Federal Register / Vol. 75, No. 140 / Thursday, July 22, 2010 / Rules and Regulations 42589 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the service information specified in this AD 

under 5 U.S.C. 552(a) and 1 CFR part 51. 

EMBRAER 170 MRBR MRB–1621, Revision 

6, dated January 14, 2010, contains the 

following effective pages: 

LIST OF EFFECTIVE PAGES

Page title/description Page Nos. Revision No. Date shown on 

page(s) 

MRBR Title Page ................................. None shown ........................................ 6 ........................................................... January 14, 2010. 

MRBR List of Effective Pages ............. A–P ...................................................... None shown* ....................................... January 14, 2010. 

MRBR Table of Contents .................... 1 ........................................................... None shown* ....................................... November 5, 2008. 

2–3 ....................................................... None shown* ....................................... January 14, 2010. 

4 ........................................................... None shown* ....................................... May 31, 2007. 

Section 1 .............................................. 1–1, 1–2, 1–8 ...................................... None shown* ....................................... May 31, 2007. 

1–3 through 1–7, 1–9, 1–13 through 

1–86.

None shown* ....................................... January 14, 2010. 

1–10 ..................................................... None shown* ....................................... November 5, 2008. 

1–11, 1–12 .......................................... None shown* ....................................... June 29, 2006. 

*Only the title page of EMBRAER 170 MRBR MRB–1621, Revision 6, contains the revision level of this document. 

(2) For service information identified in 

this AD, contact Empresa Brasileira de 

Aeronautica S.A. (EMBRAER), Technical 

Publications Section (PC 060), Av. Brigadeiro 

Faria Lima, 2170—Putim—12227–901 Sa ̃o 

Jose dos Campos—SP—BRASIL; telephone 

+55 12 3927–5852 or +55 12 3309–0732; fax 

+55 12 3927–7546; e-mail 

distrib@embraer.com.br; Internet 

http://www.flyembraer.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on June 23, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–16182 Filed 7–21–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0003; Directorate 

Identifier 2007–NM–251–AD; Amendment 

39–16368; AD 2010–15–02] 

RIN 2120–AA64 

Airworthiness Directives; Airbus Model 

A330–200 and –300 Series Airplanes, 

and A340–200, –300, –500, and –600 

Series Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

Several cases of corrosion and damage on 

the Down Drive Shafts (DDS), between the 

Down Drive Gear Box (DDGB) and the Input 

Gear Box (IPGB), on all 10 Flap Tracks (5 per 

wing), have been reported by AIRBUS Long 

Range Operators. 

Investigations have revealed that corrosion 

and wear due to absence of grease in the 

spline interfaces could cause [DDS] 

disconnection which could result in a free 

movable flap surface, potentially leading to 

aircraft asymmetry or even flap detachment. 

* * * * * 

The unsafe condition could reduce 

the ability of the flightcrew to maintain 

the safe flight and landing of the 

airplane. We are issuing this AD to 

require actions to correct the unsafe 

condition on these products. 

DATES: This AD becomes effective 

August 26, 2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of August 26, 2010. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue, SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Vladimir Ulyanov, Aerospace Engineer, 

International Branch, ANM–116, FAA, 

Transport Airplane Directorate, 1601 

Lind Avenue, SW., Renton, Washington 

98057–3356; telephone (425) 227–1138; 

fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a supplemental notice of 

proposed rulemaking (NPRM) to amend 

14 CFR part 39 to include an AD that 

would apply to the specified products. 

That supplemental NPRM was 

published in the Federal Register on 

March 29, 2010 (75 FR 15353). That 

supplemental NPRM proposed to 

correct an unsafe condition for the 

products listed above. 

Explanation of Revised Service 

Information 

Airbus has issued Mandatory Service 

Bulletin A330–27–3152, Revision 03, 

including Appendices 1 and 2, dated 

February 22, 2010. Airbus Mandatory 

Service Bulletin A330–27–3152, 

Revision 02, dated September 23, 2008, 

is referred to as the appropriate source 

of service information for accomplishing 

certain actions in the supplemental 

NPRM. The changes in Airbus 

Mandatory Service Bulletin A330–27– 


emcdonald on DSK2BSOYB1PROD with RULES
42590 Federal Register / Vol. 75, No. 140 / Thursday, July 22, 2010 / Rules and Regulations 

3152, Revision 03, dated February 22, 

2010, are minor and no additional work 

is necessary for airplanes on which the 

actions specified in Revision 02 of this 

service bulletin were done. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

considered the comments received. 

