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[Federal Register Volume 80, Number 137 (Friday, July 17, 2015)]
[Rules and Regulations]
[Pages 42373-42376]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-16580]

========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
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Federal Register / Vol. 80, No. 137 / Friday, July 17, 2015 / Rules 
and Regulations

[[Page 42373]]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0570; Directorate Identifier 2013-NM-094-AD; 
Amendment 39-18201; AD 2015-14-03]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, 
and -315 airplanes. This AD was prompted by fuel system reviews 
conducted by the manufacturer. This AD requires revising the 
maintenance or inspection program, as applicable, to incorporate new 
limitations for fuel tank systems. We are issuing this AD to prevent 
potential ignition sources within the fuel system, which could result 
in a fuel tank explosion.

DATES: This AD becomes effective August 21, 2015.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of August 21, 
2015.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-0570 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 Bombardier, 
Inc., Q-Series Technical Help Desk, 123 Garratt Boulevard, Toronto, 
Ontario M3K 1Y5, Canada; telephone: 416-375-4000; fax: 416-375-4539; 
email: thd.qseries@aero.bombardier.com; 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. It is also available on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2014-
0570.

FOR FURTHER INFORMATION CONTACT: Morton Lee, Aerospace Engineer, 
Propulsion & Services Branch, ANE-173; FAA, New York Aircraft 
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, 
NY 11590; telephone: 516-228-7355; 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 certain Bombardier, Inc. 
Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 
airplanes. The NPRM published in the Federal Register on August 18, 
2014 (79 FR 48703).
    Transport Canada Civil Aviation (TCCA), which is the aviation 
authority for Canada, has issued Canadian Airworthiness Directive CF-
2007-32R2, dated June 27, 2013 (referred to after this as the Mandatory 
Continuing Airworthiness Information, or ``the MCAI''), to correct an 
unsafe condition on certain Bombardier, Inc. Model DHC-8-102, -103, -
106, -201, -202, -301, -311, and -315 airplanes. The MCAI states:

    Bombardier Aerospace has completed a system safety review of the 
aeroplanes fuel system against fuel tank safety standards * * *. The 
identified non-compliances were then assessed * * *, to determine if 
mandatory corrective action is required.
    The assessment showed that supplemental maintenance tasks are 
required to prevent potential ignition sources within the fuel 
system, which could result in a fuel tank explosion. Revisions have 
been made to Part 2 ``Airworthiness Limitations List'' of the DHC-8 
Maintenance Program Manuals to introduce the required maintenance 
tasks.
    Revision 1 of this [Canadian] AD was issued to clarify the 
phase-in schedule for tasks FSL-02 and FSL-17.
    Revision 2 of this [Canadian] AD is issued to correct the 
effective date of [Canadian] AD CF-2013-07 [http://www.casa.gov.au/scripts/nc.dll?WCMS:OLDASSET::svPath=/ADFiles/over/dhc-8/,svFileName=CF-2013-07.pdf] referenced in Part III of the Corrective 
Actions and to clarify the revised phase-in schedules in Part II and 
Part III of the Corrective Actions.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0570-0002.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (79 FR 48703, August 18, 
2014) or on the determination of the cost to the public.

Changes to This Final Rule

    Since the NPRM (79 FR 48703, August 18, 2014) was published, the 
information in Bombardier Temporary Revision (TR) AWL-110, dated August 
31, 2007, to Part 2, ``Airworthiness Limitations List,'' of the 
Bombardier Dash 8 Series 100 Maintenance Program Manual, Product 
Support Manual PSM 1-8-7, has been merged in Subject 5-FSL of Section 
5, ``Fuel System Limitations,'' of the ``Airworthiness Limitations 
List,'' of the Bombardier Dash 8 Series 100 Maintenance Program Manual, 
PSM 1-8-7, Revision 18, dated February 23, 2012. We have removed 
paragraph (g)(1) of the proposed AD that referred to Bombardier TR AWL-
110, dated August 31, 2007, to Part 2, ``Airworthiness Limitations 
List,'' of the Bombardier Dash 8 Series 100 Maintenance Program Manual, 
Product Support Manual PSM 1-8-7, and we have redesignated paragraph 
(g)(2) of the proposed AD as paragraph (g)(1) of this AD. We have also 
added new paragraph (g)(5) of this AD to refer to Subject 5-FSL of 
Section 5, ``Fuel System Limitations,'' of the ``Airworthiness 
Limitations List,'' of the Bombardier Dash 8 Series 100 Maintenance 
Program Manual, PSM 1-8-7, Revision 18, dated February 23, 2012.
    We have included a new paragraph (j) in this AD to provide credit 
for accomplishing the revision to the maintenance or inspection 
program, as

