[Federal Register: January 19, 2006 (Volume 71, Number 12)]
[Proposed Rules]
[Page 3021-3023]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr19ja06-17]
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Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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[[Page 3021]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-23633; Directorate Identifier 2005-NM-242-AD]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A318-100 and A319-100
Series Airplanes; Model A320-111 Airplanes; Model A320-200, A321-200,
A330-200, A330-300, A340-200, and A340-300 Series Airplanes; Model
A340-541 Airplanes; and Model A340-642 Airplanes; Equipped With Certain
Sogerma-Services Powered Seats
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Airbus transport category airplanes. This proposed AD would
require inspecting to determine if a certain actuator is installed in
the pilot's or co-pilot's seat, and doing applicable corrective actions
if necessary. For certain actuators, the proposed AD also would require
replacing rotors on both vertical and horizontal movements with new
rotors, and replacing the clutch cap with a new cap. This proposed AD
results from a report of heavy wear at the driving gear of the rotor
shaft end of the electrical driven motor on certain actuators of the
pilot's and co-pilot's seats. We are proposing this AD to prevent
uncommanded movement of the pilot's or co-pilot's seat during takeoff
or landing, which could result in interference with the operation of
the airplane and consequent temporary loss of airplane control.
DATES: We must receive comments on this proposed AD by February 21,
2006.
ADDRESSES: Use one of the following addresses to submit comments on
this proposed AD.
DOT Docket Web site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to http://www.regulations.gov
and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility, U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Contact Sogerma-Services, 109-17303 Rochefort, Cedex, France; and
Messier-Bugatti, 45 Avenue Victor Hugo, 93538 Aubervilleirs, Cedex,
France; for service information identified in this proposed AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to submit any relevant written data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed in the ADDRESSES section. Include the docket number ``FAA-2006-
23633; Directorate Identifier 2005-NM-242-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the proposed AD. We will
consider all comments received by the closing date and may amend the
proposed AD in light of those comments.
We will post all comments we receive, without change, to http://dms.dot.gov
, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this proposed AD. Using the search function of
that Web site, anyone can find and read the comments in any of our
dockets, including the name of the individual who sent the comment (or
signed the comment on behalf of an association, business, labor union,
etc.). You may review the DOT's complete Privacy Act Statement in the
Federal Register published on April 11, 2000 (65 FR 19477-78), or you
may visit http://dms.dot.gov.
Examining the Docket
You may examine the AD docket on the Internet at http://dms.dot.gov
, or in person at the Docket Management Facility office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the Docket Management System
receives them.
Discussion
The Direction G[eacute]n[eacute]rale de l'Aviation Civile (DGAC),
which is the airworthiness authority for France, notified us that an
unsafe condition may exist on certain Airbus Model A318-100 and A319-
100 series airplanes; Model A320-111 airplanes; Model A320-200, A321-
200, A330-200, A330-300, A340-200, and A340-300 series airplanes; Model
A340-541 airplanes; and Model A340-642 airplanes; equipped with certain
Sogerma-Services pilot's and co-pilot's seats. The DGAC advises that,
during overhaul of the pilot's and co-pilot's seats, repair stations
found heavy wear at the driving gear of the rotor shaft end of the
electrical driven motor on certain actuators. The electrical driven
motor controls the horizontal and vertical movements of the seats.
Investigation revealed that a manufacturing process error resulted in a
batch of defective rotor shafts on certain actuators. This condition,
if not corrected, could result in uncommanded movement of the pilot's
or co-pilot's seat during takeoff or landing, which could result in
interference with the operation of the airplane and consequent
temporary loss of airplane control.
Relevant Service Information
Sogerma-Services has issued Service Bulletin TAAI1-25-617, dated
February 1, 2005. The service bulletin describes procedures for
inspecting to determine if a certain actuator is installed in the
pilot's or co-pilot's seat, and doing applicable corrective actions if
[[Page 3022]]
necessary. The corrective actions include:
Replacing certain actuators with new actuators;
Installing a new identification label for any replaced
actuator; and
Installing a new amendment label and writing the new
amendment on it.
Messier-Bugatti has issued Service Bulletins 4136290004-25-05 and
4136290005-25-02, both dated April 2005. For certain airplanes, the
service bulletins describe procedures for replacing rotors on both
vertical and horizontal movements with new rotors, and replacing the
clutch cap with a new cap.
