02-2426. Airworthiness Directives; Eurocopter France Model AS332L and AS332L1 Helicopters  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration, DOT.

    ACTION:

    Notice of proposed rulemaking (NPRM).

    SUMMARY:

    This document proposes adopting a new airworthiness directive (AD) for Eurocopter France (ECF) Model AS332L and AS332L1 helicopters. This proposal would require adding a supplement to the limitations section of the applicable Rotorcraft Flight Manual (RFM) for helicopters with “SEFA” skis installed. This proposal is prompted by the need to limit the taxi and Vne speed of those helicopters with skis. The actions specified by this proposed AD are intended to prevent structural failure of a ski and subsequent loss of control of the helicopter.

    DATES:

    Comments must be received on or before April 8, 2002.

    ADDRESSES:

    Submit comments in triplicate to the Federal Aviation Administration (FAA), Office of the Regional Counsel, Southwest Region, Start Printed Page 5527Attention: Rules Docket No. 2001-SW-46-AD, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137. You may also send comments electronically to the Rules Docket at the following address: 9-asw-adcomments@faa.gov. Comments may be inspected at the Office of the Regional Counsel between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays.

    Start Further Info

    FOR FURTHER INFORMATION CONTACT:

    Uday Garadi, Aviation Safety Engineer, FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, Fort Worth, Texas 76193-0110, telephone (817) 222-5123, fax (817) 222-5961.

    End Further Info End Preamble Start Supplemental Information

    SUPPLEMENTARY INFORMATION:

    Comments Invited

    Interested persons are invited to participate in the making of the proposed rule by submitting such written data, views, or arguments as they may desire. Communications should identify the Rules Docket number and be submitted in triplicate to the address specified above. All communications received on or before the closing date for comments will be considered before taking action on the proposed rule. The proposals contained in this document may be changed in light of the comments received.

    Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the proposed rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report summarizing each FAA-public contact concerned with the substance of this proposal will be filed in the Rules Docket.

    Commenters wishing the FAA to acknowledge receipt of their mailed comments submitted in response to this proposal must submit a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket No. 2001-SW-46-AD.” The postcard will be date stamped and returned to the commenter.

    Availability of NPRMs

    Any person may obtain a copy of this NPRM by submitting a request to the FAA, Office of the Regional Counsel, Southwest Region, Attention: Rules Docket No. 2001-SW-46-AD, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 76137.

    Discussion

    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 AS332L and L1 helicopters equipped with “SEFA” skis. ECF issued Supplements, SUP.10.14, Ski Installation, Normal Revision 2, Issue 2, dated June 2001 to the ECF Model AS332L and AS332L1 RFM. The DGAC classified these RFM supplements as mandatory and issued AD No. 2001-316-079(A), dated July 25, 2001. The DGAC advises incorporating the Ski Installation Supplement into the applicable RFM before the next flight and complying with the VNE and the maximum taxiing speed limitations 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 the FAA informed of the situation described above. The FAA has 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.

    We have identified an unsafe condition that is likely to exist or develop on other ECF Model AS332L and AS332L1 helicopters of the same type designs registered in the United States. Therefore, the proposed AD would require adding the limitations contained in SUP.10.14, Ski Installation, to the limitations section of the RFM, requiring certain speed limitations for helicopters with skis installed.

    The FAA estimates that 3 helicopters of U.S. registry would be affected by this proposed AD, that it would take approximately 10 minutes per helicopter to add the flight manual supplement, and that the average labor rate is $60 per work hour. Based on these figures, the total cost impact of the proposed AD on U.S. operators is estimated to be $30.

    The regulations proposed herein 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. Therefore, it is determined that this proposal would not have federalism implications under Executive Order 13132.

    For the reasons discussed above, I certify that this 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) if promulgated, 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. A copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.

    Start List of Subjects

    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Safety
    End List of Subjects

    The Proposed Amendment

    Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

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    PART 39—AIRWORTHINESS DIRECTIVES

    1. The authority citation for part 39 continues to read as follows:

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    Authority: 49 U.S.C. 106(g), 40113, 44701.

    End Authority
    [Amended]

    2. Section 39.13 is amended by adding a new airworthiness directive to read as follows:

    Eurocopter France: Docket No. 2001-SW-46-AD.

    Applicability: Model AS332L and AS332L1 helicopters with “SEFA” skis installed, certificated in any category.

    Note 1:

    This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (b) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

    Compliance: Required before further flight, unless accomplished previously.

    To prevent structural failure of a ski and subsequent loss of control of the helicopter, accomplish the following:

    (a) Before the next flight with skis installed, add the limitations contained in SUP.10.14, Ski Installation, Normal Revision 2, Issue 2, dated June 2001 to the limitations section of the applicable Rotorcraft Flight Manual.

    (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be Start Printed Page 5528used if approved by the Manager, Regulations Group, Rotorcraft Directorate, FAA. Operators shall submit their requests through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Regulations Group.

    Note 2:

    Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Regulations Group.

    (c) Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199 to operate the helicopter to a location where the requirements of this AD can be accomplished.

    Note 3:

    The subject of this AD is addressed in Direction General De L'Aviation Civile (France) AD 2001-316-079(A), dated July 25, 2001.

    Start Signature

    Issued in Fort Worth, Texas, on January 17, 2002.

    David A. Downey,

    Manager, Rotorcraft Directorate, Aircraft Certification Service.

    End Signature End Part End Supplemental Information

    [FR Doc. 02-2426 Filed 2-5-02; 8:45 am]

    BILLING CODE 4910-13-U

Document Information

Published:
02/06/2002
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Notice of proposed rulemaking (NPRM).
Document Number:
02-2426
Dates:
Comments must be received on or before April 8, 2002.
Pages:
5526-5528 (3 pages)
Docket Numbers:
Docket No. 2001-SW-46-AD
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Safety
PDF File:
02-2426.pdf
CFR: (1)
14 CFR 39.13