[[Page 42374]]

applicable, to incorporate new limitations for fuel tank systems before 
the effective date of this AD using Bombardier TR AWL-110, dated August 
31, 2007, to Part 2, ``Airworthiness Limitations List,'' of the 
Bombardier Dash 8 Series 100 Maintenance Program Manual, Product 
Support Manual PSM 1-8-7. The subsequent paragraphs have been 
redesignated accordingly.
    Since the NPRM (79 FR 48703, August 18, 2014) was published, we 
also received Bombardier TR AWL 2-47, dated February 16, 2011, to Part 
2, ``Airworthiness Limitations,'' of the Bombardier Dash 8 Series 200 
Maintenance Program Manual, PSM 1-82-7, which supersedes Bombardier TR 
AWL 2-43, dated August 31, 2007, to Part 2, ``Airworthiness 
Limitations,'' of the Bombardier Dash 8 Series 200 Maintenance Program 
Manual, PSM 1-82-7. We have added paragraph (g)(2) of this AD to refer 
to Bombardier TR AWL 2-47, dated February 16, 2011, to Part 2, 
``Airworthiness Limitations,'' of the Bombardier Dash 8 Series 200 
Maintenance Program Manual, PSM 1-82-7, as an appropriate source of 
service information to accomplish the revision required by paragraph 
(g) of this AD.
    Furthermore, we also received Bombardier TR AWL 3-117, dated 
February 16, 2011, to Part 2, ``Airworthiness Limitations,'' of the 
Bombardier Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7, 
which supersedes Bombardier TR AWL 3-109, dated August 31, 2007, to 
Part 2, ``Airworthiness Limitations,'' of Bombardier Dash 8 Series 300 
Maintenance Program Manual, PSM 1-83-7. We have added paragraph (g)(4) 
of this AD to refer to Bombardier TR AWL 3-117, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier Dash 
8 Series 300 Maintenance Program Manual, PSM 1-83-7, as an appropriate 
source of service information to accomplish the revision required by 
paragraph (g) of this AD.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD with the changes described 
previously and minor editorial changes. We have determined that these 
minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (79 FR 48703, August 18, 2014) for correcting the unsafe 
condition; and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (79 FR 48703, August 18, 2014).

Related Service Information Under 1 CFR Part 51

    Bombardier, Inc. has issued the following service information:
     Bombardier Temporary Revision AWL 2-43, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier Dash 
8 Series 200 Maintenance Program Manual, PSM 1-82-7.
     Bombardier Temporary Revision AWL 2-47, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier Dash 
8 Series 200 Maintenance Program Manual, PSM 1-82-7.
     Bombardier Temporary Revision AWL 3-109, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier Dash 
8 Series 300 Maintenance Program Manual, PSM 1-83-7.
     Bombardier Temporary Revision AWL 3-117, dated February 
16, 2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
     Subject 5-FSL of Section 5, ``Fuel System Limitations,'' 
of the ``Airworthiness Limitations List,'' of the Bombardier Dash 8 
Series 100 Maintenance Program Manual, PSM 1-8-7, Revision 18, dated 
February 23, 2012.
    The service information describes revising the maintenance or 
inspection program to incorporate new limitations for fuel tank 
systems. 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 122 airplanes of U.S. registry.
    We also estimate that it will take about 1 work-hour 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 $10,370, or $85 per product.

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 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 http://www.regulations.gov/#!docketDetail;D=FAA-2014-0570; 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:

[[Page 42375]]

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):

2015-14-03 Bombardier, Inc.: Amendment 39-18201. Docket No. FAA-
2014-0570; Directorate Identifier 2013-NM-094-AD.

