56150 Federal Register / Vol. 78, No. 177 / Thursday, September 12, 2013 / Rules and Regulations 

Liner (lower drive link bearing), P/N 406– 

010–417–109, installed. 

(8) Model 427 with Tail Rotor Actuator 

Output Idler, P/N 427–001–723–101, 

installed. 

(9) Model 430 with 

(i) Fitting Assembly Engine Bipod Mount, 

P/N 230–060–113–101, 230–060–113–102, 

230–060–114–101, or 230–060–114–102; 

Bearing Assembly M/R Rotating Controls, P/ 

N 430–010–449–101; Rod End Assembly Lift 

link, P/N 430–010–204–101 or 430–010–204– 

103, or 

(ii) Bellcrank Assembly Directional 

Controls, P/N 222–001–734–001, or 222– 

001–736–005, installed. 

(b) Unsafe Condition 

This AD defines the unsafe condition as 

bearings that may not have been staked as 

required and may migrate out of their proper 

position and limit the functionality of the 

affected part. This condition could result in 

failure of a bearing and the lever assembly in 

which it is installed and subsequent loss of 

control of the helicopter. 

(c) Effective Date 

This AD becomes effective October 17, 

2013. 

(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) Perform each action required by this AD 

within the compliance time for each part 

listed in the applicability paragraph of this 

AD as follows: (a)(1), (a)(2), (a)(6)(i), (a)(7), 

and (a)(8), within 10 hours time-in-service 

(TIS) or 30 days, whichever occurs first; 

(a)(3)(i), (a)(4)(i), (a)(5)(i), and (a)(9)(i), within 

5 hours TIS or 30 days, whichever occurs 

first; (a)(3)(ii), (a)(4)(ii), (a)(5)(ii), and (a)(9)(ii) 

within 150 hours TIS or 12 months, 

whichever occurs first; and (a)(6)(ii) within 

300 hours TIS or 12 months, whichever 

occurs first. 

(2) Using a 10X or higher power 

magnifying glass or using a boroscope, 

inspect each bearing and determine if the 

bearing has been properly staked for each 

part that contains a part serial number with 

a prefix of either ‘‘TI’’ or ‘‘TIFS.’’ 

(i) If a part does not contain a serial 

number, inspect the bearing of that part even 

if that part contains a supplier marking. 

(ii) If you cannot access the bearing while 

the part is installed on the helicopter to make 

a determination as to whether the bearing in 

the part is properly staked, remove the part 

and inspect the bearing using a 10X or higher 

power magnifying glass or using a boroscope. 

(iii) If you find a part that is not properly 

staked, replace the bearing or the assembly 

with an airworthy bearing or assembly before 

further flight. 

(f) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Safety Management 

Group, FAA, may approve AMOCs for this 

AD. Send your proposal to Sharon Miles, 

ASW–111, Aviation Safety Engineer, 

Rotorcraft Directorate, Regulations and 

Guidance Group, 2601 Meacham Blvd., Fort 

Worth, Texas 76137, telephone (817) 222– 

5110, email sharon.y.miles@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 

(1) Bell Alert Service Bulletin (ASB) No. 

206–09–122 for Models 206A and 206B; No. 

206L–09–156 for Models 206L, 206L–1, 

206L–3, and 206L–4; No. 222–09–107 for 

Models 222 and 222B; No. 222U–09–78 for 

Model 222U; No. 230–09–39 for Model 230; 

No. 407–09–88 for Model 407; No. 427–09– 

25 for Model 427; and No. 430–09–42 for 

Model 430, all dated April 7, 2009, which are 

not incorporated by reference, contain 

additional information about the subject of 

this AD. For service information identified in 

this AD, contact Bell Helicopter Textron 

Canada Limited, 12,800 Rue de l’Avenir, 

Mirabel, Quebec J7J1R4, telephone (450) 

437–2862 or (800) 363–8023, fax (450) 433– 

0272, or at http://www.bellcustomer.com/

files/. You may review the referenced service 

information at the FAA, Office of the 

Regional Counsel, Southwest Region, 2601 

Meacham Blvd., Room 663, Fort Worth, 

Texas 76137. 

(2) The subject of this AD is addressed in 

Transport Canada Civil Aviation AD No. CF– 

2009–32, dated July 24, 2009, which may be 

reviewed in the AD docket on the Internet at 

http://www.regulations.gov. 

