53288 Federal Register / Vol. 79, No. 174 / Tuesday, September 9, 2014 / Rules and Regulations 

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/cfr/ibrlocations.html. 

Issued in Renton, Washington, on July 14, 

2014. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–18311 Filed 9–8–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0326; Directorate 

Identifier 2013–CE–051–AD; Amendment 

39–17965; AD 2014–18–01] 

RIN 2120–AA64 

Airworthiness Directives; Rockwell 

Collins, Inc. Transponders 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Rockwell Collins TDR–94 and TDR–94D 

Mode select (S) transponders that are 

installed on airplanes. This AD was 

prompted by instances where the TDR– 

94 and TDR–94D Mode S transponders 

did not properly respond to Mode S 

Only All-Call interrogations when the 

airplane transitioned from a ground to 

airborne state. This AD requires 

inspecting the setting of the airplane 

type code category strapping and 

requires either modifying the airplane 

type code category setting or installing 

the software upgrade to convert the 

affected transponders to the new part 

number. We are issuing this AD to 

correct the unsafe condition on these 

products. 

DATES: This AD is effective October 14, 

2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of October 14, 2014. 

ADDRESSES: For service information 

identified in this AD, contact Rockwell 

Collins, Inc., Collins Aviation Services, 

350 Collins Road NE., M/S 153–250, 

Cedar Rapids, IA 52498–0001; 

telephone: 888–265–5467 (U.S.) or 319– 

265–5467; fax: 319–295–4941 (outside 

U.S.); email: techmanuals@

rockwellcollins.com; Internet: http://

www.rockwellcollins.com/Services_

and_Support/Publications.aspx. You 

may review this referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0326; 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: Ben 

Tyson, Aerospace Engineer, Wichita 

Aircraft Certification Office, FAA, 1801 

Airport Road, Room 100, Wichita, 

Kansas 67209; phone: 316–946–4174; 

fax: 316–946–4107; email: ben.tyson@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain Rockwell Collins TDR– 

94 and TDR–94D Mode select (S) 

transponders that are installed on 

airplanes. The NPRM published in the 

Federal Register on May 22, 2014, (79 

FR 29384). The NPRM was prompted by 

instances where the TDR–94 and TDR– 

94D Mode S transponders did not 

properly respond to Mode S Only AllCall interrogations when the airplane 

transitioned from a ground to airborne 

state. 

We were notified that Bombardier 

CL604 airplanes in Eurocontrol airspace 

were not transmitting the appropriate 

Mode S replies. In at least one case, the 

flight crews switched to the other 

installed transponder, resulting in 

normal operation. Rockwell Collins, Inc. 

confirmed that other types of airplane 

could exhibit this same unsafe 

condition. As a result of the issue in 

Eurocontrol airspace, EASA issued 

Airworthiness Directive 2010–0003R1, 

effective date January 11, 2010. 

The TDR–94 and TDR–94D Mode S 

transponder internal software does not 

correctly implement the air/ground 

override function when the airplane 

type code strapping is set to any value 

other than (1) or (0) and the airplane 

rotation speed is greater than 100 knots. 

The error in the air/ground override 

function inhibits the Mode S Only AllCall replies. 

The NPRM proposed to require 

inspecting the setting of the airplane 

type code category strapping and 

require either modifying the airplane 

type code category setting or installing 

the software upgrade to convert the 

affected transponders to the new part 

number. We are issuing this AD to 

correct the unsafe condition on these 

products. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comment 

received on the NPRM and the FAA’s 

response to the comment. 

Request 

Kevin Lorrigan requested we add 

Beechcraft Models B300, B300C, and 

Hawker 900XP airplanes to paragraph 

(c), Applicability, to the AD because 

typically these airplanes are equipped 

with the TDR–94 or TDR–94D 

transponders with weight-on-wheels 

input. 

The FAA agrees those airplanes were 

equipped with the TDR–94 or TDR–94D 

transponders when they were delivered 

from the factory. However, we disagree 

with adding these airplanes to 

paragraph (c), Applicability, of the AD. 

After we consulted with Beechcraft and 

reviewed their production records, we 

determined these airplanes are 

unaffected in their original ‘‘asdelivered’’ configurations. The airplanes 

were delivered with the TDR–94 or 

TDR–94D transponders, but they were 

strapped in such a manner that they 

remain unaffected. 