Comments 

Delta supports the proposed actions 

in the supplemental NPRM and asks 

that we include Airbus Mandatory 

Service Bulletin A330–27–3152, 

Revision 03, dated February 22, 2010, as 

the appropriate source of service 

information for accomplishing certain 

actions. Delta also asks that we give 

credit for Airbus Mandatory Service 

Bulletin A330–27–3152, Revision 02, 

dated September 23, 2008. 

As stated previously, Airbus issued 

Mandatory Service Bulletin A330–27– 

3152, Revision 03, dated February 22, 

2010. We have cited Airbus Mandatory 

Service Bulletin A330–27–3152, 

Revision 03, dated February 22, 2010, as 

the appropriate source of service 

information for accomplishing the 

required actions and have changed the 

service bulletin references in Tables 1 

and 2 of this AD accordingly. 

Conclusion 

We reviewed the available data, 

including the comment received, and 

determined that air safety and the 

public interest require adopting the AD 

with the changes described previously. 

We determined that these changes will 

not increase the economic burden on 

any operator or increase the scope of the 

AD. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow our FAA 

policies. Any such differences are 

highlighted in a Note within the AD. 

Costs of Compliance 

We estimate that this AD affects about 

41 products of U.S. registry. We also 

estimate that it takes 65 work-hours per 

product to comply with the basic 

requirements of this AD. The average 

labor rate is $85 per work-hour. Based 

on these figures, we estimate the cost of 

the AD on U.S. operators to be $226,525, 

or $5,525 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 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); and 

3. 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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

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 the NPRM, 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. 

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 AD: 

2010–15–02 Airbus: Amendment 39–16368. 

Docket No. FAA–2009–0003; Directorate 

Identifier 2007–NM–251–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective August 26, 2010. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Airbus Model A330– 

201, –202, –203, –223, –243, –301, –302, 

–303, –321, –322, –323, –341, –342, and –343 

series airplanes, A340–211, –212, –213, –311, 

–312, and –313 series airplanes, and A340– 

541 and –642 airplanes, certificated in any 

category; all certified models, all 

manufacturer serial numbers. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 27: Flight Controls. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

Several cases of corrosion and damage on 

the Down Drive Shafts (DDS), between the 

Down Drive Gear Box (DDGB) and the Input 

Gear Box (IPGB), on all 10 Flap Tracks (5 per 

wing), have been reported by AIRBUS Long 

Range Operators. 

Investigations have revealed that corrosion 

and wear due to absence of grease in the 

spline interfaces could cause [DDS] 

disconnection which could result in a free 

movable flap surface, potentially leading to 

aircraft asymmetry or even flap detachment. 

Emergency Airworthiness Directive (EAD) 

2007–0222–E mandated on all aircraft older 

than 6 years since AIRBUS original delivery 

date of the aircraft, an initial inspection of all 

DDS and IPGB for corrosion and wear 

detection in order to replace any damaged 

part. 

Revision 1 of EAD 2007–0222–E aimed for 

clarifying the compliance instructions. 


emcdonald on DSK2BSOYB1PROD with RULES
Federal Register / Vol. 75, No. 140 / Thursday, July 22, 2010 / Rules and Regulations 42591 

[EASA AD 2008–0026] supersedes the EAD 

2007–0222R1–E and mandates repetitive 

inspections every 6 years for all the fleet. 

The unsafe condition could reduce the ability 

of the flightcrew to maintain the safe flight 

and landing of the airplane. The corrective 

actions include replacing damaged parts. 

Compliance 

(f) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Actions 

(g) Do the applicable inspections and 

corrective actions specified in paragraphs 

(g)(1) and (g)(2) of this AD, in accordance 

with the instructions of the applicable 

service information specified in Table 1 of 

this AD. 

TABLE 1—SERVICE INFORMATION

For model— Use Airbus Mandatory Service Bulletin— For actions specified in paragraph— 

A330–200 and –300 series airplanes ... A330–27–3151, Revision 01, dated March 19, 2008 .......... (g)(1)(i) and (g)(1)(ii) of this AD. 

A330–200 and –300 series airplanes ... A330–27–3152, Revision 03, dated February 22, 2010 ...... (g)(1)(iv) and (g)(2) of this AD. 

A340–200 and –300 series airplanes ... A340-27-4151, Revision 01, dated March 19, 2008 ............ (g)(1)(i) and (g)(1)(ii) of this AD. 

A340–200 and –300 series airplanes ... A340–27–4152, Revision 02, dated September 23, 2008 ... (g)(1)(iv) and (g)(2) of this AD. 

A340–541 and –642 airplanes .............. A340–27–5040, Revision 02, dated September 23, 2008 ... (g)(2) of this AD. 

