[Federal Register Volume 76, Number 47 (Thursday, March 10, 2011)]
[Rules and Regulations]
[Pages 13072-13073]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-5116]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1198; Directorate Identifier 2010-NM-145-AD;
Amendment 39-16623; AD 2011-05-13]
RIN 2120-AA64
Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB
2000 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
Corrosion has been found on the rear spar upper cap of the
horizontal stabilizer of SAAB 2000 aeroplanes. The affected areas
are adjacent to the inboard elevator hinge where the electrical
wiring harnesses are located and wired through the lightening holes.
The upper spar cap is a primary structural element and is important
to the structural integrity of the horizontal stabilizer.
Corrosion damage in these areas, if not detected and corrected,
can result in a starting point for future crack propagation, which
would impair the integrity of the horizontal stabilizer upper spar
cap structure.
* * * * *
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective April 14, 2011.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 14,
2011.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace
Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-1112; fax (425) 227-1149.
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 was published in the Federal Register on December 14, 2010
(75 FR 77796). That NPRM proposed to correct an unsafe condition for
the specified products. The MCAI states:
Corrosion has been found on the rear spar upper cap of the
horizontal stabilizer of SAAB 2000 aeroplanes. The affected areas
are adjacent to the inboard elevator hinge where the electrical
wiring harnesses are located and wired through the lightening holes.
The upper spar cap is a primary structural element and is important
to the structural integrity of the horizontal stabilizer.
Corrosion damage in these areas, if not detected and corrected,
can result in a starting point for future crack propagation, which
would impair the integrity of the horizontal stabilizer upper spar
cap structure.
For the reasons describe above, this AD requires a detailed
visual inspection (DVI) of the LH and RH horizontal stabilizer rear
spar adjacent to the inboard elevator hinge and the harnesses
installed in the adjacent areas, installation of convoluted tubing
on the harness, and corrective actions depending on findings.
The corrective actions include installing convoluted tubing on the
harness, applying corrosion prevention compound to the inspected area,
making sure clearance exists between the spar cap and the harnesses/
convoluted tube, and contacting Saab for repair instructions and doing
the repair. You may obtain further information by examining the MCAI in
the AD docket.
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 available data and determined that air safety and
the public interest require adopting the AD as proposed.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a Note within the AD.
Costs of Compliance
We estimate that this AD will affect 8 products of U.S. registry.
We also estimate that it will take about 2 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Based on these figures, we estimate the cost of
this AD to the U.S. operators to be $1,360 or $170 per product.
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
[[Page 13073]]
products identified in this rulemaking action.
Regulatory Findings
We determined that 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 this AD:
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); and
3. 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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone (800) 647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.
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 AD:
2011-05-13 Saab AB, Saab Aerosystems: Amendment 39-16623. Docket No.
FAA-2010-1198; Directorate Identifier 2010-NM-145-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective April
14, 2011.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Saab AB, Saab Aerosystems Model SAAB
2000 airplanes, certificated in any category.
Subject
(d) Air Transport Association (ATA) of America Code 55:
Stabilizers.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
Corrosion has been found on the rear spar upper cap of the
horizontal stabilizer of SAAB 2000 aeroplanes. The affected areas
are adjacent to the inboard elevator hinge where the electrical
wiring harnesses are located and wired through the lightening holes.
The upper spar cap is a primary structural element and is important
to the structural integrity of the horizontal stabilizer.
Corrosion damage in these areas, if not detected and corrected,
can result in a starting point for future crack propagation, which
would impair the integrity of the horizontal stabilizer upper spar
cap structure.
* * * * *
Compliance
(f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Actions
(g) Within 12 months after the effective date of this AD: Do a
detailed visual inspection for corrosion of the left-hand and right-
hand horizontal stabilizers, do a detailed visual inspection for
chafing or damage on the harness installed in the adjacent area, and
install convoluted tubing on the harness, in accordance with the
Accomplishment Instructions of Saab Service Bulletin 2000-55-013,
dated July 6, 2009.
(h) If, during the inspection required by paragraph (g) of this
AD, corrosion is found, before next flight, repair the corrosion
using a method approved by the Manager, International Branch, ANM-
116, Transport Airplane Directorate, FAA, or European Aviation
Safety Agency (EASA) (or its delegated agent).
FAA AD Differences
Note 1: This AD differs from the MCAI and/or service
information as follows: No differences.
Other FAA AD Provisions
(i) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to Attn:
Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM-
116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356; telephone (425) 227-1112; fax (425)
227-1149. 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. The AMOC approval letter must specifically
reference this AD.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
Related Information
(j) Refer to MCAI EASA Airworthiness Directive 2010-0115, dated
June 17, 2010; and Saab Service Bulletin 2000-55-013, dated July 6,
2009; for related information.
Material Incorporated by Reference
(k) You must use Saab Service Bulletin 2000-55-013, dated July
6, 2009, to do the actions required by this AD, unless the AD
specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact Saab
AB, Saab Aerosystems, SE-581 88, Link[ouml]ping, Sweden; telephone
+46 13 18 5591; fax +46 13 18 4874; e-mail
[email protected]; Internet http://www.saabgroup.com.
(3) You may review copies of the 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/code_of_federal_regulations/ibr_locations.html.
Issued in Renton, Washington, on February 22, 2011.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-5116 Filed 3-9-11; 8:45 am]
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