Accomplishing the actions specified in the service information is
intended to adequately address the unsafe condition. The DGAC mandated
the service information and issued French airworthiness directive F-
2005-164, dated September 28, 2005, to ensure the continued
airworthiness of these airplanes in France.
FAA's Determination and Requirements of the Proposed AD
These airplane models are manufactured in France 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. Pursuant to this
bilateral airworthiness agreement, the DGAC has kept the FAA informed
of the situation described above. We have examined the DGAC's findings,
evaluated all pertinent information, and determined that we need to
issue an AD for airplanes of this type design that are certificated for
operation in the United States.
Therefore, we are proposing this AD, which would require
accomplishing the actions specified in the service information
described previously.
Costs of Compliance
This proposed AD would affect about 743 airplanes of U.S. registry.
The proposed inspection would take about 1 work hour per airplane, at
an average labor rate of $65 per work hour. Based on these figures, the
estimated cost of the proposed AD for U.S. operators is $48,295, or $65
per airplane.
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); 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 proposed AD and placed it in the AD docket. See the
ADDRESSES section for a location to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
Airbus: Docket No. FAA-2006-23633; Directorate Identifier 2005-NM-
242-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by February
21, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the airplanes identified in table 1 of
this AD, certificated in any category; equipped with any Sogerma-
Services pilot or co-pilot seat identified in Sogerma-Services
Service Bulletin TAAI1-25-617, dated February 1, 2005, excluding any
seat having part number (P/N) TAAI3-03PE00-01, TAAI3-03PE01-01,
TAAI3-03CE00-01, and TAAI3-03CE01-01, with a serial number (S/N)
higher than 791, on which the actuator has been replaced after the
date of issuance of the original standard airworthiness certificate
or date of issuance of the original export certificate of
airworthiness.
Table 1.--Applicability
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Airbus model
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(1) A318-111 and -112 airplanes.
(2) A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) A320-111 airplanes.
(4) A320-211, -212, -214, -231, -232, and -233 airplanes.
(5) A321-211 and -231 airplanes.
(6) A330-201, -202, -203, -223, and -243 airplanes.
(7) A330-301, -321, -322, -323, -341, -342, and -343 airplanes.
(8) A340-211, -212, and -213 airplanes.
(9) A340-311, -312, and -313 airplanes.
(10) A340-541 airplanes.
(11) A340-642 airplanes.
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Unsafe Condition
(d) This AD results from a report of heavy wear at the driving
gear of the rotor shaft end of the electrical driven motor on
certain actuators of the pilot's and co-pilot's seats. We are
issuing this AD to prevent uncommanded movement of the pilot's or
co-pilot's seat during takeoff or landing, which could result in
interference with the operation of the airplane and consequent
temporary loss of airplane control.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Inspection for the P/N of the Actuator
(f) Within 56 months after the effective date of this AD,
inspect to determine if an actuator identified in table 2 of this AD
is installed in the pilot's or co-pilot's seat, in accordance with
paragraph D., ``DESCRIPTION'' of Sogerma-Services Service Bulletin
TAAI1-25-617, dated February 1, 2005. If any actuator identified in
table 2 of this AD is found installed, within 56 months after the
effective date of this AD, do the applicable corrective actions in
accordance with paragraph 3., ``OPERATING INSTRUCTIONS,'' of the
service bulletin.
[[Page 3023]]
Table 2.--Affected Actuators
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Manufacturer Actuator P/N
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(1) Messier-Bugatti................................... 4136290004
(2) Messier-Bugatti................................... 4136290005
(3) Aviac............................................. 6147-6
(4) Artus............................................. AD8552502-1
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Concurrent Replacements
(g) For Messier-Bugatti actuators identified in table 2 of this
AD: Concurrently with the applicable corrective action required by
paragraph (f) of this AD, replace the rotors on both vertical and
horizontal movements with new rotors, and replace the clutch cap
with a new cap, in accordance with Messier-Bugatti Service Bulletin
4136290004-25-05 or 4136290005-25-02, both dated April 2005, as
applicable.
Parts Installation
(h) After the effective date of this AD, no actuator identified
in table 2 of this AD may be installed on any airplane.
Alternative Methods of Compliance (AMOCs)
(i)(1) The Manager, International Branch, ANM-116, Transport
Airplane Directorate, FAA, has the authority to approve AMOCs for
this AD, if requested in accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(j) French airworthiness directive F-2005-164, issued September
28, 2005, also addresses the subject of this AD.
Issued in Renton, Washington, on January 10, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-532 Filed 1-18-06; 8:45 am]
BILLING CODE 4910-13-P