(1) For Model A330–200 and –300 series 

airplanes, up to and including manufacturer 

serial number (MSN) 0420, and Model A340– 

200 and –300 series airplanes, up to and 

including MSN 0415, except MSNs 0385 and 

0395: Do the applicable actions specified in 

paragraphs (g)(1)(i), (g)(1)(ii), (g)(1)(iii), and 

(g)(1)(iv) of this AD at the applicable time 

specified. 

(i) For airplanes on which less than 10 

years have accumulated since the date of 

issuance of the original French standard 

airworthiness certificate or the date of 

issuance of the original French or EASA 

export certificate of airworthiness as of the 

effective date of this AD: Within 24 months 

after the effective date of this AD, perform 

simultaneous detailed visual inspections of 

the IPGB and of the DDS on all flap tracks 

on both wings for corrosion and wear 

detection and do all applicable corrective 

actions. For Type 3 damaged parts, do all 

applicable corrective actions before further 

flight. For Type 2 damaged IPGB parts, do all 

applicable corrective actions within 18 

months after doing the inspection. 

(ii) For airplanes on which 10 or more 

years have accumulated since the date of 

issuance of the original French standard 

airworthiness certificate or the date of 

issuance of the original French or EASA 

export certificate of airworthiness as of the 

effective date of this AD: Within 4 months 

after the effective date of this AD, perform 

simultaneous detailed visual inspections of 

the IPGB and of the DDS on flap tracks 2 and 

4 on both wings for corrosion and wear 

detection. For any Type 3 damaged parts on 

flap tracks 2 and 4, do all applicable 

corrective actions before further flight. For 

any Type 2 damaged IPGB parts on flap 

tracks 2 and 4, do all applicable corrective 

actions within 18 months after doing the 

inspection required by paragraph (g)(1)(ii) of 

this AD. 

(A) For wings on which Type 3 damage is 

found on the DDS of flap track 2 or 4, 

perform simultaneous detailed visual 

inspections of the IPGB and of the DDS on 

flap track 3 on both wings for corrosion and 

wear detection. For Type 3 damaged parts on 

flap track 3, do all applicable corrective 

actions before further flight. For Type 2 

damaged IPGB parts, on flap track 3, do all 

applicable corrective actions within 18 

months after doing the inspection required 

by paragraph (g)(1)(ii)(A) of this AD. 

(1) For wings on which Type 3 damage is 

found on the DDS of flap track 3, before 

further flight, perform simultaneous detailed 

visual inspections of the IPGB and of the 

DDS on flap tracks 1 and 5 on both wings for 

corrosion and wear detection. For Type 3 

damaged parts on flap tracks 1 and 5, do all 

applicable corrective actions before further 

flight. For Type 2 damaged IPGB parts on 

flap tracks 1 and 5, do all applicable 

corrective actions within 18 months after 

doing the inspection required by paragraph 

(g)(1)(ii)(A)(1) of this AD. 

(2) For wings on which no Type 3 damage 

is found on the DDS of flap track 3, within 

18 months after doing the inspection 

required by paragraph (g)(1)(ii)(A) of this AD, 

perform simultaneous detailed visual 

inspections of the IPGB and of the DDS on 

flap tracks 1 and 5 on both wings for 

corrosion and wear detection. For any Type 

3 damaged parts on flap tracks 1 and 5, do 

all applicable corrective actions before 

further flight. For any Type 2 damaged IPGB 

parts on flap tracks 1 and 5, do all applicable 

corrective actions within 18 months after 

doing the inspection required by paragraph 

(g)(1)(ii)(A)(2) of this AD. 

(B) For wings on which no Type 3 damage 

is found on the DDS of flap track 2 and 4: 

Within 18 months after doing the inspection 

required by paragraph (g)(1)(ii) of this AD, 

perform simultaneous detailed visual 

inspections of the IPGB and of the DDS on 

flap tracks 1, 3, and 5 on both wings for 

corrosion and wear detection. For any Type 

3 damaged parts on flap tracks 1, 3, and 5, 

do all applicable corrective actions before 

further flight. For Type 2 damaged IPGB parts 

on flap tracks 1, 3, and 5, do all applicable 

corrective actions within 18 months after 

doing the inspection required by paragraph 

(g)(1)(ii) of this AD. 

(iii) Within 30 days after performing an 

initial inspection required by paragraph 

(g)(1)(i) or (g)(1)(ii) of this AD, or within 30 

days after the effective date of this AD, 

whichever occurs later, report the initial 

inspection results only, whatever they are, to 

Airbus as specified in the reporting sheet of 

the applicable service information listed in 

Table 1 of this AD. 

