AD 2015-20-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Viking Air Limited | DHC-7-1 | Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes |
| aircraft | Viking Air Limited | DHC-7-100 | Airworthiness Directives; Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Airplanes |
Unsafe Condition
Reports of cracks discovered 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.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time detailed visual inspection for cracking in the outboard nacelles upper longeron channels and angles, in accordance with Viking Air Limited Service Bulletin V7-54-02, Revision NC. Repair any cracking found before further flight using an approved method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6 months after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Viking Air Limited (Type Certificate Previously Held by Bombardier, Inc.) Model DHC-7-1 and DHC-7-100 airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting 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 AD was prompted by reports of cracks that were discovered in the outboard nacelles upper longeron channels and angles. This AD requires a one-time detailed visual inspection for cracking in the outboard nacelles upper longeron channels and angles; and repair if necessary. 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.
Applicability Source Text
Show captured applicability text from the source AD
(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.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 80, Number 193 (Tuesday, October 6, 2015)]
[Rules and Regulations]
[Pages 60284-60286]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2015-25218]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-0684; Directorate Identifier 2014-NM-215-AD;
Amendment 39-18285; AD 2015-20-06]
RIN 2120-AA64
Airworthiness Directives; Viking Air Limited (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting 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 AD was prompted by
reports of cracks that were discovered in the outboard nacelles upper
longeron channels and angles. This AD requires a one-time detailed
visual inspection for cracking in the outboard nacelles upper longeron
channels and angles; and repair if necessary. 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.
DATES: This AD becomes effective November 10, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 10,
2015.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov/#!docketDetail">http://www.regulations.gov/#!docketDetail</a>;D=FAA-2015-0684 or in person at the
Docket Management Facility, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE., Washington, DC.
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
<a href="/cdn-cgi/l/email-protection#562233353e383f35373a782623343a3f3537223f39382516203f3d3f3831373f247835393b"><span class="__cf_email__" data-cfemail="d3a7b6b0bbbdbab0b2bffda3a6b1bfbab0b2a7babcbda093a5bab8babdb4b2baa1fdb0bcbe">[email protected]</span></a>; Internet <a href="http://www.vikingair.com">http://www.vikingair.com</a>. 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. It is also available on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2015-
0684.
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:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to all Viking Air Limited
(Type Certificate Previously Held by Bombardier, Inc.) Model DHC-7-1
and DHC-7-100 airplanes. The NPRM published in the Federal Register on
April 13, 2015 (80 FR 19572).
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2014-34, dated October 2, 2014, dated (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 <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;D=FAA-2015-0684-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (80 FR 19572, April 13,
2015) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed except for
minor editorial changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (80 FR 19572, April 13, 2015) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (80 FR 19572, April 13, 2015).
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. 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 of this AD.
Costs of Compliance
We estimate that this AD affects 10 airplanes of U.S. registry.
We also estimate that it will take about 3 work-hours per product
to comply with the basic requirements of this AD. The average labor
rate is $85 per work-hour. Based on these figures, we estimate the cost
of this 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 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.
[[Page 60285]]
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 AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under 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.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://www.regulations.gov/#!docketDetail">http://www.regulations.gov/#!docketDetail</a>;D=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 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2015-20-06 Viking Air Limited (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-18285. Docket No. FAA-2015-0684;
Directorate Identifier 2014-NM-215-AD.
(a) Effective Date
This AD becomes effective November 10, 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
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 <a href="http://www.regulations.gov/#!documentDetail">http://www.regulations.gov/#!documentDetail</a>;D=FAA-
2015-0684-0002.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Viking Air Limited Service Bulletin V7-54-02, Revision NC,
dated December 14, 2012.
(ii) Reserved.
(3) 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
<a href="/cdn-cgi/l/email-protection#c3b7a6a0abadaaa0a2afedb3b6a1afaaa0a2b7aaacadb083b5aaa8aaada4a2aab1eda0acae"><span class="__cf_email__" data-cfemail="c6b2a3a5aea8afa5a7aae8b6b3a4aaafa5a7b2afa9a8b586b0afadafa8a1a7afb4e8a5a9ab">[email protected]</span></a>; Internet <a href="http://www.vikingair.com">http://www.vikingair.com</a>.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
[[Page 60286]]
Issued in Renton, Washington, on September 27, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-25218 Filed 10-5-15; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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