[Federal Register Volume 75, Number 223 (Friday, November 19, 2010)]
[Rules and Regulations]
[Pages 70812-70814]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-29201]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1136; Directorate Identifier 2010-SW-069-AD;
Amendment 39-16522; AD 2010-24-04]
RIN 2120-AA64
Airworthiness Directives; Sikorsky Aircraft Corporation
(Sikorsky) Model S-92A Helicopters
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
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SUMMARY: This amendment supersedes an existing airworthiness directive
(AD) for Sikorsky Model S-92A helicopters that currently requires
cleaning and inspecting each main gearbox (MGB) assembly mounting foot
pad and rib for a crack and corrosion. If you do not find a crack, the
AD requires applying a corrosion preventive compound. If you find a
crack, the AD requires replacing the MGB before further flight. If you
find corrosion, bubbled paint, or paint discoloration, the AD requires
you to repair the MGB before further flight. This amendment retains the
current requirements and expands the applicability to include another
part-numbered MGB assembly and MGB housing. This amendment is prompted
by the need to expand the applicability to include another MGB assembly
and MGB housing that is prone to the same cracks and corrosion as the
MGB listed in the current AD. The actions specified by this AD are
intended to prevent the loss of the MGB and subsequent loss of control
of the helicopter.
DATES: Effective December 6, 2010.
The incorporation by reference of certain publications listed in
the regulations was approved previously by the Director of the Federal
Register as of February 19, 2010 (75 FR 5684, February 4, 2010).
We must receive comments on this AD by January 18, 2011.
ADDRESSES: Use one of the following addresses to comment on this AD.
Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
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.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
You may get the service information identified in this AD from
Sikorsky Aircraft Corporation, Attn: Manager, Commercial Technical
Support, mailstop s581a, 6900 Main Street, Stratford, CT, telephone
(203) 383-4866, e-mail address [email protected], or at http://www.sikorsky.com.
Examining the Docket: You may examine the docket that contains the
AD, any comments, and other information 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 Docket Operations office (telephone (800) 647-
[[Page 70813]]
5527) is located in Room W12-140 on the ground floor of the West
Building at the street address stated in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Michael Schwetz, Aviation Safety
Engineer, Boston Aircraft Certification Office, 12 New England
Executive Park, Burlington, MA 01803, telephone (781) 238-7761, fax
(781) 238-7170.
SUPPLEMENTARY INFORMATION: On December 18, 2009, we issued AD 2009-23-
51, Amendment 39-16190 (75 FR 5684, February 4, 2010), to require
cleaning and inspecting each MGB assembly mounting foot pad and rib for
a crack and corrosion. If you do not find a crack, the AD requires
applying a corrosion preventive compound. If you find a crack, the AD
requires replacing the MGB before further flight. If you find
corrosion, bubbled paint, or paint discoloration, the AD requires you
to repair the MGB before further flight. That action was prompted by
reports of cracks in the MGB mounting foot pads and foot ribs. That
condition, if not corrected, could result in loss of the MGB and
subsequent loss of control of the helicopter.
Since issuing that AD, we have determined the need to expand the
applicability to include another MGB assembly and MBG housing, which
introduced a six-stud attachment for the oil filter bowl and more edge
distance on the right and left foot pads. This new housing
configuration is added to the applicability of this AD because it is
prone to the same cracks as the MGB listed in the current AD. The
manufacturer is still investigating the root cause of these cracks.
Contributing factors may include corrosion and the bushing press fit in
the mounting foot bolt hole. The actions specified in this AD are
interim actions until the root cause of the cracking is determined.
After that determination, we anticipate further rulemaking.
Since an unsafe condition has been identified that is likely to
exist or develop on other Sikorsky S-92A helicopters of the same type
design, this AD supersedes AD 2009-23-51 to retain the same
requirements and to expand the applicability to include the MGB
assembly, part number (P/N) 92351-15000-044, with a MGB housing, P/N
92351-15110-046. This AD is being issued to prevent the loss of the MGB
and subsequent loss of control of the helicopter. This AD requires an
initial and at 10-hour time-in-service (TIS) intervals, cleaning and
inspecting each MGB assembly mounting foot pad and rib for a crack and
corrosion. If you do not find a crack, this AD requires applying a
corrosion preventive compound. If you find a crack, this AD requires
replacing the MGB before further flight. If you find corrosion, bubbled
paint, or paint discoloration, this AD requires you to repair the MGB
before further flight.
The short compliance time is required because the previously
described critical unsafe condition can adversely affect the structural
integrity and controllability of the helicopter. Therefore, because of
the short compliance time, this AD must be issued immediately.
