82 FR 21482 - Airworthiness Directives; Bombardier, Inc. (Type Certificate Previously Held by Canadair Limited) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 88 (May 9, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 88 (May 9, 2017)
| Page Range | 21482-21484 | |
| FR Document | 2017-09324 |
[Federal Register Volume 82, Number 88 (Tuesday, May 9, 2017)] [Proposed Rules] [Pages 21482-21484] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-09324] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-0333; Directorate Identifier 2017-NM-005-AD] RIN 2120-AA64 Airworthiness Directives; Bombardier, Inc. (Type Certificate Previously Held by Canadair Limited) 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 CL-215-6B11 (CL-415 Variant) airplanes. This proposed AD was prompted by a report indicating that an oxygen bottle was found loose while the clamp strap was in the locked position. This proposed AD would require modification of the clamp strap and installation of additional shims, as applicable, to the [[Page 21483]] flight crew's oxygen bottle retaining structures. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by June 23, 2017. 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: [email protected]; Internet: http://www.bombardier.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017- 0333; 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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228-7318; 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-2017-0333; Directorate Identifier 2017-NM-005-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD 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 proposed AD. Discussion Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian AD CF-2016-33, dated October 12, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Bombardier, Inc., Model CL-215-6B11 (CL-415 Variant) airplanes. The MCAI states: During the implementation of Service Bulletin (SB) 215-4051, the oxygen bottle was found loose while the clamp strap was in the locked position. This was determined to be caused by the quick release latch assembly not achieving the proper clamping pressure. The release of the oxygen bottle due to improper clamping pressure may result in a loose mass cockpit hazard or an oxygen rich environment leading to a possible fire hazard. In order to mitigate the unsafe condition, SB 215-4457 was issued to modify the clamp strap and install additional shims to add strength to the attaching structure for all affected aeroplanes. 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-2017- 0333. Related Service Information Under 1 CFR Part 51 We reviewed Bombardier Service Bulletin 215-4457, Revision 3, dated May 8, 2013. The service information describes procedures for installing shims, and, for certain airplanes, modifying the straps of the latch assembly, on the flight crew's oxygen bottles' retaining structure. 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 26 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Modification and installation 16 work-hours x $85 per $2,250 $3,610 $93,860 hour = $1,360. ---------------------------------------------------------------------------------------------------------------- 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 [[Page 21484]] safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this 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; 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. (Type Certificate Previously Held by Canadair Limited): Docket No. FAA-2017-0333; Directorate Identifier 2017-NM- 005-AD. (a) Comments Due Date We must receive comments by June 23, 2017. (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc. (Type Certificate previously held by Canadair Limited) Model CL-215-6B11 (CL-415 Variant) airplanes, certificated in any category, having serial numbers 2001, 2002, 2005 through 2007 inclusive, 2010, 2012 through 2017 inclusive, 2019, 2022 through 2024 inclusive, 2026, 2057, 2063, 2065, 2076, 2077, and 2081. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ Furnishings. (e) Reason This AD was prompted by a report indicating that an oxygen bottle was found loose while the clamp strap was in the locked position. We are issuing this AD to prevent an oxygen bottle from being released, which would result in a loose mass object in the cockpit and could also result in an oxygen-rich environment that could lead to a possible fire hazard. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Installation and Modification Within 12 months after the effective date of this AD, install additional shims and modify the clamp strap, as applicable, to the flight crew's oxygen bottle retaining structures, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 215- 4457, Revision 3, dated May 8, 2013. (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 any of the service information identified in paragraphs (h)(1), (h)(2), or (h)(3) of this AD. (1) Bombardier Service Bulletin 215-4457, Revision 2, dated October 24, 2012. (2) Bombardier Service Bulletin 215-4457, Revision 1, dated June 12, 2012. (3) Bombardier Service Bulletin 215-4457, dated April 4, 2012. (i) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, New York Aircraft Certification Office (ACO), ANE-170, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228- 7300; fax: 516-794-5531. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, New York ACO, ANE-170, FAA; or Transport Canada Civil Aviation (TCCA); or Viking Air Limited'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 AD CF-2016-33, dated October 12, 2016, 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-2017-0333. (2) For more information about this AD, contact Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228-7318; 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: [email protected]; Internet: http://www.bombardier.com. 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. Issued in Renton, Washington, on May 2, 2017. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-09324 Filed 5-8-17; 8:45 am] BILLING CODE 4910-13-P
![21482 Federal Register / Vol. 82, No. 88 / Tuesday, May 9, 2017 / Proposed Rules
recommending rulemaking to: (1) rulemaking. As you prepare your (4) Are there unintended
Require that the post-shutdown comments, consider the following consequences? Does the potential
decommissioning activities report general questions: proposed action create conditions that
(PSDAR) contain a description of how 1. Is the NRC considering appropriate would be contrary to the potential
the spent fuel stored under a general alternatives for each regulatory area proposed action’s purpose and
independent spent fuel storage described in the preliminary draft objectives? If so, what are the
installation license will be removed regulatory analysis? consequences and how should they be
from the reactor site in accordance with 2. Are there additional factors that the addressed?
