[Federal Register Volume 76, Number 74 (Monday, April 18, 2011)]
[Proposed Rules]
[Pages 21675-21677]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-9258]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1270; Directorate Identifier 2001-NE-50-AD]
RIN 2120-AA64
Airworthiness Directives; Dowty Propellers Type R321/4-82-F/8,
R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 Propeller Assemblies
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to revise an existing airworthiness directive (AD)
that applies to the products listed above. The existing AD currently
requires initial and repetitive ultrasonic inspections of propeller
hubs, part number (P/N) 660709201. Since we issued that AD, Dowty
Propellers introduced a new hub assembly P/N. This proposed AD would
revise that AD by introducing as an optional terminating action for the
initial and repetitive ultrasonic inspections of that AD, replacement
of propeller hub P/N 660709201 with a new propeller hub, P/N 660717226.
We are proposing this AD to prevent that same propeller hub failure due
to cracks in the hub, which could result in loss of control of the
airplane, and to introduce an optional terminating action.
DATES: We must receive comments on this proposed AD by June 2, 2011.
ADDRESSES: You may send comments by any of the following methods:
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: 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 AD, contact Dowty
Propellers, Anson Business Park, Cheltenham Road East, Gloucester GL
29QN, UK; telephone: 44 (0) 1452 716000; fax: 44 (0) 1452 716001. 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 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: Michael Schwetz, Aerospace Engineer,
Boston Aircraft Certification Office, FAA, 12 New England Executive
Park, Burlington, MA 01803; phone: 781-238-7761; fax: 781-238-7170; e-
mail: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2010-1270;
Directorate Identifier 2001-NE-50-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
On December 2, 2005, we issued AD 2005-25-10, Amendment 39-14403
(70 FR 73364, December 12, 2005), for Dowty Propellers type R321/4-82-
F/8, R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 propeller
assemblies. That AD requires initial and repetitive ultrasonic
inspections of propeller hubs, P/N 660709201. That AD resulted from a
report of a hub separation on a CASA 212 airplane, and mandatory
continuing airworthiness information (MCAI) issued by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. We issued that AD to prevent
propeller hub failure due to cracks in the hub, which could result in
loss of control of the airplane.
Actions Since Existing AD Was Issued
Since we issued AD 2005-25-10, the European Aviation Safety Agency
(EASA) has issued AD 2010-0196R1, dated November 12, 2010, which
requires initial and repetitive ultrasonic inspections of propeller
hubs, and introduces a new P/N propeller hub as optional terminating
action to the inspections.
Relevant Service Information
We have reviewed the technical contents of Dowty Propellers Alert
Service Bulletin (SB) No. 61-1119, Revision 5, dated July 1, 2009,
Alert SB No. 61-1124, Revision 2, dated August 25, 2010, Alert SB No.
61-1125, Revision 2, dated August 25, 2010, and Alert SB No. 61-1126,
Revision 2, dated August 25, 2010. The SBs describe procedures for
initial and repetitive ultrasonic inspections of the rear wall of the
rear half of the propeller hub for cracks on types R334/4-82-F/13,
R333/4-82-F/12, R321/4-82-F/8, and R324/4-82-F/9 propeller assemblies,
respectively. The SBs also introduce new hub assembly P/N 660717226, as
optional terminating action for the initial and repetitive inspections.
EASA
[[Page 21676]]
classified the service information as mandatory and issued AD 2010-
0196R1, dated November 12, 2010, to ensure the airworthiness of these
propeller assemblies in Europe.
Bilateral Agreement Information
These propeller assemblies are manufactured in the United Kingdom,
and are type certificated for operation in the United States under the
provisions of Section 21.29 of the Federal Aviation Regulations (14 CFR
21.29) and the applicable bilateral airworthiness agreement. Under this
bilateral airworthiness agreement, EASA kept us informed of the
situation described above. We have examined the findings of the EASA,
reviewed all available information, and determined that AD action is
necessary for products of these type designs that are certificated for
operation in the United States.
FAA's Determination
We are proposing this AD revision because we evaluated all the
relevant information and determined the unsafe condition described
previously is likely to exist or develop in other products of these
same type designs.
Proposed AD Requirements
This proposed AD would retain the inspection requirements of AD
2005-25-10. This proposed AD would introduce the installation of a new
P/N hub assembly as optional terminating action to the inspections.
This proposed AD would also eliminate the inspection reporting
requirements, since we have already collected sufficient data.
Differences Between the Proposed AD and the Service Information or MCAI
Although Appendix A of Alert SB No. 61-1119, Revision 5, dated July
1, 2009, requires reporting the inspection data to Dowty Propellers,
this proposed AD would not require any reporting.
Although the MCAI uses initial inspection compliance times of 20
days/60 days, we removed them from the proposed AD, since the unsafe
condition is not related to corrosion.
