Federal Register / Vol. 77, No. 185 / Monday, September 24, 2012 / Rules and Regulations 58765 

TABLE 1 TO PARAGRAPH (e)—INITIAL INSPECTION THRESHOLDS—Continued 

Appendix number of RR ASB Number RB.211–72–AG244, Revision 4, 

that identifies affected LP compressor blades by S/N Initial inspection threshold 

3G .......................................................................................................................... Within 58 months after the effective date of this AD. 

3H ........................................................................................................................... Within 70 months after the effective date of this AD. 

3I ............................................................................................................................ Within 82 months after the effective date of this AD. 

3J ........................................................................................................................... Within 94 months after the effective date of this AD. 

3K ........................................................................................................................... Within 106 months after the effective date of this AD. 

3L ........................................................................................................................... Within 118 months after the effective date of this AD. 

(2) Thereafter, perform repetitive UIs of the 

affected LP compressor blades within every 

100 flight cycles. 

(3) Use paragraph 3.A.(2) of 

Accomplishment Instructions of RR ASB No. 

RB.211–72–AG244, Revision 4, dated 

December 22, 2011, and paragraphs 1. 

through 3.B. of Appendix 1 of that ASB, or 

paragraphs 3.B.(3) of Accomplishment 

Instructions of RR ASB No. RB.211–72– 

AG244, Revision 4, dated December 22, 2011, 

and paragraphs 1. through 3.C. of Appendix 

2 of that ASB, to perform the UIs. Prior to 

inspecting the blades per paragraph 3.B.(3) of 

the Accomplishment Instructions remove the 

air intake fairing/spinner and spinner 

extension and annulus fillers. 

(4) Do not return to service any engine with 

blades that failed the inspection required by 

this AD. 

(5) For blades that are removed from the 

engine and pass inspection, re-apply dry film 

lubricant before re-installing the blades. 

(f) Installation Prohibition 

After the effective date of this AD, do not 

install any affected LP compressor blade that 

has reached the initial inspection threshold 

in Table 1 to paragraph (e) of this AD, unless 

it has passed the UI required by this AD. 

(g) Credit for Previous Actions 

You may take credit for the initial 

inspection that is required by paragraph 

(e)(1) of this AD if you performed the initial 

inspection before the effective date of this AD 

using RR ASB No. RB.211–72–AG244, dated 

August 7, 2009; RR ASB No. RB.211–72– 

AG244, Revision 1, dated January 26, 2010; 

RR ASB No. RB.211–72–AG244, Revision 2, 

dated August 18, 2011; RR ASB No. RB.211– 

72–AG244, Revision 3, dated December 13, 

2011; or RR RB.211–72–E175, Revision 7, 

dated April 11, 2011. 

(h) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs for this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(i) Related Information 

(1) For more information about this AD, 

contact Alan Strom, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7143; fax: 781–238–7199; 

email: alan.strom@faa.gov. 

(2) Refer to European Aviation Safety 

Agency AD 2012–0025, dated February 8, 

2012, for related information. 

(j) 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) Rolls-Royce plc Alert Service Bulletin 

No. RB.211–72–AG244, Revision 4, including 

appendices 1, 2, and 3A through 3L, dated 

December 22, 2011. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Rolls-Royce plc, Corporate 

Communications, P.O. Box 31, Derby, 

England, DE248BJ, phone: 011–44–1332– 

242424; fax: 011–44–1332–245418; email: 

http://www.rolls-royce.com/contact/ 

civil_team.jsp. 

(4) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(5) You may view this service information 

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/ 

ibr_locations.html. 

Issued in Burlington, Massachusetts, on 

August 29, 2012. 

Colleen M. D’Alessandro, 

Assistant Manager, Engine & Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–23442 Filed 9–21–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0593; Directorate 

Identifier 2011–NM–238–AD; Amendment 

39–17200; AD 2012–19–05] 

RIN 2120–AA64 

Airworthiness Directives; Fokker 

Services B.V. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Fokker Services B.V. Model F.28 Mark 

0070 and 0100 airplanes. This AD was 

prompted by reports of burned contacts 

in a certain production break plug and 

its corresponding receptacle. This AD 

requires modifying galley power supply 

wiring by disconnecting it from the 

affected plug/receptacle and 

reconnecting the power supply wiring 

through splices. We are issuing this AD 

to prevent a high electrical load, which 

might lead to overheating of the galley 

power supply wiring and/or the 

electrical connector and consequent 

smoke or fire in the galley area, which 

could result in damage to the airplane 

and injury to occupants. 

