[Federal Register: September 26, 2006 (Volume 71, Number 186)]
[Proposed Rules]
[Page 56054-56056]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr26se06-15]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-25891; Directorate Identifier 2006-NM-186-AD]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A300 and A310 Airplanes;
and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model
C4-605R Variant F Airplanes (Collectively Called A300-600 Series
Airplanes)
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 Model A300 and A310 airplanes; and Model A300 B4-
600, B4-600R, and F4-600R series airplanes, and Model C4-605R Variant F
airplanes (collectively called A300-600 series airplanes). This
proposed AD would require replacing the pressure limiter of the parking
brake system with a new or modified pressure limiter. This proposed AD
results from a report indicating that failure of the parking brake
system occurred on a Model A300-600 airplane. We are proposing this AD
to prevent failure of the parking braking system and interference with
emergency use of the brake pedals, which could lead to airplane
collision with surrounding objects or departure from the runway.
DATES: We must receive comments on this proposed AD by October 26,
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 Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France, for service information identified in this proposed AD.
FOR FURTHER INFORMATION CONTACT: Tom Stafford, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1622; 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-
25891; Directorate Identifier 2006-NM-186-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 DOT's complete Privacy Act Statement in the
Federal Register
[[Page 56055]]
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 European Aviation Safety Agency (EASA), which is the
airworthiness authority for the European Union, notified us that an
unsafe condition may exist on certain Airbus Model A300 and A310
airplanes; and Model A300 B4-600, B4-600R, and F4-600R series
airplanes, and Model C4-605R Variant F airplanes (collectively called
A300-600 series airplanes). The EASA advises it has received a report
indicating that a failure of the parking brake system occurred on a
Model A300-600 airplane. After the airplane had been braked to a halt
with both engines running and the parking brake applied, the airplane
began to move again. As engaging the parking brake inhibits all other
braking modes by design, the flightcrew was unable to stop the airplane
using the brake pedals. Investigation revealed that a wire intended to
reduce the area of one internal port of the parking brake pressure
limiter had broken and caused excess restriction of the port, which
delayed the buildup of parking brake pressure. This condition, if not
corrected, could cause failure of the parking braking system and
interference with emergency use of the brake pedals, which could lead
to airplane collision with surrounding objects or departure from the
runway.
Relevant Service Information
We have reviewed the Airbus service bulletins described in the
following table. The service bulletins describe procedures for
replacing the pressure limiter of the parking brake system with a new
or modified pressure limiter--modification includes removing a certain
wire and installing a new pressure restrictor. Accomplishing the
actions specified in the service information is intended to adequately
address the unsafe condition.
Airbus Service Information
----------------------------------------------------------------------------------------------------------------
For all model Use service bulletin Dated
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A300 airplanes.......................... A300-32-0448............... February 22, 2006.
A300 B4-600, B4-600R, and F4-600R series A300-32-6094............... February 22, 2006.
airplanes.
A310 airplanes.......................... A310-32-2133............... February 22, 2006.
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The EASA mandated the service information and issued airworthiness
directive 2006-0178, dated June 26, 2006, to ensure the continued
airworthiness of these airplanes in the European Union.
The service bulletins refer to Messier--Bugatti Service Bulletin
C24264-32-848, dated February 15, 2006, as an additional source of
service information for modifying the parking brake pressure limiter.
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. As described in FAA
Order 8100.14A, ``Interim Procedures for Working with the European
Community on Airworthiness Certification and Continued Airworthiness,''
dated August 12, 2005, the EASA has kept the FAA informed of the
situation described above. We have examined the EASA'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 229 airplanes of U.S. registry.
The proposed actions would take about 2 work hours per airplane, at an
average labor rate of $80 per work hour. The manufacturer states that
it will supply required parts to the operators at no cost. Based on
these figures, the estimated cost of the proposed AD for U.S. operators
is $36,640, or $160 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.
[[Page 56056]]
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-2006-25891; Directorate Identifier 2006-NM-
186-AD.
Comments Due Date
(a) The FAA must receive comments on this AD action by October
26, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Airbus Model A300 and A310 airplanes; and
Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-
605R, F4-622R, and C4-605R Variant F airplanes; certificated in any
category; except for airplanes on which Airbus Modification 12994
has been embodied in production.
Unsafe Condition
(d) This AD results from a report indicating that failure of the
parking brake system occurred on a Model A300-600 airplane. We are
issuing this AD to prevent failure of the parking braking system and
interference with emergency use of the brake pedals, which could
lead to airplane collision with surrounding objects or departure
from the runway.
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.
Pressure Limiter Replacement
(f) Within 18 months after the effective date of this AD,
replace the pressure limiter of the parking brake system with a new
or modified pressure limiter having part number (P/N) C24264-303 or
C24264004-1, as applicable, in accordance with the Accomplishment
Instructions of the applicable service bulletin specified in Table 1
of this AD.
Table 1.--Airbus Service Information
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Use Airbus
For all model Service Dated
Bulletin
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A300 airplanes.............. A300-32-0448... February 22, 2006.
A300 B4-601, B4-603, B4-620, A300-32-6094... February 22, 2006.
B4-622, B4-605R, B4-622R,
F4-605R, F4-622R, and C4-
605R Variant F airplanes.
A310 airplanes.............. A310-32-2133... February 22, 2006.
------------------------------------------------------------------------
Note 1: The Airbus service bulletins refer to Messier-Bugatti
Service Bulletin C24264-32-848, dated February 15, 2006, as an
additional source of service information for modifying the parking
brake pressure limiter.
Parts Installation
(g) As of the effective date of this AD, no person may install,
on the parking brake system of any airplane, a pressure limiter
having P/N C24264-302 or C24264004.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, International Branch, ANM-116, 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
(i) European Aviation Safety Agency (EASA) airworthiness
directive 2006-0178, dated June 26, 2006, also addresses the subject
of this AD.
Issued in Renton, Washington, on September 14, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-8222 Filed 9-25-06; 8:45 am]
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