Costs of Compliance
We estimate that this proposed AD would affect 132 propellers
installed on airplanes of U.S. registry. We also estimate that it would
take about 0.5 work-hour per propeller to perform the proposed
inspection and about 1 hour to replace a propeller hub. The average
labor rate is $85 per work-hour. Required parts would cost about
$19,500 per engine. Based on these figures, we estimate the total cost
of the proposed AD to U.S. operators to be $2,590,830.
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 have 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 that the 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 removing airworthiness directive
(AD) 2005-25-10, Amendment 39-14403 (70 FR 73364, December 12, 2005),
and adding the following new AD:
Dowty Propellers (formerly Dowty Aerospace; Dowty Rotol Limited; and
Dowty Rotol): Docket No. FAA-2010-1270; Directorate Identifier 2001-
NE-50-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by June 2,
2011.
Affected ADs
(b) This AD revises AD 2005-25-10, Amendment 39-14403.
Applicability
(c) This AD applies to Dowty Propellers Type R321/4-82-F/8,
R324/4-82-F/9, R333/4-82-F/12, and R334/4-82-F/13 propeller
assemblies with propeller hubs part number (P/N) 660709201.
Unsafe Condition
(d) This AD was prompted by the need to introduce an optional
terminating action for the repetitive inspections. We are issuing
this AD to prevent propeller hub failure due to cracks in the hub,
which could result in loss of control of the airplane, and to
introduce an optional terminating action.
Compliance
(e) Comply with this AD within the compliance times specified,
unless already done.
Initial Ultrasonic Inspections
(f) Perform an initial ultrasonic inspection of the rear wall of
the rear half of the propeller hub for cracks within the compliance
time specified in Table 1 of this AD. Use Appendix A or Appendix D
of the applicable Dowty Alert Service Bulletin (SB) listed in Table
1 of this AD to do the inspection.
[[Page 21677]]
Table 1--Applicable Alert SB for Propeller Type
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Initial inspection Repeat inspection
Propeller assembly type within within Applicable SB
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(1) R334/4-82-F/13................... 10 flight hours (FH) 300 FH time-since-last- Alert SB No. 61-1119,
time-in-service (TIS) inspection (TSLI) or Revision 5, dated July
after the effective 300 flight cycles- 1, 2009.
date of this AD. since-last inspection,
whichever occurs
sooner.
(2) R321/4-82-F/8.................... 50 FH TIS after the 1,000 FH TSLI.......... Alert SB No. 61-1125,
effective date of this Revision 2, dated
AD. August 25, 2010.
(3) R324/4-82-F/9.................... 50 FH TIS after the 1,000 FH TSLI.......... Alert SB No. 61-1126,
effective date of this Revision 2, dated
AD. August 25, 2010.
(4) R333/4-82-F/12................... 50 FH TIS after the 1,000 FH TSLI.......... Alert SB No. 61-1124,
effective date of this Revision 2, dated
AD. August 25, 2010.
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(g) For hubs and propellers in storage, perform an initial
ultrasonic inspection of the rear wall of the rear half of the
propeller hub for cracks, before placing in service. Use Appendix A
or Appendix D of the applicable Dowty Alert SB listed in Table 1 of
this AD to do the inspection.
Initial Inspection--Previous Credit
(h) Propeller hubs, P/N 660709201, that previously passed
inspection using Dowty Alert SBs listed in Table 1 of this AD or an
earlier issue of those SBs, have satisfied the initial inspection
requirements of this AD. However, you must comply with the
repetitive inspection requirements found in this AD.
Repetitive Ultrasonic Inspections
(i) Thereafter, perform a repetitive ultrasonic inspection of
the rear wall of the rear half of the propeller hub for cracks
within the compliance time specified in Table 1 of this AD. Use
Appendix A or Appendix D of the applicable Dowty Alert SB listed in
Table 1 of this AD to do the inspection.
Optional Terminating Action
(j) As optional terminating action for the repetitive
inspections required by this AD, replace propeller hub, P/N
660709201, with a new propeller hub, P/N 660717226.
Alternative Methods of Compliance (AMOCs)
(k) The Manager, Boston Certification Office, has the authority
to approve AMOCs for this AD if requested using the procedures found
in 14 CFR 39.19.
Related Information
(l) For more information about this AD, contact Michael Schwetz,
Aerospace Engineer, Boston Aircraft Certification Office, FAA, 12
New England Executive Park, Burlington, MA 01803; phone: 781-238-
7761; fax: 781-238-7170; e-mail: [email protected].
(m) European Aviation Safety Agency 2010-0196R1, dated November
12, 2010, pertains to the subject of this AD.
(n) For service information identified in this AD, contact Dowty
Propellers, Anson Business Park, Cheltenham Road East, Gloucester GL
29QN, UK; telephone: 44 (0) 1452 716000; fax: 44 (0) 1452 716001.
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.
Issued in Burlington, Massachusetts, on April 7, 2011.
Peter A. White,
Acting Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2011-9258 Filed 4-15-11; 8:45 am]
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