11022 Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Proposed Rules 

July 12, 2007); AD 2008–25–02, 

Amendment 39–15760 (73 FR 75307, 

December 11, 2008); AD 2010–04–09, 

Amendment 39–16202 (75 FR 7940, 

February 23, 2010; corrected March 3, 

2010 (75 FR 9515)); AD 2011–01–02, 

Amendment 39–16555 (76 FR 432, 

January 5, 2011); AD 2012–16–05, 

Amendment 39–17152 (77 FR 48425, 

August 14, 2012); and 

■ b. Adding the following new AD: 

Airbus: Docket No. FAA–2014–0060; 

Directorate Identifier 2012–NM–194–AD. 

(a) Comments Due Date 

We must receive comments by April 14, 

2014. 

(b) Affected ADs 

This AD supersedes the ADs specified in 

paragraphs (b)(1) through (b)(6) of this AD. 

(1) AD 2006–21–08, Amendment 39–14793 

(71 FR 61639, October 19, 2006). 

(2) AD 2007–14–01, Amendment 39–15123 

(72 FR 38006, July 12, 2007). 

(3) AD 2008–25–02, Amendment 39–15760 

(73 FR 75307, December 11, 2008). 

(4) AD 2010–04–09, Amendment 39–16202 

(75 FR 7940, February 23, 2010; corrected 

March 3, 2010 (75 FR 9515)). 

(5) AD 2011–01–02, Amendment 39–16555 

(76 FR 432, January 5, 2011). 

(6) AD 2012–16–05, Amendment 39–17152 

(77 FR 48425, August 14, 2012). 

(c) Applicability 

This AD applies to Airbus Model A330– 

201, –202, –203, –223, –243, –223F, –243F, 

–301, –302, –303, –321, –322, –323, –341, 

–342, and –343 airplanes, certificated in any 

category, all manufacturer serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 05, Time Limits/Maintenance 

Checks. 

(e) Reason 

This AD was prompted by a determination 

that more restrictive maintenance 

requirements and airworthiness limitations 

are necessary. We are issuing this AD to 

prevent the potential of ignition sources 

inside fuel tanks, which, in combination with 

flammable fuel vapors, could result in fuel 

tank explosions and consequent loss of the 

airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Maintenance Program Revision and 

Airworthiness Limitations Compliance 

(1) Within 3 months after the effective date 

of this AD, revise the maintenance or 

inspection program, as applicable, by 

incorporating Airbus A330 Airworthiness 

Limitations Section (ALS) Part 5—Fuel 

Airworthiness Limitations, dated November 

16, 2011. 

(2) Comply with all applicable instructions 

and airworthiness limitations included in 

Airbus A330 ALS Part 5—Fuel Airworthiness 

Limitations, dated November 16, 2011. The 

initial compliance times for the actions 

specified in Airbus A330 ALS Part 5—Fuel 

Airworthiness Limitations, dated November 

16, 2011, are at the later of the times 

specified in paragraphs (g)(2)(i) and (g)(2)(ii) 

of this AD, except as required by paragraphs 

(h) and (i) of this AD. 

(i) Within the applicable compliance times 

specified in Airbus A330 ALS Part 5—Fuel 

Airworthiness Limitations, dated November 

16, 2011. 

(ii) Within 3 months after accomplishing 

the actions required by paragraph (g)(1) of 

this AD. 

(h) Exceptions to Compliance Times for 

Design Changes 

(1) For type design changes specified in 

‘‘Sub-part 5–2 Changes to Type Design,’’ of 

Airbus A330 ALS Part 5—Fuel Airworthiness 

Limitations, dated November 16, 2011, the 

compliance times are defined as 

‘‘Embodiment Limits,’’ except as defined in 

paragraph (h)(2) of this AD. 

(2) Where Airbus A330 ALS Part 5—Fuel 

Airworthiness Limitations, dated November 

16, 2011, specifies a compliance time based 

on a calendar date for modifying the control 

circuit for the fuel pump of the center fuel 

tank (installing ground fault interrupters to 

the center tank fuel pump control circuit), 

the compliance date is September 18, 2016 

(48 months after the effective date of AD 

2012–16–05, Amendment 39–17152 (77 FR 

48425, August 14, 2012)). 

(i) No Alternative Actions, Intervals, 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, or 

CDCCLs may be used; except as specified in 

paragraphs (h) and (i) of this AD; or unless 

the actions, intervals, or CDCCLs are 

approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (j)(1) of 

this AD. 

