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

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Rules and Regulations Federal Register

42373 

Vol. 80, No. 137 

Friday, July 17, 2015 

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., QSeries 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 


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42374 Federal Register / Vol. 80, No. 137 / Friday, July 17, 2015 / Rules and Regulations 

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: 


asabaliauskas on DSK5VPTVN1PROD with RULES
Federal Register / Vol. 80, No. 137 / Friday, July 17, 2015 / Rules and Regulations 42375 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 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/


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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/ibrlocations.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 

CONSUMER PRODUCT SAFETY 

COMMISSION 

16 CFR Part 1251 

[Docket No. CPSC–2011–0081] 

Toys: Determination Regarding Heavy 

Elements Limits for Unfinished and 

Untreated Wood 

AGENCY: U.S. Consumer Product Safety 

Commission. 

ACTION: Direct final rule. 

SUMMARY: The Consumer Product Safety 

Commission (‘‘Commission,’’ or 

‘‘CPSC’’) is issuing a direct final rule 

determining that unfinished and 

untreated trunk wood does not contain 

heavy elements that would exceed the 

limits specified in the Commission’s toy 

standard, ASTM F963–11. Based on this 

determination, unfinished and 

untreated wood in toys does not require 

third party testing for the heavy element 

limits in ASTM F963. 

DATES: The rule is effective on 

September 15, 2015, unless we receive 

a significant adverse comment by 

August 17, 2015. If we receive a timely 

significant adverse comment, we will 

publish notification in the Federal 

Register, withdrawing this direct final 

rule before its effective date. 

ADDRESSES: You may submit comments, 

identified by Docket No. CPSC–2011– 

0081, by any of the following methods: 

Electronic Submissions: Submit 

electronic comments to the Federal 

eRulemaking Portal at: 

www.regulations.gov. Follow the 

instructions for submitting comments. 

The Commission does not accept 

comments submitted by electronic mail 

(email), except through 

www.regulations.gov. The Commission 

encourages you to submit electronic 

comments by using the Federal 

eRulemaking Portal, as described above. 

Written Submissions: Submit written 

submissions by mail/hand delivery/

courier to: Office of the Secretary, 

Consumer Product Safety Commission, 

Room 820, 4330 East West Highway, 

Bethesda, MD 20814; telephone (301) 

504–7923. 

Instructions: All submissions received 

must include the agency name and 

docket number for this notice. All 

comments received may be posted 

without change, including any personal 

identifiers, contact information, or other 

personal information provided, to: 

www.regulations.gov. Do not submit 

confidential business information, trade 

secret information, or other sensitive or 

protected information that you do not 

want to be available to the public. If 

furnished at all, such information 

should be submitted in writing. 

Docket: For access to the docket to 

read background documents or 

comments received, go to: 

www.regulations.gov, and insert the 

docket number CPSC–2011–0081, into 

the ‘‘Search’’ box, and follow the 

prompts. 

FOR FURTHER INFORMATION CONTACT: 

Randy Butturini, Project Manager, 

Office of Hazard Identification and 

Reduction U.S. Consumer Product 

Safety Commission, 4330 East West 

Hwy, Room 814, Bethesda, MD 20814; 

301–504–7562: email; rbutturini@

cpsc.gov. 

SUPPLEMENTARY INFORMATION: 

A. Background 

1. Third Party Testing 

Section 14(a) of the Consumer 

Product Safety Act, (‘‘CPSA’’), as 

amended by the Consumer Product 

Safety Improvement Act of 2008 

(‘‘CPSIA’’), requires that manufacturers 

of products subject to a consumer 

product safety rule or similar rule, ban, 

standard or regulation enforced by the 

CPSC must certify that the product 

complies with all applicable CPSCenforced requirements. 15 U.S.C. 

2063(a). For children’s products, 

certification must be based on testing 

conducted by a CPSC-accepted third 

party conformity assessment body. Id. 

Pub. L. 112–28 (August 12, 2011), 

directed the CPSC to seek comment on 

‘‘opportunities to reduce the cost of 

third party testing requirements 

consistent with assuring compliance 

with any applicable consumer product 

safety rule, ban, standard, or 

regulation.’’ In response to Pub. L. 112– 

28, the Commission published in the 

Federal Register a Request for Comment 

(‘‘RFC’’). See http://www.cpsc.gov//

PageFiles/103251/3ptreduce.pdf. As 

directed by the Commission, staff 

submitted a briefing package to the 

Commission that described 

opportunities that the Commission 


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