Airworthiness Directives; Eurocopter France Model EC 155B and B1 Helicopters, 12998-13000 [06-2357]

Download as PDF 12998 Federal Register / Vol. 71, No. 49 / Tuesday, March 14, 2006 / Rules and Regulations 11. In § 95.4, paragraph (a)(3) is revised to read as follows: I § 95.4 Restrictions on the importation of processed animal protein, offal, tankage, fat, glands, certain tallow other than tallow derivatives, and serum due to bovine spongiform encephalopathy. Additional Public Notification (a) * * * (3) Products containing any of the items prohibited importation under paragraphs (a)(1) and (a)(2) of this section. * * * * * Done in Washington, DC, this 8th day of March 2006. Kevin Shea, Acting Administrator, Animal and Plant Health Inspection Service. [FR Doc. 06–2406 Filed 3–13–06; 8:45 am] BILLING CODE 3410–34–P DEPARTMENT OF AGRICULTURE Food Safety and Inspection Service 9 CFR Part 352 [Docket No. 05–036C; FDMS No. 2005–0040] RIN 0583–AD21 Ante-Mortem Inspection of Horses; Correction Food Safety and Inspection Service, USDA. ACTION: Interim final rule; correction. AGENCY: SUMMARY: This document corrects the preamble to an interim final rule published in the Federal Register on February 8, 2006, amending the Federal meat inspection regulations to provide for a voluntary fee-for-service program under which official establishments that slaughter horses will be able to apply for and pay for ante-mortem inspection. This correction states that the FY 2006 Appropriations Act will be in effect until October 1, 2006 (the first day of FY 2007). FOR FURTHER INFORMATION CONTACT: Lynn Ellen Dickey, PhD, Director, Regulations and Petitions Policy Staff, Office of Policy, Program, and Employee Development, Food Safety and Inspection Service, 300 12th Street, SW., Room 112 Cotton Annex Building, Washington, DC 20250–3700, (202) 720– 5627. sroberts on PROD1PC70 with RULES Correction In the interim final rule, entitled Ante-Mortem Inspection of Horses (FSIS docket number 05–036IF), beginning on page 6337 in the issue of February 8, 2006, make the following correction, in the SUPPLEMENTARY INFORMATION section. VerDate Aug<31>2005 16:18 Mar 13, 2006 Jkt 208001 On page 6339 in the 3rd column, revise the first sentence of the second paragraph to read as follows: ‘‘The FY 2006 Appropriations Act will be in effect until October 1, 2006 (the first day of FY 2007).’’ Public awareness of all segments of rulemaking and policy development is important. Consequently, in an effort to ensure that the public and, in particular, minorities, women, and persons with disabilities are aware of this correction, FSIS will announce it on-line through the FSIS Web page located at https:// www.fsis.usda.gov/ regulations_&_policies/ 2006_Interim_&_Final_Rules_Index/ index.asp. FSIS also will make copies of this Federal Register publication available through the FSIS Constituent Update, which is used to provide information regarding FSIS policies, procedures, regulations, Federal Register notices, FSIS public meetings, recalls, and other types of information that could affect or would be of interest to our constituents and stakeholders. The update is communicated via Listserv, a free e-mail subscription service consisting of industry, trade, and farm groups, consumer interest groups, allied health professionals, scientific professionals, and other individuals who have requested to be included. The update also is available on the FSIS Web page. Through Listserv and the Web page, FSIS is able to provide information to a much broader, more diverse audience. In addition, FSIS offers an e-mail subscription service which provides an automatic and customized notification when popular pages are updated, including Federal Register publications and related documents. This service is available at https://www.fsis.usda.gov/ news_and_events/email_subscription/ and allows FSIS customers to sign up for subscription options across eight categories. Options range from recalls to export information to regulations, directives and notices. Customers can add or delete subscriptions themselves and have the option to password protect their account. Done at Washington, DC, on March 8, 2006. Barbara J. Masters, Administrator. [FR Doc. 06–2418 Filed 3–13–06; 8:45 am] BILLING CODE 3410–DM–P PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–22697; Directorate Identifier 2004–SW–46–AD; Amendment 39– 