29214 Federal Register / Vol. 77, No. 96 / Thursday, May 17, 2012 / Rules and Regulations 

missing latch pin retention bolts of the latch 

pin fittings of the lower sill of the forward 

large cargo door, and do all applicable related 

investigative and corrective actions, in 

accordance with the Accomplishment 

Instructions of Boeing Alert Service Bulletin 

777–52A0038, Revision 1, dated June 24, 

2010, except as provided by paragraph (h) of 

this AD. Do all applicable related 

investigative and corrective actions at the 

applicable times specified in paragraph 1.E., 

‘‘Compliance,’’ of Boeing Alert Service 

Bulletin 777–52A0038, Revision 1, dated 

June 24, 2010. Repeat the inspection 

thereafter at the applicable time specified in 

paragraph 1.E., ‘‘Compliance,’’ of Boeing 

Alert Service Bulletin 777–52A0038, 

Revision 1, dated June 24, 2010, except as 

specified in paragraph (j) of this AD. 

(h) Repair 

If any cut, crack, or damage is found during 

any inspection required by this AD, and 

Boeing Alert Service Bulletin 777–52A0038, 

Revision 1, dated June 24, 2010, specifies to 

contact Boeing for appropriate action: Before 

further flight, repair the cut, crack, or damage 

in accordance with a method approved by 

the Manager, Seattle, Aircraft Certification 

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

be approved, the repair must meet the 

certification basis of the airplane, and the 

approval must specifically refer to this AD. 

(i) Exception to Compliance Time 

Where Boeing Alert Service Bulletin 777– 

52A0038, Revision 1, dated June 24, 2010, 

specifies a compliance time after the date on 

that service bulletin, this AD requires 

compliance within the specified compliance 

time after the effective date of this AD. 

(j) Optional Terminating Action for 

Repetitive Inspections 

Replacing latch pin retention bolts made of 

titanium with new Inconel bolts, in 

accordance with the Accomplishment 

Instructions of Boeing Alert Service Bulletin 

777–52A0038, Revision 1, dated June 24, 

2010, terminates the repetitive inspections 

required by paragraph (g) of this AD at 

Stations 509.10, 522.75, 537.50, 554.30, 

562.90, 579.70, 591.25, and 604.90, latch pin 

fittings No. 1 through No. 8. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Seattle ACO, 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. 

(l) Related Information 

For more information about this AD, 

contact Ana Martinez Hueto, Aerospace 

Engineer, Cabin Safety and Environmental 

Systems Branch, ANM–150S, FAA, Seattle 

Aircraft Certification Office, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

phone: 425–917–6592; fax: 425–917–6590; 

email: ana.m.hueto@faa.gov. 

(m) Material Incorporated by Reference 

(1) You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. 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 of the following 

service information: 

(i) Boeing Alert Service Bulletin 777– 

52A0038, Revision 1, dated June 24, 2010. 

(2) For service information identified in 

this AD, contact Boeing Commercial 

Airplanes, Attention: Data & Services 

Management, P.O. Box 3707, MC 2H–65, 

Seattle, Washington 98124–2207; telephone 

206–544–5000, extension 1; fax 206–766– 

5680; email me.boecom@boeing.com; Internet 

https://www.myboeingfleet.com. 

(3) 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. 

(4) 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 May 4, 

2012. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–11463 Filed 5–16–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0218; Directorate 

Identifier 2012–CE–003–AD; Amendment 

39–17051; AD 2012–10–02] 

RIN 2120–AA64 

Airworthiness Directives; Hawker 

Beechcraft Corporation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Hawker Beechcraft Corporation Models 

58 and G58 airplanes. This AD was 

prompted by installation of oversized 

clamps on fuel vapor return and/or fuel 

vent lines in the outboard sections of 

the left and right wings. This AD 

requires inspecting for oversized or 

deformed fuel hose clamps and 

replacing as necessary. We are issuing 

this AD to correct the unsafe condition 

on these products. 

DATES: This AD is effective June 21, 

2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of June 21, 2012. 

ADDRESSES: For service information 

identified in this AD, contact Hawker 

Beechcraft Corporation, B091–A04, 

10511 E. Central Ave., Wichita, Kansas 

67206; telephone: (800) 429–5372 or 

(316) 676–3140; fax: (316) 676–8027; 

email: tmdc@hawkerbeechcraft.com; or 

Internet: http:// 

www.hawkerbeechcraft.com/ 

customer_support/ 

technical_and_field_support/. You may 

review copies of the referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. 

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 address for the 

Docket Office (phone: 800–647–5527) is 

Document 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: 

Thomas Teplik, Aerospace Engineer, 

Wichita Aircraft Certification Office, 

FAA, 1801 Airport Road, Room 100, 

Wichita, Kansas 67209; phone: (316) 

946–4196; fax: (316) 329–4090; email: 

thomas.teplik@faa.gov. 

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 published in the Federal 

Register on March 2, 2012 (77 FR 

12757). That NPRM proposed to require 


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Federal Register / Vol. 77, No. 96 / Thursday, May 17, 2012 / Rules and Regulations 29215 

inspection for oversized or deformed 

fuel hose clamps and replacement as 

necessary because of reports we have 

received of installation of oversized 

clamps on fuel vapor return and/or fuel 

vent lines in the outboard sections of 

the left and right wings. This condition, 

if not corrected, could result in leakage 

of fuel or vapor in areas where electrical 

wiring and other potential ignition 

sources are present, which could lead to 

an inflight fire. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the relevant 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 

12757, March 2, 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 12757, 

March 2, 2012). 

Costs of Compliance 

We estimate that this AD affects 244 

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 

Defueling, inspection of the fuel hose 

clamps, and refueling.

