Federal Register / Vol. 77, No. 242 / Monday, December 17, 2012 / Rules and Regulations 74579 

Holding Company Act of 1970, Tier One 

civil money penalties may be assessed 

pursuant to 12 U.S.C. 1972(2)(F)(i) in an 

amount not to exceed $7,500 for each 

day during which the violation 

continues. Tier Two civil money 

penalties may be assessed pursuant to 

12 U.S.C. 1972(2)(F)(ii) in an amount 

not to exceed $37,500 for each day 

during which the violation, practice or 

breach continues. Tier Three civil 

money penalties may be assessed 

pursuant to 12 U.S.C. 1972(2)(F)(iii) in 

an amount not to exceed, in the case of 

any person other than an insured 

depository institution $1,375,000 for 

each day during which the violation, 

practice, or breach continues or, in the 

case of any insured depository 

institution, an amount not to exceed the 

lesser of $1,425,000 or 1 percent of the 

total assets of such institution for each 

day during which the violation, 

practice, or breach continues. 

(x) Civil money penalties assessed, 

pursuant to the International Banking 

Act of 1978. Pursuant to the 

International Banking Act of 1978 (IBA) 

(12 U.S.C. 3108(b)), civil money 

penalties may be assessed for failure to 

comply with the requirements of the 

IBA pursuant to section 8(i)(2) of the 

FDIA (12 U.S.C. 1818(i)(2)), in the 

amounts set forth in paragraph (c)(3)(i) 

of this section. 

(xi) Civil money penalties assessed for 

appraisal violations. Pursuant to 12 

U.S.C. 3349(b), where a financial 

institution seeks, obtains, or gives any 

other thing of value in exchange for the 

performance of an appraisal by a person 

that the institution knows is not a state 

certified or licensed appraiser in 

connection with a federally related 

transaction, a civil money penalty may 

be assessed pursuant to section 8(i)(2) of 

the FDIA (12 U.S.C. 1818(i)(2)) in the 

amounts set forth in paragraph (c)(3)(i) 

of this section. 

(xii) Civil money penalties assessed 

pursuant to International Lending 

Supervision Act. Pursuant to the 

International Lending Supervision Act 

(ILSA) (12 U.S.C. 3909(d)), the CMP that 

may be assessed against any institution 

or any officer, director, employee, agent 

or other person participating in the 

conduct of the affairs of such institution 

is an amount not to exceed $1,100 for 

each day a violation of the ILSA or any 

rule, regulation or order issued pursuant 

to ILSA continues. 

(xiii) Civil money penalties assessed 

for violations of the Community 

Development Banking and Financial 

Institution Act. Pursuant to the 

Community Development Banking and 

Financial Institution Act (Community 

Development Banking Act) (12 U.S.C. 

4717(b)) a civil money penalty may be 

assessed for violations of the 

Community Development Banking Act 

pursuant to section 8(i)(2) of the FDIA 

(12 U.S.C. 1818(i)(2)), in the amount set 

forth in paragraph (c)(3)(i) of this 

section. 

(xiv) Civil money penalties assessed 

for violations of the Securities Exchange 

Act of 1934. Pursuant to section 21B of 

the Securities Exchange Act of 1934 

(Exchange Act) (15 U.S.C. 78u–2), civil 

money penalties may be assessed for 

violations of certain provisions of the 

Exchange Act, where such penalties are 

in the public interest. Tier One civil 

money penalties may be assessed 

pursuant to 15 U.S.C. 78u–2(b)(1) in an 

amount not to exceed $7,500 for a 

natural person or $70,000 for any other 

person for violations set forth in 15 

U.S.C. 78u–2(a). Tier Two civil money 

penalties may be assessed pursuant to 

15 U.S.C. 78u–2(b)(2) in an amount not 

to exceed—for each violation set forth in 

15 U.S.C. 78u–2(a)—$70,000 for a 

natural person or $350,000 for any other 

person if the act or omission involved 

fraud, deceit, manipulation, or 

deliberate or reckless disregard of a 

regulatory requirement. Tier Three civil 

money penalties may be assessed 

pursuant to 15 U.S.C. 78u–2(b)(3) for 

each violation set forth in 15 U.S.C. 

