80 FR 19572 - Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 70 (April 13, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 70 (April 13, 2015)
| Page Range | 19572-19574 | |
| FR Document | 2015-08074 |
[Federal Register Volume 80, Number 70 (Monday, April 13, 2015)] [Proposed Rules] [Pages 19572-19574] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-08074] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0684; Directorate Identifier 2014-NM-215-AD] RIN 2120-AA64 Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by 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 all Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Model DHC-7-1 and DHC-7-100 airplanes. This proposed AD was prompted by reports of cracks that were discovered in the outboard nacelles upper longeron channels and angles. This proposed AD would require a one-time detailed visual inspection for cracking in the outboard nacelles upper longeron channels and angles; and repair if necessary. We are proposing this AD to detect and correct cracks in the outboard nacelles upper longeron channels and angles, which could lead to the loss of stiffness in the forward engine mount; and possible catastrophic failure. DATES: We must receive comments on this proposed AD by May 28, 2015. 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: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Viking Air Limited, 9574 Hampden Road, Sidney, British Columbia V8L 8V5, Canada; telephone 250-656-7227; fax 250-656-0673; email technical.publications@vikingair.com; Internet http://www.vikingair.com. You may view this [[Page 19573]] 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-2015- 0684; 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, 1600 Stewart Avenue, Suite 410, Westbury, NY 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 proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2015-0684; Directorate Identifier 2014-NM-215-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- 2014-34, dated October 2, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Model DHC-7-1 and DHC-7-100 airplanes. The MCAI states: Longitudinal cracks were discovered in the outboard nacelles upper longeron channels and angles at station XN1 78. The cracks were partially hidden by bearing blocks, Part Number (P/N) 75420978, at the nacelle latch locations. Undetected, these cracks may lead to the loss of stiffness in the forward engine mount; which may lead to a catastrophic failure. Required actions include a one-time detailed visual inspection for cracking of the outboard nacelles upper longeron channels and angles. Corrective actions include repair, if necessary. 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-2015-0684. Related Service Information Under 1 CFR Part 51 Viking Air Limited has issued Service Bulletin V7-54-02, Revision NC, dated December 14, 2012. The service information describes procedures for an inspection for cracks in the outboard nacelles upper longeron channels and angles; and repair if necessary. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI. This service information is reasonably available; see ADDRESSES for ways to access this service information. 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 these same type designs. Costs of Compliance We estimate that this proposed AD affects 10 airplanes of U.S. registry. We also estimate that it would take about 3 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $2,550, or $255 per product. We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this proposed AD. 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: [[Page 19574]] 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): Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.): Docket No. FAA-2015-0684; Directorate Identifier 2014-NM-215- AD. (a) Comments Due Date We must receive comments by May 28, 2015. (b) Affected ADs None. (c) Applicability This AD applies to all Viking Air Limited (Type Certificate previously held by Bombardier, Inc.) Model DHC-7-1 and DHC-7-100 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 54, Nacelles/ Pylons. (e) Reason This AD was prompted by reports of cracks that were discovered in the outboard nacelles upper longeron channels and angles. We are issuing this AD to detect and correct cracks in the outboard nacelles upper longeron channels and angles, which could lead to the loss of stiffness in the forward engine mount; and possible catastrophic failure. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection and Repair Within 6 months after the effective date of this AD, do a one- time detailed visual inspection for cracking in the outboard nacelles upper longeron channels and angles, in accordance with the Accomplishment Instructions of Viking Air Limited Service Bulletin V7-54-02, Revision NC, dated December 14, 2012. If any cracking is found during the inspection required by this paragraph: Before further flight, repair using a method approved by the Manager, New York Aircraft Certification Office (ACO), ANE-170, FAA; or Transport Canada Civil Aviation (TCCA); or Viking Air Limited's (Type Certificate Previously Held by Bombardier, Inc.) TCCA Design Approval Organization (DAO). (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 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. The AMOC approval letter must specifically reference this AD. (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 TCCA; or Viking Air Limited's (Type Certificate Previously Held by Bombardier, Inc.) TCCA DAO. If approved by the DAO, the approval must include the DAO-authorized signature. (i) Special Flight Permits Special flight permits, as described in Section 21.197 and Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199), are not allowed. (j) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Canadian Airworthiness Directive CF-2014-34, dated October 2, 2014, 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-2015-0684. (2) For service information identified in this AD, contact Viking Air Limited, 9574 Hampden Road, Sidney, British Columbia V8L 8V5, Canada; telephone 250-656-7227; fax 250-656-0673; email technical.publications@vikingair.com; Internet http://www.vikingair.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 27, 2015. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-08074 Filed 4-10-15; 8:45 am] BILLING CODE 4910-13-P
![19572 Federal Register / Vol. 80, No. 70 / Monday, April 13, 2015 / Proposed Rules
4. Will not have a significant having part number (P/N) 38026–4–0280–000 DEPARTMENT OF TRANSPORTATION
economic impact, positive or negative, with new, improved assemblies having P/N
on a substantial number of small entities 601R44045–1, in accordance with the Federal Aviation Administration
under the criteria of the Regulatory Accomplishment Instructions of Bombardier
Flexibility Act. Service Bulletin 601R–35–018, dated May 21, 14 CFR Part 39
2013.
