Federal Register / Vol. 75, No. 225 / Tuesday, November 23, 2010 / Rules and Regulations 71353 

effective date of this AD, unless the actions 

have already been done. 

One-Time Visual Inspection of the No. 3 

Bearing Oil Pressure Tube 

(f) Perform a one-time visual inspection of 

the exterior of the No. 3 bearing oil pressure 

tube for cracks and evidence of being 

repaired. 

(1) Remove the tube from service if any 

cracks are found. 

(2) Remove the tube from service if found 

repaired, or if suspected that the tube was 

repaired. 

(g) After the effective date of this AD, do 

not install any repaired No. 3 bearing oil 

pressure tube into any engine. 

(h) Guidance on the No. 3 bearing oil 

pressure tube visual inspection can be found 

in: 

(1) Pratt & Whitney Clean, Inspect, Repair 

Manual PN 51A357, 72–41–20 for PW4000– 

94’’ and PW4000–100’’ series engines; or 

(2) Pratt & Whitney Clean, Inspect, Repair 

Manual PN 51A750, 72–41–20 for PW4000– 

112’’ series engines. 

Definitions 

(i) For the purpose of this AD, piece part 

condition means that the part is completely 

disassembled from the engine as specified in 

the disassembly instructions in the 

manufacturer’s engine manual. 

Alternative Methods of Compliance 

(j) The Manager, Engine Certification 

Office, FAA, may approve alternative 

methods of compliance for this AD, if 

requested using the procedures found in 14 

CFR 39.19. 

Related Information 

(k) For more information about this AD, 

contact James Gray, Aerospace Engineer, 

Engine Certification Office, FAA, Engine and 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

telephone (781) 238–7742; fax (781) 238– 

7199; e-mail: james.e.gray@faa.gov. 

Material Incorporated by Reference 

(l) None. 

Issued in Burlington, Massachusetts, on 

November 16, 2010. 

Robert G. Mann, 

Acting Manager, Engine & Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2010–29451 Filed 11–22–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–1076; Directorate 

Identifier 2009–CE–019–AD; Amendment 

39–16296; AD 2010–10–17] 

RIN 2120–AA64 

Airworthiness Directives; Mitsubishi 

Heavy Industries, Ltd. Various Models 

MU–2B Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that has 

published in the Federal Register. That 

AD applies to the products listed above. 

The reissue date of September 24, 1986, 

of the MU–2B–60 airplane flight manual 

(AFM) in table 3 of the Compliance 

section (e)(1)(i) is incorrect, in that it is 

‘‘September 24, 1985,’’ instead of 

‘‘September 24, 1986.’’ This document 

corrects this error. In all other respects, 

the original document remains the 

same. 

DATES: This final rule; correction is 

effective November 23, 2010. The 

effective date for AD 2010–10–17 

remains July 22, 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: Matt 

Bryant, Propulsion Engineer, FAA, Fort 

Worth ACO, 2601 Meacham Blvd., Fort 

Worth, Texas 76137; telephone: (817) 

222–5146; fax: (817) 222–5960; e-mail: 

matthew.a.bryant@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2010–10–17, 

amendment 39–16296 (75 FR 34349), 

which supersedes Airworthiness 

Directive (AD) 2006–17–01, AD 2006– 

15–07, AD 2000–02–25, and AD 97–25– 

02, currently retains from AD 2006–17– 

01 the inspection of the engine torque 

indication system and possible 

recalibration of the torque pressure 

transducers and requires incorporating 

all revisions up to and including the 

latest revisions of the AFM for certain 

MHI various Models MU–2B airplanes. 

As published, table 3 specific to the 

MHI MU–2B–60 airplane stating that the 

MU–2B–60 AFM has a reissued date of 

September 24, 1986, in the Compliance 

section (e) is incorrect, in that it is 

‘‘September 24, 1985,’’ instead of 

‘‘September 24, 1986.’’ 

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 

July 22, 2010. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

■ In the Federal Register of June 17, 

2010, AD 2010–10–17; Amendment 

39–16296 is corrected as follows: 

On page 34352, in the Compliance 

section paragraph (e)(1)(i) in table 3, 

under the third column ‘‘Date and 

version of AFM,’’ change the AFM, 

Section 6, Reissued date ‘‘September 24, 

1986,’’ to ‘‘September 24, 1985.’’ 

Issued in Kansas City, Missouri, on 

November 17, 2010. 

Patrick R. Mullen, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–29463 Filed 11–22–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

28 CFR Part 26 

[Docket No. OJP 1464; AG Order No.] 

RIN 1121–AA76 

Office of the Attorney General; 

Certification Process for State Capital 

Counsel Systems; Removal of Final 

Rule 

AGENCY: Department of Justice. 

ACTION: Final rule. 

SUMMARY: Pursuant to the USA 

PATRIOT Improvement and 

Reauthorization Act of 2005, the 

Department of Justice promulgated a 

final rule to implement certification 

procedures for States seeking to qualify 

for the special federal habeas corpus 

review procedures in capital cases. A 

Federal district court issued an 

injunction requiring the Department to 

provide an additional public comment 

period and publish a response to any 

comments received during that period. 

The Department then solicited further 

mstockstill on DSKH9S0YB1PROD with RULES