Federal Register / Vol. 77, No. 157 / Tuesday, August 14, 2012 / Rules and Regulations 48429 

(e) Reason 

This AD was prompted by a report of a 

capacitive density condensator (cadensicon) 

coil overheating during testing. We are 

issuing this AD to detect and correct 

potential overheating of the cadensicon coil, 

which could create an ignition source inside 

a fuel tank, which, in combination with 

flammable fuel vapors, could result in a fuel 

tank explosion and consequent loss of the 

airplane. 

(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) Actions 

Within 30 months after the effective date 

of this AD, inspect to determine whether any 

fuel quantity indication computer (FQIC) 

Type 1, having part number (P/N) SIC5054 or 

P/N SIC5051 (as applicable to the airplane 

model), is installed, in accordance with the 

Accomplishment Instructions of Airbus 

Mandatory Service Bulletin A300–28–6024, 

Revision 02, dated January 19, 2011; or 

Airbus Mandatory Service Bulletin A310–28– 

2039, Revision 01, dated January 19, 2011; as 

applicable. A review of airplane maintenance 

records is acceptable in lieu of this 

inspection if the part number of the FQIC can 

be conclusively determined from that review. 

If any FQIC Type 1 having P/N SIC5054 or 

P/N SIC5051 is installed, within 30 months 

after the effective date of this AD, replace the 

FQIC Type 1 with a FQIC Type 2 having P/ 

N SIC5055, P/N SIC5076, P/N SIC5082, or P/ 

N SIC5083 (as applicable to Model A310 

series airplanes) or with a FQIC Type 2 

having P/N SIC5077 (as applicable to Model 

A300 B4–600 series airplanes), and modify 

the associated wiring, in accordance with the 

Accomplishment Instructions of Airbus 

Mandatory Service Bulletin A300–28–6024, 

Revision 02, dated January 19, 2011; or 

Airbus Mandatory Service Bulletin A310–28– 

2039, Revision 01, dated January 19, 2011; as 

applicable. 

(h) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install any FQIC Type 1 having 

P/N SIC5054 or P/N SIC5051, on any 

airplane. 

(i) 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: 

Dan Rodina, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, Washington 98057– 

3356; telephone (425) 227–2125; 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. 

(j) Related Information 

Refer to MCAI European Aviation Safety 

Agency Airworthiness Directive 2011–0186, 

dated September 23, 2011, and the service 

information specified in paragraphs (j)(1) and 

(j)(2) of this AD, for related information. 

(1) Airbus Mandatory Service Bulletin 

A300–28–6024, Revision 02, dated January 

19, 2011. 

(2) Airbus Mandatory Service Bulletin 

A310–28–2039, Revision 01, dated January 

19, 2011. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the following service information 

under 5 U.S.C. 552(a) and 1 CFR part 51. 

(2) You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. 

(i) Airbus Mandatory Service Bulletin 

A300–28–6024, Revision 02, dated January 

19, 2011. 

(ii) Airbus Mandatory Service Bulletin 

A310–28–2039, Revision 01, dated January 

19, 2011. 

(3) For Airbus service information 

identified in this AD, contact Airbus SAS— 

EAW (Airworthiness Office), 1 Rond Point 

Maurice Bellonte, 31707 Blagnac Cedex, 

France; telephone +33 5 61 93 36 96; fax +33 

5 61 93 44 51; email account.airwortheas@airbus.com; Internet http:// 

www.airbus.com. 

(4) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., Renton, 

Washington. 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 31, 

2012. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–19254 Filed 8–13–12; 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 the Federal Register published on 

July 26, 2012, on page 43711, in the 

third column, in instruction 3.C., 

‘‘5A003’’ is corrected to read ‘‘5A002’’. 

[FR Doc. 2012–19955 Filed 8–13–12; 8:45 am] 

BILLING CODE 1505–01–D 

FEDERAL MINE SAFETY AND HEALTH 

REVIEW COMMISSION 

29 CFR Parts 2700, 2701, 2702, 2704, 

2705, 2706 

Commission Address Change 

AGENCY: Federal Mine Safety and Health 

Review Commission (FMSHRC). 

ACTION: Final rule. 

SUMMARY: The Federal Mine Safety and 

Health Review Commission is relocating 

its Headquarters office and is amending 

its regulations to inform the public of 

the address change. 

DATES: This final rule will take effect on 

August 27, 2012. 

ADDRESSES: This final rule is available 

on FMSHRC’s Web site, http:// 

www.fmshrc.gov. 

FOR FURTHER INFORMATION CONTACT: 

Sarah Stewart, Deputy General Counsel, 

Office of the General Counsel, Federal 

Mine Safety and Health Review 

Commission, at (202) 434–9935 or 

sstewart@fmshrc.gov. 

SUPPLEMENTARY INFORMATION: 

A. Background 

On August 24, 2012, FMSHRC will 

move its Headquarters office from 601 

New Jersey Avenue NW., Suite 9500, 

Washington, DC 20001 to 1331 

Pennsylvania Avenue NW., Suite 520N, 

Washington, DC 20004–1710. 

B. Notice and Public Procedure 

Because this amendment deals with 

agency management and procedures, the 

notice and comment provisions of the 

Administrative Procedure Act do not 

apply pursuant to 5 U.S.C. 553(a)(2) and 

(b)(3)(A). 

Good cause exists to dispense with 

the usual 30-day delay in the effective 

date because the amendments are of a 

minor and administrative nature dealing 

with only a change in address. 

The Commission is an independent 

regulatory agency and, as such, is not 


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