78u–2(a), in an amount not to exceed 

$140,000 for a natural person or 

$700,000 for any other person, if the act 

or omission involved fraud, deceit, 

manipulation, or deliberate or reckless 

disregard of a regulatory requirement; 

and such act or omission directly or 

indirectly resulted in substantial losses, 

or created a significant risk of 

substantial losses to other persons or 

resulted in substantial pecuniary gain to 

the person who committed the act or 

omission. 

(xv) Civil money penalties assessed 

for false claims and statements pursuant 

to the Program Fraud Civil Remedies 

Act. Pursuant to the Program Fraud 

Civil Remedies Act (31 U.S.C. 3802), 

civil money penalties of not more than 

$7,500 per claim or statement may be 

assessed for violations involving false 

claims and statements. 

(xvi) Civil money penalties assessed 

for violations of the Flood Disaster 

Protection Act. Pursuant to the Flood 

Disaster Protection Act (FDPA) (42 

U.S.C. 4012a(f)), as of July 1, 2012, civil 

money penalties may be assessed 

against any regulated lending institution 

that engages in a pattern or practice of 

violations of the FDPA in an amount not 

to exceed $2,000 per violation. 

(xvii) Civil money penalties assessed 

for violation of one-year restriction on 

Federal examiners of financial 

institutions. Pursuant to section 10(k) of 

the Federal Deposit Insurance Act (12 

U.S.C. 1820(k)), the Board of Directors 

or its designee may assess a civil money 

penalty of up to $275,000 against any 

covered former Federal examiner of a 

financial institution who, in violation of 

section 1820(k) and within the one-year 

period following termination of 

government service as an employee, 

serves as an officer, director, or 

consultant of a financial or depository 

institution, a holding company, or of 

any other entity listed in section 10(k), 

without the written waiver or 

permission by the appropriate Federal 

banking agency or authority under 

section 1820(k)(5). 

PART 390—REGULATIONS 

TRANSFERRED FROM THE OFFICE OF 

THRIFT SUPERVISION 

■ 4. The general authority citation for 

part 390 continues to read as follows: 

Authority: 12 U.S.C. 1819. 

§ 390.74 [Amended] 

■ 5. In § 390.74, remove paragraph (c). 

By order of the Board of Directors. 

Washington, DC, this 11th day of December 

2012. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2012–30251 Filed 12–14–12; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1225; Directorate 

Identifier 2012–NM–219–AD; Amendment 

39–17288; AD 2012–25–07] 

RIN 2120–AA64 

Airworthiness Directives; Gulfstream 

Aerospace Corporation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Gulfstream Aerospace Corporation 

Model GIV–X airplanes. This AD 

requires performing a modified system 

power-on self test (SPOST) of the flap/ 

stabilizer electronic control unit 

(FSECU), and revising the airplane flight 

manual to incorporate these test 

procedures into the daily preflight 

check. This AD was prompted by 


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74580 Federal Register / Vol. 77, No. 242 / Monday, December 17, 2012 / Rules and Regulations 

reports indicating that the FSECU does 

not detect failures of the brake feature 

within the horizontal stabilizer electric 

motor unit (HSEMU), or failures of drive 

solenoids for hydraulic valves within 

the flap hydraulic control module 

(FHCM) during the SPOST. We are 

issuing this AD to detect and correct 

such failures, which could result in 

runaway horizontal stabilizer pitch trim 

system and consequent loss of pitch 

control. 

DATES: This AD is effective December 

17, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of December 17, 2012. 

We must receive comments on this 

AD by January 31, 2013. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: 202–493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

For service information identified in 

this AD, contact Gulfstream Aerospace 

Corporation, Technical Publications 

Dept., P.O. Box 2206, Savannah, GA 

31402–2206; telephone 800–810–4853; 

fax 912–965–3520; email 

pubs@gulfstream.com; Internet http:// 

www.gulfstream.com/product_support/ 

technical_pubs/pubs/index.htm. You 

may review copies of the referenced 

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. 

