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Docket ID: [Docket No. FAA-2008-0121; Directorate Identifier 2007-NM-277-AD; Amendment 39-15363; AD 2008-03-13]
RIN ID: RIN 2120-AA64
SUBJECT CATEGORY: Airworthiness Directives; ATR Model ATR42-500 Airplanes
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of February 20, 2008.
We must receive comments on this AD by March 6, 2008.
DOCUMENT SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain ATR Model ATR42500 series airplanes. This AD requires removing metallized polyethylene terephtalate (MPET) insulation blankets installed on the left and the right sides of the airplane over frame 24 between stringers 5 and 14. This AD results from reports indicating that burnt spots were found on the MPET insulation blankets installed over frame 24. The actions specified by this AD are intended to ensure that MPET insulation blankets are removed over frame 24. Such MPET insulation blankets, if not removed, could propagate a small fire that is the result of an electrical arc and could lead to a much larger fire.
SUMMARY: ATR Model ATR42-500 Airplanes,
The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, notified us that an unsafe condition may exist on certain ATR Model ATR42500 series airplanes. The EASA advises that there have been reports of two in service aircraft where burnt spots were found on the insulation blankets installed over frame 24. Investigations concluded that due to the presence of the bleed air duct, installation of the thermal acoustical insulation blankets having a metallized polyethylene terephtalate (MPET) made the covering (also known as Mylar \TM\) at this location unsafe. Such MPET insulation blankets, if not removed, could propagate a small fire that is the result of an electrical arc and could lead to a much larger fire. This action is intended to address the identified unsafe condition.
ATR has issued Service Bulletin ATR42250155, dated April 10, 2007. The service bulletin describes procedures for removing the MPET insulation blankets installed on the left and the right sides of the airplane over frame 24 between stringers 5 and 14. Accomplishing the actions specified in the service information is intended to adequately address the unsafe condition. The EASA mandated the service information and issued emergency airworthiness directive 20070106E, dated April 18, 2007, to ensure the continued airworthiness of these airplanes in the European Union.
These airplanes 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 products of this type design that are certificated for operation in the United States.
Therefore, we are issuing this AD to ensure that MPET insulation blankets are removed over frame 24. Such MPET insulation blankets, if not removed, could propagate a small fire that is the result of an electrical arc and could lead to a much larger fire. This AD requires accomplishing the actions specified in the service information described previously.
None of the airplanes affected by this action are on the U.S. Register. All airplanes affected by this AD are currently operated by nonU.S. operators under foreign registry; therefore, they are not directly affected by this AD action. However, we consider this AD necessary to ensure that the unsafe condition is addressed if any affected airplane is imported and placed on the U.S. Register in the future.
If an affected airplane is imported and placed on the U.S. Register in the future, the required action would take about 6 work hours per airplane, at an average labor rate of $80 per work hour. Based on these figures, the estimated cost of the AD would be $480 per airplane. FAA's Determination of the Effective Date
No airplane affected by this AD is currently on the U.S. Register. [[Page 6595]]
Therefore, providing notice and opportunity for public comment is
unnecessary before this AD is issued, and this AD may be made effective
in less than 30 days after it is published in the Federal Register. Comments Invited
This AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA20080121; Directorate Identifier 2007NM277AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this 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 AD.
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.
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 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
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS 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):
20080313 ATRGIE Avions de Transport R[eacute]gional (Formerly Aerospatiale): Amendment 3915363. Docket No. FAA20080121;
Directorate Identifier 2007NM277AD.
Effective Date
(a) This AD becomes effective February 20, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to ATR Model ATR42500 series airplanes,
certificated in any category; except for airplanes modified in
accordance with ATR modification numbers 05117, 05322, and 05791, or ATR Service Bulletin ATR42251034, dated January 24, 2002.
Unsafe Condition
(d) This AD results from reports indicating that burnt spots
were found on the metallized polyethylene terephtalate (MPET)
insulation blankets installed over frame 24. We are issuing this AD
to ensure that MPET insulation blankets are removed over frame 24.
Such MPET insulation blankets, if not removed, could propagate a
small fire that is the result of an electrical arc and could lead to a much larger fire.
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.
Removal of Installation Blankets
(f) Within 15 days after the effective date of this AD, remove
the MPET insulation blankets installed on the left and the right
sides of the airplane over frame 24 between stringers 5 and 14, in
accordance with the Accomplishment Instructions of ATR Service Bulletin ATR42250155, dated April 10, 2007.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, International Branch, ANM116, 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) To request a different method of compliance or a different
compliance time for this AD, follow the procedures in 14 CFR 39.19.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your appropriate principal inspector (PI) in the FAA
Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.
Related Information
(h) EASA emergency airworthiness directive 20070106E, dated April 18, 2007, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use ATR Service Bulletin ATR42250155, dated April
10, 2007, to perform the actions that are required by this AD,
unless the AD specifies otherwise. The Director of the Federal
Register approved the incorporation by reference of this document in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact ATR, 316
Route de Bayonne, 31060 Toulouse, Cedex 03, France, for a copy of
this service information. You may review copies at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington; or at the National Archives and Records Administration (NARA).
For information on the availability of this material at NARA, call 2027416030, or go to: http://www.archives.gov/federalregister/cfr/ibrlocations.html .
Issued in Renton, Washington, on January 24, 2008. Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E82004 Filed 2408; 8:45 am]
BILLING CODE 491013P
FOR FURTHER INFORMATION CONTACT Tom Rodriguez, Aerospace Engineer, International Branch, ANM116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 980573356; telephone (425) 2271137; fax (425) 2271149.
14 CFR Part 39 40 CFR Part 52 14 CFR Part 71 33 CFR Part 165 50 CFR Part 679 26 CFR Part 1 40 CFR Part 180 47 CFR Part 73 50 CFR Part 17 33 CFR Part 117 44 CFR Part 67 50 CFR Part 648 14 CFR Part 97 33 CFR Part 100 40 CFR Part 63 26 CFR Part 301 50 CFR Part 622 39 CFR Part 111 40 CFR Part 300 44 CFR Part 65 50 CFR Part 660 40 CFR Part 271 40 CFR Parts 52 and 81 47 CFR Part 64 50 CFR Part 665 49 CFR Part 571 44 CFR Part 64 14 CFR Part 23 47 CFR Part 76 50 CFR Part 229