the regulatory requirements in § 50.82, NRC should consider in each regulatory (5) Please provide information on the
‘‘Termination of License,’’ of title 10 of area? What are these factors? costs and benefits of the potential
the Code of Federal Regulations (10 3. Is there additional information proposed action. This information will
CFR), 10 CFR 50.54(bb), 10 CFR 52.110, concerning regulatory impacts that the be used to support additional regulatory
‘‘Termination of License,’’ and 10 CFR NRC should include in its regulatory analysis by the NRC.
72.218, ‘‘Termination of Licenses;’’ and analysis for this rulemaking?
(2) amend 10 CFR 51.53, V. Plain Writing
4. Are all costs and benefits properly
‘‘Postconstruction Environmental addressed to determine the economic The Plain Writing Act of 2010 (Pub.
Reports,’’ and 10 CFR 51.95, impact of the rulemaking alternatives? L. 111–274) requires Federal agencies to
‘‘Postconstruction Environmental 5. What additional costs or cost write documents in a clear, concise,
Impact Statements,’’ to clarify that the savings will the rulemaking alternatives well-organized manner. The NRC has
requirements for a license amendment cause to society, industry, and written this document to be consistent
before decommissioning activities may government? with the Plain Writing Act as well as the
commence applies only to non-power Presidential Memorandum, ‘‘Plain
reactors, as specified in 10 CFR 50.82(b). IV. Cumulative Effects of Regulation Language in Government Writing,’’
In the draft regulatory basis, the NRC The cumulative effects of regulation published in the Federal Register on
concludes that regulatory activities (CER) describe the challenges that June 10, 1998 (63 FR 31883). The NRC
other than rulemaking—such as licensees or other impacted entities requests comment on this document
guidance development—should be used (such as State agency partners) may face with respect to the clarity and
to address stakeholder concerns while implementing new regulatory effectiveness of the language used.
regarding the appropriate role of State
positions, programs, and requirements Dated at Rockville, Maryland, this 3rd day
and local governments in the of May 2017.
(e.g., rules, generic letters, backfits,
decommissioning process, the level of
inspections). The CER is an For the Nuclear Regulatory Commission.
NRC review and approval of the PSDAR,
organizational effectiveness challenge Gregory T. Bowman,
and the 60 year limit for power reactor
that results from a licensee or impacted Deputy Director, Division of Policy and
decommissioning. The NRC also
entity implementing a number of Rulemaking, Office of Nuclear Reactor
determined that additional stakeholder
complex positions, programs, or Regulation.
input is needed prior to finalizing
requirements within a limited [FR Doc. 2017–09332 Filed 5–4–17; 11:15 am]
recommendations related to cyber
implementation period and with
security, drug and alcohol testing, BILLING CODE 7590–01–P
certified fuel handler training and available resources (which may include
minimum staffing, aging management, limited available expertise to address a
and fatigue management. The NRC is specific issue). The NRC has DEPARTMENT OF TRANSPORTATION
seeking specific public input on these implemented CER enhancements to the
topics as part of the public comment rulemaking process to facilitate public Federal Aviation Administration
request on the entire draft regulatory involvement throughout the rulemaking
basis. process. In developing comments on the 14 CFR Part 39
To supplement the draft regulatory preliminary draft regulatory analysis,
[Docket No. FAA–2017–0333; Directorate
basis, the NRC has prepared a consider the following questions: Identifier 2017–NM–005–AD]
preliminary draft regulatory analysis, in (1) In light of any current or projected
CER challenges, what should be a RIN 2120–AA64
which the costs, benefits, and other
impacts of each rulemaking alternative reasonable effective date, compliance
date, or submittal date(s) from the time Airworthiness Directives; Bombardier,
are presented in order to determine the Inc. (Type Certificate Previously Held
economic impact to industry and to the final rule is published to the actual
implementation of any new proposed by Canadair Limited) Airplanes
government from the proposed
rulemaking. The NRC prepared the requirements, including changes to AGENCY: Federal Aviation
preliminary draft regulatory analysis to programs, procedures, or the facility? Administration (FAA), DOT.
