82 FR 14837 - Airworthiness Directives; Bombardier, Inc. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 55 (March 23, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 55 (March 23, 2017)
| Page Range | 14837-14839 | |
| FR Document | 2017-05520 |
[Federal Register Volume 82, Number 55 (Thursday, March 23, 2017)] [Proposed Rules] [Pages 14837-14839] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-05520] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9387; Directorate Identifier 2016-NM-182-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-100-1A10 airplanes. This proposed AD was prompted by a report that the equipment racks were not designed to support the weight of all the equipment and the secondary direct current power centers. This proposed AD would require modifying the equipment racks. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by May 8, 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-2016- 9387; 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: Aziz Ahmed, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY [[Page 14838]] 11590; telephone: 516-228-7329; 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-2016-9387; Directorate Identifier 2016-NM-182-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 Airworthiness Directive CF- 2016-26, dated September 14, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Bombardier, Inc. Model BD-100- 1A10 airplanes. The MCAI states: During a recent design review, a Bombardier equipment supplier discovered that the weight of the Secondary Direct Current (DC) Power Center was incorrectly reported to the structural partner(s) via their equipment interface drawing. Consequently, the left-hand side (LHS) and right-hand side (RHS) equipment racks were not designed to support the actual weight of all the equipment and the Secondary DC Power Centers under all loading conditions. In the event of a high energy emergency landing or runway excursion, the structural failure of the LHS or RHS equipment racks may result in the blockage of the emergency escape route for the pilot(s) and crew if this condition is not corrected. Required actions include modifying the equipment racks. 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-2016- 9387. Related Service Information Under 1 CFR Part 51 We reviewed Bombardier Service Bulletin 100-25-39, dated October 26, 2015; and Bombardier Service Bulletin 350-25-002, dated October 26, 2015. This service information describes procedures for modifying the equipment racks. These documents are distinct since they apply to airplanes having different serial numbers. 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 161 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost on U.S. Action Labor cost Parts cost Cost per product operators ---------------------------------------------------------------------------------------------------------------- Modify equipment racks......... Up to 10 work-hours x $1,755 Up to $2,605........ Up to $419,405. $85 per hour = $850. ---------------------------------------------------------------------------------------------------------------- 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. 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. [[Page 14839]] 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-2016-9387; Directorate Identifier 2016-NM-182-AD. (a) Comments Due Date We must receive comments by May 8, 2017. (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc. Model BD-100-1A10 airplanes, certificated in any category, serial numbers (S/Ns) 20003 through 20532 inclusive. (d) Subject Air Transport Association (ATA) of America Code 25, Equipment/ Furnishings. (e) Reason This AD was prompted by a recent design review of the equipment racks which revealed that the left-hand side (LHS) and right-hand side (RHS) equipment racks were not designed to support the actual weight of all the equipment and the secondary direct current power centers under all loading conditions. We are issuing this AD to prevent structural failure of the LHS or RHS equipment racks in the event of a high energy emergency landing or runway excursion, which could result in blockage of the emergency exit for the flightcrew. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Modification of the Equipment Racks Within 90 months after the effective date of this AD, do the modification required by paragraph (g)(1) or (g)(2) of this AD, as applicable. (1) For airplanes having S/Ns 20003 through 20500 inclusive: Modify the equipment racks having part numbers (P/Ns) K1000070316- 003 (LHS) and K1000070316-004 (RHS), in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 100-25- 39, dated October 26, 2015. (2) For airplanes having S/Ns 20501 through 20532 inclusive: Modify the equipment rack having P/N K1000070316-004 (RHS only), in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 350-25-002, dated October 26, 2015. (h) 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 New York 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 Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (i) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian Airworthiness Directive CF-2016-26, dated September 14, 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-2016-9387. (2) 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 March 14, 2017. Dionne Palermo, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-05520 Filed 3-22-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 55 / Thursday, March 23, 2017 / Proposed Rules 14837
(d) Subject ACO, to make those findings. To be We propose to adopt a new
SUMMARY:
Air Transport Association (ATA) of approved, the repair method, modification airworthiness directive (AD) for certain
America Code 53; Fuselage. deviation, or alteration deviation must meet Bombardier, Inc. Model BD–100–1A10
the certification basis of the airplane, and the
(e) Unsafe Condition approval must specifically refer to this AD.
airplanes. This proposed AD was
(4) For service information that contains prompted by a report that the
This AD was prompted by a report of equipment racks were not designed to
fatigue cracking found in a certain fuselage steps that are labeled as Required for
frame common to the water tank support Compliance (RC), the provisions of support the weight of all the equipment
intercostal clip located between certain and the secondary direct current power
paragraphs (i)(4)(i) and (i)(4)(ii) of this AD
stringers. We are issuing this AD to detect apply. centers. This proposed AD would
and correct cracking, which could grow in (i) The steps labeled as RC, including require modifying the equipment racks.
