96-3886. Airworthiness Directives; Air Tractor, Incorporated Models AT-802 and AT-802A Airplanes  

  • [Federal Register Volume 61, Number 37 (Friday, February 23, 1996)]
    [Rules and Regulations]
    [Pages 6934-6935]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 96-3886]
    
    
    
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    DEPARTMENT OF TRANSPORTATION
    14 CFR Part 39
    
    [Docket No. 95-CE-59-AD; Amendment 39-9520; AD 96-04-08]
    
    
    Airworthiness Directives; Air Tractor, Incorporated Models AT-802 
    and AT-802A Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD) that 
    applies to Air Tractor, Incorporated (Air Tractor) Models AT-802 and 
    AT-802A airplanes. This action requires repetitively replacing the main 
    landing gear legs. Failure of the main landing gear legs on an AT-802A 
    prompted this action. The actions specified by this AD are intended to 
    prevent possible failure of the main landing gear legs, which, if not 
    detected and corrected, could result in loss of control of the airplane 
    during landing operations.
    
    DATES: Effective April 12, 1996.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of April 12, 1996.
    
    ADDRESSES: Service information that applies to this AD may be obtained 
    from Air Tractor Incorporated, P.O. Box 485, Olney, Texas 76374; 
    telephone (817) 564-5616, facsimile (817) 564-2348. This information 
    may also be examined at the Federal Aviation Administration (FAA), 
    Central Region, Office of the Assistant Chief Counsel, Attention: Rules 
    Docket 95-CE-59-AD, Room 1558, 601 E. 12th Street, Kansas City, 
    Missouri 64106; or at the Office of the Federal Register, 800 North 
    Capitol Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Bob May, Aerospace Engineer, FAA, 
    Aircraft Certification Office, 2601 Meacham Boulevard, Fort Worth, 
    Texas 76193-0150; telephone (817) 222-5155, facsimile (817) 222-5960.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) to include an AD that would apply 
    to Air Tractor, Incorporated (Air Tractor) Models AT-802 and AT-802A 
    airplanes was published in the Federal Register on October 5, 1995 (60 
    FR 52130). The action proposed to require repetitively replacing the 
    main landing gear legs in accordance with Snow Engineering Company 
    Service Letter (SL) 104A, dated July 29, 1995.
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment. No comments were received on the 
    proposed rule or the FAA's determination of the cost to the public.
        After careful review of all available information related to the 
    subject presented above, the FAA has determined that air safety and the 
    public interest require the adoption of the rule as proposed except for 
    minor editorial corrections. The FAA has determined that these minor 
    corrections will not change the meaning of the AD and will not add any 
    additional burden upon the public than was already proposed.
        The FAA estimates that 18 airplanes in the U.S. registry will be 
    affected by this AD, that it will take approximately 12 hours per 
    airplane to accomplish this action, and that the average labor rate is 
    approximately $60 an hour. Parts cost approximately $2,816 per 
    airplane. Based on these figures, the total cost impact of this AD on 
    U.S. operators is estimated to be $63,648 ($3,536 per airplane). This 
    figure is based on the assumption that no affected airplane owner/
    operator has replaced the main landing gear legs and does not take into 
    account the number of repetitive replacements each operator would incur 
    over the life of the airplane. The FAA has no way of determining how 
    many main landing gear replacements each owner/operator will incur.
        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 copy of the final evaluation prepared for this 
    action is 
    
    [[Page 6935]]
    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.
    
    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 a new airworthiness directive 
    (AD) to read as follows:
    
    Ad No. 96-04-08  Air Tractor Incorporated: Amendment 39-9520; Docket 
    No. 95-CE-59-AD.
    
        Applicability: Model AT-802 and AT-802A Airplanes (all serial 
    numbers), 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 upon the accumulation of 3,000 
    landings or within the next 25 landings after the effective date of 
    this AD, whichever occurs later, unless already accomplished, and 
    thereafter at intervals not to exceed 3,000 landings.
    
        Note 2: If the number of landings is not known, calculate by 
    multiplying three landings per one hour time-in-service (TIS).
    
        To prevent possible failure of the main landing gear legs, which 
    could result in loss of control of landing operations and possible 
    loss of the airplane, accomplish the following:
        (a) Replace the main landing gear legs, Air Tractor part number 
    (P/N) 40091-2, in accordance with Air Tractor Service Bulletin (SB) 
    104A, dated July 29, 1995.
        (b) 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.
        (c) An alternative method of compliance or adjustment of the 
    initial or repetitive compliance times that provides an equivalent 
    level of safety may be approved by the Manager, Fort Worth Aircraft 
    Certification Office, FAA, Aircraft Certification Office, 2601 
    Meacham Boulevard, Fort Worth, Texas 76193-0150. The request shall 
    be forwarded through an appropriate FAA Maintenance Inspector, who 
    may add comments and then send it to the Manager, Fort Worth 
    Aircraft Certification Office.
    
        Note 3: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Fort Worth Aircraft Certification Office.
    
        (d) The replacements required by this AD shall be done in 
    accordance with Air Tractor Service Bulletin 104A, dated July 29, 
    1995. 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 Air Tractor Incorporated, P.O. 
    Box 485, Olney, Texas 76374. Copies may be inspected at the FAA, 
    Central Region, Office of the Assistant Chief Counsel, Room 1558, 
    601 E. 12th Street, Kansas City, Missouri, or at the Office of the 
    Federal Register, 800 North Capitol Street, NW., 7th Floor, suite 
    700, Washington, DC.
        (e) This amendment (39-9520) becomes effective on April 12, 
    1996.
    
        Issued in Kansas City, Missouri, on February 13, 1996.
    Michael Gallagher,
    Manager, Small Airplane Directorate, Aircraft Certification Service.
    [FR Doc. 96-3886 Filed 2-22-96; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Effective Date:
4/12/1996
Published:
02/23/1996
Department:
Transportation Department
Entry Type:
Rule
Action:
Final rule.
Document Number:
96-3886
Dates:
Effective April 12, 1996.
Pages:
6934-6935 (2 pages)
Docket Numbers:
Docket No. 95-CE-59-AD, Amendment 39-9520, AD 96-04-08
PDF File:
96-3886.pdf
CFR: (1)
14 CFR 39.13