–53–025, dated July 14, 2016. BILLING CODE 4910–13–P
39 as follows: (2) Bombardier Service Bulletin 700–53–
050, dated July 14, 2016.
PART 39—AIRWORTHINESS (3) Bombardier Service Bulletin 700–53– DEPARTMENT OF TRANSPORTATION
DIRECTIVES 5009, dated July 14, 2016.
(4) Bombardier Service Bulletin 700–53– Federal Aviation Administration
■ 1. The authority citation for part 39 6008, dated July 14, 2016.
continues to read as follows: (i) Other FAA AD Provisions 14 CFR Part 39
Authority: 49 U.S.C. 106(g), 40113, 44701. The following provisions also apply to this [Docket No. FAA–2018–0556; Product
AD: Identifier 2018–NM–015–AD]
§ 39.13 [Amended] (1) Alternative Methods of Compliance
RIN 2120–AA64
■ 2. The FAA amends § 39.13 by adding (AMOCs): The Manager, New York ACO
the following new airworthiness Branch, FAA, has the authority to approve
Airworthiness Directives; Airbus
directive (AD): AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. In Airplanes
Bombardier, Inc.: Docket No. FAA–2018– accordance with 14 CFR 39.19, send your
0546; Product Identifier 2017–NM–171– AGENCY: Federal Aviation
request to your principal inspector or local Administration (FAA), DOT.
AD. Flight Standards District Office, as
appropriate. If sending information directly ACTION: Notice of proposed rulemaking
(a) Comments Due Date
to the manager of the certification office, (NPRM).
We must receive comments by August 6, send it to ATTN: Program Manager,
2018. Continuing Operational Safety, FAA, New
SUMMARY: We propose to adopt a new
(b) Affected ADs York ACO Branch, 1600 Stewart Avenue, airworthiness directive (AD) for all
Suite 410, Westbury, NY 11590; telephone Airbus Model A318 series; Model A319
None. series; Model A320 series; and Model
516–228–7300; fax 516–794–5531. Before
(c) Applicability using any approved AMOC, notify your A321–111, –112, –131, –211, –212,
This AD applies to Bombardier, Inc., appropriate principal inspector, or lacking a –213, –231, and –232 airplanes. This
Model BD–700–1A10 and BD–700–1A11 principal inspector, the manager of the local proposed AD was prompted by reports
airplanes, certificated in any category, serial flight standards district office/certificate of multiple angle of attack (AoA) probe
numbers 9002 through 9770 inclusive, 9772 holding district office. blockages. This proposed AD would
through 9781 inclusive, and 9998. (2) Contacting the Manufacturer: For any
require all elevator aileron computer
requirement in this AD to obtain corrective
(d) Subject actions from a manufacturer, the action must (ELAC) units to be upgraded with new
be accomplished using a method approved software, or replaced with upgraded
Air Transport Association (ATA) of
America Code 53, Fuselage. by the Manager, New York ACO Branch, units. We are proposing this AD to
FAA; or Transport Canada Civil Aviation address the unsafe condition on these
(e) Reason (TCCA); or Bombardier Inc.’s TCCA Design products.
This AD was prompted by reports of Approval Organization (DAO). If approved by
DATES: We must receive comments on
multiple in-flight departures of the aft belly the DAO, the approval must include the
DAO-authorized signature. this proposed AD by August 6, 2018.
fairing access panels. We are issuing this AD
to prevent in-flight departures of the aft belly ADDRESSES: You may send comments,
(j) Related Information using the procedures found in 14 CFR
fairing access panels, which could result in
runway hazards or hazards to people on the (1) Refer to Mandatory Continuing 11.43 and 11.45, by any of the following
ground. Airworthiness Information (MCAI) Canadian methods:
Airworthiness Directive CF–2017–31, dated • Federal eRulemaking Portal: Go to
sradovich on DSK3GMQ082PROD with PROPOSALS
(f) Compliance September 22, 2017, for related information. http://www.regulations.gov. Follow the
Comply with this AD within the This MCAI may be found in the AD docket
on the internet at http://www.regulations.gov
instructions for submitting comments.
compliance times specified, unless already • Fax: 202–493–2251.
done. by searching for and locating Docket No.
FAA–2018–0546. • Mail: U.S. Department of
(g) Access Panel Modification (2) For more information about this AD, Transportation, Docket Operations, M–
Within 15 months after the effective date contact Andrea Jimenez, Aerospace Engineer, 30, West Building Ground Floor, Room
of this AD, modify the aft belly fairing access Airframe and Mechanical Systems Section, W12–140, 1200 New Jersey Avenue SE,
panels by replacing the attachments, in FAA, New York ACO Branch, 1600 Stewart Washington, DC 20590.
VerDate Sep<11>2014 16:51 Jun 19, 2018 Jkt 244001 PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 E:\FR\FM\20JNP1.SGM 20JNP1](https://thefederalregister.org/doc/83_FR_28672/page/3.svg)
Document Created: 2018-06-20 00:20:16
Document Modified: 2018-06-20 00:20:16
| 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 | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by August 6, 2018. | |
| Contact | Andrea Jimenez, Aerospace Engineer, Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7330; fax 516-794-5531. | |
| FR Citation | 83 FR 28553 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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