substeps under an RC step and any figures
size and result in a severed frame. Multiple We are proposing this AD to address the
identified in an RC step, must be done to
adjacent severed frames would result in unsafe condition on these products.
comply with the AD. If a step or substep is
reduced structural integrity of the airplane. DATES: We must receive comments on
labeled ‘‘RC Exempt,’’ then the RC
(f) Compliance requirement is removed from that step or this proposed AD by May 8, 2017.
substep. An AMOC is required for any ADDRESSES: You may send comments,
Comply with this AD within the
deviations to RC steps, including substeps
compliance times specified, unless already
and identified figures.
using the procedures found in 14 CFR
done. 11.43 and 11.45, by any of the following
(ii) Steps not labeled as RC may be
(g) Inspection deviated from using accepted methods in methods:
accordance with the operator’s maintenance • Federal eRulemaking Portal: Go to
Before the accumulation of 34,000 total
flight cycles or within 6,000 flight cycles
or inspection program without obtaining http://www.regulations.gov. Follow the
approval of an AMOC, provided the RC steps, instructions for submitting comments.
after the effective date of this AD, whichever
occurs later, do a high frequency eddy
including substeps and identified figures, can • Fax: 202–493–2251.
current (HFEC) inspection for any cracking in
still be done as specified, and the airplane • Mail: U.S. Department of
can be put back in an airworthy condition. Transportation, Docket Operations, M–
the fuselage frame at station (STA) 947.5
common to the water tank support intercostal (j) Related Information 30, West Building Ground Floor, Room
clip located between stringer S–24R and S– (1) For more information about this AD, W12–140, 1200 New Jersey Avenue SE.,
25R, in accordance with the Accomplishment contact Galib Abumeri, Aerospace Engineer, Washington, DC 20590.
Instructions of Boeing Alert Service Bulletin Airframe Branch, ANM–120L, FAA, Los • Hand Delivery: Deliver to Mail
737–53A1357, dated August 9, 2016. Angeles ACO, 3960 Paramount Boulevard, address above between 9 a.m. and 5
(1) If no cracking is found, repeat the Lakewood, CA 90712–4137; phone: 562–627– p.m., Monday through Friday, except
inspection thereafter at intervals not to 5324; fax: 562–627–5210; email:
exceed 12,000 flight cycles. Federal holidays.
galib.abumeri@faa.gov.
(2) If any cracking is found: Before further For service information identified in
(2) For service information identified in
flight, repair in accordance with the this AD, contact Boeing Commercial this NPRM, contact Bombardier, Inc.,
Accomplishment Instructions of Boeing Alert Airplanes, Attention: Contractual & Data 400 Côte-Vertu Road West, Dorval,
Service Bulletin 737–53A1357, dated August Services (C&DS), 2600 Westminster Blvd., Québec H4S 1Y9, Canada; telephone:
9, 2016. MC 110–SK57, Seal Beach, CA 90740–5600; 514–855–5000; fax: 514–855–7401;
(h) Terminating Action telephone 562–797–1717; Internet https:// email: thd.crj@aero.bombardier.com;
www.myboeingfleet.com. You may view this Internet http://www.bombardier.com.
Accomplishing the repair in accordance referenced service information at the FAA,
with the Accomplishment Instructions of You may view this referenced service
Transport Airplane Directorate, 1601 Lind
Boeing Alert Service Bulletin 737–53A1357, information at the FAA, Transport
Avenue SW., Renton, WA. For information
dated August 9, 2016, terminates the on the availability of this material at the Airplane Directorate, 1601 Lind Avenue
inspection requirements of paragraph (g) of FAA, call 425–227–1221. SW., Renton, WA. For information on
this AD. the availability of this material at the
Issued in Renton, Washington, on March
(i) Alternative Methods of Compliance 14, 2017.
FAA, call 425–227–1221.
