Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations 50871 

(i) Before further flight, insert Temporary 

Revision No. 12 to PC–12/47E Pilot’s 

Operating Handbook, dated October 15, 2009, 

into the normal procedures section of the 

aircraft flight manual (AFM). 

(ii) Within 12 months after September 22, 

2010 (the effective date of this AD), modify 

the engine control console assembly 

following the accomplishment instructions in 

paragraph 3.B. of Pilatus Aircraft Ltd. Service 

Bulletin No: 76–002, dated October 15, 2009. 

(iii) Before further flight after the 

modification required by paragraph (f)(2)(ii) 

of this AD, remove Temporary Revision No. 

12 to PC–12/47E Pilot’s Operating Handbook, 

dated October 15, 2009, from the AFM. 

(3) If during the inspection specified in 

paragraph (f)(1) of this AD you determine the 

reverse thrust latch moves freely and the idle 

detent is present, no further action is 

required. 

FAA AD Differences 

Note: This AD differs from the MCAI and/ 

or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Doug Rudolph, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4059; fax: (816) 329– 

4090. Before using any approved AMOC on 

any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

(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 

(h) Refer to MCAI European Aviation 

Safety Agency (EASA) AD No. 2010–0093, 

dated May 20, 2010; Pilatus Aircraft Ltd. 

Service Bulletin No: 76–002, dated October 

15, 2009; and Temporary Revision No. 12 to 

PC–12/47E Pilot’s Operating Handbook, 

dated October 15, 2009, for related 

information. 

Material Incorporated by Reference 

(i) You must use Pilatus Aircraft Ltd. 

Service Bulletin No: 76–002, dated October 

15, 2009; and Temporary Revision No. 12 to 

PC–12/47E Pilot’s Operating Handbook, 

dated October 15, 2009, to do the actions 

required by this AD, unless the AD specifies 

otherwise. 

(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 PILATUS AIRCRAFT LTD., 

Customer Service Manager, CH–6371 

STANS, Switzerland; telephone: +41 (0) 41 

619 62 08; fax: +41 (0) 41 619 73 11; Internet: 

http://www.pilatus-aircraft.com; e-mail: 

SupportPC12@pilatus-aircraft.com. 

(3) You may review copies of the service 

information incorporated by reference for 

this AD at the FAA, Central Region, Office of 

the Regional Counsel, 901 Locust, Kansas 

City, Missouri 64106. For information on the 

availability of this material at the Central 

Region, call (816) 329–3768. 

(4) You may also review copies of the 

service information incorporated by reference 

for this AD 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 Kansas City, Missouri, on August 

5, 2010. 

Brian A. Yanez, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–19821 Filed 8–17–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0041; Directorate 

Identifier 2009–NM–218–AD; Amendment 

39–16392; AD 2010–17–02] 

RIN 2120–AA64 

Airworthiness Directives; Airbus Model 

A330–201, –202, –203, –223, –243, 

–301, –302, –303, –321, –322, –323, 

–341, –342, and –343 Airplanes, Model 

A340–211, –212, –213, –311, –312, and 

–313 Airplanes, and Model A340–541 

and –642 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 reports have recently been received 

of loose pneumatic quick-disconnect unions 

on Goodrich pitot probes P/N (part number) 

0851HL. These may be the result of mistorque of the affected unions at equipment 

manufacturing level. Investigations are still 

on-going to determine the root cause(s). 

This condition, if not corrected, could lead 

to an air leak, resulting in incorrect total 

pressure measurement and consequent 

erroneous Calibrated Airspeed (CAS)/MACH 

parameters delivered by the Air Data 

Computer (ADC). 

* * * * * 

Loss or fluctuation of indicated airspeed 

could result in misleading information 

provided to the flightcrew. We are 

issuing this AD to require actions to 

correct the unsafe condition on these 

products. 

DATES: This AD becomes effective 

September 22, 2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of September 22, 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 notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on January 21, 2010 (75 FR 

3420). That NPRM proposed to correct 

an unsafe condition for the specified 

products. 