DATES: This AD becomes effective 

October 29, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of October 29, 2012. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone (425) 227–1137; 

fax (425) 425–227–1149. 

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 June 12, 2012 (77 FR 34872). 

That NPRM proposed to correct an 

unsafe condition for the specified 

products. The MCAI states: 

Reports have been received about burned 

contacts in production break plug P 4259B 

and corresponding receptacle J 4259A. After 

investigation, it was concluded that the high 


emcdonald on DSK67QTVN1PROD with RULES
58766 Federal Register / Vol. 77, No. 185 / Monday, September 24, 2012 / Rules and Regulations 

electrical load on the contacts M, L and X, 

in combination with the electrical loads on 

the adjacent connections, may have resulted 

in these occurrences. 

This condition, if not detected and 

corrected, can lead to overheating of the 

galley power supply wiring and/or the 

electrical connector and consequent smoke or 

fire in the galley area, possibly resulting in 

damage to the aeroplane and injury to 

occupants. 

For the reasons described above, this 

[European Aviation Safety Agency] AD 

requires modification of the galley power 

supply wiring by disconnecting it from the 

affected plug/receptacle and reconnecting the 

power supply wiring through splices. 

You may obtain further information by 

examining the MCAI in the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (77 

FR 34872, June 12, 2012) 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—except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (77 FR 

34872, June 12, 2012) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (77 FR 34872, 

June 12, 2012). 

Costs of Compliance 

We estimate that this AD will affect 4 

products of U.S. registry. We also 

estimate that it will take about 4 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 $210 per 

product. Where the service information 

lists required parts costs that are 

covered under warranty, we have 

assumed that there will be no charge for 

these parts. As we do not control 

warranty coverage for affected parties, 

some parties may incur costs higher 

than estimated here. Based on these 

figures, we estimate the cost of this AD 

to the U.S. operators to be $2,200, or 

$550 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 that this AD: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

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. 

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 Operations office between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains the NPRM (77 FR 34872, June 

12, 2012), the regulatory evaluation, any 

comments received, and other 

information. The street address for the 

Docket Operations 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: 

2012–19–05 Fokker Services B.V.: 

Amendment 39–17200. Docket No. 

FAA–2012–0593; Directorate Identifier 

2011–NM–238–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective October 29, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Fokker Services B.V. 

Model F.28 Mark 0070 and 0100 airplanes, 

certificated in any category; serial numbers 

(S/N) 11340 through 11343 inclusive, 11347, 

11348, 11350 through 11356 inclusive, 

11359, 11360, 11361, 11367 through 11371 

inclusive, 11374 through 11378 inclusive, 

11382 through 11385 inclusive, 11387 

through 11390 inclusive, 11394 through 

11397 inclusive, 11400 through 11423 

inclusive, 11425 through 11432 inclusive, 

11434 through 11439 inclusive, 11441 

through 11453 inclusive, and 11456 through 

11585 inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 24, Electrical Power. 

(e) Reason 

This AD was prompted by reports of 

burned contacts in a certain production break 

plug and its corresponding receptacle. We are 

issuing this AD to prevent a high electrical 

load, which might lead to overheating of the 

galley power supply wiring and/or the 

electrical connector and consequent smoke or 

fire in the galley area, which could result in 

damage to the airplane and injury to 

occupants. 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Modification 

Within 24 months after the effective date 

of this AD: Modify the galley power supply 

wiring, in accordance with the 

Accomplishment Instructions of Fokker 

Service Bulletin SBF100–24–044, dated July 

14, 2011, including Fokker Manual Change 

Notification—Maintenance Documentation 

MCNM–F100–148, dated July 14, 2011. 

(h) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 


emcdonald on DSK67QTVN1PROD with RULES
Federal Register / Vol. 77, No. 185 / Monday, September 24, 2012 / Rules and Regulations 58767 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, 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 International Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA 1601 Lind Avenue 

SW., Renton, WA 98057–3356; telephone 

(425) 227–1137; fax (425) 227–1149. 

Information may be emailed to: 9-ANM-116- 

AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter 

must specifically reference this AD. 

(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 FAA-approved 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. 