Paragraph (c), Applicability, of this 

AD is not intended as all-inclusive. 

Paragraph (c) of this AD states, ‘‘. . . 

transponders that are installed on but 

not limited to the airplanes . . .’’ and 

gives a partial listing of airplanes known 

to have the affected transponders 

installed. Due to the possibility of 

modification of the airplane after 

delivery, each owner must evaluate the 

airplane’s current configuration to 

determine compliance with the AD. 

We did not change the final rule AD 

action based on this comment. 

Conclusion 

We reviewed the relevant data, 

considered the comment received, and 

determined that air safety and the 

public interest require adopting this AD 

as proposed except for minor editorial 


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Federal Register / Vol. 79, No. 174 / Tuesday, September 9, 2014 / Rules and Regulations 53289 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (79 FR 

29384, May 22, 2014) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (79 FR 29384, 

May 22, 2014). 

Costs of Compliance 

We estimate that this AD affects 8,000 

products installed on airplanes of U.S. 

registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspect the setting of the airplane 

type category strapping.

1 work-hour × $85 per hour = $85 Not applicable ................................ $85 $680,000 

We estimate the following costs to do 

any necessary corrections that will be 

required based on the results of the 

inspection. We have no way of 

determining the number of airplane that 

might need these corrections: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per product 

Modify the airplane type code category strapping.1 work-hour × $85 per hour = $85 Not applicable ............................... $85. 

Convert the part number of the 

equipment.

2 work-hours × $85 per hour = 

$170.

See conversion parts cost table ... Varies depending on applicable 

part number or service bulletin. 

CONVERSION PARTS COST TABLE—TDR–94 AND TDR–94D 

Starting part number Service bulletin 

505 

Service bulletin 

507 

Service bulletin 

508 

Service bulletin 

509 

–007 ................................................................................................. N/A $5,886 $12,636 $18,465

–008 ................................................................................................. $2,323 5,886 3,414 9,429 

–108 ................................................................................................. 2,323 N/A N/A 6,816 

–207 ................................................................................................. N/A 5,886 9,234 15,057 

–308 ................................................................................................. 2,323 5,886 3,414 9,429 

–309 ................................................................................................. N/A 5,886 3,414 9,429 

–310 ................................................................................................. N/A N/A N/A 6,183 

–408 ................................................................................................. 2,323 N/A N/A 3,414 

–409 ................................................................................................. N/A N/A N/A 3,414 

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. 

Regulatory Findings 

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 that this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) 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. 

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 airworthiness 

directive (AD): 

2014–18–01 Rockwell Collins, Inc.: 

Amendment 39–17965; Docket No. 

FAA–2014–0326; Directorate Identifier 

2013–CE–051–AD. 


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53290 Federal Register / Vol. 79, No. 174 / Tuesday, September 9, 2014 / Rules and Regulations 

(a) Effective Date 

This AD is effective October 14, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

(1) This AD applies to the following 

Rockwell Collins, Inc. part number (P/N) 

Mode S transponders that are known to be 

installed on but not limited to the airplanes 

listed in paragraphs (c)(2)(i) through 

(c)(2)(xiv) of this AD, except for those 

airplanes listed in paragraphs (c)(3)(i) 

through (c)(3)(vi) of this AD, that have been 

modified in-production or in-service: 

(i) TDR–94: CPN 622–9352–008, 622– 

9352–108, 622–9352–308, 622–9352–408; 

and 

(ii) TDR–94D: CPN 622–9210–008, 622– 

9210–108, 622–9210–308, 622–9210–408. 

(2) The products listed in paragraphs 

(c)(1)(i) and (c)(1)(ii) of this AD may be 

installed on but not limited to the following 

airplanes featuring weight-on wheels input to 

the transponder, certificated in any category: 

(i) ATR42 and ATR72; 

(ii) Bombardier (Canadair) CL–600–2B16 

(604 Variant); 

(iii) Bombardier CL–600–2B19 (RJ100 and 

RJ200); 

(iv) Cessna 525, serial numbers (S/N) 525– 

0600 through 525–0684 (CJ1); 

(v) Cessna 525A, S/N 525A–0300 through 

525A–0438 (CJ2); 

(vi) Cessna 525B, S/N 525B–0001 through 

525B–0293 (CJ3); 

(vii) Cessna 560, S/N 560–0751 through 

560–0802 (Citation Encore); 

(viii) Cessna 560XL, S/N 560–6001 and 

subsequent; 

(ix) Dassault Aviation Mystere-Falcon 50; 

(x) Dassault Aviation Mystere-Falcon 900; 

(xi) Dassault Aviation Falcon 2000; 

(xii) Dassault Aviation Falcon 2000EX; 

(xiii) Piaggio Aero Industries P.180 (Avanti 

and Avanti II); and 

(xiv) SAAB 2000. 

