46946 Federal Register / Vol. 77, No. 152 / Tuesday, August 7, 2012 / Rules and Regulations 

2, Groups 1 and 3 airplanes require top kits 

015U1854–3 and 015U1854–4. 

(4) Where Paragraph 1., ‘‘Kits/Parts,’’ of 

Paragraph 2.C., ‘‘Parts Necessary for Each 

Airplane,’’ of Boeing Alert Service Bulletin 

747–25A3555, Revision 1, dated July 27, 

2011, states that Group 2 airplanes require 

top kits 015U1854–3 and 015U1854–4, Group 

2 airplanes require top kits 015U1854–1 and 

015U1854–2. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle 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 the 

Related Information section of this AD. 

Information may be emailed to: 9-ANMSeattle-ACO-AMOC-Requests@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. 

(j) Related Information 

For more information about this AD, 

contact Francis Smith, Aerospace Engineer, 

Cabin Safety and Environmental Systems 

Branch, ANM–150S, FAA, Seattle Aircraft 

Certification Office, 1601 Lind Avenue SW., 

Renton, WA 98057–3356; phone: 425–917– 

6596; fax: 425–917–6590; email: 

francis.smith@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) Boeing Alert Service Bulletin 747– 

25A3555, Revision 1, dated July 27, 2011. 

(ii) Reserved. 

(3) 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. 

(4) You may review copies of the 

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. 

(5) You may also review copies of the 

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/ibr-locations.html. 

Issued in Renton, Washington, on July 20, 

2012. 

Kalene C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–18583 Filed 8–6–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0269; Directorate 

Identifier 2011–NM–105–AD; Amendment 

39–17140; AD 2012–15–11] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Dassault Aviation Model FALCON 7X 

airplanes. This AD was prompted by a 

report that a passenger oxygen pipe at 

frame 10 was chafing against the 

forward lavatory rear structure, raising 

the risk of the oxygen pipe developing 

a crack. This AD requires modifying the 

routing of and, if necessary, replacing, 

the oxygen pipe. We are issuing this AD 

to prevent rupture of the oxygen pipe 

which, in case of a cabin 

depressurization, would impair 

operation of the passenger oxygen 

distribution system. 

DATES: This AD becomes effective 

September 11, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of September 11, 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, 

Washington 98057–3356; telephone 

(425) 227–1137; fax (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 March 20, 2012 (77 FR 

16186). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

Inspections of two aeroplanes during cabin 

completions have shown that a passenger 

oxygen line at frame 10 was chafing with the 

forward lavatory rear structure. 

Design review of the area confirmed a local 

low clearance value which raises the risk of 

the oxygen line developing a crack. 

This condition, if not detected and 

corrected, could lead to rupture of the oxygen 

line which, in case of a cabin 

depressurization, would impair operation of 

the passengers’ oxygen distribution system. 

To address this unsafe condition, Dassault 

Aviation have designed a modification with 

a new oxygen line routing. 

This AD requires an [general visual] 

inspection of the oxygen line for interference 

or damage and, in case of discrepancies 

[damage, or clearance less than 3 mm], 

accomplishment of the modification 

[including general visual inspections, and, if 

necessary, replacing the oxygen line/pipe] 

before next flight. It requires as well 

accomplishment of the modification of the 

oxygen line routing for the aeroplanes in 

which [clearance of 3 mm or more but less 

than 12 mm] were identified. 

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 16186, March 20, 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 

16186, March 20, 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 16186, 

March 20, 2012). 

Costs of Compliance 

We estimate that this AD will affect 

about 11 products of U.S. registry. We 

also estimate that it will take about 11 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Based on these figures, we estimate the 

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

be $10,285, or $935 per product. 


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Federal Register / Vol. 77, No. 152 / Tuesday, August 7, 2012 / Rules and Regulations 46947 

In addition, we estimate that any 

necessary follow-on actions would take 

about 16 work-hours and require parts 

costing $655, for a cost of $2,015 per 

product. We have no way of 

determining the number of products 

that may need these actions. 

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 16186, March 

20, 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: 

2012–15–11 Dassault Aviation: 

Amendment 39–17140. Docket No. 

