Federal Register / Vol. 80, No. 20 / Friday, January 30, 2015 / Rules and Regulations 5017 

with the Administrative Procedure Act, 

5 U.S.C. 701 et seq., and any other 

applicable law. The Office of 

Management and Budget has 

determined that the Final Rule is not a 

‘‘major rule’’ within the meaning of 

SBREFA. 

D. The Economic Growth and 

Regulatory Paperwork Reduction Act 

Under section 2222 of the Economic 

Growth and Regulatory Paperwork 

Reduction Act of 1996 (‘‘EGRPRA’’), the 

FDIC is required to review all of its 

regulations, at least once every 10 years, 

in order to identify any outdated or 

otherwise unnecessary regulations 

imposed on insured institutions. The 

FDIC completed the last comprehensive 

review of its regulations under EGRPRA 

in 2006 and has commenced the next 

decennial review. The action taken on 

this rule will be included as part of the 

EGRPRA review that is currently under 

way. 

E. Plain Language 

Section 722 of the Gramm-LeachBliley Act, Public Law 106–102, 113 

Stat. 1338, 1471, 12 U.S.C. 4809, 

requires each Federal banking agency to 

use plain language in all of its proposed 

and final rules published after January 

1, 2000. As a federal banking agency 

subject to the provisions of this section, 

the FDIC has sought to present the final 

rule to rescind and remove subpart N in 

a simple and straightforward manner. 

The FDIC’s proposal to rescind and 

remove subpart N invited comments on 

whether the proposal was clearly stated 

and effectively organized, and how the 

FDIC might make the proposal easier to 

understand. No comments were 

received. 

List of Subjects in Part 390 

Banks and banking, Savings 

associations. 

Authority and Issuance 

For the reasons stated in the preamble 

and under the authority of 12 U.S.C. 

5412, the Board of Directors of the 

Federal Deposit Insurance Corporation 

amends 12 CFR part 390 as follows: 

PART 390—REGULATIONS 

TRANSFERRED FROM THE OFFICE OF 

THRIFT SUPERVISION 

■ 1. The authority citation for part 390 

is revised to read as follows: 

Authority: 12 U.S.C. 1819. 

Subpart F also issued under 5 U.S.C. 552; 

559; 12 U.S.C. 2901 et seq. 

Subpart G also issued under 12 U.S.C. 2810 

et seq., 2901 et seq.; 15 U.S.C. 1691; 42 U.S.C. 

1981, 1982, 3601–3619. 

Subpart I also issued under 12 U.S.C. 

1831x. 

Subpart J also issued under 12 U.S.C. 

1831p–1. 

Subpart L also issued under 12 U.S.C. 

1831p–1. 

Subpart M also issued under 12 U.S.C. 

1818. 

Subpart O also issued under 12 U.S.C. 

1828. 

Subpart P also issued under 12 U.S.C. 

1470; 1831e; 1831n; 1831p–1; 3339. 

Subpart Q also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464. 

Subpart R also issued under 12 U.S.C. 

1463; 1464; 1831m; 1831n; 1831p–1. 

Subpart S also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1468a; 1817; 1820; 

1828; 1831e; 1831o; 1831p–1; 1881–1884; 

3207; 3339; 15 U.S.C. 78b; 78 l; 78m; 78n; 

78p; 78q; 78w; 31 U.S.C. 5318; 42 U.S.C. 

4106. 

Subpart T also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78 l; 78m; 

78n; 78w. 

Subpart V also issued under 12 U.S.C. 

3201–3208. 

Subpart W also issued under 12 U.S.C. 

1462a; 1463; 1464; 15 U.S.C. 78c; 78 l; 78m; 

78n; 78p; 78w. 

Subpart X also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828; 3331 et seq. 

Subpart Y also issued under 12 

U.S.C.1831o. 

Subpart Z also issued under 12 U.S.C. 

1462; 1462a; 1463; 1464; 1828 (note). 

Subpart N—[Removed and Reserved] 

■ 2. Remove and reserve subpart N 

consisting of §§ 390.240 through 

390.241. 

Dated at Washington, DC, this 21st day of 

January, 2015. 

By order of the Board of Directors. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman. 

Executive Secretary. 