(a) Effective Date

    This AD becomes effective August 21, 2015.

(b) Affected ADs

    This AD affects AD 2008-13-09, Amendment 39-15572 (73 FR 47029, 
August 13, 2008).

(c) Applicability

    This AD applies to Bombardier, Inc. Model DHC-8-102, -103, -106, 
-201, -202, -301, -311, and -315 airplanes, certificated in any 
category, serial numbers (S/N) 003 through 624 inclusive, and 626.

(d) Subject

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) Reason

    This AD was prompted by fuel system reviews conducted by the 
manufacturer. We are issuing this AD to prevent potential ignition 
sources within the fuel system, which could result in a fuel tank 
explosion.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Maintenance or Inspection Program Revision

    Within 30 days after the effective date of this AD, revise the 
maintenance or inspection program, as applicable, to include fuel 
system limitation (FSL) Task Numbers FSL-02, ``Detailed Inspection 
of the Fuel Tank Bonding Jumpers''; and FSL-17, ``Functional Check 
of the Fuel Tank Components and the Plumbing Lines Electrical 
Bonding''; as specified in the applicable service information 
identified in paragraphs (g)(1) through (g)(5) of this AD. The 
initial compliance times for accomplishing the tasks are specified 
in paragraphs (h)(1), (h)(2), and (h)(3) of this AD. Doing this 
revision terminates the requirements of paragraph (f) of AD 2008-13-
09, Amendment 39-15572 (73 FR 47029, August 13, 2008), for Task 
Numbers FSL-02 and FSL-17 only.
    (1) Bombardier Temporary Revision AWL 2-43, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
    (2) Bombardier Temporary Revision AWL 2-47, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
    (3) Bombardier Temporary Revision AWL 3-109, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
    (4) Bombardier Temporary Revision AWL 3-117, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
    (5) Subject 5-FSL of Section 5, ``Fuel System Limitations,'' of 
the ``Airworthiness Limitations List,'' of the Bombardier Dash 8 
Series 100 Maintenance Program Manual, PSM 1-8-7, Revision 18, dated 
February 23, 2012.

(h) Phase-in Compliance Times

    For airplanes having S/Ns 003 through 624 inclusive, and S/N 
626, the initial compliance times are specified in paragraphs 
(h)(1), (h)(2), and (h)(3) of this AD, as applicable.
    (1) For airplanes having S/Ns 003 through 624 inclusive on which 
the applicable modification summaries (ModSums) specified in 
paragraphs (h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of this AD have 
been incorporated before the effective date of this AD: The 
compliance time for the initial inspection in FSL Task Number FSL-
02, ``Detailed Inspection of the Fuel Tank Bonding Jumpers''; and 
the initial functional check in FSL Task Number FSL-17, ``Functional 
Check of the Fuel Tank Components and the Plumbing Lines Electrical 
Bonding''; is within 6,000 flight hours or 36 months after the 
effective date of this AD, whichever occurs first. Airplane 
configurations can be a combination of the configurations specified 
in paragraphs (h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of this AD.
    (i) For airplanes having S/Ns 003 through 624 inclusive: 
Bombardier ModSum Package 8Q101512, Revision G, dated June 10, 2009; 
and Bombardier ModSum Package 8Q101865, Revision B, dated May 26, 
2008.
    (ii) For airplanes having S/Ns 003 through 624 inclusive with 
auxiliary power unit (APU) option: Bombardier ModSum Package 
8Q902144, Revision E, dated June 17, 2009.
    (iii) For airplanes having S/Ns 003 through 624 inclusive with a 
long-range fuel system installed: Bombardier ModSum Package 
8Q902091, Revision C, dated December 22, 2006.
    (2) For airplanes having S/Ns 003 through 624 inclusive on which 
the applicable ModSum packages specified in paragraphs (h)(1)(i), 
(h)(1)(ii), and (h)(1)(iii) of this AD have not been incorporated 
before the effective date of this AD: The compliance time for the 
initial inspection in FSL Task Number FSL-02, ``Detailed Inspection 
of the Fuel Tank Bonding Jumpers''; and the initial functional check 
in FSL Task Number FSL-17, ``Functional Check of the Fuel Tank 
Components and the Plumbing Lines Electrical Bonding''; is before 
further flight after incorporation of all applicable ModSum packages 
specified in paragraphs (h)(1)(i), (h)(1)(ii), and (h)(1)(iii) of 
this AD. Airplane configurations can be a combination of the 
configurations specified in paragraphs (h)(1)(i), (h)(1)(ii), and 
(h)(1)(iii) of this AD.
    (3) For the airplane having serial number 626: The initial 
compliance time is at the applicable time specified in paragraph 
(h)(3)(i) or (h)(3)(ii) of this AD.
    (i) If Bombardier ModSum Package 8Q902091, Revision C, dated 
December 22, 2006, has been accomplished before the effective date 
of this AD: The compliance time for doing the initial inspection 
specified in FSL Task Number FSL-02, ``Detailed Inspection of the 
Fuel Tank Bonding Jumpers''; and the initial functional check 
specified in FSL Task Number FSL-17, ``Functional Check of the Fuel 
Tank Components and the Plumbing Lines Electrical Bonding''; is 
within 6,000 flight hours or within 36 months after the effective 
date of this AD, whichever occurs first.
    (ii) If Bombardier ModSum Package 8Q902091 Revision C, dated 
December 22, 2006, has not been accomplished before the effective 
date of this AD: The compliance time for doing the initial 
inspection in FSL Task Number FSL-02, ``Detailed Inspection of the 
Fuel Tank Bonding Jumpers''; and the initial functional check in FSL 
Task Number FSL-17, ``Functional Check of the Fuel Tank Components 
and the Plumbing Lines Electrical Bonding''; is before further 
flight after accomplishment of Bombardier ModSum Package 8Q901091.