FAA–2012–0269; Directorate Identifier 

2011–NM–105–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective September 11, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Dassault Aviation 

Model FALCON 7X airplanes, certificated in 

any category, serial numbers 3, 10, 13, 18, 19, 

20, 22, 23, 24, 26, 27, 29, 30, 31, 32, 33, 35, 

36, 38, 41, 42, 43, 47, 48, 58, 63, 64, 66, 67, 

68, 71, 76, 78, 79, 83, 84, 85, 86, 87, and 93; 

except for airplanes on which the Dassault 

Aviation modification specified in Dassault 

Mandatory Service Bulletin 7X–174 has been 

incorporated. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 35: Oxygen. 

(e) Reason 

This AD was prompted by a report that a 

passenger oxygen pipe at frame 10 was 

chafing against the forward lavatory rear 

structure, raising the risk of the oxygen pipe 

developing a crack. We are issuing this AD 

to prevent rupture of the oxygen pipe which, 

in case of a cabin depressurization, would 

impair operation of the passenger oxygen 

distribution system. 

(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) Inspection 

Within 2 months after the effective date of 

this AD, do a boroscope inspection of the 

passenger oxygen pipe for clearance and a 

general visual inspection for damage of the 

oxygen pipe, in accordance with the 

Accomplishment Instructions of Dassault 

Mandatory Service Bulletin 7X–174, dated 

March 10, 2011. 

(h) Corrective Actions 

If during any inspection required by 

paragraph (g) of this AD any damage is found 

or oxygen pipe clearance is less than 3 

millimeters (mm) (0.12 inch): Before further 

flight, modify the oxygen pipe routing, 

including doing a general visual inspection 

for chafing of the pipe and doing all 

applicable replacements, in accordance with 

the Accomplishment Instructions of Dassault 

Mandatory Service Bulletin 7X–174, dated 

March 10, 2011. 

(i) Oxygen Pipe Routing Modification 

If, during any inspection required by 

paragraph (g) of this AD, oxygen pipe 

clearance is 3 mm (0.12 inch) or more but 

less than 12 mm (0.47 inch): Within 98 

months or 4,000 flight cycles after the 

effective date of this AD, whichever occurs 

first, modify the routing of the passenger 

oxygen pipe, including doing a general visual 

inspection for chafing of the pipe and doing 

all applicable replacements, in accordance 

with the Accomplishment Instructions of 

Dassault Mandatory Service Bulletin 7X–174, 

dated March 10, 2011. 

(j) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(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, Washington 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. 


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46948 Federal Register / Vol. 77, No. 152 / Tuesday, August 7, 2012 / Rules and Regulations 

(k) Related Information 

Refer to MCAI European Aviation Safety 

Agency (EASA) Airworthiness Directive 

2011–0070, dated April 18, 2011; and 

Dassault Mandatory Service Bulletin 7X–174, 

dated March 10, 2011; for related 

information. 

(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) Dassault Mandatory Service Bulletin 

7X–174, dated March 10, 2011. 

(ii) Reserved. 

(3) For Dassault service information 

identified in this AD, contact Dassault Falcon 

Jet, P.O. Box 2000, South Hackensack, New 

Jersey 07606; telephone 201–440–6700; 

Internet http://www.dassaultfalcon.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 also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at an NARA facility, call 202–741– 

6030, or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on July 20, 

2012. 

Kalene C. Yanamura, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–18582 Filed 8–6–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 774 

The Commerce Control List 

CFR Correction 

In Title 15 of the Code of Federal 

Regulations, Parts 300 to 799, revised as 

of January 1, 2012, in supplement no. 1 

to part 774, make the following 

corrections: 

■ 1. In Category 7: 

■ A. On page 838, in 7A002, under the 

table in ‘‘Licensing Requirements’’, add 

a ‘‘License Requirements Note’’ as set 

forth below. 

■ B. On page 839, in 7A005, above 

‘‘License Requirements’’, remove the 

Note to 7A005. 

■ C. On page 840, in 7A008, add 

‘‘License Requirements’’ above ‘‘Reason 

for Control’’. 

■ D. On page 843, in 7B101, in the 

heading, add a quotation mark before 

‘‘Production’’. 

■ E. On page 847, in 7E003, at the end 

of ‘‘Related Definition’’, add ‘‘for 

‘Maintenance Level I’ or ‘Maintenance 

Level II’’’. 