[FR Doc. 2015–01326 Filed 1–29–15; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0231; Directorate 

Identifier 2013–NM–163–AD; Amendment 

39–18073; AD 2015–02–06] 

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 CL–600–2B16 

(CL–604 Variant) airplanes. This AD 

was prompted by reports of loose, 

broken, or backed-out spur gear bolts on 

the horizontal stabilizer trim actuator 

(HSTA). This AD requires a revision to 

the airplane flight manual, a revision to 

the maintenance or inspection program, 

as applicable, and replacement of 

HSTAs having certain part numbers. We 

are issuing this AD to detect and correct 

loose spur gear bolts on the HSTA, 

which, if combined with the failure of 

the primary load path, could lead to 

failure of the HSTA and subsequent loss 

of the airplane. 

DATES: This AD becomes effective 

March 6, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of March 6, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov/

#!docketDetail;D=FAA-2014-0231; 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., 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. 

FOR FURTHER INFORMATION CONTACT: 

Ricardo Garcia, Aerospace Engineer, 

Airframe and Propulsion Branch, ANE– 

171, FAA, New York Aircraft 

Certification Office, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 

11590; telephone 516–28–7331; 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 

CL–600–2B16 (CL–604 Variant) 

airplanes. The NPRM published in the 

Federal Register on April 15, 2014 (79 

FR 21158). Transport Canada Civil 

Aviation (TCCA), which is the aviation 

authority for Canada, has issued 

Canadian Airworthiness Directive CF– 

2013–18, dated July 16, 2013 (referred to 


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5018 Federal Register / Vol. 80, No. 20 / Friday, January 30, 2015 / Rules and Regulations 

after this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for certain Bombardier, Inc. Model CL– 

600–2B16 (CL–604 Variant) airplanes. 

The MCAI states: 

There have been a number of reports where 

the HSTA spur gear bolts were found loose, 

broken or backed out. Investigation revealed 

that the root cause of the bolt loosening is 

due to incorrect bending of the anti-rotation 

tab washer and the improper application of 

Loctite glue during installation. Loose bolt(s) 

on the HSTA spur gear combined with the 

failure of the primary load path, could lead 

to failure of the HSTA and subsequent loss 

of the aeroplane. 

Bombardier Aerospace has introduced a 

modified HSTA [part number] P/N 604– 

92305–5 (vendor P/N 8454–2) to rectify the 

loose bolt problem. However, this modified 

HSTA has several quality control problems 

which could affect safety. 

This AD is issued to mandate the 

replacement of the affected HSTA with the 

new HSTA P/N 604–92305–7 (vendor P/N 

8454–3). 

In addition to requiring the 

replacement of any HSTA having the 

affected part number, this AD requires 

revising both the airplane flight manual 

and airplane maintenance or inspection 

program. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov/

#!documentDetail;D=FAA-2014-0231- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comment 

received on the NPRM (79 FR 21158, 

April 15, 2014) and the FAA’s response 

to the comment. 

Request To Refer to Revised Service 

Information 

Mher Krikorian stated that the current 

revision of the service information is not 

referenced in the NPRM (79 FR 21158, 

April 15, 2014) and requested that the 

NPRM be revised to refer to Bombardier 

Service Bulletin 604–27–032, Revision 

02, dated April 22, 2014; and 

Bombardier Service Bulletin 605–27– 

002, Revision 02, dated April 22, 2014. 

Mr. Krikorian suggested that referring to 

the current revision of the service 

information would help to avoid 

requests for approval of alternative 

methods of compliance. 

We agree with the commenter’s 

request and have revised paragraph (j) of 

this AD to refer to Bombardier Service 

Bulletin 604–27–032, Revision 02, dated 

April 22, 2014; and Bombardier Service 

Bulletin 605–27–002, Revision 02, dated 

April 22, 2014. The revised service 

information includes only minor 

changes and does not include any 

substantive changes or new actions. We 

also added a new paragraph (k) to this 

AD to provide credit for actions 

accomplished prior to the effective date 

of this AD using Bombardier Service 

Bulletin 604–27–032, dated September 

10, 2012; 604–27–032, Revision 01, 

dated April 29, 2013; 605–27–002, dated 

September 10, 2012; or Bombardier 

Service Bulletin 605–27–002, Revision 

01, April 29, 2013; as applicable. We 

redesignated the subsequent paragraphs 

accordingly. 