(j) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, 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 International Branch, send it to ATTN: 

Vladimir Ulyanov, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone (425) 227–1138; fax (425) 227– 

1149. Information may be emailed to: 9- 

ANM-116-AMOC-REQUESTS@faa.gov. 

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) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer, use these actions if they are 

FAA-approved. Corrective actions are 

considered FAA-approved if they were 

approved by the State of Design Authority (or 

its delegated agent, or the DAH with a State 

of Design Authority’s design organization 

approval, as applicable). You are required to 

ensure the product is airworthy before it is 

returned to service. 

(k) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) European 

Aviation Safety Agency Airworthiness 

Directive 2012–0168, dated August 31, 2012; 

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–2014–0060. 

(2) For service information identified in 

this AD, contact Airbus SAS, Airworthiness 

Office—EAL, 1 Rond Point Maurice Bellonte, 

31707 Blagnac Cedex, France; telephone +33 

5 61 93 36 96; fax +33 5 61 93 45 80; email 

airworthiness.A330-A340@airbus.com; 

Internet http://www.airbus.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 February 

14, 2014. 

Jeffrey E. Duven, 

Manager. Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–04258 Filed 2–26–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0120; Directorate 

Identifier 2013–NM–056–AD] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for certain 

Bombardier, Inc. Model CL–215–6B11 

(CL–215T Variant), and CL–215–6B11 

(CL–415 Variant) airplanes. This 

proposed AD was prompted by several 

reports indicating that shorter nacelle 

strut bushings were inadvertently 

installed on certain airplanes. This 

proposed AD would require a general 

visual inspection of the left and right 


TKELLEY on DSK3SPTVN1PROD with PROPOSALS
Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Proposed Rules 11023 

nacelle upper strut bushings; 

installation of the bolts and preload 

indicating (PLI) washers, if necessary; 

and replacement of the bushing or 

repair of the bushing installation, if 

necessary. We are proposing this AD to 

detect and correct inadequate nacelle 

strut bushings, which provide 

insufficient engagement in the strut fork 

end, and could deform under the 

bearing load and lead to the failure of 

the joint. 

DATES: We must receive comments on 

this proposed AD by April 14, 2014. 

ADDRESSES: You may send comments 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 Bombardier, 

Inc., 400 Coˆte-Vertu Road West, Dorval, 

Que ́bec H4S 1Y9, Canada; telephone 

514–855–5000; fax 514–855–7401; email 

thd.crj@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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov; or in person at the 

Docket Operations office 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: 

Ricardo Garcia, Aerospace Engineer, 

Airframe and Mechanical Systems 

Branch, ANE–171, FAA, New York 

Aircraft Certification Office, 1600 

Stewart Avenue, Suite 410, Westbury, 

NY 11590; phone (516) 228–7331; 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–2014–0120; Directorate Identifier 

2013–NM–056–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, 

which is the aviation authority for 

Canada, has issued Canadian 

Airworthiness Directive CF–2013–06, 

dated February 27, 2013 (referred to 

after this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for the specified products. The MCAI 

states: 

It was discovered in several cases that 

nacelle strut bushings with part number (P/ 

N), 85410265–105, have been inadvertently 

installed in lieu of P/N 85410265–103. 

Bushing P/N 85410265–105 is shorter than 

bushing P/N 85410265–103 and provides for 

less engagement in the strut fork end, P/N 

215T16534–12/–13, which may deform 

under the bearing load leading to the failure 

of the joint. 

The actions for this proposed AD 

include a general visual inspection of 

the left and right nacelle upper strut 

bushings; installation of the bolts and 

PLI washers, if necessary; and 

replacement of the bushing or repair of 

the bushing installation, if necessary. 

You may examine the MCAI in the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating it in Docket No. FAA– 

2014–0120. 

Relevant Service Information 

Bombardier, Inc. has issued Alert 

Service Bulletin 215–A3173, dated 

April 11, 2012, and Alert Service 

Bulletin 215–A4453, dated April 10, 

2012. The actions described in this 

service information are intended to 

correct the unsafe condition identified 

in the MCAI. 

FAA’s Determination and Requirements 

of This Proposed AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are proposing this 

AD because we evaluated all pertinent 

information and determined an unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Costs of Compliance 

We estimate that this proposed AD 

affects 5 airplanes of U.S. registry. 