(h) Subject 

Joint Aircraft System/Component (JASC) 

Code: 6700 Rotorcraft Flight Controls and 

6710 Main Rotor Control. 

Issued in Fort Worth, Texas, on August 27, 

2013. 

Kim Smith, 

Directorate Manager, Rotorcraft Directorate, 

Aircraft Certification Service. 

[FR Doc. 2013–21716 Filed 9–11–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0535; Directorate 

Identifier 2013–CE–018–AD; Amendment 

39–17489; AD 2013–13–01] 

RIN 2120–AA64 

Airworthiness Directives; Piper 

Aircraft, Inc. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting an 

airworthiness directive (AD) that 

published in the Federal Register. AD 

2013–13–01 applies to certain Piper 

Aircraft, Inc. Models PA–46–310P, PA– 

46–350P, PA–46R–350T, and PA–46– 

500TP airplanes. There is an incorrect 

reference to a paragraph designation, 

four instances of an incorrect reference 

to the paragraph in the service bulletin 

that references an airworthiness 

limitation, and an incomplete email 

address for the person to contact in the 

Related Information section. This 

document corrects those errors. In all 

other respects, the original document 

remains the same. 

DATES: This final rule is effective 

September 12, 2013. The effective date 

for AD 2013–13–01 (78 FR 41277, July 

10, 2013) remains July 10, 2013. 

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: Gary 

Wechsler, Aerospace Engineer, Atlanta 

Aircraft Certification Office, FAA, 1701 

Columbia Avenue, College Park, Georgia 

30337; telephone: (404) 474–5575; fax: 

(404) 474–5606; email: gary.wechsler@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2013–13–01, 

Amendment 39–17489 (78 FR 41277, 

July 10, 2013), currently requires 

inspecting the fuel vent valves to 

identify if the nitrile parts are installed 

and modifying and eventually replacing 

the fuel vent valves if the nitrile parts 

are installed for certain Piper Aircraft, 

Inc. Models PA–46–310P, PA–46–350P, 

PA–46R–350T, and PA–46–500TP 

airplanes. 

As published, there is an incomplete 

email address in the For Further 

Information Contact section of the 

preamble. There is an incorrect 

reference to a paragraph designation, 

four instances of an incorrect reference 

to the paragraph in the service bulletin 

that references an airworthiness 

limitation, and an incomplete email 

address for the person to contact in the 

regulatory information. 


tkelley on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 78, No. 177 / Thursday, September 12, 2013 / Rules and Regulations 56151 

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 10, 2013. 

Correction of Non-Regulatory Text 

In the Federal Register of July 10, 

2013, AD 2013–13–01; Amendment 39– 

17489 is corrected as follows: 

On page 41278, in the first column, on 

line 6 under FOR FURTHER INFORMATION

CONTACT:, change the email address 

from ‘‘gary.wechsler@faa’’ to 

‘‘gary.wechsler@faa.gov.’’ 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

In the Federal Register of July 10, 

2013, on page 41279, in the third 

column, the last sentence of paragraph 

(g)(3) of AD 2013–13–01 is corrected to 

read as follows: 

* * * * * 

. . . A copy of the limitations from 

paragraph 4 of Part II of Piper Aircraft, Inc. 

Mandatory Service Bulletin No. 1258, dated 

June 15, 2013, must be inserted in the pilot’s 

operating handbook. 

* * * * * 

In the Federal Register of July 10, 

2013, on page 41280, in the first 

column, the text in line 7 of 

subparagraph (h)(1) of AD 2013–13–01 

is corrected to read as follows: 

* * * * * 

. . . paragraph (g)(4) of this AD, replace 

the nitrile . . . . 

* * * * * 

In the Federal Register of July 10, 

2013, on page 41280, in the first 

column, the last sentence of 

subparagraph (h)(1) of AD 2013–13–01 

is corrected to read as follows: 

* * * * * 

. . . This would include removing the 

limitations requirement in paragraph 4 of 

Part II of the service bulletin. 

* * * * * 

In the Federal Register of July 10, 

2013, on page 41280, in the first 

column, the last sentence of 

subparagraph (h)(2) of AD 2013–13–01 

is corrected to read as follows: 

* * * * * 

. . . This would include removing the 

limitations requirement in paragraph 4 of 

Part II of the service bulletin. 