List of Subjects in 14 CFR Part 39 [Docket No. FAA–2015–0684; Directorate
(h) Parts Installation Prohibition Identifier 2014–NM–215–AD]
Air transportation, Aircraft, Aviation
safety, Incorporation by reference, As of the effective date of this AD, no RIN 2120–AA64
person may install an oxygen hose assembly,
Safety.
P/N 38026–4–0280–000, on any airplane. Airworthiness Directives; Viking Air
The Proposed Amendment Limited (Type Certificate Previously
(i) Other FAA AD Provisions
Accordingly, under the authority Held by Bombardier, Inc.) Airplanes
The following provisions also apply to this
delegated to me by the Administrator, AD: AGENCY: Federal Aviation
the FAA proposes to amend 14 CFR part (1) Alternative Methods of Compliance Administration (FAA), DOT.
39 as follows: (AMOCs): The Manager, New York Aircraft ACTION: Notice of proposed rulemaking
Certification Office (ACO), ANE–170, FAA, (NPRM).
PART 39—AIRWORTHINESS has the authority to approve AMOCs for this
DIRECTIVES AD, if requested using the procedures found SUMMARY: We propose to adopt a new
■ 1. The authority citation for part 39 in 14 CFR 39.19. Send information to ATTN: airworthiness directive (AD) for all
Program Manager, Continuing Operational Viking Air Limited (Type Certificate
continues to read as follows:
Safety, FAA, New York ACO, 1600 Stewart Previously Held by Bombardier, Inc.)
Authority: 49 U.S.C. 106(g), 40113, 44701. Avenue, Suite 410, Westbury, NY 11590; Model DHC–7–1 and DHC–7–100
telephone 516–228–7300; fax 516–794–5531. airplanes. This proposed AD was
§ 39.13 [Amended]
Before using any approved AMOC, notify
■ 2. The FAA amends § 39.13 by adding prompted by reports of cracks that were
your appropriate principal inspector, or
the following new airworthiness discovered in the outboard nacelles
lacking a principal inspector, the manager of
directive (AD): the local flight standards district office/
upper longeron channels and angles.
certificate holding district office. The AMOC This proposed AD would require a one-
Bombardier, Inc.: Docket No. FAA–2015–
0823; Directorate Identifier 2014–NM– approval letter must specifically reference time detailed visual inspection for
211–AD. this AD. cracking in the outboard nacelles upper
(2) Contacting the Manufacturer: For any longeron channels and angles; and
(a) Comments Due Date repair if necessary. We are proposing
requirement in this AD to obtain corrective
We must receive comments by May 28, actions from a manufacturer, the action must this AD to detect and correct cracks in
2015. be accomplished using a method approved the outboard nacelles upper longeron
(b) Affected ADs by the Manager, New York ACO, ANE–170, channels and angles, which could lead
None.
FAA; or Transport Canada Civil Aviation to the loss of stiffness in the forward
(TCCA); or Bombardier, Inc.’s TCCA Design engine mount; and possible catastrophic
(c) Applicability Approval Organization (DAO). If approved by failure.
This AD applies to Bombardier, Inc. Model the DAO, the approval must include the DATES: We must receive comments on
CL–600–2B19 (Regional Jet Series 100 & 440) DAO-authorized signature.
this proposed AD by May 28, 2015.
airplanes, certificated in any category, serial
(j) Related Information ADDRESSES: You may send comments,
numbers 7003 and subsequent.
(1) Refer to Mandatory Continuing using the procedures found in 14 CFR
(d) Subject Airworthiness Information (MCAI) Canadian 11.43 and 11.45, by any of the following
Air Transport Association (ATA) of Airworthiness Directive CF–2014–36, dated methods:
America Code 35, Oxygen. October 17, 2014, for related information. • Federal eRulemaking Portal: Go to
(e) Reason This MCAI may be found in the AD docket http://www.regulations.gov. Follow the
on the Internet at http://www.regulations.gov instructions for submitting comments.
