[Federal Register: July 5, 2006 (Volume 71, Number 128)]
[Rules and Regulations]
[Page 38059-38062]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr05jy06-4]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22524; Directorate Identifier 2005-NM-135-AD;
Amendment 39-14672; AD 2006-14-01]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A330-200, A330-300, A340-
200, and A340-300 Series Airplanes, and Model A340-541 and A340-642
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Model A330-200, A330-300, A340-200, and A340-300 series
airplanes, and Model A340-541 and A340-642 airplanes. This AD requires
inspecting to determine if certain emergency escape slides/slide rafts
(referred to as slide/rafts) are installed in certain crew/passenger
doors; and, if so, performing a one-time inspection to determine if the
electrical harnesses of the slide/rafts are properly routed, and
rerouting the harnesses if necessary. This AD results from report that
a slide/raft failed to deploy properly during a deployment test. We are
issuing this AD to detect and correct improper routing of the
electrical harnesses of certain slide/rafts, which could prevent proper
deployment of the slide/rafts and delay evacuation of passengers and
flightcrew during an emergency.
DATES: This AD becomes effective August 9, 2006.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of August 9,
2006.
ADDRESSES: You may examine the AD docket on the Internet at http://dms.dot.gov
or in person at the Docket
[[Page 38060]]
Management Facility, U.S. Department of Transportation, 400 Seventh
Street, SW., Nassif Building, Room PL-401, Washington, DC.
Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex,
France, for service information identified in this AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
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 street address stated in the
ADDRESSES section.
Discussion
The FAA issued a supplemental notice of proposed rulemaking (NPRM)
to amend 14 CFR part 39 to include an AD that would apply to certain
Airbus Model A330-200, A330-300, A340-200, and A340-300 series
airplanes, and Model A340-541 and A340-642 airplanes. That supplemental
NPRM was published in the Federal Register on March 27, 2006 (71 FR
15073). That supplemental NPRM proposed to require inspecting to
determine if certain emergency escape slides/slide rafts (referred to
as slide/rafts) are installed in certain crew/passenger doors; and, if
so, performing a one-time inspection to determine if the electrical
harnesses of the slide/rafts are properly routed, and rerouting the
harnesses if necessary.
Comments
We provided the public the opportunity to participate in the
development of this AD. We have considered the single comment received.
Request for Clarification of Compliance Time
The Air Transport Association (ATA), on behalf of its member
Northwest Airlines (NWA), requests that the compliance time be
clarified. NWA asserts that some operators may have prior knowledge of
airplanes having slide/rafts with affected part numbers before the
release of this AD. NWA requests that the compliance time be clarified
to ensure that operators having such prior knowledge have the full span
of 1,700 flight hours specified by this AD to accomplish corrective
actions on any affected airplane. Though NWA did not specifically make
such a statement, it appears that NWA is concerned that such prior
knowledge might require immediate grounding of some airplanes because
of the ``before further flight'' clause of the NPRM.
We partially agree. For any AD, compliance times are mandated
during which operators are responsible for accomplishing the
requirements of an AD. For example, operators may perform an inspection
or, as allowed by this AD, review the maintenance records to comply
with the AD. ``Compliance time'' specifies a period of time during
which operators may determine the best time to accomplish the
inspection, and we have no knowledge of individual operator inspection
or review schedules within the compliance time limits. However, we
acknowledge the concern of NWA and have determined that, in this case,
``before further flight'' is not needed to ensure an acceptable level
of safety, provided that corrective actions are accomplished within the
specified compliance time. Therefore, we have revised paragraphs
(f)(1)(ii) and (f)(2)(ii) of the AD to read ``within 1,700 flight hours
after the effective date of this AD.''
Conclusion
We have carefully reviewed the available data, including the
comment received, and determined that air safety and the public
interest require adopting the AD with the change described previously.
We have determined that this change will neither increase the economic
burden on any operator nor increase the scope of the AD.
Costs of Compliance
This AD will affect about 27 airplanes of U.S. registry. The
required actions will take about 3 work hours per airplane, at an
average labor rate of $65 per work hour. Based on these figures, the
estimated cost of the AD for U.S. operators is $5,265 or $195 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 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); 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 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, 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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-14-01 Airbus: Amendment 39-14672. Docket No. FAA-2005-22524;
Directorate Identifier 2005-NM-135-AD.
[[Page 38061]]
Effective Date
(a) This AD becomes effective August 9, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model A330-201, -202, -203, -
223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343
airplanes; Model A340-211, -212, -213, -311, -312, and -313
airplanes; and Model A340-541 and -642 airplanes; certificated in
any category.
Unsafe Condition
(d) This AD results from a report that an emergency escape
slide/slide raft (referred to hereafter as a ``slide/raft'') failed
to deploy properly during a deployment test. We are issuing this AD
to detect and correct improper routing of the electrical harnesses
of certain slide/rafts, which could prevent proper deployment of the
slide/raft and delay evacuation of passengers and flightcrew during
an emergency.
