Federal Register / Vol. 79, No. 106 / Tuesday, June 3, 2014 / Rules and Regulations 31849 

duplicates of paragraphs (a)(2) and 

(b)(2). SBA is correcting this duplication 

in § 127.503 by removing paragraphs 

(a)(3) and (b)(3). 

List of Subjects 

13 CFR Part 125 

Government contracts, Government 

procurement, Reporting and 

recordkeeping requirements, Small 

businesses, Technical assistance. 

13 CFR Part 127 

Government procurement, Reporting 

and recordkeeping requirements, Small 

businesses. 

Accordingly, 13 CFR Parts 125 and 

127 are corrected by making the 

following correcting amendments: 

PART 125—GOVERNMENT 

CONTRACTING PROGRAMS 

■ 1. The authority citation for part 125 

continues to read as follows: 

Authority: 15 U.S.C. 632(p), (q); 634(b)(6); 

637; 644, 657(f); and 657(q). 

■ 2. Amend § 125.6 by adding 

paragraphs (a)(1) through (a)(4) to read 

as follows: 

§ 125.6 What are the prime contractor 

performance requirements (limitations on 

subcontracting)? 

(a) * * * 

(1) In the case of a contract for 

services (except construction), the 

concern will perform at least 50 percent 

of the cost of the contract incurred for 

personnel with its own employees. 

(2) In the case of a contract for 

supplies or products (other than 

procurement from a non-manufacturer 

in such supplies or products), the 

concern will perform at least 50 percent 

of the cost of manufacturing the 

supplies or products (not including the 

costs of materials). 

(3) In the case of a contract for general 

construction, the concern will perform 

at least 15 percent of the cost of the 

contract with its own employees (not 

including the costs of materials). 

(4) In the case of a contract for 

construction by special trade 

contractors, the concern will perform at 

least 25 percent of the cost of the 

contract with its own employees (not 

including the cost of materials). 

* * * * * 

PART 127—WOMEN-OWNED SMALL 

BUSINESS FEDERAL CONTRACT 

ASSISTANCE PROGRAM 

■ 3. The authority for part 127 

continues to read as follows: 

Authority: 15 U.S.C. 632, 634(b)(6), 

637(m), and 644. 

§ 127.503 [Amended] 

■ 4. In § 127.503, remove paragraphs 

(a)(3) and (b)(3). 

Calvin Jenkins, 

Deputy Associate Administrator for 

Government Contracting and Business 

Development. 

[FR Doc. 2014–12609 Filed 6–2–14; 8:45 am] 

BILLING CODE 8025–01–M 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–1073; Directorate 

Identifier 2012–NM–039–AD; Amendment 

39–17856; AD 2014–11–06] 

RIN 2120–AA64 

Airworthiness Directives; Airplanes 

Originally Manufactured by Lockheed 

for the Military as Model P–3A and P3A 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

airplanes originally manufactured by 

Lockheed Martin Aeronautics Company 

for the military as Model P–3A or P3A 

airplanes. This AD was prompted by a 

determination that the existing 

maintenance or inspection program 

must be revised to address fatigue 

cracking of the airplane. This AD 

requires revising the maintenance or 

inspection program, as applicable, to 

incorporate certain limitations. We are 

issuing this AD to detect and correct 

fatigue cracking, which could result in 

reduced structural integrity of the 

airplane. 

DATES: This AD is effective July 8, 2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 8, 2014. 

ADDRESSES: For service information 

identified in this AD, contact Avenger 

Aircraft and Services, 103 N. Main 

Street, Suite 106, Greenville, SC 29601– 

4833; telephone: 864–232–8073; fax: 

864–232–8074; email: AAS@

AvengerAircraft.com. You may view 

this referenced 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. 

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–2013– 

1073; 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 

Docket 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: 

George Garrido, Aerospace Engineer, 

Airframe Branch, ANM–120L, FAA, Los 

Angeles Aircraft Certification Office, 

3960 Paramount Boulevard, Lakewood, 

CA 90712–4137; phone: 562–627–5357; 

fax: 562–627–5210; email: 

george.garrido@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 airplanes originally 

manufactured by Lockheed Martin 

Aeronautics Company for the military as 

Model P–3A or P3A airplanes. The 

NPRM published in the Federal 

Register on January 21, 2014 (79 FR 

3341). The NPRM was prompted by a 

determination that the existing 

maintenance program must be revised to 

address fatigue cracking of the airplane. 

The NPRM proposed to require revising 

the maintenance or inspection program, 

as applicable, to incorporate certain 

limitations. We are issuing this AD to 

detect and correct fatigue cracking, 

which could result in reduced structural 

integrity of the airplane. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

have considered the comment received. 

The single commenter, Lockheed Martin 

(Lockheed) did not request a change to 

the NPRM (79 FR 3341, January 21, 

2014). 