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 this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (phone: 800–647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Sanford Proveaux, Aerospace Engineer, 

Continued Operational Safety and 

Certificate Management Branch, ACE– 

102A, FAA, Atlanta Aircraft 

Certification Office (ACO), 1701 

Columbia Avenue, College Park, Georgia 

30337; phone: 404–474–5566; fax: 404– 

474–5606; email: 

sanford.proveaux@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We have received reports that the 

flap/stabilizer electronic control unit 

(FSECU) is not detecting failures of the 

brake feature in the horizontal stabilizer 

electric motor unit (HSEMU), or failures 

of drive solenoids for hydraulic valves 

in the flap hydraulic control module 

(FHCM) during the system power-on 

self test (SPOST). The potential for 

undetected horizontal stabilizer actuator 

(HSA) brake failures results from the 

FSECU executing its SPOST before 

115VAC and hydraulic power are 

available during the airplane power-on 

sequence. The root cause of this issue is 

the failure of the system power-up test 

logic to first consider whether hydraulic 

and electrical power have been supplied 

to the system articles under test; the test 

logic therefore does not provide 

accurate information about the 

condition of the articles. Failure to test 

the brake-holding torque functionality 

and capability exposes the airplane to a 

potential latent failure of a protective 

feature critical to the safe operation of 

the horizontal stabilizer system. These 

conditions, if not corrected, could result 

in a potential runaway horizontal 

stabilizer pitch trim system and 

consequent loss of pitch control. 

Further, failure of the FHCM drive 

solenoid valves to halt uncommanded 

flap motion could result in 

uncommanded flap motion or flap 

runaway. 

Relevant Service Information 

We reviewed the following service 

information: 

• Gulfstream G350 Alert Customer 

Bulletin 11, including Service Reply 

Card, dated December 4, 2012, which 

includes Revision 31, dated December 4, 

2012, of the Gulfstream G350 Airplane 

Flight Manual Document GAC–AC– 

G350–OPS–0001. 

• Gulfstream G450 Alert Customer 

Bulletin 11, including Service Reply 

Card, dated December 4, 2012, which 

includes Revision 33, dated December 4, 

2012, of the Gulfstream G450 Airplane 

Flight Manual Document GAC–AC– 

G450–OPS–0001. 

• Section 1–27–40, ‘‘Flap/Stabilizer 

System Preflight Check,’’ of the 

Gulfstream G350 Airplane Flight 

Manual Document GAC–AC–G350– 

OPS–0001, Revision 31, dated December 

4, 2012. 

• Section 1–27–40, ‘‘Flap/Stabilizer 

System Preflight Check,’’ of the 

Gulfstream G450 Airplane Flight 

Manual Document GAC–AC–G450– 

OPS–0001, Revision 33, dated December 

4, 2012. 

• Section 2–03–20, ‘‘Before Starting 

Engines,’’ of the Gulfstream G350 

Airplane Flight Manual Document 

GAC–AC–G350–OPS–0001, Revision 31, 

dated December 4, 2012. 

• Section 2–03–20, ‘‘Before Starting 

Engines,’’ of the Gulfstream G450 

Airplane Flight Manual Document 

GAC–AC–G450–OPS–0001, Revision 33, 

dated December 4, 2012. 

For information on the procedures 

and compliance times, see this service 

information at http:// 

www.regulations.gov by searching for 

Docket No. FAA–2012–1225. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of the same 

type design. 

AD Requirements 

This AD requires accomplishing the 

actions specified in the service 

information identified previously, 

except as discussed under ‘‘Differences 

Between the AD and the Service 

Information.’’ 

Differences Between the AD and the 

Service Information 

This AD requires compliance within 3 

days. However, these actions are 

recommended before further flight by 

Gulfstream G350 Alert Customer 

Bulletin 11, dated December 4, 2012; 

and Gulfstream G450 Alert Customer 

Bulletin 11, dated December 4, 2012. 

We have determined that the 3-day 

compliance time required by this AD 

will adequately ensure safety while 

avoiding the need to ground the fleet. 

Although the service information 

recommends that operators contact 

Gulfstream if a successful test is not 

achieved, this AD requires operators to 

repair those conditions before further 

flight in accordance with a method 

approved by the FAA. 


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Federal Register / Vol. 77, No. 242 / Monday, December 17, 2012 / Rules and Regulations 74581 

Interim Action 

We consider this AD interim action. 

Gulfstream is in the process of updating 

software intended to terminate the 

actions required by this AD. Once this 

upgrade is developed, approved, and 

available, we might consider further 

rulemaking to require the upgraded 

software. 

FAA’s Justification and Determination 

of the Effective Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because failure of the brake feature 

in the HSEMU could result in a 

runaway horizontal stabilizer pitch trim 

system which, if left uncorrected, could 

result in loss of airplane pitch control. 

