[Federal Register Volume 77, Number 42 (Friday, March 2, 2012)]
[Proposed Rules]
[Pages 12757-12759]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-5086]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0218; Directorate Identifier 2012-CE-003-AD]
RIN 2120-AA64


Airworthiness Directives; Hawker Beechcraft Corporation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Hawker Beechcraft Corporation Models 58 and G58 airplanes. This 
proposed 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 proposed AD would require inspecting for 
oversized or deformed fuel hose clamps and replacing as necessary. We 
are proposing this AD to correct the unsafe condition on these 
products.

DATES: We must receive comments on this proposed AD by April 16, 2012.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <bullet> Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact 
Hawker Beechcraft Corporation, B091-A04, 10511 E. Central Ave., 
Wichita, Kansas 67206; telephone: 1 (800) 429-5372 or (316) 676-3140; 
fax: (316) 676-8027; email: <a href="/cdn-cgi/l/email-protection#3d4950595e7d555c4a56584f5f58585e555e4f5c5b49135e5250"><span class="__cf_email__" data-cfemail="40342d2423002821372b2532222525232823322126346e232f2d">[email protected]</span></a>; 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 proposed 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: 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: <a href="/cdn-cgi/l/email-protection#3f4b5750525e4c114b5a4f5356547f595e5e11585049"><span class="__cf_email__" data-cfemail="86f2eee9ebe7f5a8f2e3f6eaefedc6e0e7e7a8e1e9f0">[email protected]</span></a>.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-12-0218; 
Directorate Identifier 2012-CE-003-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed 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 proposed AD.

Discussion

    We received reports of installation of oversized clamps on fuel 
vapor return and/or fuel vent lines in the outboard sections of the 
left and right wings on Hawker Beechcraft Corporation Models 58 and G58 
airplanes. 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.

Relevant Service Information

    We reviewed Hawker Beechcraft Mandatory Service Bulletin No. SB 28-
4039, Revision 1, dated October 2011. The service bulletin describes 
procedures for inspecting for oversized or deformed fuel hose clamps 
and replacing as necessary.

FAA's Determination

    We are proposing 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.

Proposed AD Requirements

    This proposed AD would require accomplishing the actions specified 
in the service information described previously.

Costs of Compliance

    We estimate that this proposed AD affects 244 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed 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 $85 per  Not applicable....         $297.50          $72,590
 fuel hose clamps, and refueling.  hour = $297.50.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary replacements 
that would be required based on the results of the proposed inspection. 
We have no way of determining the number of aircraft that might need 
these replacements:

[[Page 12758]]



                                               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).
----------------------------------------------------------------------------------------------------------------


    Note: According to the manufacturer, some of the costs of this 
proposed 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

    We determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    (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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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.


Sec.  39.13  [Amended]

    2. The FAA amends Sec.  39.13 by adding the following new 
airworthiness directive (AD):

Hawker Beechcraft Corporation: Docket No. FAA-2012-0218; Directorate 
Identifier 2012-CE-003-AD.

(a) Comments Due Date

    We must receive comments by April 16, 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
    (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 the effective 
date of this AD or within the next 6 calendar months after 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:  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

    (1) 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: <a href="/cdn-cgi/l/email-protection#14607c7b7975673a607164787d7f547275753a737b62"><span class="__cf_email__" data-cfemail="bdc9d5d2d0dcce93c9d8cdd1d4d6fddbdcdc93dad2cb">[email protected]</span></a>.
    (2) For service information identified in this AD, contact 
Hawker Beechcraft Corporation, B091-A04, 10511 E. Central Ave. 
Wichita, Kansas 67206; telephone: 1 (800) 429-5372 or (316) 676-
3140; fax: (316) 676-8027; email: <a href="/cdn-cgi/l/email-protection#e99d848d8aa981889e828c9b8b8c8c8a818a9b888f9dc78a8684"><span class="__cf_email__" data-cfemail="ccb8a1a8af8ca4adbba7a9beaea9a9afa4afbeadaab8e2afa3a1">[email protected]</span></a>; 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.


[[Page 12759]]


    Issued in Kansas City, Missouri, on February 24, 2012.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-5086 Filed 3-1-12; 8:45 am]
BILLING CODE 4910-13-P


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