(i) Related Information 

Refer to MCAI European Aviation Safety 

Agency Airworthiness Directive 2011–0183, 

dated September 23, 2011; and Fokker 

Service Bulletin SBF100–24–044, dated July 

14, 2011, including Fokker Manual Change 

Notification—Maintenance Documentation 

MCNM–F100–148, dated July 14, 2011; for 

related information. 

(j) 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) Fokker Service Bulletin SBF100–24– 

044, dated July 14, 2011, including Fokker 

Manual Change Notification—Maintenance 

Documentation MCNM–F100–148, dated July 

14, 2011. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Fokker Services B.V., 

Technical Services Dept., P.O. Box 231, 2150 

AE Nieuw-Vennep, the Netherlands; 

telephone +31 (0)252–627–350; fax +31 

(0)252–627–211; email 

technicalservices.fokkerservices@stork.com; 

Internet http://www.myfokkerfleet.com. 

(4) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., Renton, 

WA. For information on the availability of 

this material at the FAA, call 425–227–1221. 

(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 Renton, Washington, on 

September 11, 2012. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–23055 Filed 9–21–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF JUSTICE 

Drug Enforcement Administration 

21 CFR Part 1300 

Definitions Relating to Electronic 

Orders and Prescriptions for 

Controlled Substances 

CFR Correction 

In Title 21 of the Code of Federal 

Regulations, Part 1300 to End, revised as 

of April 1, 2012, on page 14, § 1300.03 

is reinstated to read as follows: 

§ 1300.03 Definitions relating to electronic 

orders for controlled substances and 

electronic prescriptions for controlled 

substances. 

For the purposes of this chapter, the 

following terms shall have the meanings 

specified: 

Application service provider means 

an entity that sells electronic 

prescription or pharmacy applications 

as a hosted service, where the entity 

controls access to the application and 

maintains the software and records on 

its servers. 

Audit trail means a record showing 

who has accessed an information 

technology application and what 

operations the user performed during a 

given period. 

Authentication means verifying the 

identity of the user as a prerequisite to 

allowing access to the information 

application. 

Authentication protocol means a well 

specified message exchange process that 

verifies possession of a token to 

remotely authenticate a person to an 

application. 

Biometric authentication means 

authentication based on measurement of 

the individual’s physical features or 

repeatable actions where those features 

or actions are both distinctive to the 

individual and measurable. 

Biometric subsystem means the 

hardware and software used to capture, 

store, and compare biometric data. The 

biometric subsystem may be part of a 

larger application. The biometric 

subsystem is an automated system 

capable of: 

(1) Capturing a biometric sample from 

an end user. 

(2) Extracting and processing the 

biometric data from that sample. 

(3) Storing the extracted information 

in a database. 

(4) Comparing the biometric data with 

data contained in one or more reference 

databases. 

(5) Determining how well the stored 

data matches the newly captured data 

and indicating whether an identification 

or verification of identity has been 

achieved. 

Cache means to download and store 

information on a local server or hard 

drive. 

Certificate policy means a named set 

of rules that sets forth the applicability 

of the specific digital certificate to a 

particular community or class of 

application with common security 

requirements. 

Certificate revocation list (CRL) means 

a list of revoked, but unexpired 

certificates issued by a certification 

authority. 

Certification authority (CA) means an 

organization that is responsible for 

verifying the identity of applicants, 

authorizing and issuing a digital 

certificate, maintaining a directory of 

public keys, and maintaining a 

Certificate Revocation List. 

Certified information systems auditor 

(CISA) means an individual who has 

been certified by the Information 

Systems Audit and Control Association 

as qualified to audit information 

systems and who performs compliance 

audits as a regular ongoing business 

activity. 

Credential means an object or data 

structure that authoritatively binds an 

identity (and optionally, additional 

attributes) to a token possessed and 

controlled by a person. 

Credential service provider (CSP) 

means a trusted entity that issues or 

registers tokens and issues electronic 

credentials to individuals. The CSP may 

be an independent third party or may 

issue credentials for its own use. 

CSOS means controlled substance 

ordering system. 

Digital certificate means a data record 

that, at a minimum— 

(1) Identifies the certification 

authority issuing it; 

(2) Names or otherwise identifies the 

certificate holder; 

(3) Contains a public key that 

corresponds to a private key under the 

sole control of the certificate holder; 

(4) Identifies the operational period; 

and 

(5) Contains a serial number and is 

digitally signed by the certification 

authority issuing it. 


emcdonald on DSK67QTVN1PROD with RULES