AD 2012-21-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | G58 | Airworthiness Directives; Hawker Beechcraft Corporation Airplanes |
Unsafe Condition
Certain aircraft were produced with the incorrect gauge wiring installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the supply wire of the three-light strobe system following Hawker Beechcraft Mandatory Service Bulletin No. SB 33-4053, dated February 2011.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 50 hours time-in-service (TIS) after November 27, 2012, or within the next 6 calendar months after November 27, 2012, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Hawker Beechcraft Corporation Model G58 airplanes, serial numbers (S/N) TH-2218 through TH-2285, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Model G58 airplanes. This AD was prompted by notification from Hawker Beechcraft Corporation that certain affected aircraft were produced with the incorrect gauge wiring installed. This AD requires replacement of the incorrect gauge wiring with the correct wiring required by type design and the aircraft's circuit protection. We are issuing this AD to correct the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Hawker Beechcraft Corporation Model G58
airplanes, serial numbers (S/N) TH-2218 through TH-2285, that are
certificated in any category.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 77, Number 205 (Tuesday, October 23, 2012)]
[Rules and Regulations]
[Pages 64693-64694]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2012-25664]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
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having general applicability and legal effect, most of which are keyed
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Federal Register / Vol. 77, No. 205 / Tuesday, October 23, 2012 /
Rules and Regulations
[[Page 64693]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0829; Directorate Identifier 2012-CE-024-AD;
Amendment 39-17221; AD 2012-21-05]
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 Model G58 airplanes. This AD was prompted
by notification from Hawker Beechcraft Corporation that certain
affected aircraft were produced with the incorrect gauge wiring
installed. This AD requires replacement of the incorrect gauge wiring
with the correct wiring required by type design and the aircraft's
circuit protection. We are issuing this AD to correct the unsafe
condition on these products.
DATES: This AD is effective November 27, 2012.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of November 27,
2012.
ADDRESSES: 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#1b6f767f785b737a6c707e69797e7e787378697a7d6f35787476"><span class="__cf_email__" data-cfemail="ed9980898ead858c9a86889f8f88888e858e9f8c8b99c38e8280">[email protected]</span></a>; or Internet:
<a href="http://www.hawkerbeechcraft.com/customer_support/technical_and_field_support/">http://www.hawkerbeechcraft.com/customer_support/technical_and_field_support/</a>. 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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: Richard Rejniak, Aerospace Engineer,
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; phone: (316) 946-4128; fax: (316) 946-4107;
email: <a href="/cdn-cgi/l/email-protection#16647f757e7764723864737c787f777d5670777738717960"><span class="__cf_email__" data-cfemail="21534842494053450f53444b4f48404a614740400f464e57">[email protected]</span></a>.
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 August 9, 2012 (77 FR
47568). That NPRM proposed to require replacement of the incorrect
gauge wiring with the correct wiring required by type design and the
aircraft's circuit protection.
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:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 47568, August 9, 2012) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this AD affects 40 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
----------------------------------------------------------------------------------------------------------------
Replace supply wire of the three light 16 work-hours x $85 per $50 $1,410 $56,400
strobe system. hour = $1,360.
----------------------------------------------------------------------------------------------------------------
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
[[Page 64694]]
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):
2012-21-05 Hawker Beechcraft Corporation Airplanes: Amendment 39-
17221; Docket No. FAA-2012-0829; Directorate Identifier 2012-CE-024-
AD.
(a) Effective Date
This AD is effective November 27, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Hawker Beechcraft Corporation Model G58
airplanes, serial numbers (S/N) TH-2218 through TH-2285, that are
certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 24, Electrical power.
(e) Unsafe Condition
This AD was prompted by notification from Hawker Beechcraft
Corporation that certain aircraft were produced with the incorrect
gauge wiring installed. 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) Replace Supply Wire of the Three-Light Strobe System
Within the next 50 hours time-in-service (TIS) after November 27,
2012 (the effective date of this AD) or within the next 6 calendar
months after November 27, 2012 (the effective date of this AD),
whichever occurs first, replace the supply wire of the three-light
strobe system. Do the replacement following Hawker Beechcraft Mandatory
Service Bulletin No. SB 33-4053, dated February 2011.
(h) Special Flight Permit
Special flight permits are permitted with the following limitation:
visual flight rules (VFR) day conditions only.
(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 Richard Rejniak,
Aerospace Engineer, Wichita ACO, 1801 Airport Road, Room 100, Wichita,
Kansas 67209; phone: (316) 946-4128; fax: (316) 946-4107; email:
<a href="/cdn-cgi/l/email-protection#e3918a808b829187cd9186898d8a8288a3858282cd848c95"><span class="__cf_email__" data-cfemail="88fae1ebe0e9faeca6faede2e6e1e9e3c8eee9e9a6efe7fe">[email protected]</span></a>.
(k) 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) Hawker Beechcraft Mandatory Service Bulletin No. SB 33-4053,
dated February 2011.
(ii) Reserved.
(3) For Hawker Beechcraft Corporation 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#f2869f9691b29a9385999780909797919a9180939486dc919d9f"><span class="__cf_email__" data-cfemail="5f2b323b3c1f373e28343a2d3d3a3a3c373c2d3e392b713c3032">[email protected]</span></a>; or Internet: <a href="http://www.hawkerbeechcraft.com/customer_support/technical_and_field_support/">http://www.hawkerbeechcraft.com/customer_support/technical_and_field_support/</a>.
(4) You may view this service information at 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.
(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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Kansas City, Missouri, on October 11, 2012.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-25664 Filed 10-22-12; 8:45 am]
BILLING CODE 4910-13-P
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