Federal Register / Vol. 76, No. 46 / Wednesday, March 9, 2011 / Rules and Regulations 12845 

applicable normal nonoperating temperature 

shall be as described in sections 2.9.3.1, 

2.9.3.2, 2.9.3.3, and 2.9.3.4, as applicable. 

* * * * * 

2.9.1.3 Standby mode and off mode watt 

meter. The watt meter used to measure 

standby mode and off mode shall have a 

resolution as specified in Section 4, 

Paragraph 4.5 of IEC 62301 (incorporated by 

reference; see § 430.3). The watt meter shall 

also be able to record a ‘‘true’’ average power 

as specified in Section 5, Paragraph 5.3.2(a) 

of IEC 62301. 

* * * * * 

3. Test Methods and Measurements 

3.1. Test methods. 

3.1.1 Conventional oven. Perform a test 

by establishing the testing conditions set 

forth in section 2, ‘‘TEST CONDITIONS,’’ of 

this Appendix, and adjust any pilot lights of 

a conventional gas oven in accordance with 

the manufacturer’s instructions and turn off 

the gas flow to the conventional cooking top, 

if so equipped. Before beginning the test, the 

conventional oven shall be at its normal 

nonoperating temperature as defined in 

section 1.7 and described in section 2.6. Set 

the conventional oven test block W1

approximately in the center of the usable 

baking space. If there is a selector switch for 

selecting the mode of operation of the oven, 

set it for normal baking. If an oven permits 

baking by either forced convection by using 

a fan, or without forced convection, the oven 

is to be tested in each of those two modes. 

The oven shall remain on for at least one 

complete thermostat ‘‘cut-off/cut-on’’ of the 

electrical resistance heaters or gas burners 

after the test block temperature has increased 

234 °F (130 °C) above its initial temperature. 

3.1.1.1 Self-cleaning operation of a 

conventional oven. Establish the test 

conditions set forth in section 2, ‘‘TEST 

CONDITIONS,’’ of this Appendix. Adjust any 

pilot lights of a conventional gas oven in 

accordance with the manufacturer’s 

instructions and turn off the gas flow to the 

conventional cooking top. The temperature of 

the conventional oven shall be its normal 

nonoperating temperature as defined in 

section 1.7 and described in section 2.6. 

Then set the conventional oven’s selfcleaning process in accordance with the 

manufacturer’s instructions. If the selfcleaning process is adjustable, use the 

average time recommended by the 

manufacturer for a moderately soiled oven. 

* * * * * 

3.1.2 Conventional cooking top. Establish 

the test conditions set forth in section 2, 

‘‘TEST CONDITIONS,’’ of this Appendix. 

Adjust any pilot lights of a conventional gas 

cooking top in accordance with the 

manufacturer’s instructions and turn off the 

gas flow to the conventional oven(s), if so 

equipped. The temperature of the 

conventional cooking top shall be its normal 

nonoperating temperature as defined in 

section 1.7 and described in section 2.6. Set 

the test block in the center of the surface unit 

under test. The small test block, W2, shall be 

used on electric surface units of 7 inches (178 

mm) or less in diameter. The large test block, 

W3, shall be used on electric surface units 

over 7 inches (177.8 mm) in diameter and on 

all gas surface units. Turn on the surface unit 

under test and set its energy input rate to the 

maximum setting. When the test block 

reaches 144 °F (80 °C) above its initial test 

block temperature, immediately reduce the 

energy input rate to 25 ± 5 percent of the 

maximum energy input rate. After 15 ± 0.1 

minutes at the reduced energy setting, turn 

off the surface unit under test. 

* * * * * 

3.1.3 Microwave oven. 

3.1.3.1 Microwave oven test standby 

mode and off mode power. Establish the 

testing conditions set forth in section 2, 

‘‘TEST CONDITIONS,’’ of this Appendix. For 

microwave ovens that drop from a higher 

power state to a lower power state as 

discussed in Section 5, Paragraph 5.1, Note 

1 of IEC 62301 (incorporated by reference; 

see section 430.3), allow sufficient time for 

the microwave oven to reach the lower power 

state before proceeding with the test 

measurement. Follow the test procedure as 

specified in Section 5, Paragraph 5.3 of IEC 

62301. For units in which power varies as a 

function of displayed time in standby mode, 

set the clock time to 3:23 and use the average 

power approach described in Section 5, 

Paragraph 5.3.2(a), but with a single test 

period of 10 minutes +0/¥2 sec after an 

additional stabilization period until the clock 

time reaches 3:33. If a microwave oven is 

capable of operation in either standby mode 

or off mode, as defined in sections 1.12 and 

1.8, respectively, or both, test the microwave 

oven in each mode in which it can operate. 

* * * * * 

3.2.3 Microwave oven test standby mode 

and off mode power. Make measurements as 

specified in Section 5, Paragraph 5.3 of IEC 

62301 (incorporated by reference; see 

§ 430.3). If the microwave oven is capable of 

operating in standby mode, measure the 

average standby mode power of the 

microwave oven, PSB, in watts as specified in 

section 3.1.3.1. If the microwave oven is 

capable of operating in off mode, measure the 

average off mode power of the microwave 

oven, POFF, as specified in section 3.1.3.1. 

