00-501. Airworthiness Directives; Saab Model SAAB 2000 Series Airplanes  

  • [Federal Register Volume 65, Number 8 (Wednesday, January 12, 2000)]
    [Rules and Regulations]
    [Pages 1762-1763]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 00-501]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 99-NM-244-AD; Amendment 39-11501; AD 2000-01-04]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Saab Model SAAB 2000 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 all Saab Model SAAB 2000 series airplanes, that requires 
    a one-time general visual inspection to verify the proper orientation 
    of the aft exterior light; and corrective actions, if necessary. 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 improper illumination of 
    the ground under the service door due to incorrect installation of the 
    aft exterior light, which could result in injury to the passengers or 
    crew members during an emergency evacuation.
    
    DATES: Effective February 16, 2000.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of February 16, 2000.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Saab Aircraft AB, SAAB Aircraft Product Support, S-
    581.88, Linkoping, Sweden. 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 all Saab Model SAAB 2000 series 
    airplanes was published in the Federal Register on November 15, 1999 
    (64 FR 61794). That action proposed to require a one-time general 
    visual inspection to verify the proper orientation of the aft exterior 
    light; and corrective actions, if necessary.
    
    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 3 airplanes of U.S. registry will be 
    affected by this AD, that it will take approximately 1 work hour per 
    airplane to accomplish the required inspection, and that the average 
    labor rate is $60 per work hour. Based on these figures, the cost 
    impact of the AD on U.S. operators is estimated to be $180, or $60 per 
    airplane.
        The cost impact figure discussed above is based on assumptions that 
    no
    
    [[Page 1763]]
    
    operator has yet accomplished any of the proposed 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 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 final rule does not have federalism 
    implications under Executive Order 13132.
        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:
    
    2000-01-04 Saab Aircraft AB: Amendment 39-11501. Docket 99-NM-244-
    AD.
        Applicability: All Model SAAB 2000 series airplanes, 
    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 improper illumination of the ground under the service 
    door due to incorrect installation of the aft exterior light, which 
    could result in injury to the passengers or crew members during an 
    emergency evacuation, accomplish the following:
        (a) Within 4 months after the effective date of this AD, perform 
    a one-time general visual inspection of the aft exterior light to 
    verify proper orientation, in accordance with Saab Service Bulletin 
    2000-33-016, dated April 21, 1999.
        (1) If the aft exterior light is correctly installed, as 
    specified in the service bulletin, reinstall the lens in accordance 
    with the service bulletin.
        (2) If the aft exterior light is incorrectly installed, as 
    specified in the service bulletin, prior to further flight, correct 
    the orientation of the aft exterior light in accordance with the 
    service bulletin.
    
        Note 2: For the purposes of this AD, a general visual inspection 
    is defined as: ``A visual examination of an interior or exterior 
    area, installation, or assembly to detect obvious damage, failure, 
    or irregularity. This level of inspection is made under normally 
    available lighting conditions such as daylight, hangar lighting, 
    flashlight, or drop-light, and may require removal or opening of 
    access panels or doors. Stands, ladders, or platforms may be 
    required to gain proximity to the area being checked.''
    
    Alternative Methods of Compliance
    
        (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 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.
    
    Special Flight Permits
    
        (c) Special flight permits may be issued in accordance with 
    Secs.  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.
    
    Incorporation by Reference
    
        (d) The actions shall be done in accordance with Saab Service 
    Bulletin 2000-33-016, dated April 21, 1999. 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 Saab Aircraft AB, SAAB Aircraft Product Support, S-
    581.88, Linkping, Sweden. 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 Swedish 
    airworthiness directive No. 1-140, dated April 21, 1999.
    
        (e) This amendment becomes effective on February 16, 2000.
    
        Issued in Renton, Washington, on January 4, 2000.
    Donald L. Riggin,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 00-501 Filed 1-11-00; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
2/16/2000
Published:
01/12/2000
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
00-501
Dates:
Effective February 16, 2000.
Pages:
1762-1763 (2 pages)
Docket Numbers:
Docket No. 99-NM-244-AD, Amendment 39-11501, AD 2000-01-04
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
00-501.pdf
CFR: (1)
14 CFR 39.13