14509; AD 2006–06–01] RIN 2120–AA64 Airworthiness Directives; Eurocopter France Model EC 155B and B1 Helicopters Federal Aviation Administration, DOT. ACTION: Final rule. AGENCY: SUMMARY: This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (ECF) model helicopters that requires inspecting an electrical cable bundle for wear. If wear is present, the AD requires installing an airworthy cable bundle and modifying the routing of the electrical cable bundles. This amendment is prompted by reports of a short circuit in the wiring, which led to failure of the normal and emergency landing gear operation modes. The actions specified by this AD are intended to prevent interference of the wiring with the structure resulting in an electrical short circuit, failure of the landing gear to extend, and an emergency landing. DATES: Effective April 18, 2006. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of April 18, 2006. ADDRESSES: You may get the service information identified in this AD from American Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, Texas 75053–4005, telephone (972) 641–3460, fax (972) 641–3527. Examining the Docket You may examine the docket that contains this AD, any comments, and other information on the Internet at https://dms.dot.gov, or at the Docket Management System (DMS), U.S. Department of Transportation, 400 Seventh Street, SW., Room PL–401, on the plaza level of the Nassif Building, Washington, DC. FOR FURTHER INFORMATION CONTACT: Jorge Castillo, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Regulations and Policy Group, Fort Worth, Texas 76193–0111, telephone (817) 222–5127, fax (817) 222–5961. SUPPLEMENTARY INFORMATION: A proposal to amend 14 CFR part 39 to include an AD for the specified ECF E:\FR\FM\14MRR1.SGM 14MRR1 sroberts on PROD1PC70 with RULES Federal Register / Vol. 71, No. 49 / Tuesday, March 14, 2006 / Rules and Regulations model helicopters was published in the Federal Register on October 17, 2005 (70 FR 199). The action proposed to require inspecting an electrical cable bundle for wear. If wear is present, the AD proposed installing an airworthy cable bundle and modifying the routing of the electrical cable bundles. A correction to that proposal was published in the Federal Register on January 20, 2006 (71 FR 3248). That action corrected the docket number throughout the proposal changing it from FAA–2005–22696 to FAA–2005– 22697. The Direction Generale de l’Aviation Civile (DGAC), the airworthiness authority for France, notified the FAA that an unsafe condition may exist on ECF Model EC 155 helicopters. The DGAC advises of the occurrence of a short circuit that occurred in the wiring of panel 12 Alpha making the landing gear inoperative. ECF has issued Alert Service Bulletin No. 24A011 (ASB), dated March 11, 2004, subsequently revised on May 14, 2004, which specifies checking the condition of the wiring and modifying its routing to preclude the risk of interference and associated damage. The May 14, 2004, revision to the ASB also specifies preventing any interference of the wiring with the head of the vent line attaching clamp by replacing wiring kit 365A0739C28.71 with wiring kit 365A0739C28.72. The DGAC classified these ASBs as mandatory and issued AD No. F–2004–057 R1 dated July 21, 2004, to ensure the continued airworthiness of these helicopters in France. These helicopter models are manufactured in France and are type certificated for operation in the United States under the provisions of 14 CFR 21.29 and the applicable bilateral agreement. Pursuant to the applicable bilateral agreement, the DGAC has kept us informed of the situation described above. We have examined the findings of the DGAC, reviewed all available information, and determined that AD action is necessary for products of this type design that are certificated for operation in the United States. Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were received on the proposal or the FAA’s determination of the cost to the public. The FAA has determined that air safety and the public interest require the adoption of the rule as proposed except for correcting the docket number from FAA–2005–22696 to FAA–2005–22697. Also, we have expanded the contact address in paragraph (b) in the body of the AD to provide more information to VerDate Aug<31>2005 16:18 Mar 13, 2006 Jkt 208001 12999 the public. These changes will neither increase the economic burden on any operator nor increase the scope of this AD. We estimate that this AD will affect 7 helicopters of U.S. registry. It will take about 16 work hours to inspect and modify the wiring per helicopter at an average labor rate of $65 per work hour. Required parts and material will cost about $240. Based on these figures, we estimate the total cost impact of the AD on U.S. operators to be $8,960, assuming that all of the helicopters are modified. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Regulatory Findings I 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 an economic evaluation of the estimated costs to comply with this AD. See the DMS to examine the economic evaluation. 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. PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: I 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. § 39.13 [Amended] 2. Section 39.13 is amended by adding a new airworthiness directive to read as follows: I 2006–06–01 Eurocopter France: Amendment 39–14509. Docket No. FAA–2005–22697, Directorate Identifier 2004–SW–46–AD. Applicability Model EC 155B and B1 helicopters, certificated in any category. Compliance Required as indicated, unless accomplished previously. To prevent interference of the wiring with the structure resulting in an electrical short circuit, failure of the landing gear to extend, and an emergency landing, accomplish the following: (a) Within 50 hours time-in-service (TIS), (1) Inspect the wiring of panel 12 Alpha (wiring) electrical cable bundle for wear. If wear is present, replace the worn cable bundle with an airworthy cable bundle by following the Accomplishment Instructions, paragraphs 2.A.1, 2.B.1., and 2.B.2 of Eurocopter Alert Service Bulletin EC155 No. 24A011, Revision 1, dated May 14, 2004 (ASB). Note 1: Aircraft Maintenance Manual (AMM): Tasks 24.00.00.911 and 32–30–00– 721 and Standard Practices Manual (MTC) Work Cards 20.02.01.415, 20.06.01.310, 20.06.01.406, and 20.02.06.409 pertain to the subject of this AD. (2) Modify the routing of the electrical wiring (MOD 0739C28) and replace spreaders and spacers by following the Accomplishment Instructions, paragraph 2.B.3. through 2.B.9. of the ASB. (b) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Contact the Rotorcraft Directorate, Regulations and Policy Group, FAA, ATTN: Jorge Castillo, Aviation Safety Engineer, Fort Worth, Texas 76193–0111, telephone (817) 222–5127, fax (817) 222–5961 for information about previously approved alternative methods of compliance. (c) Special flight permits will not be issued. E:\FR\FM\14MRR1.SGM 14MRR1 13000 Federal Register / Vol. 71, No. 49 / Tuesday, March 14, 2006 / Rules and Regulations (d) Inspect and modify the routing of the electrical wiring and replace any electrical parts in accordance with the specified portions of Eurocopter Alert Service Bulletin EC155 No. 24A011, Revision 1, dated May 14, 2004. The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from American Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, Texas 75053– 4005, telephone (972) 641–3460, fax (972) 641–3527. Copies may be inspected at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives. gov/federal_register/code_of_federal_ regulations/ibr_locations.html. (e) This amendment becomes effective on April 18, 2006. wrong page number for the original Federal Register document. FR Doc. 06– 2155 is clarified and corrected as follows: On page 11304, column 1, under SUPPLEMENTARY INFORMATION, change ‘‘(71 FR 9698)’’ to ‘‘(71 FR 9695)’’ and ‘‘On page 9698 * * *’’ to ‘‘On page 9695’’. Note 2: The subject of this AD is addressed in Direction Generale de l’Aviation Civile (France) AD F–2004–057 R1, dated July 21, 2004. Food and Drug Administration Issued in Fort Worth, Texas, on February 23, 2006. David A. Downey, Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 06–2357 Filed 3–13–06; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF ENERGY Federal Energy Regulatory Commission 18 CFR Part 35 [Docket No. RM06–13–000; Order No. 674] Conditions for Public Utility MarketBased Rate Authorization Holders sroberts on PROD1PC70 with RULES 21 CFR Part 520 Oral Dosage Form New Animal Drugs; Sulfamerazine, Sulfamethazine, and Sulfaquinoxaline Powder AGENCY: Food and Drug Administration, HHS. ACTION: Final rule. SUMMARY: The Food and Drug Administration (FDA) is amending the animal