Since that NPRM was issued, the 

European Aviation Safety Agency 

(EASA), which is the aviation authority 

for the Member States of the European 

Community, has issued EASA 

Airworthiness Directive 2009–0202R1, 

dated April 15, 2010 (referred to after 

this as ‘‘the MCAI’’), to correct an unsafe 

condition for the specified products. 

(MCAI 2009–0202–E, dated September 

21, 2009, and corrected September 22, 

2009, was referred to in the NPRM.) The 


erowe on DSK5CLS3C1PROD with RULES
50872 Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations 

MCAI has been revised to exclude pitot 

probes marked with a red torque checkindicating mark. If the red indicating 

mark is on the pitot probe, it can be 

installed with no further action. The 

MCAI states: 

Several reports have recently been received 

of loose pneumatic quick-disconnect unions 

on Goodrich pitot probes P/N (part number) 

0851HL. These may be the result of mistorque of the affected unions at equipment 

manufacturing level. Investigations are still 

on-going to determine the root cause(s). 

This condition, if not corrected, could lead 

to an air leak, resulting in incorrect total 

pressure measurement and consequent 

erroneous Calibrated Airspeed (CAS)/MACH 

parameters delivered by the Air Data 

Computer (ADC). 

As a precautionary measure, this AD 

requires a torque check of the pneumatic 

quick-disconnect union on certain Goodrich 

P/N 0851HL pitot probes and corrective 

action, depending on findings. 

* * * * * 

This AD [MCAI] is revised in order to 

exclude from the torque-check required by 

paragraph (4) of this AD those pitot probes 

marked with a red torque check-mark. 

Loss or fluctuation of indicated airspeed 

could result in misleading information 

provided to the flightcrew. If the quickdisconnect union fitted on the pitot 

probe is not adequately torqued, the 

corrective action includes applying 

torque. You may obtain further 

information by examining the MCAI in 

the AD docket. 

Revised Service Information 

Airbus has issued All Operators 

Telexes (AOTs) A330–34A3235 (for 

Model A330–201, –202, –203, –223, 

–243, –301, –302, –303, –321, –322, 

–323, –341, –342, and –343 airplanes); 

A340–34A4241 (for Model A340–211, 

–212, –213, –311, –312, and –313 

airplanes); and A340–34A5074 (for 

Model A340–541 and –642 airplanes); 

all Revision 02, all dated March 1, 2010. 

We have revised Table 1 of this AD to 

add Revision 02 of the AOTs as the 

appropriate source of service 

information for accomplishing the 

specified actions. We have also added a 

new Table 2 to this AD to give credit for 

accomplishing the actions using the 

previous issues of the AOTs. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

considered the comments received. 

Support for NPRM 

The Airline Pilots Association (ALPA) 

supports the intent of the NPRM and 

appreciates the opportunity to 

comment. 

Request for Credit for Actions 

Accomplished Previously 

Delta Airlines asks that the NPRM be 

revised to allow credit for either 

adequate torqueing of the pneumatic 

quick-disconnect union of each pitot 

probe for affected pitot probes, or 

updating the aircraft maintenance 

manual (AMM) to ensure that the 

pneumatic quick-disconnect union of 

each pitot probe is torqued properly 

during installation. Delta states that 

Airbus AOT A330–34A3235, Revision 

02, dated March 1, 2010, specifies that 

for pitot probes that are still held as 

spares there are two choices of actions 

as noted above. 

Delta also asks that the NPRM be 

revised to give credit for pitot probes 

remanufactured and returned to Delta 

by Goodrich on which the proposed 

requirements were done before Airbus 

AOT A330–32A3235 dated September 

10, 2009, or Revision 1, dated 

September 21, 2009, were issued. Delta 

notes that those pitot probes were 

returned with adequate torque but do 

not have a torque check indicating mark 

(Airbus AOT A330–32A3235, Revision 

02, dated March 1, 2010, adds a torque 

check indicating mark after the pitot 

probe is adequately torqued). Delta 

states that it was proactive in correcting 

any deficiencies by taking immediate 

corrective actions. Delta adds that an 

allowance for this method of 

compliance should be included in the 

NPRM to avoid processing an 

alternative method of compliance 

(AMOC). 