Therefore, we find that notice and 

opportunity for prior public comment 

are impracticable and that good cause 

exists for making this amendment 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety and 

was not preceded by notice and an 

opportunity for public comment. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include the docket number 

FAA–2012–1225 and Directorate 

Identifier 2012–NM–219–AD at the 

beginning of your comments. We 

specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this AD because of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

Costs of Compliance 

We estimate that this AD affects 200 

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 

Preflight procedure test ................................... 1 work-hour × $85 per hour = $85 ................. $0 $85 $17,000 

AFM revision ................................................... 1 work-hour × $85 per hour = $85 ................. 0 85 17,000 

We have received no definitive data 

that would enable us to provide cost 

estimates for the on-condition actions 

specified in this AD. 

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): 

2012–25–07 Gulfstream Aerospace 

Corporation: Amendment 39–17288; 

Docket No. FAA–2012–1225; Directorate 

Identifier 2012–NM–219–AD. 

(a) Effective Date 

This AD is effective December 17, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Gulfstream Aerospace 

Corporation Model GIV–X airplanes, 

certificated in any category, serial numbers 

4001 through 4271 inclusive. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code 27, Flight controls. 

(e) Unsafe Condition 

This AD was prompted by reports 

indicating that the flap/stabilizer electronic 

control unit (FSECU) does not detect failures 

of the brake feature within the horizontal 

stabilizer electric motor unit (HSEMU), or 

failures of the drive solenoids for hydraulic 

valves within the flap hydraulic control 

module (FHCM) during the system power-on 

self test (SPOST). We are issuing this AD to 

detect and correct such failures, which could 

result in runaway horizontal stabilizer pitch 

trim system and consequent loss of pitch 

control. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 


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(g) SPOST 

Within 3 days after the effective date of 

this AD, perform an SPOST of the FSECU, in 

accordance with the applicable service 

information identified in paragraph (h)(1) or 

(h)(2) of this AD. 

(1) For Model GIV–X (G350) airplanes: Use 

Gulfstream G350 Alert Customer Bulletin 11, 

dated December 4, 2012, excluding Service 

Reply Card, dated December 4, 2012, and 

excluding Revision 31, dated December 4, 

2012, of the Gulfstream G350 Airplane Flight 

Manual Document GAC–AC–G350–OPS– 

0001. 

(2) For Model GIV–X (G450) airplanes: Use 

Gulfstream G450 Alert Customer Bulletin 11, 

dated December 4, 2012, excluding Service 

Reply Card, dated December 4, 2012, and 

excluding Revision 33, dated December 4, 

2012, of the Gulfstream G450 Airplane Flight 

Manual Document GAC–AC–G450–OPS– 

0001. 

(h) Revision of Aircraft Flight Manual (AFM) 

Before further flight after the FSECU passes 

the SPOST required by paragraph (g) of this 

AD, revise the Normal Procedures and 

Limitations sections of the AFM to 

incorporate the information identified in 

paragraph (g)(1) or (g)(2) of this AD, as 

applicable. 

(1) For Model GIV–X (G350) airplanes: 

Incorporate the information in Section 1–27– 

40, ‘‘Flap/Stabilizer System Preflight Check,’’ 

and Section 2–03–20, ‘‘Before Starting 

Engines,’’ of the Gulfstream G350 Airplane 

Flight Manual Document GAC–AC–G350– 

OPS–0001, Revision 31, dated December 4, 

2012. This may be accomplished by inserting 

into the AFM a copy of Gulfstream G350 

Airplane Flight Manual Document GAC–AC– 

G350–OPS–0001, Revision 31, dated 

December 4, 2012. 

(2) For Model GIV–X (G450) airplanes: 

Section 1–27–40, ‘‘Flap/Stabilizer System 

Preflight Check,’’ and Section 2–03–20, 

‘‘Before Starting Engines,’’ of the Gulfstream 

G450 Airplane Flight Manual Document 

GAC–AC–G450–OPS–0001, Revision 33, 

dated December 4, 2012. This may be 

accomplished by inserting into the AFM a 

copy of Gulfstream G450 Airplane Flight 

Manual Document GAC–AC–G450–OPS– 

0001, Revision 33, dated December 4, 2012. 