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 

changes. We have determined that these 

minor changes: 


wreier-aviles on DSK5TPTVN1PROD with RULES
31850 Federal Register / Vol. 79, No. 106 / Tuesday, June 3, 2014 / Rules and Regulations 

• Are consistent with the intent that 

was proposed in the NPRM (79 FR 3341, 

January 21, 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 3341, 

January 21, 2014). 

Costs of Compliance 

We estimate that this AD affects 8 

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 

Revise the maintenance or inspection program.1 work-hour × $85 per hour = $85 ................. $0 $85 $680 

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): 

2014–11–06 Lockheed (Original 

Manufacturer): Amendment 39–17856; 

Docket No. FAA–2013–1073; Directorate 

Identifier 2012–NM–039–AD. 

(a) Effective Date 

This AD is effective July 8, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Model P–3A or P3A 

airplanes originally manufactured by 

Lockheed Martin Aeronautics Company for 

the military, as identified in paragraphs (c)(1) 

and (c)(2) of this AD, certificated in any 

category: 

(1) Aero Union Corporation Model P3A 

airplanes; and 

(2) USDA Forest Service Model P–3A 

airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 55, Stabilizers; 57, Wings. 

(e) Unsafe Condition 

This AD was prompted by a determination 

that the existing maintenance or inspection 

program must be revised to address fatigue 

cracking of the airplane. We are issuing this 

AD to detect and correct fatigue cracking, 

which could result in reduced structural 

integrity of the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Maintenance or Inspection Program 

Revision 

Within 12 months after the effective date 

of this AD, revise the maintenance or 

inspection program, as applicable, by 

incorporating airworthiness limitations 

specified in Avenger Aircraft and Services 

P3A Airworthiness Limitations Section— 

FAA TCDS A32NM & TCDS T00006LA, 

Forest and Wildlife Conservation Usage 

(Includes Aerial Dispensing of Liquids), 

AAS–ALS–07–001, Revision D, dated August 

2, 2010. 

(h) Compliance Times for Modifications, 

Replacements, and Inspections 

For the tasks specified in Part-I, Sections 

B. through E., of Procedure 01–00–005, of 

Avenger Aircraft and Services P3A 

Airworthiness Limitations Section—FAA 

TCDS A32NM & TCDS T00006LA, Forest and 

Wildlife Conservation Usage (Includes Aerial 

Dispensing of Liquids), AAS–ALS–07–001, 

Revision D, dated August 2, 2010, the 

compliance times are specified in paragraphs 

(h)(1) through (h)(4) of this AD. For airplanes 

with combined baseline and aerial 

dispensing usage accumulated, the total 

remaining life and the total remaining hours 

or flights until inspection is due for the 

principle structural element (PSE) inspection 

requirements is determined by combining the 

fatigue damage accumulated during the 

baseline and the aerial dispensing of liquids 

usage. The usage must be combined in 

accordance with a method approved by the 

Manager, Los Angeles Aircraft Certification 

Office (ACO), FAA. 

(1) For the baseline life limits, the 

compliance time is: At the applicable ‘‘flight 

hours’’ or ‘‘flights,’’ whichever occurs first, 

specified in Part-I, Section B, ‘‘Life 

Limitations Baseline Usage,’’ of Procedure 

01–00–005, of Avenger Aircraft and Services 

P3A Airworthiness Limitations Section— 

FAA TCDS A32NM & TCDS T00006LA, 

Forest and Wildlife Conservation Usage 

(Includes Aerial Dispensing of Liquids), 

AAS–ALS–07–001, Revision D, dated August 

2, 2010; or within 12 months after the 

effective date of this AD; whichever occurs 

later. 

(2) For the baseline PSE inspection 

requirements, the compliance time is: At the 

applicable ‘‘threshold interval hours’’ or 

‘‘threshold interval flights’’ since new, 

whichever occurs first, as specified in Tables 

C.1, C.2, and C.3, of Part-I, Section C, 

‘‘Principle Structural Element Inspection 

Requirements—Baseline Usage,’’ of 


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Federal Register / Vol. 79, No. 106 / Tuesday, June 3, 2014 / Rules and Regulations 31851 

Procedure 01–00–005, of Avenger Aircraft 

and Services P3A Airworthiness Limitations 

Section—FAA TCDS A32NM & TCDS 

T00006LA, Forest and Wildlife Conservation 

Usage (Includes Aerial Dispensing of 

Liquids), AAS–ALS–07–001, Revision D, 

dated August 2, 2010; or within 12 months 

after the effective date of this AD; whichever 

occurs later. Where compliance times are 

specified as ‘‘threshold interval hours,’’ those 

compliance times are total flight hours. 

Where the compliance times are specified as 

‘‘threshold interval flights,’’ those 

compliance times are total flight cycles. 