‘‘Contacting the Manufacturer’’ 

Paragraph in This AD 

Since late 2006, we have included a 

standard paragraph titled ‘‘Airworthy 

Product’’ in all MCAI ADs in which the 

FAA develops an AD based on a foreign 

authority’s AD. 

We have become aware that some 

operators have misunderstood or 

misinterpreted the Airworthy Product 

paragraph to allow the owner/operator 

to use messages provided by the 

manufacturer as approval of deviations 

during the accomplishment of an ADmandated action. The Airworthy 

Product paragraph does not approve 

messages or other information provided 

by the manufacturer for deviations to 

the requirements of the AD-mandated 

actions. The Airworthy Product 

paragraph only addresses the 

requirement to contact the manufacturer 

for corrective actions for the identified 

unsafe condition and does not cover 

deviations from other AD requirements. 

However, deviations to AD-required 

actions are addressed in 14 CFR 39.17, 

and anyone may request the approval 

for an alternative method of compliance 

to the AD-required actions using the 

procedures found in 14 CFR 39.19. 

To address this misunderstanding and 

misinterpretation of the Airworthy 

Product paragraph, we have changed the 

paragraph and retitled it ‘‘Contacting the 

Manufacturer.’’ This paragraph now 

clarifies that for any requirement in this 

AD to obtain corrective actions from a 

manufacturer, the actions must be 

accomplished using a method approved 

by the FAA, TCCA, or Bombardier, 

Inc.’s TCCA Design Approval 

Organization (DAO). 

The Contacting the Manufacturer 

paragraph also clarifies that, if approved 

by the DAO, the approval must include 

the DAO-authorized signature. The DAO 

signature indicates that the data and 

information contained in the document 

are TCCA-approved, which is also FAAapproved. Messages and other 

information provided by the 

manufacturer that do not contain the 

DAO-authorized are not TCCAapproved, unless TCCA directly 

approves the manufacturer’s message or 

other information. 

This clarification does not remove 

flexibility previously afforded by the 

Airworthy Product paragraph. 

Consistent with long-standing FAA 

policy, such flexibility was never 

intended for required actions. This is 

also consistent with the 

recommendation of the Airworthiness 

Directive Implementation Aviation 

Rulemaking Committee to increase 

flexibility in complying with ADs by 

identifying those actions in 

manufacturers’ service instructions that 

are ‘‘Required for Compliance’’ with 

ADs. We continue to work with 

manufacturers to implement this 

recommendation. But once we 

determine that an action is required, any 

deviation from the requirement must be 

approved as an alternative method of 

compliance. 

We also have decided not to include 

a generic reference to either the 

‘‘delegated agent’’ or ‘‘design approval 

holder (DAH) with State of Design 

Authority design organization 

approval,’’ but instead we have 

provided the specific delegation 

approval granted by the State of Design 

Authority for the DAH throughout this 

AD. 

Additional Changes to This AD 

We revised paragraph (h) of this AD 

to require operators to revise the 

maintenance or inspection program, as 

applicable, by incorporating procedures 

for an Operational Test (BITE) of the 

Horizontal Stabilizer Trim Controls 

System (HSTCS), in accordance with a 

method approved by the Manager, New 

York ACO, ANE–170, FAA; or TCCA; or 

Bombardier, Inc.’s TCCA DAO. 

Bombardier Task 27–41–00–101, 

Operational Test (BITE) of the 

Horizontal Stabilizer Trim Controls 

System (HSTCS), is referenced as 

guidance material in new Note 1 to 

paragraph (h) of this AD. 

Conclusion 

We reviewed the relevant data, 

considered the comment received, 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 

21158, April 15, 2014) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 


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Federal Register / Vol. 80, No. 20 / Friday, January 30, 2015 / Rules and Regulations 5019 

proposed in the NPRM (79 FR 21158, 

April 15, 2014). 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of this AD. 