Since a situation exists that requires the immediate adoption of
this regulation, it is found that notice and opportunity for prior
public comment hereon are impracticable, and that good cause exists for
making this amendment effective in less than 30 days.
We estimate this AD will affect 44 helicopters of U.S. registry,
and inspecting the MGB assembly mounting foot pads and foot ribs for
corrosion or a crack will take about:
2 work hours to do the visual inspection, assuming 2200
(50 inspections X 44 helicopters) inspections per year for commercial
and part 91 operators; and
24 work hours to remove and replace an MGB.
The average labor rate is $85 per work hour and required parts will
cost about $590,000 per helicopter. Based on these figures, we estimate
the total cost impact of the AD on U.S. operators to be $26,423,760
assuming all 44 helicopters will require an MGB replacement.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and an opportunity for
public comment. We invite you to send any written relevant data, views,
or arguments regarding this AD. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2010-1136;
Directorate Identifier 2010-SW-069-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD. We will consider
all comments received by the closing date and may amend the AD in light
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 concerning this AD. Using the search function of the docket Web
site, you can find and read the comments to any of our dockets,
including the name of the individual who sent the comment. You may
review the DOT's complete Privacy Act Statement in the Federal Register
published on April 11, 2000 (65 FR 19477-78).
Regulatory Findings
We have 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 that the 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); 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 an economic evaluation of the estimated costs to comply
with this AD. See the AD docket to examine the economic evaluation.
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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
[[Page 70814]]
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 removing Airworthiness Directive (AD)
2009-23-51, Amendment 39-16190 (75 FR 5684, dated February 4, 2010),
and by adding a new AD to read as follows:
2010-24-04 Sikorsky Aircraft Corporation: Amendment 39-16522; Docket
No. FAA-2010-1136; Directorate Identifier 2010-SW-069-AD. Supersedes
AD 2009-23-51; Amendment 39-16190; Docket No. FAA-2010-0066;
Directorate Identifier 2009-SW-52-AD.
Applicability: Model S-92A helicopters, with main gearbox (MGB)
assembly, part number (P/N) 92351-15000-042, -043, or -044, with MGB
housing, P/N 92351-15110-042, -043, -044, -045, or -046, installed,
certificated in any category.
Compliance: Required as indicated.
To prevent loss of an MGB and subsequent loss of control of the
helicopter, do the following:
(a) Within 10 hours time-in-service (TIS), unless accomplished
previously, and thereafter at intervals not to exceed 10 hours TIS,
clean and inspect each MGB assembly mounting foot pad and rib for a
crack and corrosion in the area depicted in Figure 1 and as shown in
the examples in Figures 2, 3, and 4 of Sikorsky Alert Service
Bulletin No. 92-63-020, dated September 11, 2009 (ASB). If no crack
is found, apply the corrosion preventive compound to each foot pad
and rib area.
Note 1: When conducting a visual inspection, use a bright, non-
LED light.
(1) If you find a crack, replace the MGB before further flight.
(2) If you find corrosion, bubbled paint, or paint
discoloration, before further flight, repair the affected area.
Note 2: Even though MGB assembly, P/N 92351-15000-044, with MGB
housing, P/N 92351-15110-046, is not included in the ASB, following
the Accomplishment Instructions in the ASB accomplishes the intent
of this AD.
(b) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Contact the Manager, Boston Aircraft Certification Office, ATTN:
Michael Schwetz, Aviation Safety Engineer, 12 New England Executive
Park, Burlington, MA 01803, telephone (781) 238-7761, fax (781) 238-
7170, for information about previously approved alternative methods
of compliance.
(c) The Joint Aircraft System/Component (JASC) Code is 6320:
Main Rotor Gearbox.
(d) Do the inspections by following the specified portions of
Sikorsky Alert Service Bulletin No. 92-63-020, dated September 11,
2009. The Director of the Federal Register approved this
incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51
as of February 19, 2010 (75 FR 5684, February 4, 2010). Copies may
be obtained from Sikorsky Aircraft Corporation, Attn: Manager,
Commercial Technical Support, mailstop s581a, 6900 Main Street,
Stratford, CT, telephone (203) 383-4866, e-mail address
[email protected], or at http://www.sikorsky.com. Copies may
be inspected at the FAA, Office of the Regional Counsel, Southwest
Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas, or 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.
(e) This amendment becomes effective on December 6, 2010.
Issued in Fort Worth, Texas, on November 9, 2010.
Kim Smith,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2010-29201 Filed 11-18-10; 8:45 am]
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