Airworthiness Directives; Hawker Beechcraft Corporation Airplanes, 29214-29216 [2012-11812]

Download as PDF 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. 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 (m) Material Incorporated by Reference on these products. (1) You must use the following service DATES: This AD is effective June 21, information to do the actions required by this 2012. AD, unless the AD specifies otherwise. The The Director of the Federal Register Director of the Federal Register approved the approved the incorporation by reference incorporation by reference (IBR) of the of a certain publication listed in the AD following service information under 5 U.S.C. as of June 21, 2012. 552(a) and 1 CFR part 51 of the following ADDRESSES: For service information service information: identified in this AD, contact Hawker (i) Boeing Alert Service Bulletin 777– 52A0038, Revision 1, dated June 24, 2010. Beechcraft Corporation, B091–A04, (2) For service information identified in 10511 E. Central Ave., Wichita, Kansas this AD, contact Boeing Commercial 67206; telephone: (800) 429–5372 or Airplanes, Attention: Data & Services (316) 676–3140; fax: (316) 676–8027; Management, P.O. Box 3707, MC 2H–65, email: tmdc@hawkerbeechcraft.com; or Seattle, Washington 98124–2207; telephone Internet: http:// 206–544–5000, extension 1; fax 206–766– 5680; email me.boecom@boeing.com; Internet www.hawkerbeechcraft.com/ customer_support/ https://www.myboeingfleet.com. technical_and_field_support/. You may (3) You may review copies of the referenced service information at the FAA, review copies of the referenced service Transport Airplane Directorate, 1601 Lind information at the FAA, Small Airplane Avenue SW., Renton, Washington. For Directorate, 901 Locust, Kansas City, information on the availability of this Missouri 64106. For information on the material at the FAA, call 425–227–1221. availability of this material at the FAA, (4) You may also review copies of the call (816) 329–4148. service information that is incorporated by (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. 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 srobinson on DSK4SPTVN1PROD with RULES (k) Alternative Methods of Compliance (AMOCs) Federal Aviation Administration (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. 14 CFR Part 39 VerDate Mar<15>2010 16:15 May 16, 2012 Jkt 226001 [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 Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Models SUMMARY: PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 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 E:\FR\FM\17MYR1.SGM 17MYR1 29215 Federal Register / Vol. 77, No. 96 / Thursday, May 17, 2012 / Rules and Regulations 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. srobinson on DSK4SPTVN1PROD with RULES 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 VerDate Mar<15>2010 16:15 May 16, 2012 Jkt 226001 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. PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 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 E:\FR\FM\17MYR1.SGM 17MYR1 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) srobinson on DSK4SPTVN1PROD with RULES 16:15 May 16, 2012 Jkt 226001 (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] (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. VerDate Mar<15>2010 (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. 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: ACTION: Final rule. 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. SUMMARY: 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. 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. SUPPLEMENTARY INFORMATION: Food and Drug Administration, HHS. PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\17MYR1.SGM 17MYR1

Agencies

[Federal Register Volume 77, Number 96 (Thursday, May 17, 2012)]
[Rules and Regulations]
[Pages 29214-29216]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2012-11812]


-----------------------------------------------------------------------

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

[[Page 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
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
            Action                Labor cost               Parts cost               product         operators
----------------------------------------------------------------------------------------------------------------
Defueling, inspection of the   3.5 work-hours x  Not applicable...............         $297.50          $72,590
 fuel hose clamps, and          $85 per hour =
 refueling.                     $297.50.
----------------------------------------------------------------------------------------------------------------

    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
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                Action                                Labor cost                   Parts cost        product
----------------------------------------------------------------------------------------------------------------
Replacement of fuel hose clamps (Cost   3 work-hours x $85 per hour = $255....             $20             $275
 represents replacement of a maximum
 of 20 clamps depending on airplane
 configuration).
----------------------------------------------------------------------------------------------------------------

    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

0
1. The authority citation for part 39 continues to read as follows:

    Authority:  49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  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

[[Page 29216]]

    (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