* * * * * 

In the Federal Register of July 10, 

2013, on page 41280, in the first 

column, the text in line 10 of paragraph 

(i) of AD 2013–13–01 is corrected to 

read as follows: 

* * * * * 

. . . the limitations from paragraph 4 of 

. . . . 

* * * * * 

In the Federal Register of July 10, 

2013, on page 41280, in the second 

column, the email address in line 6 of 

paragraph (k), heading Related 

Information, of AD 2013–13–01 is 

corrected to read as follows: 

* * * * * 

. . . gary.wechsler@faa.gov. 

* * * * * 

Issued in Kansas City, Missouri, on 

September 3, 2013. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–22184 Filed 9–11–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 165 

[Docket No. USCG–2013–0755] 

RIN 1625–AA00 

Safety Zone, North Atlantic Ocean; 

Virginia Beach, VA 

AGENCY: Coast Guard, DHS. 

ACTION: Temporary final rule. 

SUMMARY: The Coast Guard is 

establishing a safety zone on the 

navigable waters of the North Atlantic 

Ocean in Virginia Beach, VA to support 

the Virginia Symphony Orchestra 

fireworks display. This action is 

intended to restrict vessel traffic 

movement in the designated area in 

order to protect the life and property of 

the maritime public and spectators from 

the hazards associated with fireworks 

displays. 

DATES: This rule will be effective from 

9:20 p.m. to 10:10 p.m. on September 

12, 2013. 

ADDRESSES: Documents mentioned in 

this preamble are part of docket [USCG– 

2013–0755]. To view documents 

mentioned in this preamble as being 

available in the docket, go to http://

www.regulations.gov, type the docket 

number in the ‘‘SEARCH’’ box and click 

‘‘SEARCH.’’ Click on Open Docket 

Folder on the line associated with this 

rulemaking. You may also visit the 

Docket Management Facility in Room 

W12–140 on the ground floor of the 

Department of Transportation West 

Building, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

FOR FURTHER INFORMATION CONTACT: If 

you have questions on this rule, call or 

email LCDR Hector Cintron, Waterways 

Management Division Chief, Sector 

Hampton Roads, Coast Guard; telephone 

(757) 668–5581, email 

Hector.L.Cintron@uscg.mil. If you have 

questions on viewing or submitting 

material to the docket, call Barbara 

Hairston, Program Manager, Docket 

Operations, telephone (202) 366–9826. 

SUPPLEMENTARY INFORMATION: 

Table of Acronyms 

DHS Department of Homeland Security 

FR Federal Register 

NPRM Notice of Proposed Rulemaking 

A. Regulatory History and Information 

The Coast Guard is issuing this 

temporary final rule without prior 

notice and opportunity to comment 

pursuant to authority under section 4(a) 

of the Administrative Procedure Act 

(APA) (5 U.S.C. 553(b)). This provision 

authorizes an agency to issue a rule 

without prior notice and opportunity to 

comment when the agency for good 

cause finds that those procedures are 

‘‘impracticable, unnecessary, or contrary 

to the public interest.’’ Under 5 U.S.C. 

553(b)(B), the Coast Guard finds that 

good cause exists for not publishing a 

notice of proposed rulemaking (NPRM) 

with respect to this rule because the 

Coast Guard received the application for 

a marine event well short of the 135 day 

window required for a new marine 

event application. As such, it is 

impracticable to provide a full comment 

period due to lack of time. Any delay 

encountered in this regulation’s 

effective date to provide for a comment 

period would be contrary to the public 

interest as immediate action is needed 

to ensure the safety of the event 

participants, patrol vessels, spectator 

craft and other vessels transiting the 

event area. The Coast Guard will 

provide advance notifications to users of 

the affected waterways of the safety 

zone via marine information broadcasts 

and/or local notice to mariners. 

B. Basis and Purpose 

The legal basis for this rule is 33 

U.S.C. 1231; 46 U.S.C. Chapter 701, 

3306, 3703; 50 U.S.C. 191, 195; 33 CFR 

1.05–1, 6.04–1, 6.04–6, 160.5; Pub. L. 

107–295, 116 Stat. 2064; Department of 

Homeland Security Delegation No. 

0170.1. 


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