support decision making during the (2) If current or projected CER ACTION: Notice of proposed rulemaking
preparation of the draft regulatory basis challenges exist, what should be done to (NPRM).
document, which includes an address this situation (e.g., if more time
evaluation of possible regulatory is required to implement the new SUMMARY: We propose to adopt a new
improvements for reactors transitioning requirements, what period of time airworthiness directive (AD) for certain
to decommissioning. would be sufficient, and why such a Bombardier, Inc., Model CL–215–6B11
nlaroche on DSK30NT082PROD with PROPOSALS
time frame is necessary)? (CL–415 Variant) airplanes. This
III. Request for Comment (3) Do other regulatory actions (e.g., proposed AD was prompted by a report
The NRC is requesting comment on orders, generic communications, license indicating that an oxygen bottle was
the preliminary draft regulatory analysis amendment requests, and inspection found loose while the clamp strap was
that was prepared to support the draft findings of a generic nature) by the NRC in the locked position. This proposed
regulatory basis for the ‘‘Regulatory or other agencies influence the AD would require modification of the
Improvements for Reactors implementation of the potential clamp strap and installation of
Transitioning to Decommissioning’’ proposed requirements? additional shims, as applicable, to the
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![21484 Federal Register / Vol. 82, No. 88 / Tuesday, May 9, 2017 / Proposed Rules
safety in air commerce. This regulation Variant) airplanes, certificated in any be accomplished using a method approved
is within the scope of that authority category, having serial numbers 2001, 2002, by the Manager, New York ACO, ANE–170,
because it addresses an unsafe condition 2005 through 2007 inclusive, 2010, 2012 FAA; or Transport Canada Civil Aviation
through 2017 inclusive, 2019, 2022 through (TCCA); or Viking Air Limited’s TCCA
that is likely to exist or develop on Design Approval Organization (DAO). If
2024 inclusive, 2026, 2057, 2063, 2065, 2076,
products identified in this rulemaking 2077, and 2081. approved by the DAO, the approval must
action. include the DAO-authorized signature.
(d) Subject
Regulatory Findings Air Transport Association (ATA) of (j) Related Information
We determined that this proposed AD America Code 25, Equipment/Furnishings. (1) Refer to Mandatory Continuing
would not have federalism implications Airworthiness Information (MCAI) Canadian
(e) Reason AD CF–2016–33, dated October 12, 2016, for
under Executive Order 13132. This
This AD was prompted by a report related information. This MCAI may be
proposed AD would not have a
indicating that an oxygen bottle was found found in the AD docket on the Internet at
substantial direct effect on the States, on loose while the clamp strap was in the locked http://www.regulations.gov by searching for
the relationship between the national position. We are issuing this AD to prevent and locating Docket No. FAA–2017–0333.
Government and the States, or on the an oxygen bottle from being released, which (2) For more information about this AD,
distribution of power and would result in a loose mass object in the contact Cesar Gomez, Aerospace Engineer,
responsibilities among the various cockpit and could also result in an oxygen- Airframe and Mechanical Systems Branch,
levels of government. rich environment that could lead to a ANE–171, FAA, New York Aircraft
For the reasons discussed above, I possible fire hazard. Certification Office (ACO), 1600 Stewart
certify this proposed regulation: (f) Compliance Avenue, Suite 410, Westbury, NY 11590;
1. Is not a ‘‘significant regulatory telephone: 516–228–7318; fax: 516–794–
Comply with this AD within the 5531.
action’’ under Executive Order 12866; compliance times specified, unless already
2. Is not a ‘‘significant rule’’ under the (3) For service information identified in
done. this AD, contact Bombardier, Inc., 400 Côte-
DOT Regulatory Policies and Procedures
(g) Installation and Modification Vertu Road West, Dorval, Québec H4S 1Y9,
(44 FR 11034, February 26, 1979); Canada; telephone: 514–855–5000; fax: 514–
3. Will not affect intrastate aviation in Within 12 months after the effective date
855–7401; email: thd.crj@
Alaska; and of this AD, install additional shims and
aero.bombardier.com; Internet: http://
4. Will not have a significant modify the clamp strap, as applicable, to the
www.bombardier.com. You may view this
economic impact, positive or negative, flight crew’s oxygen bottle retaining
service information at the FAA, Transport
structures, in accordance with the
on a substantial number of small entities Accomplishment Instructions of Bombardier
Airplane Directorate, 1601 Lind Avenue SW.,
under the criteria of the Regulatory Renton, WA. For information on the
Service Bulletin 215–4457, Revision 3, dated
Flexibility Act. availability of this material at the FAA, call
May 8, 2013.