(iv) Within 6 years after performing the 

applicable inspection required by paragraph 

(g)(1)(i) or (g)(1)(ii) of this AD, and thereafter 

at intervals not exceeding 6 years: Perform 

simultaneous detailed visual inspections of 

the IPGB and of the DDS on all flap tracks 

on both wings for corrosion and wear 

detection and do all applicable corrective 

actions. For Type 3 damaged parts, do all 

applicable corrective actions before further 

flight. For Type 2 damaged IPGB parts, do all 

applicable corrective actions within 18 

months after doing the inspection. 

(2) For airplanes other than those 

identified in paragraph (g)(1) of this AD: 

Within 6 years after issuance of the original 

French standard airworthiness certificate or 

the date of issuance of the original French or 

EASA export certificate of airworthiness, or 

within 20 months after the effective date of 

this AD, whichever occurs later; and 

thereafter at intervals not exceeding 6 years; 

perform simultaneous detailed visual 

inspections of the IPGB and of the DDS on 

all flap tracks on both wings for corrosion 

and wear detection and do all applicable 

corrective actions. For Type 3 damaged parts, 

do all applicable corrective actions before 

further flight. For Type 2 damaged IPGB 

parts, do all applicable corrective actions 

within 18 months after doing the inspection. 

(3) Actions done before the effective date 

of this AD in accordance with the applicable 

service information specified in Table 2 of 

this AD are acceptable for compliance with 

the corresponding requirements of this AD. 

TABLE 2—CREDIT SERVICE INFORMATION

Airbus mandatory service bulletin— Revision— Dated— 

A330–27–3151 ................................................................... Original ............................................................................... August 9, 2007. 

A330–27–3152 ................................................................... Original ............................................................................... August 9, 2007. 


emcdonald on DSK2BSOYB1PROD with RULES
42592 Federal Register / Vol. 75, No. 140 / Thursday, July 22, 2010 / Rules and Regulations 

TABLE 2—CREDIT SERVICE INFORMATION—Continued 

Airbus mandatory service bulletin— Revision— Dated— 

A330–27–3152 ................................................................... 01 ....................................................................................... March 19, 2008. 

A330–27–3152 ................................................................... 02 ....................................................................................... September 23, 2008. 

A340–27–4151 ................................................................... Original ............................................................................... August 9, 2007. 

A340–27–4152 ................................................................... Original ............................................................................... August 9, 2007. 

A340–27–4152 ................................................................... 01 ....................................................................................... March 19, 2008. 

A340–27–5040 ................................................................... Original ............................................................................... August 9, 2007. 

A340–27–5040 ................................................................... 01 ....................................................................................... March 19, 2008. 

Note 1: Airbus should be contacted in 

order to get appropriate information for 

airplanes on which the original delivery date 

of the airplane is unknown to the operator. 

FAA AD Differences 

Note 2: This AD differs from the MCAI 

and/or service information as follows: No 

differences. 

Other FAA AD Provisions 

(h) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

Send information to ATTN: Vladimir 

Ulyanov, Aerospace Engineer, International 

Branch, ANM–116, FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington 98057–3356; telephone (425) 

227–1138; fax (425) 227–1149. Before using 

any approved AMOC on any airplane to 

which the AMOC applies, notify your 

principal maintenance inspector (PMI) or 

principal avionics inspector (PAI), as 

appropriate, or lacking a principal inspector, 

your local Flight Standards 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 or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(i) Refer to MCAI EASA Airworthiness 

Directive 2008–0026, dated February 12, 

2008, and the service information specified 

in Table 1 of this AD, for related information. 

Material Incorporated by Reference 

(j) You must use the service information 

contained in Table 3 of this AD to do the 

actions required by this AD, unless the AD 

specifies otherwise. 

TABLE 3—MATERIAL INCORPORATED BY REFERENCE

Airbus mandatory service bulletin— Revision— Dated— 

A330–27–3151, including Appendix 1 .................................................................................................... 01 March 19, 2008 

A330–27–3152, including Appendices 1 and 2 ...................................................................................... 03 February 22, 2010 

A340–27–4151, including Appendix 1 .................................................................................................... 01 March 19, 2008 

A340–27–4152, including Appendices 1 and 2 ...................................................................................... 02 September 23, 2008 

A340–27–5040, including Appendix 1 .................................................................................................... 02 September 23, 2008 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(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, e-mail 

airworthiness.A330-A340@airbus.com; 

Internet http://www.airbus.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on June 30, 

2010. 

Todd G. Dixon, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2010–17064 Filed 7–21–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0671; Directorate 

Identifier 2010–NM–142–AD; Amendment 

39–16363; AD 2010–14–18] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Model 767–200, –300, and 

–300F Series Airplanes Powered by 

General Electric or Pratt & Whitney 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD) 

that applies to certain Model 767–200, 

–300, and –300F series airplanes. The 


emcdonald on DSK2BSOYB1PROD with RULES