We estimate the following costs to 

comply with this proposed AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspection ................................ 4 work-hours × $85 per hour = $340 ..................................... $0 $340 $1,700 

We estimate the following costs to do 

any necessary repairs or replacements 

that would be required based on the 

results of the proposed inspection. We 

have no way of determining the number 

of aircraft that might need these repairs 

or replacements: 


TKELLEY on DSK3SPTVN1PROD with PROPOSALS
11024 Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Proposed Rules 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per 

product 

Replacement .................................... 4 work-hours × $85 per hour = $340 ........................................................ $0 $340 

Repair .............................................. 4 work-hours × $85 per hour = $340 ........................................................ 0 340 

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 

■ 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 AD: 

Bombardier, Inc.: Docket No. FAA–2014– 

0120; Directorate Identifier 2013–NM– 

056–AD. 

(a) Comments Due Date 

We must receive comments by April 14, 

2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the Bombardier, Inc. 

airplanes, certificated in any category, 

identified in paragraphs (c)(1) and (c)(2) of 

this AD. 

(1) Model CL–215–6B11 (CL–215T Variant) 

airplanes, serial numbers 1056, 1057, 1061, 

1080, 1109, 1113, 1114, 1115, 1116, 1117, 

1118, 1119, 1120, 1121, 1122, and 1125. 

(2) Model CL–215–6B11 (CL–415 Variant) 

airplanes, serial numbers 2001 through 2067 

inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 54, Nacelles/Pylons. 

(e) Reason 

This AD was prompted by several reports 

indicating that shorter nacelle strut bushings 

were inadvertently installed on certain 

airplanes. We are issuing this AD to detect 

and correct inadequate nacelle strut 

bushings, which provide insufficient 

engagement in the strut fork end, and could 

deform under the bearing load and lead to 

the failure of the joint. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection of the Bushing 

Within 3 months after the effective date of 

this AD: Do a general visual inspection to 

determine the part number of the left and 

right nacelle upper strut bushings, in 

accordance with the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes). 

(1) If any bushing with part number (P/N) 

85410265–103 is installed: Before further 

flight, install the bolts and preload indicating 

(PLI) washers, in accordance with paragraph 

2.G. of the Accomplishment Instructions of 

Bombardier Alert Service Bulletin 215– 

A3173, dated April 11, 2012 (for Model CL– 

215–6B11 (CL–215T Variant) airplanes); or 

Bombardier Alert Service Bulletin 215– 

A4453, dated April 10, 2012 (for Model CL– 

215–6B11 (CL–415 Variant) airplanes). 

(2) If any bushing with P/N 85410265–105 

is installed in either the left or right nacelle: 

Do the actions in paragraph (h) of this AD. 

(h) Replacement or Repair of the Bushing 

If any bushing with P/N 85410265–105 is 

found installed during the inspection 

required by paragraph (g) of this AD: Before 

further flight, do the actions specified in 

paragraph (h)(1) or (h)(2) of this AD. 

(1) Replace the bushing in accordance with 

paragraph 2.E. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes); and continue with the installation 

of bolt and PLI washer, in accordance with 

paragraph 2.G. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes). 

(2) Repair the bushing in accordance with 

paragraph 2.F. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes); and continue with the installation 

of bolt and PLI washer, in accordance with 

paragraph 2.G. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes). 

(i) Replacement of Repaired Bushing 

For any bushing that has been repaired as 

specified in paragraph (h)(2) of this AD: 

Within 5,000 flight hours after accomplishing 

the repair or at the next engine removal, 


TKELLEY on DSK3SPTVN1PROD with PROPOSALS
Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Proposed Rules 11025 

whichever occurs first, replace the bushing 

with P/N 85410265–103, in accordance with 

paragraph 2.E. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes); and continue with the installation 

of bolt and PLI washer, in accordance with 

paragraph 2.G. of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin 215–A3173, dated April 11, 2012 

(for Model CL–215–6B11 (CL–215T Variant) 

airplanes); or Bombardier Alert Service 

Bulletin 215–A4453, dated April 10, 2012 

(for Model CL–215–6B11 (CL–415 Variant) 

airplanes). 

(j) No Further Action Required 

(1) For airplanes on which a general visual 

inspection specified in paragraph (g) of this 

AD is done and it is determined that the 

nacelle strut bushings having P/N 85410265– 

103 are installed in the airplane: No further 

actions are required by this AD, provided the 

actions specified in paragraph (g)(1) of this 

AD have been done. 