This AD was prompted by results of a
design review indicating that the burst
by searching for and locating Docket No. • Fax: 202–493–2251.
pressure of the flexible hose, used to vent
FAA–2015–0823. • Mail: U.S. Department of
(2) For service information identified in Transportation, Docket Operations, M–
oxygen from the high-pressure relief valve of
the oxygen cylinder overboard, was lower this AD, contact Bombardier, Inc., 400 Côte- 30, West Building Ground Floor, Room
than the opening pressure of the high- Vertu Road West, Dorval, Québec H4S 1Y9, W12–140, 1200 New Jersey Avenue SE.,
pressure relief valve, which could cause the Canada; telephone 514–855–5000; fax 514–
Washington, DC 20590.
855–7401; email thd.crj@
flexible hose to burst before it can vent the • Hand Delivery: U.S. Department of
excess oxygen overboard. We are issuing this aero.bombardier.com; Internet http://
Transportation, Docket Operations, M–
AD to prevent the accumulation of oxygen in www.bombardier.com. You may view this
service information at the FAA, Transport
30, West Building Ground Floor, Room
an enclosed space, which could result in an
uncontrolled oxygen-fed fire if an ignition Airplane Directorate, 1601 Lind Avenue SW., W12–140, 1200 New Jersey Avenue SE.,
source is nearby. Renton, WA. For information on the Washington, DC, between 9 a.m. and 5
availability of this material at the FAA, call p.m., Monday through Friday, except
wreier-aviles on DSK5TPTVN1PROD with PROPOSALS
(f) Compliance Federal holidays.
425–227–1221.
Comply with this AD within the For service information identified in
compliance times specified, unless already Issued in Renton, Washington, on March
this proposed AD, contact Viking Air
done. 27, 2015.
Limited, 9574 Hampden Road, Sidney,
Michael Kaszycki, British Columbia V8L 8V5, Canada;
(g) Replacement
Acting Manager, Transport Airplane telephone 250–656–7227; fax 250–656–
Before the accumulation of 5,800 total
Directorate, Aircraft Certification Service. 0673; email technical.publications@
flight hours or within 44 months after the
effective date of this AD, whichever occurs [FR Doc. 2015–08073 Filed 4–10–15; 8:45 am] vikingair.com; Internet http://
first, replace all oxygen hose assemblies BILLING CODE 4910–13–P www.vikingair.com. You may view this
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![19574 Federal Register / Vol. 80, No. 70 / Monday, April 13, 2015 / Proposed Rules
Authority: 49 U.S.C. 106(g), 40113, 44701. Safety, FAA, New York ACO, 1600 Stewart SUMMARY: We propose to adopt a new
Avenue, Suite 410, Westbury, NY 11590; airworthiness directive (AD) for certain
§ 39.13 [Amended] telephone 516–228–7300; fax 516–794–5531. Bombardier, Inc. Model CL–600–2C10
■ 2. The FAA amends § 39.13 by adding Before using any approved AMOC, notify
(Regional Jet Series 700, 701, & 702)
the following new airworthiness your appropriate principal inspector, or
lacking a principal inspector, the manager of airplanes, Model CL–600–2D15
directive (AD): (Regional Jet Series 705) airplanes,
the local flight standards district office/
Viking Air Limited (Type Certificate certificate holding district office. The AMOC Model CL–600–2D24 (Regional Jet
Previously Held by Bombardier, Inc.): approval letter must specifically reference Series 900) airplanes, and Model CL–
Docket No. FAA–2015–0684; Directorate this AD. 600–2E25 (Regional Jet Series 1000)
Identifier 2014–NM–215–AD. (2) Contacting the Manufacturer: For any airplanes. This proposed AD was
requirement in this AD to obtain corrective
(a) Comments Due Date prompted by results of a design review
actions from a manufacturer, the action must
We must receive comments by May 28, be accomplished using a method approved indicating that the burst pressure of the
2015. by the Manager, New York ACO, ANE–170, flexible hose, used to vent oxygen from
FAA; or TCCA; or Viking Air Limited’s (Type the high-pressure relief valve of the
(b) Affected ADs
Certificate Previously Held by Bombardier, oxygen cylinder overboard, was lower
None. Inc.) TCCA DAO. If approved by the DAO, than the opening pressure of the high-
(c) Applicability the approval must include the DAO- pressure relief valve, which could cause
authorized signature. the flexible hose to burst before it can
This AD applies to all Viking Air Limited
(Type Certificate previously held by (i) Special Flight Permits vent the excess oxygen overboard. This
Bombardier, Inc.) Model DHC–7–1 and DHC– Special flight permits, as described in proposed AD would require replacing
7–100 airplanes, certificated in any category. Section 21.197 and Section 21.199 of the the oxygen hose assembly with a new,
(d) Subject Federal Aviation Regulations (14 CFR 21.197 improved assembly. We are proposing
and 21.199), are not allowed. this AD to prevent the accumulation of
Air Transport Association (ATA) of oxygen in an enclosed space, which
America Code 54, Nacelles/Pylons. (j) Related Information
could result in an uncontrolled oxygen-
(e) Reason (1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
fed fire if an ignition source is nearby.