drug regulations to reflect approval of a new animal drug application (NADA) filed by Alpharma Inc. The NADA provides revised labeling for a soluble powder containing sulfamerazine, sulfamethazine, and sulfaquinoxaline used in drinking water of chickens and turkeys as an aid in the control of coccidiosis and acute fowl cholera. The rule is effective March 14, FOR FURTHER INFORMATION CONTACT: FOR FURTHER INFORMATION CONTACT: Frank Karabetsos, Office of General Counsel, Federal Energy Regulatory Commission, 888 First Street, NE., Washington, DC 20426, (202) 502–8133, Frank.Karabetsos@ferc.gov. SUPPLEMENTARY INFORMATION: In FR Doc. 06–2155, published in the Federal Register on March 7, 2006 (71 FR 11304), the correction language cited the Jkt 208001 DEPARTMENT OF HEALTH AND HUMAN SERVICES 2006. SUMMARY: This document clarifies a correction that was published in the Federal Register on March 7, 2006. That action amended an effective date for a Final Rule that published in the Federal Register on February 27, 2006. The correction document referenced the wrong Federal Register page number. DATES: Effective Date: February 27, 2006. 16:18 Mar 13, 2006 BILLING CODE 6717–01–P DATES: Federal Energy Regulatory Commission, DOE. ACTION: Final rule: clarification. AGENCY: VerDate Aug<31>2005 Magalie R. Salas, Secretary. [FR Doc. 06–2404 Filed 3–13–06; 8:45 am] Dianne T. McRae, Center for Veterinary Medicine (HFV–104), Food and Drug Administration, 7500 Standish Pl., Rockville, MD 20855, 301–827–0161, email: dianne.mcrae@fda.hhs.gov. SUPPLEMENTARY INFORMATION: Alpharma Inc., One Executive Drive, Fort Lee, NJ 07024, filed NADA 100–094 for POULTRYSULFA (sulfamerazine, sulfamethazine, and sulfaquinoxaline) Antimicrobial Soluble Powder, an overthe-counter product used in the drinking water of chickens and turkeys as an aid in the control of coccidiosis and acute fowl cholera. The NADA relies on the National Academy of Sciences/National Research Council (NAS/NRC), Drug Efficacy Study Group’s (DESI) effectiveness evaluation and subsequent FDA conclusions. The findings were published in the Federal Register of July 5, 1984 (49 FR 27543). PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 Using the official analytical method of detection, residues of sulfamethazine and sulfamerazine in edible tissues coelute and cannot be quantified individually. There are no products containing only sulfamerazine approved for use in chickens or turkeys. Therefore, a tolerance for sulfamerazine residues in edible tissues of chickens or turkeys is not established at this time. Products that comply with the NAS/ NRC findings and FDA’s conclusions regarding those findings are eligible for immediate copying under the Generic Animal Drug and Patent Term Restoration Act (GADPTRA) (see the eighth in a series of policy letters issued to facilitate implementation of GADPTRA that published in the Federal Register of August 21, 1991 (56 FR 41561), available online at https:// www.fda.gov/cvm/Documents/ 8thltr.doc). The NADA is approved as of February 2, 2006, and part 520 (21 CFR part 520) is amended by adding new § 520.2218 to reflect the approval. The basis of approval is discussed in the freedom of information summary. In accordance with the freedom of information provisions of 21 CFR part 20 and 21 CFR 514.11(e)(2)(ii), a summary of safety and effectiveness data and information submitted to support approval of this application may be seen in the Division of Dockets Management (HFA–305), Food and Drug Administration, 5630 Fishers Lane, rm. 1061, Rockville, MD 20852, between 9 a.m. and 4 p.m., Monday through Friday. FDA has determined under 21 CFR 25.33(a)(1) that this action is of a type that does not individually or cumulatively have a significant effect on the human environment. Therefore, neither an environmental assessment nor an environmental impact statement is required. This rule does not meet the definition of ‘‘rule’’ in 5 U.S.C. 804(3)(A) because it is a rule of ‘‘particular applicability.’’ Therefore, it is not subject to the congressional review requirements in 5 U.S.C. 801–808. List of Subjects in 21 CFR Part 520 Animal drugs. Therefore, under the Federal Food, Drug, and Cosmetic Act and under authority delegated to the Commissioner of Food and Drugs and redelegated to the Center for Veterinary Medicine, 21 CFR part 520 is amended as follows: I E:\FR\FM\14MRR1.SGM 14MRR1