(i) Corrective Action for Failed SPOST 

If the FSECU fails any SPOST required by 

this AD or as specified in the applicable 

AFM, repair before further flight in 

accordance with a method approved by the 

Manager, Atlanta Aircraft Certification Office 

(ACO), FAA. For a repair method to be 

approved by the Manager, Atlanta ACO, as 

required by this paragraph, the Manager’s 

approval letter must specifically refer to this 

AD. 

(j) Special Flight Permit 

Special flight permits, as described in 

Section 21.197 and Section 21.199 of the 

Federal Aviation Regulations (14 CFR 21.197 

and 21.199), are not allowed. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Atlanta 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. 

(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. 

(l) Related Information 

For more information about this AD, 

contact Sanford Proveaux, Aerospace 

Engineer, Continued Operational Safety and 

Certificate Management Branch, ACE–102A, 

FAA, Atlanta Aircraft Certification Office 

(ACO), 1701 Columbia Avenue, College Park, 

Georgia 30337; phone: 404–474–5566; fax: 

404–474–5606; email: 

sanford.proveaux@faa.gov. 

(m) 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) Gulfstream G350 Alert Customer 

Bulletin 11, dated December 4, 2012. 

(ii) Gulfstream G450 Alert Customer 

Bulletin 11, dated December 4, 2012. 

(iii) Section 1–27–40, ‘‘Flap/Stabilizer 

System Preflight Check,’’ of the Gulfstream 

G350 Airplane Flight Manual Document 

GAC–AC–G350–OPS–0001, Revision 31, 

dated December 4, 2012. The document 

number of this document is identified on the 

revision transmittal page and the first page of 

the Record of Revisions; no other page of this 

document contains this information. 

(iv) Section 1–27–40, ‘‘Flap/Stabilizer 

System Preflight Check,’’ of the Gulfstream 

G450 Airplane Flight Manual Document 

GAC–AC–G450–OPS–0001, Revision 33, 

dated December 4, 2012. The document 

number of this document is identified on the 

revision transmittal page and the first page of 

the Record of Revisions; no other page of this 

document contains this information. 

(v) Section 2–03–20, ‘‘Before Starting 

Engines,’’ of the Gulfstream G350 Airplane 

Flight Manual Document GAC–AC–G350– 

OPS–0001, Revision 31, dated December 4, 

2012. The document number of this 

document is identified on the revision 

transmittal page and the first page of the 

Record of Revisions; no other page of this 

document contains this information. 

(vi) Section 2–03–20, ‘‘Before Starting 

Engines,’’ of the Gulfstream G450 Airplane 

Flight Manual Document GAC–AC–G450– 

OPS–0001, Revision 33, dated December 4, 

2012. The document number of this 

document is identified on the revision 

transmittal page and the first page of the 

Record of Revisions; no other page of this 

document contains this information. 

(3) For service information identified in 

this AD, contact Gulfstream Aerospace 

Corporation, Technical Publications Dept., 

P.O. Box 2206, Savannah, GA 31402–2206; 

telephone 800–810–4853; fax 912–965–3520; 

email pubs@gulfstream.com; Internet http:// 

www.gulfstream.com/product_support/ 

technical_pubs/pubs/index.htm. 

(4) You may view this service information 

at FAA, Transport Airplane Directorate, 

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 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 

December 7, 2012. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–30058 Filed 12–14–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 1 

[Docket No FDA–2012–D–1003] 

Small Entity Compliance Guide: What 

You Need To Know About Registration 

of Food Facilities; Availability 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Notice of availability. 

SUMMARY: The Food and Drug 

Administration (FDA) is announcing the 

availability of an updated guidance for 

industry entitled ‘‘What You Need To 

Know About Registration of Food 

Facilities—Small Entity Compliance 

Guide.’’ FDA has prepared this guidance 

to restate the legal requirements 

pertaining to registration of food 

facilities in the Federal Food, Drug, and 

Cosmetic Act (the FD&C Act), as 

amended by the FDA Food Safety 

Modernization Act (FSMA). Previously, 

this guidance restated the legal 

requirements of FDA’s food facility 

registration regulation. This document 

also served as FDA’s Small Entity 

Compliance Guide for FDA’s food 

facility registration regulation in 

accordance with the Small Business 

Regulatory Enforcement Fairness Act. 

FDA is revising this document to 

provide guidance intended to help any 

entity comply with the requirements 

pertaining to registration of food 


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