[Federal Register Volume 75, Number 221 (Wednesday, November 17, 2010)]
[Rules and Regulations]
[Pages 70096-70098]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-28449]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0732; Directorate Identifier 2010-NE-04-AD;
Amendment 39-16509; AD 2010-23-20]
RIN 2120-AA64
Airworthiness Directives; General Electric Company (GE) CT7-9C
and -9C3 Turboprop Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD requires inspecting certain serial
number (S/N) gas generator turbine (GGT) shafts for nonconforming land
balance-cuts, and if found, removing the shaft from service. This AD
was prompted by reports of a manufacturing quality problem. We are
issuing this AD to detect nonconforming GGT shaft land balance-cuts,
which could result in the shaft failing before its published life
limit, and which could result in an uncontained engine failure and
damage to the airplane.
DATES: This AD is effective December 22, 2010.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of December 22,
2010.
ADDRESSES: For service information identified in this AD, contact
General Electric Company, GE-Aviation, Room 285, 1 Neumann Way,
Cincinnati, Ohio 45215; e-mail [email protected]; telephone (513) 552-
3272; fax (513) 552-3329. You may review copies of the referenced
service information at the FAA, Engine & Propeller Directorate, 12 New
England Executive Park, Burlington, MA. For information on the
availability of this material at the FAA, call (781) 238-7125.
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: Walter Meibaum, Aerospace Engineer,
Engine Certification Office, FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; telephone (781) 238-
7119; fax (781) 238-7199; e-mail: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an airworthiness directive (AD) that would apply to
the specified products. That NPRM published in the Federal Register on
July 23, 2010 (75 FR 43099). That NPRM proposed to require inspecting
certain S/N GGT shafts, P/N 6068T44P02, for nonconforming land balance-
cuts, and if found, replacing the shaft.
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.
[[Page 70097]]
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed.
Costs of Compliance
We estimate that this AD affects five engines installed on
airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
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Cost on U.S.
Action Labor cost Parts cost Cost per product operators
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Inspect........................ 1 work-hour x $85 per ................. $85 $425
hour = $85..
Replace shaft.................. 1.5 work-hour x $85 $28,633 28,760.50 143,802
per hour = $127.50.
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Total...................... ...................... ................. ................. 144,227
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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
0
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):
2010-23-20 General Electric Company (GE): Amendment 39-16509; Docket
No. FAA-2010-0732; Directorate Identifier 2010-NE-04-AD.
Effective Date
(a) This AD is effective December 22, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to GE CT7-9C and -9C3 turboprop engines with
gas generator turbine (GGT) shafts, part number (P/N) 6068T44P02, that
have a serial number (S/N) listed in Table 1 of this AD, installed.
These engines are installed on, but not limited to, EADS CASA (formerly
Construcciones Aeronauticas, S.A.) CN-235 series airplanes.
Table 1--Affected GGT Shaft S/Ns
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Affected Shaft S/Ns
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GATHHCPC GATHHJR7 GATHHJR9 GATHHKG6
GATHHM9R GATHHWM3 GATHJ4ED GATHJ9FL
GATHJ19J GATHJE8P GATHJWWR GATHK0KM
GATHK2N1 GATHK3M3 GATHK90K GATHK96D
GATHKF9R GATHKH36 GATHKMP7 GATHKRKN
NCE715DA
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Unsafe Condition
(d) This AD results from reports of a manufacturing quality
problem. We are issuing this AD to detect nonconforming GGT shaft land
balance-cuts, which could result in the shaft failing before its
published life limit, and which could result in an uncontained engine
failure and damage to the airplane.
Compliance
(e) You are responsible for having the actions required by this AD
performed at the first shop visit after the effective date of this AD,
or within 5,000 cycles-
[[Page 70098]]
since-new, whichever occurs first, unless the actions have already been
done.
Inspection for Nonconforming Land Balance-Cuts
(f) For CT7-9C and -9C3 engines with a GGT shaft, P/N 6068T44P02,
that has a S/N listed in Table 1 of this AD, installed, inspect the
shaft for nonconforming land balance-cuts. Use the Accomplishment
Instructions 3.A.(1) through 3.A.(4) of GE CT7-TP Alert Service
Bulletin 72-A0501, Revision 01, dated March 3, 2010, to perform the
inspection.
(g) If you find any nonconforming land balance-cuts, remove the
shaft from service.
Alternative Methods of Compliance
(h) The Manager, Engine Certification Office, has the authority to
approve alternative methods of compliance for this AD if requested
using the procedures found in 14 CFR 39.19.
Related Information
(i) For more information about this AD, contact Walter Meibaum,
Aerospace Engineer, Engine Certification Office, FAA, Engine &
Propeller Directorate, 12 New England Executive Park, Burlington, MA
01803; telephone (781) 238-7119; fax (781) 238-7199; e-mail:
[email protected].
Material Incorporated by Reference
(j) You must use GE CT7-TP Alert Service Bulletin 72-A0501,
Revision 01, dated March 3, 2010, 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 GE CT7-TP Alert Service Bulletin 72-A0501, Revision 01,
dated March 3, 2010, under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact General
Electric Company, GE-Aviation, Room 285, 1 Neumann Way, Cincinnati,
Ohio 45215; e-mail [email protected]; telephone (513) 552-3272; fax (513)
552-3329.
(3) You may review copies of the service information at the FAA, 12
New England Executive Park, Burlington, MA. For information on the
availability of this material at the FAA, call (781) 238-7125.
(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 an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Burlington, Massachusetts, on October 29, 2010.
Peter A. White,
Assistant Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2010-28449 Filed 11-16-10; 8:45 am]
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