We disagree with the commenter’s 

request to give credit for pitot probes 

remanufactured by Goodrich because 

non-marked pitot probes may be 

unintentionally installed on the airplane 

without performing a proper torque 

check. However, under the provisions of 

paragraph (h) of the final rule, we will 

consider requests for approval of an 

alternative method of compliance for 

using specific pitot probes identified by 

an operator if sufficient data are 

submitted to substantiate that the pitot 

probes would provide an acceptable 

level of safety. 

Regarding Delta’s comment on spare 

parts, we have revised paragraph (g)(4) 

of this AD to give credit for installing 

parts that have the torque check 

indicating mark. 

Conclusion 

We reviewed the available data, 

including the comments 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. 

Explanation of Change to Costs of 

Compliance 

Since issuance of the NPRM, we have 

increased the labor rate used in the 

Costs of Compliance from $80 per workhour to $85 per work-hour. The Costs of 

Compliance information, below, reflects 

this increase in the specified hourly 

labor rate. 

Costs of Compliance 

We estimate that this AD will affect 

47 products of U.S. registry. We also 

estimate that it will take about 1 workhour 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 

$3,995, 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. 


erowe on DSK5CLS3C1PROD with RULES
Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations 50873 

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: 

2010–17–02 Airbus: Amendment 39–16392. 

Docket No. FAA–2010–0041; Directorate 

Identifier 2009–NM–218–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective September 22, 2010. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to the Airbus airplanes 

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

(c)(3) of this AD; certificated in any category; 

all manufacturer serial numbers; with pitot 

probes having Goodrich part number (P/N) 

0851HL, serial numbers 267328 through 

270714 inclusive. 

(1) Model A330–201, –202, –203, –223, 

–243, –301, –302, –303, –321, –322, –323, 

–341, –342, and –343 airplanes. 

(2) Model A340–211, –212, –213, –311, 

–312, and –313 airplanes. 

(3) Model A340–541 and –642 airplanes. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 34: Navigation. 

Reason 

(e) The mandatory continued airworthiness 

information (MCAI) states: 

Several reports have recently been received 

of loose pneumatic quick-disconnect unions 

on Goodrich pitot probes P/N (part number) 

0851HL. These may be the result of mistorque of the affected unions at equipment 

manufacturing level. Investigations are still 

on-going to determine the root cause(s). 

This condition, if not corrected, could lead 

to an air leak, resulting in incorrect total 

pressure measurement and consequent 

erroneous Calibrated Airspeed (CAS)/MACH 

parameters delivered by the Air Data 

Computer (ADC). 

As a precautionary measure, this AD 

requires a torque check of the pneumatic 

quick-disconnect union on certain Goodrich 

P/N 0851HL pitot probes and corrective 

action, depending on findings. 

* * * * * 

This AD [MCAI] is revised in order to 

exclude from the torque-check required by 

paragraph (4) of this AD those pitot probes 

marked with a red torque check-mark. 

Loss or fluctuation of indicated airspeed 

could result in misleading information 

provided to the flightcrew. If the quickdisconnect union fitted on the pitot probe is 

not adequately torqued, the corrective action 

includes applying torque. 

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) At the time specified, do the following 

actions. 

(1) Within 14 days after the effective date 

of this AD: Perform a torque check of the 

pneumatic quick-disconnect union of each 

pitot probe having Goodrich P/N 0851HL, 

serial numbers 267328 through 270714 

inclusive, to determine if the torque is 

adequate, in accordance with the instructions 

of the applicable service information 

specified in Table 1 of this AD. Before further 

flight, do all applicable corrective actions in 

accordance with the instructions of the 

applicable service information specified in 

Table 1 of this AD. 