Agencies

[Federal Register Volume 71, Number 49 (Tuesday, March 14, 2006)]
[Rules and Regulations]
[Pages 12998-13000]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-2357]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22697; Directorate Identifier 2004-SW-46-AD; 
Amendment 39-14509; AD 2006-06-01]
RIN 2120-AA64


Airworthiness Directives; Eurocopter France Model EC 155B and B1 
Helicopters

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: This amendment adopts a new airworthiness directive (AD) for 
the specified Eurocopter France (ECF) model helicopters that requires 
inspecting an electrical cable bundle for wear. If wear is present, the 
AD requires installing an airworthy cable bundle and modifying the 
routing of the electrical cable bundles. This amendment is prompted by 
reports of a short circuit in the wiring, which led to failure of the 
normal and emergency landing gear operation modes. The actions 
specified by this AD are intended to prevent interference of the wiring 
with the structure resulting in an electrical short circuit, failure of 
the landing gear to extend, and an emergency landing.

DATES: Effective April 18, 2006.
    The incorporation by reference of certain publications listed in 
the regulations is approved by the Director of the Federal Register as 
of April 18, 2006.

ADDRESSES: You may get the service information identified in this AD 
from American Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, 
Texas 75053-4005, telephone (972) 641-3460, fax (972) 641-3527.

Examining the Docket

    You may examine the docket that contains this AD, any comments, and 
other information on the Internet at https://dms.dot.gov, or at the 
Docket Management System (DMS), U.S. Department of Transportation, 400 
Seventh Street, SW., Room PL-401, on the plaza level of the Nassif 
Building, Washington, DC.

FOR FURTHER INFORMATION CONTACT: Jorge Castillo, Aviation Safety 
Engineer, FAA, Rotorcraft Directorate, Regulations and Policy Group, 
Fort Worth, Texas 76193-0111, telephone (817) 222-5127, fax (817) 222-
5961.

SUPPLEMENTARY INFORMATION: A proposal to amend 14 CFR part 39 to 
include an AD for the specified ECF

[[Page 12999]]

model helicopters was published in the Federal Register on October 17, 
2005 (70 FR 199). The action proposed to require inspecting an 
electrical cable bundle for wear. If wear is present, the AD proposed 
installing an airworthy cable bundle and modifying the routing of the 
electrical cable bundles.
    A correction to that proposal was published in the Federal Register 
on January 20, 2006 (71 FR 3248). That action corrected the docket 
number throughout the proposal changing it from FAA-2005-22696 to FAA-
2005-22697.
    The Direction Generale de l'Aviation Civile (DGAC), the 
airworthiness authority for France, notified the FAA that an unsafe 
condition may exist on ECF Model EC 155 helicopters. The DGAC advises 
of the occurrence of a short circuit that occurred in the wiring of 
panel 12 Alpha making the landing gear inoperative.
    ECF has issued Alert Service Bulletin No. 24A011 (ASB), dated March 
11, 2004, subsequently revised on May 14, 2004, which specifies 
checking the condition of the wiring and modifying its routing to 
preclude the risk of interference and associated damage. The May 14, 
2004, revision to the ASB also specifies preventing any interference of 
the wiring with the head of the vent line attaching clamp by replacing 
wiring kit 365A0739C28.71 with wiring kit 365A0739C28.72. The DGAC 
classified these ASBs as mandatory and issued AD No. F-2004-057 R1 
dated July 21, 2004, to ensure the continued airworthiness of these 
helicopters in France.
    These helicopter models are manufactured in France and are type 
certificated for operation in the United States under the provisions of 
14 CFR 21.29 and the applicable bilateral agreement. Pursuant to the 
applicable bilateral agreement, the DGAC has kept us informed of the 
situation described above. We have examined the findings of the DGAC, 
reviewed all available information, and determined that AD action is 
necessary for products of this type design that are certificated for 
operation in the United States.
    Interested persons have been afforded an opportunity to participate 
in the making of this amendment. No comments were received on the 
proposal or the FAA's determination of the cost to the public. The FAA 
has determined that air safety and the public interest require the 
adoption of the rule as proposed except for correcting the docket 
number from FAA-2005-22696 to FAA-2005-22697. Also, we have expanded 
the contact address in paragraph (b) in the body of the AD to provide 
more information to the public. These changes will neither increase the 
economic burden on any operator nor increase the scope of this AD.
    We estimate that this AD will affect 7 helicopters of U.S. 
registry. It will take about 16 work hours to inspect and modify the 
wiring per helicopter at an average labor rate of $65 per work hour. 
Required parts and material will cost about $240. Based on these 
figures, we estimate the total cost impact of the AD on U.S. operators 
to be $8,960, assuming that all of the helicopters are modified.