* * * * * 

3.3.13 Record the average standby mode 

power, PSB, for the microwave oven standby 

mode, as determined in section 3.2.3 for a 

microwave oven capable of operating in 

standby mode. Record the average off mode 

power, POFF, for the microwave oven off 

mode power test, as determined in section 

3.2.3 for a microwave oven capable of 

operating in off mode. 

* * * * * 

[FR Doc. 2011–5044 Filed 3–8–11; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–1296; Directorate 

Identifier 2010–CE–063–AD; Amendment 

39–16625; AD 2011–06–01] 

RIN 2120–AA64 

Airworthiness Directives; APEX 

Aircraft Model CAP 10 B Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

issued by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

A fatal accident occurred to a CAP 10C, in 

which the pilot lost control of the aeroplane. 

The following investigation has revealed 

that the probable cause of the accident was 

the improper locking of a turnbuckle (locking 

clip missing) of the flight control cables, and 

the subsequent inadvertent release of the 

pitchup control cable from the turnbuckle. 

We are issuing this AD to require 

actions to correct the unsafe condition 

on these products. 

DATES: This AD becomes effective April 

13, 2011. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at 

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: 

Sarjapur Nagarajan, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329– 

4145; fax: (816) 329–4090. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on December 30, 2010 (75 FR 

82335). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

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12846 Federal Register / Vol. 76, No. 46 / Wednesday, March 9, 2011 / Rules and Regulations 

A fatal accident occurred to a CAP 10C, in 

which the pilot lost control of the aeroplane. 

The following investigation has revealed 

that the probable cause of the accident was 

the improper locking of a turnbuckle (locking 

clip missing) of the flight control cables, and 

the subsequent inadvertent release of the 

pitchup control cable from the turnbuckle. 

For the above described reasons, this AD 

requires repetitive inspections to verify the 

correct installation of the turnbuckles of the 

flight control cables and, if foreseen by the 

applicable design configuration of the 

turnbuckles and found to be missing, to 

restore the locking clip and the safety wire. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

Differences Between This AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow FAA policies. 

Any such differences are highlighted in 

a NOTE within the AD. 

Costs of Compliance 

We estimate that this AD will affect 

28 products of U.S. registry. We also 

estimate that it will take about 3 workhours per product to comply with the 

basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts will cost about $100 per 

product. 

Based on these figures, we estimate 

the cost of this AD to the U.S. operators 

to be $9,940 or $355 per product. 

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 

We determined that 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 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); and 

(3) 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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD Docket. 

Examining the AD Docket 

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 the NPRM, the 

regulatory evaluation, any comments 

received, and other information. The 

street address for the Docket Office 

(telephone (800) 647–5527) is in the 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

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 AD: 

2011–06–01 APEX Aircraft: Amendment 

39–16625; Docket No. FAA–2010–1296; 

Directorate Identifier 2010–CE–063–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective April 13, 2011. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to APEX Aircraft 

Model CAP10 B and CAP10 B airplanes with 

Major Change 000302 (commercial name 

CAP10C), all serial numbers, certificated in 

any category. 

Subject 

(d) Air Transport Association of America 

(ATA) Code 27: Flight Controls. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

A fatal accident occurred to a CAP 10C, in 

which the pilot lost control of the aeroplane. 

The following investigation has revealed 

that the probable cause of the accident was 

the improper locking of a turnbuckle (locking 

clip missing) of the flight control cables, and 

the subsequent inadvertent release of the 

pitchup control cable from the turnbuckle. 

For the above described reasons, this AD 

requires repetitive inspections to verify the 

correct installation of the turnbuckles of the 

flight control cables and, if foreseen by the 

applicable design configuration of the 

turnbuckles and found to be missing, to 

restore the locking clip and the safety wire. 

Actions and Compliance 

(f) Unless already done, do the following 

actions: 

(1) Within the next 2 months after April 13, 

2011 (the effective date of this AD): 

(i) If the turnbuckles are designed to be 

locked with locking clips and safety wire, 

verify that the locking clips are properly 

installed in the corresponding groove, that 

the safety wire of a minimum diameter of 0.8 

millimeter (mm) is correctly installed, and 

that there is no damage to the whole 

turnbuckle installation. 

(ii) For all other designs of turnbuckles, 

verify the correct installation of the safety 

locking devices. 

(iii) If any discrepancy is found during the 

inspection required by paragraph (f)(1)(i) or 

(f)(1)(ii) of this AD, before further flight, 

restore the correct turnbuckle installation in 

accordance with standard maintenance 

practice. 