(2) For airplanes on which nacelle strut 

bushings having P/N 85410265–103 are 

installed as specified in paragraph (h)(1) or 

(i) of this AD, no further actions are required 

by 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/

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer, use these actions if they are 

FAA-approved. Corrective actions are 

considered FAA-approved if they were 

approved by the State of Design Authority (or 

its delegated agent, or the DAH with a State 

of Design Authority’s design organization 

approval). For a repair method to be 

approved, the repair approval must 

specifically refer to this AD. You are required 

to ensure the product is airworthy before it 

is returned to service. 

(l) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

Airworthiness Directive CF–2013–06, dated 

February 27, 2013, 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 it in Docket No. 

FAA–2014–0120. 

(2) For service information identified in 

this AD, contact Bombardier, Inc., 400 CoˆteVertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–5000; fax 514– 

855–7401; email thd.crj@

aero.bombardier.com; Internet http://

www.bombardier.com. You may view this 

service information at the FAA, Transport 

Airplane Directorate, 1601 Lind Avenue SW., 

Renton, WA. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

Issued in Renton, Washington, on February 

14, 2014. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–04260 Filed 2–26–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Office of the Secretary 

15 CFR Part 4 

[Docket No. 140127076–4076–01] 

RIN 0605–AA33 

Public Information, Freedom of 

Information Act and Privacy Act 

Regulations 

AGENCY: Department of Commerce. 

ACTION: Notice of proposed rulemaking. 

SUMMARY: This rule proposes revisions 

to the Department of Commerce’s 

(Department) regulations under the 

Freedom of Information Act (FOIA) and 

Privacy Act. The FOIA regulations are 

being revised to clarify, update and 

streamline the language of several 

procedural provisions, including 

methods for submitting FOIA requests 

and appeals and the time limits for 

filing an administrative appeal, and to 

incorporate certain of the changes 

brought about by the amendments to the 

FOIA under the OPEN Government Act 

of 2007. Additionally, the FOIA 

regulations are being updated to reflect 

developments in the case law. The 

Privacy regulations are being revised to 

clarify, update and streamline several 

procedural provisions, including the 

methods for submitting appeals of 

Privacy Act requests and the time limits 

for filing a Privacy Act appeal. 

Additionally, the Privacy Act 

regulations are being updated to make 

technical changes to the applicable 

exemptions. 

DATES: Written comments must be 

postmarked and electronic comments 

must be submitted on or before March 

31, 2014. Comments received by mail 

will be considered timely if they are 

postmarked on or before that date. The 

electronic Federal Docket Management 

System (FDMS) will accept comments 

until Midnight Eastern Time at the end 

of that day. 

ADDRESSES: You may submit comments, 

identified by Regulatory Information 

Number (RIN) 0605–AA33, by any of the 

following methods: 

• Federal eRulemaking Portal: http:// 

www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: (202) 482–2552. Include the 

RIN 0605–AA33 in the subject line. 

• Mail: Mark R. Tallarico, Senior 

Counsel, Office of the General Counsel, 

Department of Commerce, 1401 

Constitution Avenue NW., Room 5099, 

Washington, DC 20230. 

Instructions: All submissions received 

must include the agency name and 

docket number or RIN for this 

rulemaking. All comments received will 

be posted without change to 

regulations.gov, including any personal 

information provided. For detailed 

instructions on submitting comments 

and additional information on the 

rulemaking process, see the ‘‘Public 

Participation’’ heading of the 

SUPPLEMENTARY INFORMATION section of 

this document. 

FOR FURTHER INFORMATION CONTACT: 

Mark R. Tallarico, 202–482–8156, or 

Britt E. Carlson, 202–482–8155. 

SUPPLEMENTARY INFORMATION: Public 

Participation: Comments sent by any 

other method, to any other address or 

individual, or received after the end of 

the comment period, may not be 

considered by the Department. 

If you want to submit personal 

identifying information (such as your 

name, address, etc.) as part of your 

comment, but do not want it to be 

posted online, you must include the 

phrase ‘‘PERSONAL IDENTIFYING 

INFORMATION’’ in the first paragraph 

of your comment. You must also locate 

all the personal identifying information 

you do not want posted online in the 

first paragraph of your comment and 

identify what information you want 

redacted. 

If you want to submit confidential 

business information as part of your 

comment but do not want it to be posted 

online, you must include the phrase 

‘‘CONFIDENTIAL BUSINESS 

INFORMATION’’ in the first paragraph 

of your comment. You must also 

prominently identify confidential 

business information to be redacted 

within the comment. If a comment has 

so much confidential business 


TKELLEY on DSK3SPTVN1PROD with PROPOSALS