Related Service Information 

We reviewed Bombardier Temporary 

Revision (TR) 604/37, dated May 21, 

2013, to the Bombardier Challenger CL– 

604 Airplane Flight Manual, PSP 604– 

1; and Bombardier TR 605/18, dated 

May 21, 2013, to the Bombardier 

Challenger CL–605 Airplane Flight 

Manual, PSP 605–1. This service 

information describes procedures for the 

stabilizer trim system check. We also 

reviewed Bombardier Service Bulletin 

604–27–032, Revision 02, dated April 

22, 2014; and Bombardier Service 

Bulletin 605–27–002, Revision 02, dated 

April 22, 2014. This service information 

describes procedures for replacing 

HSTAs. You can find this information at 

http://www.regulations.gov by searching 

for and locating Docket No. FAA–2014– 

0231. 

Costs of Compliance 

We estimate that this AD affects 125 

airplanes of U.S. registry. 

We also estimate that it will take 

about 21 work-hours per product to 

comply with the basic requirements of 

this AD. The average labor rate is $85 

per work-hour. Required parts will cost 

about $0 per product. Based on these 

figures, we estimate the cost of this AD 

on U.S. operators to be $223,125, or 

$1,785 per product. 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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-2014-0231; 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 

■ 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): 

2014–02–06 Bombardier, Inc.: Amendment 

39–18073. Docket No. FAA–2014–0231; 

Directorate Identifier 2013–NM–163–AD. 

(a) Effective Date 

This AD becomes effective March 6, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Bombardier, Inc. Model 

CL–600–2B16 (CL–604 Variant) airplanes, 

certificated in any category, serial numbers 

5301 and subsequent, equipped with 

horizontal stabilizer trim actuator (HSTA) 

part number (P/N) 604–92305–3 (vendor P/N 

8454–1) or P/N 604–92305–5 (vendor P/N 

8454–2). 

(d) Subject 

Air Transport Association (ATA) of 

America Code 27, Flight Controls. 

(e) Reason 

This AD was prompted by reports of loose, 

broken, or backed out spur gear bolts on the 

horizontal stabilizer trim actuator (HSTA). 

We are issuing this AD to detect and correct 

loose spur gear bolts on the HSTA, which, if 

combined with the failure of the primary 

load path, could lead to failure of the HSTA 

and subsequent loss of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Airplane Flight Manual (AFM) Revision 

Within 30 days after the effective date of 

this AD, revise the Normal Procedures 

section of the applicable Bombardier AFM to 

include the information in the applicable 

temporary revision (TR) specified in 

paragraph (g)(1) or (g)(2) of this AD. The TRs 

introduce revised procedures for the 

stabilizer trim system check. Operate the 

airplane according to the limitations and 

procedures in the applicable TR. The 

revision may be done by inserting a copy of 

the applicable TR specified in paragraph 

(g)(1) or (g)(2) of this AD into the AFM. When 

the TR has been included in the general 

revisions of the AFM, the general revisions 

may be inserted into the AFM, provided the 

relevant information in the general revision 

is identical to that in the applicable TR, and 

the TR may be removed. 

(1) Bombardier Temporary Revision (TR) 

604/37, dated May 21, 2013, to the 

Bombardier Challenger CL–604 Airplane 

Flight Manual, PSP 604–1. 

(2) Bombardier TR 605/18, dated May 21, 

2013, to the Bombardier Challenger CL–605 

Airplane Flight Manual, PSP 605–1. 

(h) Maintenance or Inspection Program 

Revision 

Within 30 days after the effective date of 

this AD: Revise the maintenance or 

inspection program, as applicable, by 

incorporating procedures for an Operational 

Test (BITE) of the Horizontal Stabilizer Trim 

Controls System (HSTCS), in accordance 

with a method approved by the Manager, 

New York Aircraft Certification Office (ACO), 


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5020 Federal Register / Vol. 80, No. 20 / Friday, January 30, 2015 / Rules and Regulations 

ANE–170, FAA; or Transport Canada Civil 

Aviation (TCCA); or Bombardier, Inc.’s TCCA 

Design Approval Organization (DAO). The 

initial compliance time for the operational 

test is within 100 flight hours after the 

effective date of this AD. 

Note 1 to paragraph (h) of this AD: 

Bombardier Task 27–41–00–101, Operational 

Test (BITE) of the Horizontal Stabilizer Trim 

Controls System (HSTCS), provides guidance 

for the operational test specified in paragraph 

(h) of this AD. Bombardier Task 27–41–00– 

101 is included in the Bombardier Challenger 

604 Time Limits/Maintenance Checks 

(TLMC) Manual; and in the Bombardier 

Challenger 605 TLMC Manual. 