425–227–1221.
List of Subjects in 14 CFR Part 39 (h) Credit for Previous Actions
Issued in Renton, Washington, on May 2,
Air transportation, Aircraft, Aviation This paragraph provides credit for actions 2017.
safety, Incorporation by reference, required by paragraph (g) of this AD, if those Michael Kaszycki,
Safety. actions were performed before the effective
date of this AD using any of the service Acting Manager, Transport Airplane
The Proposed Amendment information identified in paragraphs (h)(1), Directorate, Aircraft Certification Service.
(h)(2), or (h)(3) of this AD. [FR Doc. 2017–09324 Filed 5–8–17; 8:45 am]
Accordingly, under the authority
(1) Bombardier Service Bulletin 215–4457, BILLING CODE 4910–13–P
delegated to me by the Administrator, Revision 2, dated October 24, 2012.
the FAA proposes to amend 14 CFR part (2) Bombardier Service Bulletin 215–4457,
39 as follows: Revision 1, dated June 12, 2012. DEPARTMENT OF TRANSPORTATION
(3) Bombardier Service Bulletin 215–4457,
PART 39—AIRWORTHINESS dated April 4, 2012. Federal Aviation Administration
DIRECTIVES
(i) Other FAA AD Provisions
■ 1. The authority citation for part 39 The following provisions also apply to this 14 CFR Part 39
continues to read as follows: AD: [Docket No. FAA–2017–0334; Directorate
(1) Alternative Methods of Compliance Identifier 2017–NM–008–AD]
Authority: 49 U.S.C. 106(g), 40113, 44701. (AMOCs): The Manager, New York Aircraft
Certification Office (ACO), ANE–170, FAA, RIN 2120–AA64
§ 39.13 [Amended]
has the authority to approve AMOCs for this
■ 2. The FAA amends § 39.13 by adding AD, if requested using the procedures found Airworthiness Directives; Bombardier,
the following new airworthiness in 14 CFR 39.19. In accordance with 14 CFR Inc., Airplanes
directive (AD): 39.19, send your request to your principal
inspector or local Flight Standards District AGENCY: Federal Aviation
Bombardier, Inc. (Type Certificate
Office, as appropriate. If sending information Administration (FAA), DOT.
Previously Held by Canadair Limited):
Docket No. FAA–2017–0333; Directorate directly to the manager of the ACO, send it ACTION: Notice of proposed rulemaking
Identifier 2017–NM–005–AD. to ATTN: Program Manager, Continuing (NPRM).
Operational Safety, FAA, New York ACO,
(a) Comments Due Date 1600 Stewart Avenue, Suite 410, Westbury, SUMMARY: We propose to supersede
We must receive comments by June 23, NY 11590; telephone: 516–228–7300; fax: Airworthiness Directive (AD) 2014–25–
nlaroche on DSK30NT082PROD with PROPOSALS
2017. 516–794–5531. Before using any approved 01, for certain Bombardier, Inc., Model
AMOC, notify your appropriate principal DHC–8–400 series airplanes. AD 2014–
(b) Affected ADs inspector, or lacking a principal inspector,
25–01 currently requires modifying the
None. the manager of the local flight standards
district office/certificate holding district nose landing gear (NLG) trailing arm
(c) Applicability office. and installing a new pivot pin retention
This AD applies to Bombardier, Inc. (Type (2) Contacting the Manufacturer: For any mechanism. Since we issued AD 2014–
Certificate previously held by Canadair requirement in this AD to obtain corrective 25–01, we have received reports of
Limited) Model CL–215–6B11 (CL–415 actions from a manufacturer, the action must discrepancies of a certain bolt at the
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Document Created: 2018-11-08 08:41:10
Document Modified: 2018-11-08 08:41:10
| 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 June 23, 2017. | |
| Contact | Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-228-7318; fax: 516-794-5531. | |
| FR Citation | 82 FR 21482 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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