TABLE 1—AIRBUS SERVICE INFORMATION

Airbus all operators telex— Revision— Dated— 

A330–34A3235 (for Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, –341, 

–342, and –343 airplanes).

02 ................ March 1, 2010. 

A340-34A4241 (for Model A340–211, –212, –213, –311, –312, and –313 airplanes) .......................................... 02 ................ March 1, 2010. 

A340–34A5074 (for Model A340–541 and –642 airplanes) ................................................................................... 02 ................ March 1, 2010. 

(2) Within 30 days after performing the 

torque check required by paragraph (g)(1) of 

this AD, or within 30 days after the effective 

date of this AD, whichever occurs later: 

Report the torque check results to Airbus, 

including no findings, as specified in the 

instructions of the applicable service 

information listed in Table 1 of this AD. 

(3) Actions done before the effective date 

of this AD, in accordance with the applicable 

service information listed in Table 2 of this 

AD, are acceptable for compliance with the 

corresponding requirements in paragraph 

(g)(1) of this AD. 

TABLE 2—AIRBUS CREDIT SERVICE INFORMATION

Airbus all operators telex— Revision— Dated— 

A330–34A3235 ............................................................................................................................................... Original ........ September 10, 2009. 

A330–34A3235 ............................................................................................................................................... 1 .................. September 21, 2009. 


erowe on DSK5CLS3C1PROD with RULES
50874 Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations 

TABLE 2—AIRBUS CREDIT SERVICE INFORMATION—Continued 

Airbus all operators telex— Revision— Dated— 

A340–34A4241 ............................................................................................................................................... Original ........ September 10, 2009. 

A340–34A4241 ............................................................................................................................................... 1 .................. September 21, 2009. 

A340–34A5074 ............................................................................................................................................... Original ........ September 10, 2009. 

A340–34A5074 ............................................................................................................................................... 1 .................. September 21, 2009. 

(4) As of the effective date of this AD, no 

person may install a pitot probe having 

Goodrich P/N 0851HL, serial numbers 

267328 through 270714 inclusive, on any 

airplane, unless the actions required by 

paragraph (g)(1) of this AD have been done; 

or an intact red torque check mark is visible 

on the interface of the pnuematic quick 

disconnect union and the union mount. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: 

Where the MCAI includes a compliance 

time of ‘‘5 days,’’ we have determined that a 

compliance time of ‘‘within 14 days after the 

effective date of the AD’’ is appropriate. The 

manufacturer and EASA agree with this 

expansion in compliance time. 

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, FAA, Transport Airplane 

Directorate, 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 Airworthiness Directive 

2009–0202R1, dated April 15, 2010; 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, as 

applicable, to do the actions required by this 

AD, unless the AD specifies otherwise. (The 

document number, revision level, and date of 

these documents are listed only on the first 

page of these documents; no other page of 

these documents contains this information.) 

TABLE 3—MATERIAL INCORPORATED BY REFERENCE

Airbus all operators telex— Revision— Dated— 

A330–34A3235 ........................................................................................................................................................ 02 ................ March 1, 2010. 

A340–34A4241 ........................................................................................................................................................ 02 ................ March 1, 2010. 

A340–34A5074 ........................................................................................................................................................ 02 ................ March 1, 2010. 

(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 July 30, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–19701 Filed 8–17–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0782; Directorate 

Identifier 2010–SW–053–AD; Amendment 

39–16396; AD 2010–11–51] 

RIN 2120–AA64 

Airworthiness Directives; Eurocopter 

France (Eurocopter) Model AS350B, 

BA, B1, B2, C, D, and D1 Helicopters 

and Model AS355E, F, F1, F2, and N 

Helicopters 

AGENCY: Federal Aviation 

Administration, DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: This document publishes in 

the Federal Register an amendment 

adopting Airworthiness Directive (AD) 

2010–11–51, which was sent previously 

to all known U.S. owners and operators 


erowe on DSK5CLS3C1PROD with RULES