(3) For the aerial dispensing of liquids life 

limits, the compliance time is: At the 

applicable ‘‘flight hours’’ or ‘‘flights,’’ 

whichever occurs first, specified in Part-I, 

Section D, ‘‘Life Limitations—Aerial 

Dispensing of Liquids Usage’’ of Procedure 

01–00–005, of Avenger Aircraft and Services 

P3A Airworthiness Limitations Section— 

FAA TCDS A32NM & TCDS T00006LA, 

Forest and Wildlife Conservation Usage 

(Includes Aerial Dispensing of Liquids), 

AAS–ALS–07–001, Revision D, dated August 

2, 2010; or within 12 months after the 

effective date of this AD; whichever occurs 

later. 

(4) For the aerial dispensing of liquids PSE 

inspection requirements, the compliance 

time is: At the applicable ‘‘threshold interval 

hours’’ or threshold interval flights,’’ 

whichever occurs first, as specified in Tables 

E.1, E.2, and E.3, of Part-I, Section E, 

‘‘Principle Structural Element Inspection 

Requirements—Aerial Dispensing of Liquids 

Usage,’’ of Procedure 01–00–005, of Avenger 

Aircraft and Services P3A Airworthiness 

Limitations Section—FAA TCDS A32NM & 

TCDS T00006LA, Forest and Wildlife 

Conservation Usage (Includes Aerial 

Dispensing of Liquids), AAS–ALS–07–001, 

Revision D, dated August 2, 2010; or within 

12 months after the effective date of this AD; 

whichever occurs later. 

(i) No Alternative Actions or Intervals 

After accomplishing the revision required 

by paragraph (g) of this AD, no alternative 

actions (e.g., inspections) or intervals may be 

used unless the actions or intervals are 

approved as an alternative method of 

compliance in accordance with the 

procedures specified in paragraph (j) of this 

AD. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Los Angeles 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 (k) of this AD. Information may be 

emailed to: 9-ANM-LAACO-AMOCRequests@faa.gov. 

(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. 

(k) Related Information 

For more information about this AD, 

contact George Garrido, Aerospace Engineer, 

Airframe Branch, ANM–120L, FAA, Los 

Angeles Aircraft Certification Office, 3960 

Paramount Boulevard, Lakewood, CA 90712– 

4137; phone: 562–627–5357; fax: 562–627– 

5210; email: george.garrido@faa.gov. 

(l) 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) Avenger Aircraft and Services P3A 

Airworthiness Limitations Section—FAA 

TCDS A32NM & TCDS T00006LA, Forest and 

Wildlife Conservation Usage (Includes Aerial 

Dispensing of Liquids), AAS–ALS–07–001, 

Revision D, dated August 2, 2010. (ii) 

Reserved. 

(3) For service information identified in 

this AD, contact Avenger Aircraft and 

Services, 103 N. Main Street, Suite 106, 

Greenville, SC 29601–4833; telephone: 864– 

232–8073; fax: 864–232–8074; email: AAS@

AvengerAircraft.com. 

(4) You may view this service information 

at 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 May 16, 

2014. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–12606 Filed 6–2–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0368; Directorate 

Identifier 2012–NM–058–AD; Amendment 

39–17851; AD 2014–11–01] 

RIN 2120–AA64 

Airworthiness Directives; The Boeing 

Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

The Boeing Company Model 777–200 

and –300 series airplanes. This AD was 

prompted by reports of smoke or flames 

in the passenger cabin of various 

transport category airplanes related to 

the wiring for the passenger cabin inflight entertainment (IFE) system, cabin 

lighting, and passenger seats. This AD 

requires installing wiring and making 

changes to certain electrical load 

management system (ELMS) panels and 

other concurrent requirements to ensure 

the flightcrew is able to turn off 

electrical power to the IFE systems and 

other non-essential electrical systems 

through one or two switches in the 

flight deck in the event of smoke or 

flames. In the event of smoke or flames 

in the airplane flight deck or passenger 

cabin, the flightcrew’s inability to turn 

off electrical power to the IFE system 

and other non-essential electrical 

systems could result in the inability to 

control smoke or flames in the airplane 

flight deck or passenger cabin during a 

non-normal or emergency situation, and 

consequent loss of control of the 

airplane. 

DATES: This AD is effective July 8, 2014. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of July 8, 2014. 

ADDRESSES: For service information 

identified in this AD, contact Boeing 

Commercial Airplanes, Attention: Data 

& Services Management, P. O. Box 3707, 

MC 2H–65, Seattle, WA 98124–2207; 

telephone 206–544–5000, extension 1; 

fax 206–766–5680; Internet https://

www.myboeingfleet.com. You may view 

this referenced 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. 

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–2013– 

0368; 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 

Docket 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. 


wreier-aviles on DSK5TPTVN1PROD with RULES