(AMOCs) Dionne Palermo, Examining the AD Docket
(1) The Manager, Los Angeles Aircraft Acting Manager, Transport Airplane You may examine the AD docket on
Certification Office (ACO), FAA, has the Directorate, Aircraft Certification Service.
authority to approve AMOCs for this AD, if the Internet at http://
[FR Doc. 2017–05519 Filed 3–22–17; 8:45 am] www.regulations.gov by searching for
requested using the procedures found in 14
CFR 39.19. In accordance with 14 CFR 39.19, BILLING CODE 4910–13–P and locating Docket No. FAA–2016–
send your request to your principal inspector 9387; or in person at the Docket
or local Flight Standards District Office, as Management Facility between 9 a.m.
appropriate. If sending information directly DEPARTMENT OF TRANSPORTATION and 5 p.m., Monday through Friday,
to the manager of the ACO, send it to the except Federal holidays. The AD docket
attention of the person identified in Federal Aviation Administration
contains this proposed AD, the
paragraph (j)(1) of this AD. Information may
regulatory evaluation, any comments
be emailed to: 9-ANM-LAACO-AMOC- 14 CFR Part 39
Requests@faa.gov. received, and other information. The
(2) Before using any approved AMOC, [Docket No. FAA–2016–9387; Directorate street address for the Docket Operations
notify your appropriate principal inspector, Identifier 2016–NM–182–AD] office (telephone 800–647–5527) is in
or lacking a principal inspector, the manager RIN 2120–AA64 the ADDRESSES section. Comments will
sradovich on DSK3GMQ082PROD with PROPOSALS
of the local flight standards district office/ be available in the AD docket shortly
certificate holding district office. Airworthiness Directives; Bombardier, after receipt.
(3) An AMOC that provides an acceptable Inc. Airplanes FOR FURTHER INFORMATION CONTACT: Aziz
level of safety may be used for any repair,
modification, or alteration required by this AGENCY: Federal Aviation Ahmed, Aerospace Engineer, Airframe
AD if it is approved by the Boeing Administration (FAA), DOT. and Mechanical Systems Branch, ANE–
Commercial Airplanes Organization 171, FAA, New York Aircraft
ACTION: Notice of proposed rulemaking
Designation Authorization (ODA) that has Certification Office (ACO), 1600 Stewart
(NPRM).
been authorized by the Manager, Los Angeles Avenue, Suite 410, Westbury, NY
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![Federal Register / Vol. 82, No. 55 / Thursday, March 23, 2017 / Proposed Rules 14839
§ 39.13 [Amended] inspector or local Flight Standards District at Soldotna Airport, Soldotna, AK. After
■ 2. The FAA amends § 39.13 by adding Office, as appropriate. If sending information review of the airspace, the FAA found
the following new airworthiness directly to the New York ACO, send it to redesign is necessary due to procedure
ATTN: Program Manager, Continuing
directive (AD): modifications. The FAA also proposes
Operational Safety, FAA, New York ACO,
Bombardier, Inc.: Docket No. FAA–2016– 1600 Stewart Avenue, Suite 410, Westbury, to remove the reference to the Soldotna
9387; Directorate Identifier 2016–NM– NY 11590; telephone: 516–228–7300; fax: nondirectional radio beacon (NDB) in
182–AD. 516–794–5531. Before using any approved the legal description. This action would
AMOC, notify your appropriate principal enhance the safety and management of
(a) Comments Due Date
inspector, or lacking a principal inspector, IFR operations at the airport.
We must receive comments by May 8, the manager of the local flight standards DATES: Comments must be received on
2017. district office/certificate holding district or before May 8, 2017.
(b) Affected ADs office.
(2) Contacting the Manufacturer: For any ADDRESSES: Send comments on this
None. requirement in this AD to obtain corrective proposal to the U.S. Department of
(c) Applicability actions from a manufacturer, the action must Transportation, Docket Operations, 1200
be accomplished using a method approved New Jersey Avenue SE., West Building
This AD applies to Bombardier, Inc. Model
BD–100–1A10 airplanes, certificated in any
by the Manager, New York ACO, ANE–170, Ground Floor, Room W12–140,
FAA; or Transport Canada Civil Aviation Washington, DC 20590; telephone: 1–
category, serial numbers (S/Ns) 20003
through 20532 inclusive. (TCCA); or Bombardier, Inc.’s TCCA Design 800–647–5527, or (202) 366–9826. You
Approval Organization (DAO). If approved by must identify FAA Docket No. FAA–
(d) Subject the DAO, the approval must include the
DAO-authorized signature.
2016–9588; Airspace Docket No. 16–
Air Transport Association (ATA) of AAL–5, at the beginning of your
America Code 25, Equipment/Furnishings. (i) Related Information comments. You may also submit
(e) Reason (1) Refer to Mandatory Continuing comments through the Internet at http://
This AD was prompted by a recent design Airworthiness Information (MCAI) Canadian www.regulations.gov. You may review
review of the equipment racks which Airworthiness Directive CF–2016–26, dated the public docket containing the
revealed that the left-hand side (LHS) and September 14, 2016, for related information. proposal, any comments received, and
right-hand side (RHS) equipment racks were This MCAI may be found in the AD docket any final disposition in person in the
not designed to support the actual weight of on the Internet at http://www.regulations.gov
by searching for and locating Docket No.