(i) No Alternative Actions, Intervals, and/or Critical Design 
Configuration Control Limitations (CDCCLs)

    After accomplishing the revision required by paragraph (g) of 
this AD, no alternative actions (e.g., inspections), intervals, and/
or CDCCLs may be used unless the actions, intervals, and/or CDCCLs 
are approved as an alternative method of compliance (AMOC) in 
accordance with the procedures specified in paragraph (k) of this 
AD.

(j) 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 Bombardier TR AWL-110, dated August 31, 2007, 
to Part 2, ``Airworthiness Limitations List,'' of the Bombardier 
Dash 8 Series 100 Maintenance Program Manual, Product Support Manual 
PSM 1-8-7, which is not incorporated by reference in this AD.

(k) 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/

[[Page 42376]]

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 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.

(l) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) Canadian Airworthiness Directive CF-2007-32R2, dated June 27, 
2013, for related information. This MCAI may be found in the AD 
docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-0570-0002.
    (2) Service information identified in this AD that is not 
incorporated by reference is available at the addresses specified in 
paragraphs (m)(3) and (m)(4) of this AD.

(m) 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) Bombardier Temporary Revision AWL 2-43, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
    (ii) Bombardier Temporary Revision AWL 2-47, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
    (iii) Bombardier Temporary Revision AWL 3-109, dated August 31, 
2007, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
    (iv) Bombardier Temporary Revision AWL 3-117, dated February 16, 
2011, to Part 2, ``Airworthiness Limitations,'' of the Bombardier 
Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
    (v) Subject 5-FSL of Section 5, ``Fuel System Limitations,'' of 
the ``Airworthiness Limitations List,'' of the Bombardier Dash 8 
Series 100 Maintenance Program Manual, PSM 1-8-7, Revision 18, dated 
February 23, 2012.
    (3) For service information identified in this AD, contact 
Bombardier, Inc., Q-Series Technical Help Desk, 123 Garratt 
Boulevard, Toronto, Ontario M3K 1Y5, Canada; telephone 416-375-4000; 
fax 416-375-4539; email thd.qseries@aero.bombardier.com; Internet 
http://www.bombardier.com.
    (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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on June 29, 2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2015-16580 Filed 7-16-15; 8:45 am]
 BILLING CODE 4910-13-P
```