(3) This AD action does not apply to the 

excepted airplane models, identified in 

paragraphs (c)(3)(i) through (c)(3)(vi) of this 

AD, that have been modified in-production 

or in-service. They do not have the unsafe 

condition described in this AD. 

(i) Dassault airplanes that have been 

modified in-service or in-production 

following the applicable Dassault Aviation 

service information as listed in table 1 of 

paragraph (c)(3)(i) of this AD. 

TABLE 1 OF PARAGRAPH (C)(3)(I) OF THIS AD: EXCEPTED DASSAULT AIRPLANES

Airplane models Service bulletin Modification(s) 

Mystere-Falcon 50 .............................................. F50–457 ........................................................... M2966 and M2968 

Mystere-Falcon 900 ............................................ F900–354 ......................................................... M3896 

Falcon 900EX ..................................................... F900EX–239 .................................................... M3896 

Falcon 2000 ........................................................ F2000–312 ....................................................... M2624 and M2632 

Falcon 2000EX ................................................... F2000EX–043 .................................................. M2624 

(ii) Model ATR 42 airplanes or ATR 72 

airplanes that had P/N 622–9210–108 

transponders installed in production using 

ATR modification 05614 or installed inservice using ATR Service Bulletin ATR42– 

34–0167 or ATR Service Bulletin ATR72–34– 

1094, as applicable. 

(iii) SAAB Model 2000 airplanes that had 

P/N 622–9210–008 transponders installed in 

production using SAAB modifications 6231, 

6243, and 6249 or installed in-service using 

SAAB Service Bulletins 2000–34–066, 2000– 

34–072, and 2000–34–076. 

(iv) Bombardier Aerospace (Canadair) 

airplanes Model CL–600–2B16 (604 Variant) 

that had P/N 622–9210–008 transponders 

installed and incorporated the corrective 

actions recommended in the Bombardier 

Advisory Wire AW 604–34–0078 using the 

instructions in Bombardier Aerospace 

Service Bulletin 604–34–054 (drawing 604– 

70482 Engineering Order, Revison D–1) or 

using a service request for product support. 

Bombardier Aerospace (Canadair) airplanes 

Model CL–600–2B19 (RJ100 and RJ200) that 

had P/N 622–9210–008 transponders 

installed in production using Bombardier 

Aerospace Modification TC601R16789 or in 

service using Bombardier Aerospace Service 

Bulletin 601R–34–142 (Modification 

TC601R16790). 

(v) Cessna Aircraft Company Models 525, 

525A, and 525B airplanes that had P/N 622– 

9352–008 transponders installed in 

production using Cessna Engineering Change 

Records (ECRs) 55298, 58654, and 59567; and 

Model 525B airplanes that had P/N 622– 

9352–008 transponders installed in service 

using Cessna Aircraft Company Service 

Bulletin SB525B–34–03 or SB525B–34–08. 

Cessna Aircraft Company Models 525, 525A, 

525B, 560, and 560XL airplanes that had P/ 

N 622–9210–008 transponders installed in 

production using Cessna ECRs 55298, 58654, 

59567, 56135, and 58032; and Model 525B 

airplanes that had P/N 622–9210–008 

transponders installed in service using 

Cessna Service Bulletin SB525B–34–03 or 

SB525B–34–08. 

(vi) Piaggio Aero Industries Model P.180 

(Avanti) airplanes that had P/N 622–9210– 

008 transponders installed in production 

using Piaggio modification 80–0773 or in 

service using Piaggio Service Bulletin SB– 

80–0227. Piaggio Aero Industries Model 

P.180 (Avanti II) airplanes that had P/N 622– 

9210–008 transponders installed in 

production using Piaggio modification 80– 

0588 and 80–0598. 