Dockets Office between 9:00 a.m. and
all the equipment and the secondary direct 5:00 p.m., Monday through Friday,
current power centers under all loading FAA–2016–9387.
conditions. We are issuing this AD to prevent (2) For service information identified in except federal holidays.
structural failure of the LHS or RHS this AD, contact Bombardier, Inc., 400 Côte- FAA Order 7400.11A, Airspace
equipment racks in the event of a high energy Vertu Road West, Dorval, Québec H4S 1Y9, Designations and Reporting Points, and
emergency landing or runway excursion, Canada; telephone: 514–855–5000; fax: 514– subsequent amendments can be viewed
which could result in blockage of the 855–7401; email: thd.crj@ online at http://www.faa.gov/air_traffic/
emergency exit for the flightcrew. aero.bombardier.com; Internet http:// publications/. For further information,
www.bombardier.com. You may view this you can contact the Airspace Policy
(f) Compliance service information at the FAA, Transport Group, Federal Aviation
Comply with this AD within the Airplane Directorate, 1601 Lind Avenue SW.,
Renton, WA. For information on the
Administration, 800 Independence
compliance times specified, unless already
done. availability of this material at the FAA, call Avenue SW, Washington, DC, 20591;
425–227–1221. telephone: 202–267–8783. The Order is
(g) Modification of the Equipment Racks also available for inspection at the
Issued in Renton, Washington, on March
Within 90 months after the effective date
14, 2017.
National Archives and Records
of this AD, do the modification required by Administration (NARA). For
paragraph (g)(1) or (g)(2) of this AD, as Dionne Palermo,
information on the availability of FAA
applicable. Acting Manager, Transport Airplane Order 7400.11A at NARA, call 202–741–
(1) For airplanes having S/Ns 20003 Directorate, Aircraft Certification Service.
6030, or go to http://www.archives.gov/
through 20500 inclusive: Modify the [FR Doc. 2017–05520 Filed 3–22–17; 8:45 am]
equipment racks having part numbers (P/Ns)
federal_register/code_of_federal-
BILLING CODE 4910–13–P regulations/ibr_locations.html.
K1000070316–003 (LHS) and K1000070316–
004 (RHS), in accordance with the FAA Order 7400.11, Airspace
Accomplishment Instructions of Bombardier Designations and Reporting Points, is
DEPARTMENT OF TRANSPORTATION published yearly and effective on
Service Bulletin 100–25–39, dated October
26, 2015.
Federal Aviation Administration September 15.
(2) For airplanes having S/Ns 20501 FOR FURTHER INFORMATION CONTACT:
through 20532 inclusive: Modify the Robert LaPlante, Federal Aviation
equipment rack having P/N K1000070316– 14 CFR Part 71
Administration, Operations Support
004 (RHS only), in accordance with the [Docket No. FAA–2016–9588; Airspace
Accomplishment Instructions of Bombardier Group, Western Service Center, 1601
Docket No. 16–AAL–5] Lind Avenue SW., Renton, WA 98057;
Service Bulletin 350–25–002, dated October
26, 2015. Proposed Amendment of Class E telephone (425) 203–4566.
Airspace, Soldotna, AK SUPPLEMENTARY INFORMATION:
(h) Other FAA AD Provisions
sradovich on DSK3GMQ082PROD with PROPOSALS
The following provisions also apply to this AGENCY: Federal Aviation Authority for This Rulemaking
AD: Administration (FAA), DOT. The FAA’s authority to issue rules
(1) Alternative Methods of Compliance
ACTION: Notice of proposed rulemaking regarding aviation safety is found in
(AMOCs): The Manager, New York Aircraft
Certification Office (ACO), ANE–170, FAA, (NPRM). Title 49 of the United States Code.
has the authority to approve AMOCs for this Subtitle I, Section 106 describes the
AD, if requested using the procedures found SUMMARY: This action proposes to authority of the FAA Administrator.
in 14 CFR 39.19. In accordance with 14 CFR modify Class E airspace extending Subtitle VII, Aviation Programs,
39.19, send your request to your principal upward from 700 feet above the surface describes in more detail the scope of the
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Document Created: 2017-03-23 02:45:33
Document Modified: 2017-03-23 02:45:33
| 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 May 8, 2017. | |
| Contact | Aziz Ahmed, 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: 516-228-7329; fax: 516-794-5531. | |
| FR Citation | 82 FR 14837 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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