(i) No Alternative Actions or Intervals 

After the maintenance or inspection 

program has been revised, as required by 

paragraph (h) of this AD, no alternative 

actions (e.g., inspections) or intervals may be 

used unless the actions or intervals are 

approved as an alternative method of 

compliance (AMOC) in accordance with the 

procedures specified in paragraph (m)(1) of 

this AD. 

(j) HSTA Replacement 

For airplanes equipped with a HSTA 

having P/N 604–92305–3 (vendor P/N 

845401) or P/N 604–92305–5 (vendor P/N 

8454–2): Within 3,000 flight hours or 26 

months after the effective date of this AD, 

whichever occurs first, replace any HSTA 

having P/N 604–92305–3 (vendor P/N 

845401) or P/N 604–92305–5 (vendor P/N 

8454–2) with a HSTA having P/N 604– 

92305–7 (vendor P/N 8454–3), in accordance 

with the Accomplishment Instructions of 

Bombardier Service Bulletin 604–27–032, 

Revision 02, dated April 22, 2014; or 

Bombardier Service Bulletin 605–27–002, 

Revision 02, dated April 22, 2014; as 

applicable. 

(k) Credit for Previous Actions 

This paragraph provides credit for the 

actions required by paragraph (j) of this AD 

if those actions were performed before the 

effective date of this AD using the service 

information identified in paragraphs (k)(1) 

through (k)(4) of this AD, as applicable. This 

service information is not incorporated by 

reference in this AD. 

(1) Bombardier Service Bulletin 604–27– 

032, dated September 10, 2012. 

(2) Bombardier Service Bulletin 604–27– 

032, Revision 01, dated April 29, 2013. 

(3) Bombardier Service Bulletin 605–27– 

002, dated September 10, 2012. 

(4) Bombardier Service Bulletin 605–27– 

002, Revision 01, April 29, 2013. 

(l) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install any HSTA having P/N 

604–92305–3 (vendor P/N 8454–1) or 604– 

92305–5 (vendor P/N 8454–2) on any 

airplane. 

(m) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York 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; 

or TCCA; or Bombardier, Inc.’s TCCA Design 

DAO. If approved by the DAO, the approval 

must include the DAO-authorized signature. 

(n) Related Information 

(1) Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

Airworthiness Directive CF–2013–18 dated 

July 16, 2013, for related information. This 

MCAI may be found in the AD docket on the 

Internet at http://www.regulations.gov/

#!documentDetail;D=FAA-2014-0231-0002. 

(2) Service information identified in this 

AD that is not incorporated by reference is 

available at the addresses specified in 

paragraphs (o)(3) and (o)(4) of this AD. 

(o) 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 Service Bulletin 604–27– 

032, Revision 02, dated April 22, 2014. 

(ii) Bombardier Service Bulletin 605–27– 

002, Revision 02, dated April 22, 2014. 

(iii) Bombardier Temporary Revision 604/ 

37, dated May 21, 2013, to the Bombardier 

Challenger CL–604 Airplane Flight Manual, 

PSP 604–1. 

(iv) Bombardier Temporary Revision 605/ 

18, dated May 21, 2013, to the Bombardier 

Challenger CL–605 Airplane Flight Manual, 

PSP 605–1. 

(3) For service information identified in 

this 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. 

(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 January 

11, 2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–01171 Filed 1–29–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–0079; Directorate 

Identifier 2013–NM–091–AD; Amendment 

39–18085; AD 2015–02–18] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Airbus Model A330–201, –202, –203, 

–301, –302, and –303 airplanes. This AD 

requires a one-time ultrasonic 

inspection for fractures of all aft mountpylon bolts of each engine. This AD was 

prompted by a report of one bolt on the 

aft engine mount upper beam found 

totally broken. We are issuing this AD 

to detect and correct fracture of the aft 

mount-pylon bolts, which could result 

in failure of the engine mount and 

consequent detachment of the engine. 

DATES: This AD becomes effective 

February 17, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of February 17, 2015. 

We must receive comments on this 

AD by March 16, 2015. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 


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