65224 Federal Register / Vol. 75, No. 204 / Friday, October 22, 2010 / Rules and Regulations 

TABLE 1—Continued 

Component Part No. (P/N) Serial No. (S/N) 

P/N SC5083–1 ............ S/N 2902 through 2921, inclusive. 

P/N 5084 ..................... S/N 30, 84, 104, 186, 438, 575, or 695. 

P/N 5084–1 ................. S/N 1462 through 1481, inclusive. 

Tail rotor servo-control ......................................................... P/N SC5072 ................ S/N 222M, 306M, or 309. 

Compliance: Required, as indicated. 

To prevent the distributor slide valve 

jamming in its sleeve, leading to reduced 

controllability of the rotors and subsequent 

loss of control of the helicopter, accomplish 

the following: 

(a) Within the next 50 hours time-inservice (TIS), or when a ‘‘hard point’’ is 

detected in the flight controls, whichever 

occurs earlier, replace each installed servo 

control that has a serial number listed in 

Table 1 of this AD, with an airworthy servo 

control. 

Note 1: Eurocopter EASB No. 01.00.58 and 

No. 01.00.53, both Revision 1, and dated 

April 19, 2007, which are not incorporated 

by reference, contain additional information 

about the subject of this AD. 

(b) To request a different method of 

compliance or a different compliance time 

for this AD, follow the procedures in 14 CFR 

39.19. Contact the Manager, Safety 

Management Group, Rotorcraft Directorate, 

FAA, ATTN: J. R. Holton, Aviation Safety 

Engineer, Regulations and Policy Group, 

ASW–111, 2601 Meacham Blvd., Fort Worth, 

Texas 76137, telephone (817) 222–4964, fax 

(817) 222–5961, for information about 

previously approved alternative methods of 

compliance. 

(c) The Joint Aircraft System/Component 

(JASC) Code is 6730: Rotorcraft Servo 

System. 

(d) This amendment becomes effective on 

November 26, 2010. 

Note 2: The subject of this AD is addressed 

in European Aviation Safety Agency (France) 

Emergency AD No. 2007–0141–E, dated May 

21, 2007. 

Issued in Fort Worth, Texas, on October 12, 

2010. 

Kim Smith, 

Manager, Rotorcraft Directorate, Aircraft 

Certification Service. 

[FR Doc. 2010–26565 Filed 10–21–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0449; Directorate 

Identifier 2009–SW–38–AD; Amendment 39– 

16456; AD 2010–20–21] 

RIN 2120–AA64 

Airworthiness Directives; Agusta 

S.p.A. Model A109E Helicopters 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. That 

AD applies to the products listed above. 

The AD number, as shown in the PART 

39—AIRWORTHINESS DIRECTIVES 

section, is incorrect. This document 

corrects that error. In all other respects, 

the original document remains the 

same. 

DATES: This final rule is effective 

November 9, 2010. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov; 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 address for the 

Docket Office (phone: 800–647–5527) is 

Document 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 20590. 

FOR FURTHER INFORMATION CONTACT: 

DOT/FAA Southwest Region, Mark 

Wiley, ASW–111, Aviation Safety 

Engineer, Rotorcraft Directorate, 

Regulations and Policy Group, 2601 

Meacham Blvd., Fort Worth, Texas 

76137, telephone (817) 222–5114, fax 

(817) 222–5961. 

SUPPLEMENTARY INFORMATION: This AD, 

Amendment 39–16456 (75 FR 61341, 

October 5, 2010), requires modifying the 

fuselage electrical installation and the 

overhead panel electrical installation for 

Agusta S.p.A. Model A109E helicopters. 

As published, the AD number shown 

in the third column on Federal Register 

page 61342 under item 2. of PART 39— 

AIRWORTHINESS DIRECTIVES section 

is incorrect. The AD number shown is 

‘‘2020–20–21;’’ the correct AD number 

should be ‘‘2010–20–21.’’ 

No other part of the preamble or 

regulatory information has been 

changed; therefore, only the changed 

portion of the final rule is being 

published in the Federal Register. 

The effective date of this AD remains 

November 9, 2010. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

In the Federal Register document 

2010–24723, filed October 4, 2010 and 

published on October 5, 2010 (75 FR 

61341), on page 61342, in the third 

column, under ‘‘§ 39.13 [Amended],’’ the 

AD number is corrected to read as 

follows: 

2010–20–21 AGUSTA S.p.A.: Amendment 

39–16456; Docket No. FAA–2010–0449; 

Directorate Identifier 2009–SW–38–AD. 

Issued in Fort Worth, Texas, on October 12, 

2010. 

Kim Smith, 

Manager, Rotorcraft Directorate, Aircraft 

Certification Service. 

[FR Doc. 2010–26569 Filed 10–21–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2010–0407; Airspace 

Docket No. 10–AGL–7] 

Amendment of Class E Airspace; 

Williston, ND 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action amends Class E 

airspace for Williston, ND, to 

accommodate Area Navigation (RNAV) 

Standard Instrument Approach 

Procedures (SIAPs) at Sloulin Field 


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