This AD was prompted by reports of cracks Airworthiness Directive CF–2014–34, dated DATES: We must receive comments on
that were discovered in the outboard nacelles October 2, 2014, for related information. This this proposed AD by May 28, 2015.
upper longeron channels and angles. We are MCAI may be found in the AD docket on the ADDRESSES: You may send comments by
issuing this AD to detect and correct cracks Internet at http://www.regulations.gov by
in the outboard nacelles upper longeron any of the following methods:
searching for and locating Docket No. FAA–
channels and angles, which could lead to the 2015–0684. • Federal eRulemaking Portal: Go to
loss of stiffness in the forward engine mount; (2) For service information identified in http://www.regulations.gov. Follow the
and possible catastrophic failure. this AD, contact Viking Air Limited, 9574 instructions for submitting comments.
Hampden Road, Sidney, British Columbia • Fax: (202) 493–2251.
(f) Compliance
V8L 8V5, Canada; telephone 250–656–7227; • Mail: U.S. Department of
Comply with this AD within the fax 250–656–0673; email Transportation, Docket Operations, M–
compliance times specified, unless already technical.publications@vikingair.com; 30, West Building Ground Floor, Room
done. Internet http://www.vikingair.com. You may W12–140, 1200 New Jersey Avenue SE.,
(g) Inspection and Repair view this service information at the FAA,
Transport Airplane Directorate, 1601 Lind
Washington, DC 20590.
Within 6 months after the effective date of Avenue SW., Renton, WA. For information • Hand Delivery: U.S. Department of
this AD, do a one-time detailed visual on the availability of this material at the Transportation, Docket Operations, M–
inspection for cracking in the outboard FAA, call 425–227–1221. 30, West Building Ground Floor, Room
nacelles upper longeron channels and angles, W12–140, 1200 New Jersey Avenue SE.,
in accordance with the Accomplishment Issued in Renton, Washington, on March
27, 2015. Washington, DC, between 9 a.m. and 5
Instructions of Viking Air Limited Service
Michael Kaszycki, p.m., Monday through Friday, except
Bulletin V7–54–02, Revision NC, dated
December 14, 2012. If any cracking is found Federal holidays.
Acting Manager, Transport Airplane
during the inspection required by this Directorate, Aircraft Certification Service. For service information identified in
paragraph: Before further flight, repair using this proposed AD, contact Bombardier,
[FR Doc. 2015–08074 Filed 4–10–15; 8:45 am]
a method approved by the Manager, New Inc., 400 Côte-Vertu Road West, Dorval,
BILLING CODE 4910–13–P
York Aircraft Certification Office (ACO), Québec H4S 1Y9, Canada; telephone
ANE–170, FAA; or Transport Canada Civil 514–855–5000; fax 514–855–7401; email
Aviation (TCCA); or Viking Air Limited’s thd.crj@aero.bombardier.com; Internet
(Type Certificate Previously Held by DEPARTMENT OF TRANSPORTATION
http://www.bombardier.com. You may
Bombardier, Inc.) TCCA Design Approval
Federal Aviation Administration view this referenced service information
Organization (DAO).
at the FAA, Transport Airplane
(h) Other FAA AD Provisions 14 CFR Part 39 Directorate, 1601 Lind Avenue SW.,
The following provisions also apply to this Renton, WA. For information on the
AD: [Docket No. FAA–2015–0822; Directorate availability of this material at the FAA,
(1) Alternative Methods of Compliance Identifier 2014–NM–210–AD]
call 425–227–1221.
wreier-aviles on DSK5TPTVN1PROD with PROPOSALS
(AMOCs): The Manager, New York Aircraft RIN 2120–AA64
Certification Office (ACO), ANE–170, FAA, Examining the AD Docket
has the authority to approve AMOCs for this Airworthiness Directives; Bombardier, You may examine the AD docket on
AD, if requested using the procedures found Inc. Airplanes the Internet at http://
in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal AGENCY: Federal Aviation www.regulations.gov by searching for
inspector or local Flight Standards District Administration (FAA), DOT. and locating Docket No. FAA–2015–
Office, as appropriate. If sending information 0822; or in person at the Docket
ACTION: Notice of proposed rulemaking
directly to the ACO, send it to ATTN: Management Facility between 9 a.m.
(NPRM).
Program Manager, Continuing Operational and 5 p.m., Monday through Friday,
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Document Created: 2015-12-18 11:22:25
Document Modified: 2015-12-18 11:22:25
| 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 28, 2015. | |
| Contact | Aziz Ahmed, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228 7329; fax 516-794 5531. | |
| FR Citation | 80 FR 19572 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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