(d) Subject 

Joint Aircraft System Component (JASC)/

Air Transport Association (ATA) of America 

Code 34, Navigation. 

(e) Unsafe Condition 

This AD was prompted by instances where 

the TDR–94 and TDR–94D Mode S 

transponders did not properly respond to 

Mode S Only All-Call interrogations when 

the airplane transitioned from a ground to 

airborne state. We are issuing this AD to 

detect and correct Mode S transponders that 

do not respond correctly to Mode S Only AllCall interrogations, which could result in 

increased pilot and air traffic controller 

workload as well as reduced separation of 

airplanes. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection 

Within the next 2 years after October 14, 

2014 (the effective date of this AD), inspect 

the airplane type code category strapping 

setting for a value of zero (0) or one (1) 

following Rockwell Collins, Inc. Service 

Information Letter 07–2, 523–0810069– 

101000, TDR–94() SIL 07–02, Revision 1, 

dated September 2, 2008. If the airplane type 

code category strapping is set to a value of 

zero (0) or one (1), no further action is 

required by this AD. 

(h) Modification 

If the airplane type code category strapping 

is not set to a value of zero (0) or one (1), 

within two years after October 14, 2014 (the 

effective date of this AD), do the actions 

required in either paragraph (h)(1) or (h)(2), 

to include all subparagraphs, of this AD. 

(1) Modify the airplane type code category 

strapping setting to a value of zero (0) or one 

(1) following Rockwell Collins, Inc. Service 

Information Letter 07–2, 523–0810069– 

101000, TDR–94() SIL 07–02, Revision 1, 

dated September 2, 2008. 

(2) Install a software upgrade to convert the 

part numbers of the transponders to the new 

part numbers using the following Rockwell 

Collins, Inc. service information, as 

applicable: 

Note 1 to paragraph (h)(2) of this AD: More 

than one of the bulletins may apply to your 

particular P/N transponder, but each bulletin 

brings different capabilities and associated 

costs. We recommend reviewing each 

bulletin to determine the optimal choice for 

your installation. 

(i) Service Bulletin 505, 523–0816034– 

001000, TDR–94()–34–505, dated September 

2, 2008; 

(ii) Service Bulletin 507, 523–0816423– 

301000, TDR–94/94D–34–507, Revision 3, 

dated December 5, 2011; 

(iii) Service Bulletin 508, 523–0817821– 

001000, TDR–94()–34–508, dated September 

16, 2009; or 


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Federal Register / Vol. 79, No. 174 / Tuesday, September 9, 2014 / Rules and Regulations 53291 

(iv) Service Bulletin 509, 523–0817822– 

001000, TDR–94()–34–509, dated September 

16, 2009. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Wichita Aircraft 

Certification Office (ACO), FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. In accordance with 14 CFR 39.19, 

send your request to your principal inspector 

or local Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the ACO, send it to the 

attention of the person identified in 

paragraph (j)(1) of this AD. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/

certificate holding district office. 

(j) Related Information 

(1) For more information about this AD, 

contact Ben Tyson, Aerospace Engineer, 

Wichita Aircraft Certification Office, FAA, 

1801 Airport Road, Room 100, Wichita, 

Kansas 67209; phone: 316–946–4174; fax: 

316–946–4107; email: ben.tyson@faa.gov. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) Rockwell Collins, Inc. Service 

Information Letter 07–2, 523–0810069– 

101000, TDR–94() SIL 07–2, Revision 1, 

dated September 2, 2008. 

(ii) Rockwell Collins, Inc. Service Bulletin 

505, 523–0816034–001000, TDR–94()–34– 

505, dated September 2, 2008. 

(iii) Rockwell Collins, Inc. Service Bulletin 

507, 523–0816423–301000, TDR–94/94D–34– 

507, Revision 3, dated December 5, 2011. 

(iv) Rockwell Collins, Inc. Service Bulletin 

508, 523–0817821–001000, TDR–94()–34– 

508, dated September 16, 2009. 

(v) Rockwell Collins, Inc. Service Bulletin 

509, 523–0817822–001000, TDR–94()–34– 

509, dated September 16, 2009. 

