Federal Register / Vol. 80, No. 141 / Thursday, July 23, 2015 / Rules and Regulations 43617 

113 installed, if the grip was ever installed 

on a Model 212 helicopter or if it is unknown 

whether a grip was ever installed on a Model 

212 helicopter; and 

(2) Bell Model 212 helicopters, with a grip 

P/N ASI–4011–121–113 installed. 

(b) Unsafe Condition 

This AD defines the unsafe condition as 

installation of a grip that does not meet type 

design. This condition could result in grip 

failure, separation of the M/R blade, and 

subsequent loss of control of the helicopter. 

(c) Effective Date 

This AD becomes effective August 7, 2015. 

(d) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has 

already been accomplished prior to that time. 

(e) Required Actions 

(1) Within 5 hours time-in-service, remove 

each grip from service. 

(2) Do not install a grip listed in paragraph 

(a) of this AD on any helicopter. 

(f) Alternative Methods of Compliance 

(AMOC) 

(1) The Manager, Fort Worth Aircraft 

Certification Office, FAA, may approve 

AMOCs for this AD. Send your proposal to: 

Scott Franke, Aviation Safety Engineer, Fort 

Worth Aircraft Certification Office, Rotorcraft 

Directorate, FAA, 10101 Hillwood Pkwy, Fort 

Worth, TX 76177; telephone (817) 222–5170; 

email scott.franke@faa.gov. 

(2) For operations conducted under a 14 

CFR part 119 operating certificate or under 

14 CFR part 91, subpart K, we suggest that 

you notify your principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office or 

certificate holding district office before 

operating any aircraft complying with this 

AD through an AMOC. 

(g) Additional Information 

Timken T–700 Service Bulletin, Revision 

B, dated October 20, 2014, which is not 

incorporated by reference, contains 

additional information about the subject of 

this AD. For Timken service information 

identified in this AD, contact Timken Alcor 

Aerospace Technologies, Inc., Aftermarket 

Customer Service, 3110 N. Oakland, Mesa, 

AZ 85215; telephone 1–480–606–3130; email 

timkenaftermarketsales@timken.com; or at 

http://www.timken.com/en-us/solutions/

aerospace/aftermarket/Pages/default.aspx. 

You may review a copy of this service 

information at the FAA, Office of the 

Regional Counsel, Southwest Region, 10101 

Hillwood Pkwy, Room 6N–321, Fort Worth, 

TX 76177. 

(h) Subject 

Joint Aircraft Service Component (JASC) 

Code: 6620, Main Rotor Blade Grip. 

Issued in Fort Worth, Texas, on July 13, 

2015. 

Bruce E. Cain, 

Acting Directorate Manager, Rotorcraft 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–17953 Filed 7–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 73 

[Docket No. FAA–2014–0640; Airspace 

Docket No. 14–ACE–4] 

RIN 2120–AA66 

Modification of Restricted Areas R– 

4501A, R–4501B, R–4501C, R–4501D, 

R–4501F, and R–4501H; Fort Leonard 

Wood, MO 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: This action corrects a final 

rule published in the Federal Register 

on May 26, 2015 by adding one set of 

geographic latitude/longitude 

coordinates that was inadvertently 

omitted from the restricted area R– 

4501H boundary description. 

DATES: Effective date 0901 UTC, August 

20, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Colby Abbott, Airspace Policy and 

Regulations Group, Office of Airspace 

Services, Federal Aviation 

Administration, 800 Independence 

Avenue SW., Washington, DC 20591; 

telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

History 

A final rule was published in the 

Federal Register on May 26, 2015 (80 

FR 29941), that established a single 

ceiling of one restricted area (R–4501B), 

added exclusions to three restricted 

areas (R–4501C, R–4501F, and R– 

4501H) to prevent overlapped restricted 

areas being active at the same time, 

made administrative changes to the title 

of two restricted areas (R–4501A and R– 

4501B), and made administrative 

changes to the using agency information 

of six restricted areas (R–4501A–D, R– 

4501F, and R–4501H) in Fort Leonard 

Wood, MO. Subsequent to publication, 

the FAA determined that one set of 

geographic latitude/longitude 

coordinates was inadvertently omitted 

from the R–4501H boundary 

description. This correction inserts the 

set of geographic latitude/longitude 

coordinates back into the R–4501H 

boundary description to retain the 

lateral boundary of the restricted area as 

it existed prior to the published final 

rule. 

Correction to Final Rule 

Accordingly, pursuant to the 

authority delegated to me, in Docket No. 

FAA–2014–0640, the boundary 

description for restricted area R–4501H, 

as published in the Federal Register on 

May 26, 2015 (80 FR 29941), FR Doc. 

2015–12627, modifying the restricted 

areas at Fort Leonard Wood, MO, is 

corrected as follows: 

§ 73.45 (Amended) 

On page 29942, column 2, line 57, 

after the words ‘‘Reservation boundary;’’ 

insert ‘‘to lat. 37°46′45′′ N., long. 

92°01′41′′ W.;’’. 

Issued in Washington, DC, on July 16, 

2015. 

Gary A. Norek, 

Manager, Airspace Policy and Regulations 

Group. 

[FR Doc. 2015–18012 Filed 7–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No. 31030; Amdt. No. 521] 

IFR Altitudes; Miscellaneous 

Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This amendment adopts 

miscellaneous amendments to the 

required IFR (instrument flight rules) 

altitudes and changeover points for 

certain Federal airways, jet routes, or 

direct routes for which a minimum or 

maximum en route authorized IFR 

altitude is prescribed. This regulatory 

action is needed because of changes 

occurring in the National Airspace 

System. These changes are designed to 

provide for the safe and efficient use of 

the navigable airspace under instrument 

conditions in the affected areas. 

DATES: Effective 0901 UTC, August 20, 

2015. 

FOR FURTHER INFORMATION CONTACT: 

Richard A. Dunham, Flight Procedure 

Standards Branch (AMCAFS–420), 

Flight Technologies and Programs 

Division, Flight Standards Service, 

Federal Aviation Administration, Mike 

Monroney Aeronautical Center, 6500 

South MacArthur Blvd. Oklahoma City, 

OK 73169 (Mail Address: P.O. Box 


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