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.
Inspections and Corrective Actions
(f) Within 1,700 flight hours after the effective date of this
AD: Inspect certain crew/passenger doors as required by paragraph
(f)(1) or (f)(2), as applicable, of this AD to determine if slide/
rafts having certain part numbers (P/Ns) are installed. A review of
airplane maintenance records is acceptable in lieu of this
inspection if the presence of the subject slide/rafts can be
conclusively determined from that review.
(1) For Model A330-201, -202, -203, -223, -243, -301, -302, -
303, -321, -322, -323, -341, -342, and -343 airplanes and Model
A340-211, -212, -213, -311, -312, and -313 airplanes: On both right-
and left-hand sides, inspect to determine the P/N of the slide/rafts
of crew/passenger doors 1 and 4, and--only if it is a type 1 door--
crew/passenger door 3. If crew/passenger door 3 is not a type 1
door, it is not subject to any requirement of this AD.
(i) If a slide/raft does not have P/N 7A1508-( ) or 7A1509-( ),
no further action is required for that slide/raft by this paragraph.
(ii) If a slide/raft has P/N 7A1508-( ) or 7A1509-( ), within
1,700 flight hours after the effective date of this AD, perform a
general visual inspection of the electrical harness of that slide/
raft and reroute the harness, as applicable, in accordance with
paragraphs 4.2 through 4.2.4 of Airbus All Operators Telex (AOT)
A330-25A3272, Revision 02; or Airbus AOT A340-25A4259, Revision 02,
both dated June 1, 2005, as applicable.
(2) For Model A340-541 and -642 airplanes: On both right- and
left-hand sides, inspect to determine the P/N of the slide/rafts of
crew/passenger doors 1 and 4.
(i) If a slide/raft does not have P/N 7A1508-( ), no further
action is required for that slide/raft by this paragraph.
(ii) If a slide/raft has P/N 7A1508-( ), within 1,700 flight
hours after the effective date of this AD, perform a general visual
inspection of the electrical harness of that slide/raft and reroute
the harness, as applicable, in accordance with paragraphs 4.2
through 4.2.4 of Airbus AOT A340-25A5091, Revision 02, dated June 1,
2005.
Note 1: For the purposes of this AD, a general visual inspection
is: ``A visual examination of an interior or exterior area,
installation, or assembly to detect obvious damage, failure, or
irregularity. This level of inspection is made from within touching
distance unless otherwise specified. A mirror may be necessary to
ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
droplight and may require removal or opening of access panels or
doors. Stands, ladders, or platforms may be required to gain
proximity to the area being checked.''
Actions Accomplished According to Previous Issues of AOTs
(g) Actions accomplished before the effective date of this AD in
accordance with the Airbus AOTs listed in Table 1 of this AD, as
applicable, are considered acceptable for compliance with the
corresponding actions specified in paragraph (f) of this AD.
Table 1.--Previous Issues of AOTs
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Airbus AOT Revision level Date
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A330-25A3272 \1\............ Original............ March 17, 2005.
A330-25A3272-2005 \1\....... 01.................. March 24, 2005.
A340-25A4259 \2\............ Original............ March 17, 2005.
A340-25A4259-2005 \2\....... 01.................. March 24, 2005.
A340-25A5091 \3\............ Original............ March 17, 2005.
A340-25A5091-2005 \3\....... 01.................. March 24, 2005.
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\1\ For Model A330-200 and -300 series airplanes.
\2\ For Model A340-200 and -300 series airplanes.
\3\ For Model A340-541 and -642 airplanes.
Parts Installation
(h) After the effective date of this AD, no person may install
any slide/raft having P/N 7A1508-( ) or 7A1509-( ) on any airplane
unless the electrical harness of that slide/raft is determined to be
properly routed in accordance with the requirements of this AD.
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 14 CFR
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-2005-077, dated May 11,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(k) You must use the service information specified in Table 2 of
this AD, as applicable, to perform the actions that are required by
this AD, unless the AD specifies otherwise.
Table 2.--Material Incorporated by Reference
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Airbus All Operators Telex Revision level Date
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A330-25A3272................ 02.................. June 1, 2005.
A340-25A4259................ 02.................. June 1, 2005.
A340-25A5091................ 02.................. June 1, 2005.
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[[Page 38062]]
The Director of the Federal Register approved the incorporation
by reference of these documents in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. Contact Airbus, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France, for a copy of this service information.
You may review copies at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Room PL-401,
Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov
; or at the National Archives and Records Administration
(NARA). For information on the availability of this material at the
NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
.
Issued in Renton, Washington, on June 23, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-5944 Filed 7-3-06; 8:45 am]
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