(3) For service information identified in 

this AD, contact Rockwell Collins, Inc., 

Collins Aviation Services, 350 Collins Road 

NE., M/S 153–250, Cedar Rapids, IA 52498– 

0001; telephone: 888–265–5467 (U.S.) or 

319–265–5467; fax: 319–295–4941 (outside 

U.S.); email: techmanuals@

rockwellcollins.com; Internet: http://

www.rockwellcollins.com/Services_and_

Support/Publications.aspx. 

(4) You may review this referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, call 

(816) 329–4148. 

(5) You may view this 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/cfr/ibrlocations.html. 

Issued in Kansas City, Missouri, on August 

28, 2014. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2014–21027 Filed 9–8–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Economic Analysis 

15 CFR Part 801 

[Docket No. 111201710–4701–01] 

RIN 0691–AA82 

Direct Investment Surveys: BE–13, 

Survey of New Foreign Direct 

Investment in the United States; 

Correction 

AGENCY: Bureau of Economic Analysis, 

Commerce. 

ACTION: Final rule; correcting 

amendment. 

SUMMARY: This final rule corrects: The 

Regulation Identifier Number (RIN) for 

this action; the effective date; and the 

statement that the Office of Management 

and Budget (OMB) has approved the 

information collection for the BE–13, 

Survey of New Foreign Direct 

Investment in the United States, 

pursuant to the Paperwork Reduction 

Act. BEA’s information collection 

request is pending at OMB. 

DATES: The effective date of the final 

rule published on August 14, 2014 (79 

FR 47573), will be announced after the 

Office of Management and Budget 

approves the Bureau of Economic 

Analysis’ information collection 

request. 

FOR FURTHER INFORMATION CONTACT: 

Barbara K. Hubbard, Chief, Direct 

Transactions and Positions Branch (BE– 

49NI), Bureau of Economic Analysis, 

U.S. Department of Commerce, 

Washington, DC 20230; phone (202) 

606–9846. 

SUPPLEMENTARY INFORMATION: On 

Thursday, August 14, 2014, BEA 

published a final rule reinstating in the 

Code of Federal Regulations BEA’s BE– 

13 Survey of New Foreign Direct 

Investment in the United States (79 FR 

47573). That rule incorrectly identified 

the Regulation Identifier Number (RIN) 

as 0691–XC025. The correct RIN for this 

action is 0691–AA82. 

The document also stated that OMB 

had approved the information collection 

for BE–13 under OMB control number 

0608–0035. This control number has 

expired, and BEA has requested it be 

renewed by OMB. That request is 

currently pending approval at OMB. 

Once OMB approves the information 

collection, BEA will publish a 

document in the Federal Register 

informing the public that the control 

number has been approved. Until that 

time, no party is required to provide any 

information to BEA based on OMB 

control number 0608–0035. 

Finally, the document stated that the 

final rule is effective on September 15, 

2014. The effective date of the final rule 

will be announced after OMB issues a 

valid OMB control number for the 

information collection. 

Correction 

Accordingly, in final rule FR Doc. 

2014–19256, appearing on page 47573 

in the issue published on Thursday, 

August 14, 2014 (79 FR 47573), the 

following revisions are being made. 

1. On page 47573, in the heading of 

the document, first column, the RIN is 

revised to read 0691–AA82. 

2. On page 47573, the sentence in the 

second column under DATES is revised 

to read: ‘‘The effective date of this final 

rule will be announced after OMB 

issues a valid OMB control number for 

this information collection.’’ 

3. On page 47574, second column 

under Paperwork Reduction Act, the 

last sentence of the first paragraph is 

revised to read: ‘‘A new information 

collection request is pending approval 

at OMB.’’ 

Authority: 5 U.S.C. 301; 15 U.S.C. 4908; 22 

U.S.C. 3101–3108; E.O. 11961 (3 CFR, 1977 

Comp., p. 86), as amended by E.O. 12318 (3 

CFR 1981 Comp., p. 173); and E.O. 12518 (3 

CFR 1985 Comp., p. 348). 

Dated: August 25, 2014. 

Brian C. Moyer, 

Acting Director, Bureau of Economic 

Analysis. 

[FR Doc. 2014–21334 Filed 9–8–14; 8:45 am] 

BILLING CODE 3510–06–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket Number USCG–2014–0691] 

RIN 1625–AA08 

Special Local Regulation, Hydrocross, 

Lake Dora; Tavares, FL 

AGENCY: Coast Guard, DHS. 

ACTION: Temporary final rule. 


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