3.5 work-hours × $85 per hour = 

$297.50.

Not applicable ............. $297.50 $72,590 

We estimate the following costs to do 

any necessary replacements that would 

be required based on the results of the 

inspection. We have no way of 

determining the number of aircraft that 

might need these replacements: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per product 

Replacement of fuel hose clamps (Cost represents replacement of a maximum of 20 clamps depending 

on airplane configuration).

3 work-hours × $85 per hour = $255 .......................... $20 $275 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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): 

2012–10–02 Hawker Beechcraft 

Corporation: Amendment 39–17051; 

Docket No. FAA–2012–0218; Directorate 

Identifier 2012–CE–003–AD. 

(a) Effective Date 

This AD is effective June 21, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

(1) This AD applies to the following 

Hawker Beechcraft Corporation airplanes that 

are certificated in any category: 

(i) Model 58, serial numbers TH–1931 

through TH–2124, and 


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29216 Federal Register / Vol. 77, No. 96 / Thursday, May 17, 2012 / Rules and Regulations 

(ii) Model G58, serial numbers TH–2125 

through TH–2281, TH–2283, and TH–2284. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code 28; fuel. 

(e) Unsafe Condition 

This AD was prompted by installation of 

oversized clamps on fuel vapor return and/ 

or fuel vent lines in the outboard sections of 

the left and right wings. We are issuing this 

AD to correct the unsafe condition on these 

products. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection 

Within the next 50 hours time-in-service 

after June 21, 2012 (the effective date of this 

AD) or within the next 6 calendar months 

after June 21, 2012 (the effective date of this 

AD), whichever occurs first, inspect the fuel 

hose clamps for oversized or deformed 

clamps following Hawker Beechcraft 

Mandatory Service Bulletin No. SB 28–4039, 

Revision 1, dated October 2011. 

Note 1 to paragraph (g) of this AD: If you 

have a scheduled inspection before the 

compliance time of this AD, the FAA 

recommends you comply with this AD at that 

time. 

(h) Replacement 

If any oversized or deformed clamps are 

found during the inspection required in 

paragraph (g) of this AD, before further flight, 

replace the clamps following Hawker 

Beechcraft Mandatory Service Bulletin No. 

SB 28–4039, Revision 1, dated October 2011. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Wichita 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. 

(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 Thomas Teplik, Aerospace Engineer, 

Wichita ACO, FAA, 1801 Airport Road, 

Room 100, Wichita, Kansas 67209; phone: 

(316) 946–4196; fax: (316) 329–4090; email: 

thomas.teplik@faa.gov. 

(k) Material Incorporated by Reference 

(1) You must use Hawker Beechcraft 

Mandatory Service Bulletin No. SB 28–4039, 

Revision 1, dated October 2011, to do the 

actions required by this AD, unless the AD 

specifies otherwise. The Director of the 

Federal Register approved the incorporation 

by reference (IBR) under 5 U.S.C. 552(a) and 

1 CFR part 51. 

(2) For service information identified in 

this AD, contact Hawker Beechcraft 

Corporation, B091–A04, 10511 E. Central 

Ave., Wichita, Kansas 67206; telephone: 

(800) 429–5372 or (316) 676–3140; fax: (316) 

676–8027; email: 

tmdc@hawkerbeechcraft.com; or Internet: 

http://www.hawkerbeechcraft.com/ 

customer_support/ 

technical_and_field_support/. 

(3) You may review copies of the 

referenced service information at the FAA, 

Small Airplane Directorate, 901 Locust, 

Kansas City, Missouri 64106. For information 

on the availability of this material at the 

FAA, call (816) 329–4148. 

(4) 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 Kansas City, Missouri, on May 9, 

2012. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2012–11812 Filed 5–16–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Parts 510, 520, 522, and 558 

[Docket No. FDA–2012–N–0002] 

New Animal Drugs; Ceftiofur Sodium; 

Lincomycin Powder; Naracin; Tylosin 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule. 

SUMMARY: The Food and Drug 

Administration (FDA) is amending the 

animal drug regulations to reflect 

approval actions for new animal drug 

applications (NADAs) and abbreviated 

new animal drug applications 

(ANADAs) during March 2012. FDA is 

also informing the public of the 

availability of summaries of the basis of 

approval and of environmental review 

documents, where applicable. 

DATES: This rule is effective May 17, 

2012. 

FOR FURTHER INFORMATION CONTACT: 

George K. Haibel, Center for Veterinary 

Medicine (HFV–6), Food and Drug 

Administration, 7519 Standish Pl., 

Rockville, MD 20855, 240–276–9019, 

email:george.haibel@fda.hhs.gov. 

SUPPLEMENTARY INFORMATION: FDA’s 

Center for Veterinary Medicine (CVM) is 

adopting use of a monthly Federal 

Register document to codify approval 

actions for NADAs and abbreviated 

ANADAs. CVM will no longer publish 

a separate rule for each action. This 

approach will allow a more efficient use 

of available resources. 

In this document, FDA is amending 

the animal drug regulations to reflect 

the original and supplemental approval 

actions during March 2012, as listed in 

table 1 of this document. FDA is also 

informing the public of the availability 

of environmental review documents 

required under the National 

Environmental Policy Act (NEPA), 

where applicable. For actions requiring 

review of safety or effectiveness data, 

summaries of the basis of approval (FOI 

Summaries) under the Freedom of 

Information Act (FOIA) may be seen in 

the Division of Dockets Management 

(HFA–305), Food and Drug 

Administration, 5630 Fishers Lane, rm. 

1061, Rockville, MD 20852, between 

9 a.m. and 4 p.m., Monday through 

Friday. 


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