■ 2. In Category 9, on page 870, in 

9E003, below paragraph a.10, remove 

Note 1 and Note 2. 

The text to be added is set forth 

below: 

Supplement No. 1 to Part 774—The 

Commerce Control List 

* * * * * 

Category 7 

* * * * * 

7A002 Gyros or angular rate sensors, 

having any of the following see List of Items 

Controlled) and specially designed 

components therefor. 

* * * * * 

License Requirement Note: For the purpose 

of MT controls only, the term ‘stability’ is 

defined as a measure of the ability of a 

specific mechanism or performance 

coefficient to remain invariant when 

continuously exposed to a fixed operating 

condition. (This definition does not refer to 

dynamic or servo stability.) (IEEE STD 528– 

2001 paragraph 2.247) 

* * * * * 

[FR Doc. 2012–19389 Filed 8–6–12; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF LABOR 

Occupational Safety and Health 

Administration 

29 CFR Parts 1910 and 1926 

[Docket No. OSHA–2006–0049] 

Respiratory Protection; Mechanical 

Power Presses; Scaffold 

Specifications; Correction and 

Technical Amendment 

AGENCY: Occupational Safety and Health 

Administration (OSHA), Labor. 

ACTION: Final rule; correction and 

technical amendment. 

SUMMARY: OSHA is correcting the 

medical evaluation questionnaire in 

Appendix C of its Respiratory Protection 

standard by removing the term ‘‘fits’’ in 

a question. OSHA also is correcting its 

Mechanical Power Presses standard for 

general industry by restoring 

requirements that were removed 

inadvertently from the regulatory text. 

Finally, the Agency is correcting a cross 

reference made in two paragraphs in 

Appendix A to subpart L of its scaffold 

standards for construction. 

DATES: The effective date for the 

corrections and technical amendment to 

the standards is August 7, 2012. 

FOR FURTHER INFORMATION CONTACT: 

Press inquiries: Frank Meilinger, 

Director, Office of Communications, 

OSHA, U.S. Department of Labor, Room 

N–3647, 200 Constitution Avenue NW., 

Washington, DC 20210; telephone: (202) 

693–1999; email: 

meilinger.francis2@dol.gov. 

General and technical information: 

Kenneth Stevanus, OSHA Office of 

Engineering Safety, OSHA, Room N– 

3621, U.S. Department of Labor, 200 

Constitution Avenue NW., Washington, 

DC 20210; telephone: (202) 693 2260; 

email: stevanus.ken@dol.gov. 

SUPPLEMENTARY INFORMATION: 

I. Background 

A. Appendix C (Mandatory) to 

§ 1910.134 (Respiratory Protection) 

In the Standards Improvement 

Project-Phase III (SIP–III) final rule, 

published on June 8, 2011 (76 FR 

33590), OSHA revised question 2.a in 

the OSHA Respirator Medical 

Evaluation Questionnaire, Appendix C, 

Part A, Section 2, of its Respiratory 

Protection standard (§ 1910.134) by 

deleting the word ‘‘fits,’’ leaving only 

the word ‘‘seizures’’ to describe the 

applicable medical condition. OSHA 

received no public comment on this 

revision in the proposed SIP–III rule (75 

FR 38646, 38650). Therefore, in the final 

SIP–III rule, OSHA determined that (1) 

use of the term ‘‘fits’’ is outdated, 

unnecessary, and offensive, and (2) this 

revision would have no effect on 

administration of, or responses to, the 

questionnaire (76 FR 33590, 33595). 

Subsequent to publication of the SIP–III 

final rule, OSHA found an additional 

use of the term ‘‘fits’’ in Appendix C of 

§ 1910.134: namely, question 7.d. This 

Federal Register notice will remove the 

term ‘‘fits’’ from question 7.d. 

In addition, when OSHA promulgated 

the revised Respiratory Protection 

standard on January 8, 1998 (63 FR 

1152), the introductory language of 

Appendix C included the following 

prefatory question to the employee: 

‘‘Can you read (circle one): Yes/No.’’ 

Because this question is illogical (i.e., 

employees who cannot read cannot 

respond validly to the question), this 

Federal Register notice will remove this 

question from Appendix C of 

§ 1910.134. 

B. Mechanical Power Presses (§ 1910.21) 

On December 27, 2011, OSHA 

published a Federal Register notice 


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