(2) Repeat the inspection required by 

paragraph (f)(1)(i) or (f)(1)(ii) of this AD, as 

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Federal Register / Vol. 76, No. 46 / Wednesday, March 9, 2011 / Rules and Regulations 12847 

applicable to the turnbuckles design, and the 

associated corrective actions required by 

paragraph (f)(1)(iii) of this AD at intervals not 

to exceed 110 hours time-in-service or 13 

months since the last inspection, whichever 

occurs first. 

FAA AD Differences 

Note: This AD differs from the MCAI and/ 

or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Sarjapur Nagarajan, Aerospace 

Engineer, FAA, Small Airplane Directorate, 

901 Locust, Room 301, Kansas City, Missouri 

64106; telephone: (816) 329–4145; fax: (816) 

329–4090. Before using any approved AMOC 

on any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

(2) Airworthy Product: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer or other source, 

use these actions if they are FAA-approved. 

Corrective actions are considered FAAapproved if they are approved by the State 

of Design Authority (or their delegated 

agent). You are required to assure the product 

is airworthy before it is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a Federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave., SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

Related Information 

(h) Refer to MCAI European Aviation 

Safety Agency (EASA) AD No.: 2010–0233, 

dated November 26, 2010, for related 

information. 

Issued in Kansas City, Missouri, on 

February 28, 2011. 

John Colomy, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2011–5101 Filed 3–8–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 201 

[Docket No. FDA–2011–N–0101] 

Change of Address; Requests for 

Exemption From the Bar Code Label 

Requirements 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; technical 

amendment. 

SUMMARY: The Food and Drug 

Administration (FDA) is amending its 

regulations to update the address for 

submitting bar code exemption requests 

to the Center for Drug Evaluation and 

Research (CDER). This action is being 

taken to ensure accuracy and clarity in 

the Agency’s regulations. 

DATES: This rule is effective March 9, 

2011. 

FOR FURTHER INFORMATION CONTACT: 

Rikin Mehta, Center for Drug Evaluation 

and Research, Food and Drug 

Administration, 10903 New Hampshire 

Ave., Bldg. 51, Rm. 5235, Silver Spring, 

MD 20993–0002, 301–796–3937. 

SUPPLEMENTARY INFORMATION: FDA is 

amending 21 CFR 201.25(d)(2) to update 

the address for submitting bar code 

exemption requests to CDER. The new 

address for these submissions is Office 

of Compliance, Center for Drug 

Evaluation and Research, Food and 

Drug Administration, 10903 New 

Hampshire Ave., Bldg. 51, Silver Spring, 

MD 20993–0002. This action is being 

taken to ensure accuracy and clarity in 

the Agency’s regulations. 

Publication of this document 

constitutes final action on these changes 

under the Administrative Procedure Act 

(5 U.S.C. 553). FDA has determined that 

notice and public comment are 

unnecessary because this amendment to 

the regulations provides only technical 

changes to update an address for 

submitting bar code exemption requests 

to CDER. 

List of Subjects in 21 CFR Part 201 

Drugs, Labeling, Reporting and 

recordkeeping requirements. 

Therefore, under the Federal Food, 

Drug, and Cosmetic Act and under 

authority delegated to the Commissioner 

of Food and Drugs, 21 CFR part 201 is 

amended as follows: 

PART 201—LABELING 

■ 1. The authority citation for 21 CFR 

part 201 continues to read as follows: 

Authority: 21 U.S.C. 321, 331, 351, 352, 

353, 355, 358, 360, 360b, 360gg-360ss, 371, 

374, 379e; 42 U.S.C. 216, 241, 262, 264. 

■ 2. Section 201.25 is amended by 

revising paragraph (d)(2) to read as 

follows: 

§ 201.25 Bar code label requirements. 

* * * * * 

(d) * * * 

(2) Requests for an exemption should 

be sent to the Office of Compliance, 

Center for Drug Evaluation and 

Research, Food and Drug 

Administration, 10903 New Hampshire 

Ave., Bldg. 51, Silver Spring, MD 

20993–0002 (requests involving a drug 

product) or to the Office of Compliance 

and Biologics Quality (HFM–600), 

Center for Biologics Evaluation and 

Research, Food and Drug 

Administration, 1401 Rockville Pike, 

Rockville, MD 20852 (requests involving 

a biological product). 

Dated: March 3, 2011. 

Leslie Kux, 

Acting Assistant Commissioner for Policy. 

[FR Doc. 2011–5288 Filed 3–8–11; 8:45 am] 

BILLING CODE 4160–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Highway Administration 

23 CFR Part 460 

RIN 2125–AF42 

Public Road Mileage for 

Apportionment of Highway Safety 

Funds; Correction 

AGENCY: Federal Highway 

Administration (FHWA), DOT. 

ACTION: Correcting amendment. 

SUMMARY: This rule makes a technical 

correction to the regulations found at 23 

CFR 460.2(e). The amendment 

contained herein makes no substantive 

change to the FHWA regulations, 

policies, or procedures. This rule 

updates the language of a regulatory 

definition to be consistent with the 

statutory definition for the Highway 

Safety Program. 

DATES: This rule is effective April 8, 

2011. 

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