98-6500. Airworthiness Directives; Dassault Model Mystere Falcon 900 Series Airplanes  

  • [Federal Register Volume 63, Number 50 (Monday, March 16, 1998)]
    [Rules and Regulations]
    [Pages 12613-12614]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-6500]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 97-NM-193-AD; Amendment 39-10395; AD 98-06-17]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Dassault Model Mystere Falcon 900 
    Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD), 
    applicable to certain Dassault Aviation Model Mystere Falcon 900 series 
    airplanes, that requires replacement of the water heater control relays 
    with improved relays having high-power contactors; the addition of a 
    testing and monitoring circuit for each contactor; and installation of 
    improved electrical bonding of the potable water tank. This amendment 
    is prompted by issuance of mandatory continuing airworthiness 
    information by a foreign civil airworthiness authority. The actions 
    specified by this AD are intended to prevent overheating of the water 
    heaters for the galley or the washbasin, which could result in damage 
    to the water heater and nearby electrical wiring, and consequent smoke 
    in the cabin.
    
    DATES: Effective April 20, 1998.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of April 20, 1998.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Dassault Falcon Jet Corporation, Teterboro Airport, P.O. 
    Box 2000, South Hackensack, New Jersey 07606. This information may be 
    examined at the Federal Aviation Administration (FAA), Transport 
    Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton, 
    Washington; or at the Office of the Federal Register, 800 North Capitol 
    Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager, 
    International Branch, ANM-116, FAA, Transport Airplane Directorate, 
    1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
    227-2110; fax (425) 227-1149.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) to include an airworthiness 
    directive (AD) that is applicable to certain Dassault Aviation Model 
    Mystere Falcon 900 series airplanes was published in the Federal 
    Register on January 5, 1998 (63 FR 171). That action proposed to 
    require replacement of the water heater control relays with improved 
    relays having high-power contactors; the addition of a testing and 
    monitoring circuit for each contactor; and installation of improved 
    electrical bonding of the potable water tank.
    
    Comments
    
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. No comments were submitted in response 
    to the proposal or the FAA's determination of the cost to the public.
    
    Conclusion
    
        The FAA has determined that air safety and the public interest 
    require the adoption of the rule as proposed.
    
    Cost Impact
    
        The FAA estimates that 1 airplane of U.S. registry will be affected 
    by this AD, that it will take approximately 24 work hours per airplane 
    to accomplish the required actions, and that the average labor rate is 
    $60 per work hour. Required parts will cost approximately $6,300 per 
    airplane. Based on these figures, the cost impact of the AD on the 
    single U.S. operator is estimated to be $7,740.
        The cost impact figure discussed above is based on assumptions that 
    no operator has yet accomplished any of the requirements of this AD 
    action, and that no operator would accomplish those actions in the 
    future if this AD were not adopted.
    
    Regulatory Impact
    
        The regulations adopted herein will not have substantial direct 
    effects 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, in 
    accordance with Executive Order 12612, it is determined that this final 
    rule does not have sufficient federalism implications to warrant the 
    preparation of a Federalism Assessment.
        For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action 
    and it is contained in the Rules Docket. A copy of it may be obtained 
    from the Rules Docket at the location provided under the caption 
    ADDRESSES.
    
    List of Subjects in 14 CFR Part 39
    
        Air transportation, Aircraft, Aviation safety, Incorporation by 
    reference, Safety.
    
    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:
    
    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. Section 39.13 is amended by adding the following new 
    airworthiness directive:
    
    98-06-17 Dassault Aviation: Amendment 39-10395. Docket 97-NM-193-AD.
    
        Applicability: Model Mystere Falcon 900 airplanes; equipped with 
    l'HOTELLIER water
    
    [[Page 12614]]
    
    system gauges having part number (P/N) 5250, 5251, 5250-1 or 5251-1; 
    certificated in any category.
    
        Note 1: This AD applies to each airplane identified in the 
    preceding applicability provision, regardless of whether it has been 
    modified, altered, or repaired in the area subject to the 
    requirements of this AD. For airplanes 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 as indicated, unless accomplished 
    previously.
        To prevent overheating of the water heaters for the galley or 
    the washbasin, which could result in damage to the water heater and 
    nearby electrical wiring, and consequent smoke in the cabin, 
    accomplish the following:
        (a) Within 7 months or 330 flight hours after the effective date 
    of this AD, whichever occurs first: Replace the water heater control 
    relays with improved relays; add a testing and monitoring circuit 
    for each contactor; and install improved electrical bonding of the 
    potable water tank; in accordance with Dassault Service Bulletin 
    F900-181 (F900-38-12), dated December 4, 1996.
        (b) An alternative method of compliance or adjustment of the 
    compliance time that provides an acceptable level of safety may be 
    used if approved by the Manager, International Branch, ANM-116, FAA, 
    Transport Airplane Directorate. Operators shall submit their 
    requests through an appropriate FAA Principal Maintenance Inspector, 
    who may add comments and then send it to the Manager, International 
    Branch, ANM-116.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the International Branch, ANM-116.
    
        (c) Special flight permits may be issued in accordance with 
    sections 21.197 and 21.199 of the Federal Aviation Regulations (14 
    CFR 21.197 and 21.199) to operate the airplane to a location where 
    the requirements of this AD can be accomplished.
        (d) The actions shall be done in accordance with Dassault 
    Service Bulletin F900-181 (F900-38-12), dated December 4, 1996. This 
    incorporation by reference was approved by the Director of the 
    Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 
    51. Copies may be obtained from Dassault Falcon Jet Corporation, 
    Teterboro Airport, P.O. Box 2000, South Hackensack, New Jersey 
    07606. Copies may be inspected at the FAA, Transport Airplane 
    Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the 
    Office of the Federal Register, 800 North Capitol Street, NW., suite 
    700, Washington, DC.
    
        Note 3: The subject of this AD is addressed in French 
    airworthiness directive 96-279-018(B), dated December 4, 1996.
        (e) This amendment becomes effective on April 20, 1998.
    
        Issued in Renton, Washington, on March 9, 1998.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-6500 Filed 3-13-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
4/20/1998
Published:
03/16/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
98-6500
Dates:
Effective April 20, 1998.
Pages:
12613-12614 (2 pages)
Docket Numbers:
Docket No. 97-NM-193-AD, Amendment 39-10395, AD 98-06-17
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-6500.pdf
CFR: (1)
14 CFR 39.13