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 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 an economic evaluation of the estimated costs to comply 
with this AD. See the DMS to examine the economic evaluation.

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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration amends part 39 of 
the Federal Aviation Regulations (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. Section 39.13 is amended by adding a new airworthiness directive to 
read as follows:

2006-06-01 Eurocopter France: Amendment 39-14509. Docket No. FAA-
2005-22697, Directorate Identifier 2004-SW-46-AD.

Applicability

    Model EC 155B and B1 helicopters, certificated in any category.

Compliance

    Required as indicated, unless accomplished previously.
    To prevent interference of the wiring with the structure 
resulting in an electrical short circuit, failure of the landing 
gear to extend, and an emergency landing, accomplish the following:
    (a) Within 50 hours time-in-service (TIS),
    (1) Inspect the wiring of panel 12 Alpha (wiring) electrical 
cable bundle for wear. If wear is present, replace the worn cable 
bundle with an airworthy cable bundle by following the 
Accomplishment Instructions, paragraphs 2.A.1, 2.B.1., and 2.B.2 of 
Eurocopter Alert Service Bulletin EC155 No. 24A011, Revision 1, 
dated May 14, 2004 (ASB).


    Note 1: Aircraft Maintenance Manual (AMM): Tasks 24.00.00.911 
and 32-30-00-721 and Standard Practices Manual (MTC) Work Cards 
20.02.01.415, 20.06.01.310, 20.06.01.406, and 20.02.06.409 pertain 
to the subject of this AD.


    (2) Modify the routing of the electrical wiring (MOD 0739C28) 
and replace spreaders and spacers by following the Accomplishment 
Instructions, paragraph 2.B.3. through 2.B.9. of the ASB.
    (b) To request a different method of compliance or a different 
compliance time for this AD, follow the procedures in 14 CFR 39.19. 
Contact the Rotorcraft Directorate, Regulations and Policy Group, 
FAA, ATTN: Jorge Castillo, Aviation Safety Engineer, Fort Worth, 
Texas 76193-0111, telephone (817) 222-5127, fax (817) 222-5961 for 
information about previously approved alternative methods of 
compliance.
    (c) Special flight permits will not be issued.

[[Page 13000]]

    (d) Inspect and modify the routing of the electrical wiring and 
replace any electrical parts in accordance with the specified 
portions of Eurocopter Alert Service Bulletin EC155 No. 24A011, 
Revision 1, dated May 14, 2004. The Director of the Federal Register 
approved this incorporation by reference in accordance with 5 U.S.C. 
552(a) and 1 CFR part 51. Copies may be obtained from American 
Eurocopter Corporation, 2701 Forum Drive, Grand Prairie, Texas 
75053-4005, telephone (972) 641-3460, fax (972) 641-3527. Copies may 
be inspected at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal
_register/code_of_federal_regulations/ibr_locations.html.
    (e) This amendment becomes effective on April 18, 2006.

    Note 2: The subject of this AD is addressed in Direction 
Generale de l'Aviation Civile (France) AD F-2004-057 R1, dated July 
21, 2004.


    Issued in Fort Worth, Texas, on February 23, 2006.
David A. Downey,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 06-2357 Filed 3-13-06; 8:45 am]
BILLING CODE 4910-13-P
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