98-17419. Airworthiness Directives; Dornier Model 328-100 Series Airplanes  

  • [Federal Register Volume 63, Number 126 (Wednesday, July 1, 1998)]
    [Rules and Regulations]
    [Pages 35790-35792]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-17419]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-103-AD; Amendment 39-10639; AD 98-14-05]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Dornier Model 328-100 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 Dornier Model 328-100 series airplanes, that 
    requires modification of the ground cooling fan. 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 failure of the ground cooling fan, 
    which could result in smoke in the flight deck and cabin and consequent 
    inability of the flight crew to perform duties or possible passenger 
    injury due to smoke inhalation.
    
    DATES: Effective August 5, 1998.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of August 5, 1998.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from FAIRCHILD DORNIER, DORNIER Luftfahrt GmbH, P.O. Box 1103, 
    D-82230 Wessling, Germany. 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
    
    [[Page 35791]]
    
    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 Dornier Model 328-100 
    series airplanes was published in the Federal Register on May 5, 1998 
    (63 FR 24758). That action proposed to require modification of the 
    ground cooling fan.
    
    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.
    
    Explanation of Changes Made to this Final Rule
    
        In the proposal, the FAA inadvertently omitted reference to the 
    Price/Material Information Sheet, dated July 16, 1997, of Dornier 
    Service Bulletin SB-328-21-227, dated July 16, 1997. Therefore, the FAA 
    has revised the final rule accordingly.
    
    Conclusion
    
        The FAA has determined that air safety and the public interest 
    require the adoption of the rule with the change previously described. 
    The FAA has determined that this change will neither increase the 
    economic burden on any operator nor increase the scope of the AD.
    
    Cost Impact
    
        The FAA estimates that 50 airplanes of U.S. registry will be 
    affected by this AD. It will take approximately 1 work hour per 
    airplane to accomplish the required actions, at average labor rate of 
    $60 per work hour. Required parts will be supplied by the manufacturer 
    at no cost to operators. Based on these figures, the cost impact of the 
    AD on U.S. operators is estimated to be $3,000, or $60 per airplane.
        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:
    
    98-14-05  Dornier Luftfahrt GmbH: Amendment 39-10639. Docket 98-NM-
    103-AD.
    
        Applicability: Model 328-100 series airplanes, serial numbers 
    3005 through 3095 inclusive, 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 (c) 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 failure of the ground cooling fan, which could result 
    in smoke in the flight deck and cabin and consequent inability of 
    the flight crew to perform duties or possible passenger injury due 
    to smoke inhalation, accomplish the following:
        (a) Within 3 months after the effective date of this AD, modify 
    the ground cooling fan and rotate the modified check valve, in 
    accordance with Dornier Service Bulletin SB-328-21-227, dated July 
    16, 1997, including Price/Material Information Sheet, dated July 16, 
    1997.
    
        Note 2: The service bulletin references EG&G Rotron Service 
    Bulletin 011389500-21-1, dated April 30, 1997, as an additional 
    source of service information to accomplish the actions required by 
    this AD.
    
        (b) As of the effective date of this AD, no person shall install 
    on any airplane a ground cooling fan, part number 011389500, unless 
    it has been modified in accordance with Dornier Service Bulletin SB-
    328-21-227, dated July 16, 1997.
        (c) 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 3: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the International Branch, ANM-116.
    
        (d) 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.
        (e) The modification shall be done in accordance with Dornier 
    Service Bulletin SB-328-21-227, dated July 16, 1997, including 
    Price/Material Information Sheet, dated July 16, 1997. 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 FAIRCHILD DORNIER, DORNIER Luftfahrt 
    GmbH, P.O. Box 1103, D-82230 Wessling, Germany. 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 4: The subject of this AD is addressed in German 
    airworthiness directive 97-243, dated August 28, 1997.
    
        (f) This amendment becomes effective on August 5, 1998.
    
    
    [[Page 35792]]
    
    
        Issued in Renton, Washington, on June 24, 1998.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 98-17419 Filed 6-30-98; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
8/5/1998
Published:
07/01/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
98-17419
Dates:
Effective August 5, 1998.
Pages:
35790-35792 (3 pages)
Docket Numbers:
Docket No. 98-NM-103-AD, Amendment 39-10639, AD 98-14-05
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-17419.pdf
CFR: (1)
14 CFR 39.13