99-17677. Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT Sailplanes  

  • [Federal Register Volume 64, Number 134 (Wednesday, July 14, 1999)]
    [Rules and Regulations]
    [Pages 37841-37842]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-17677]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 99-CE-07-AD; Amendment 39-11222; AD 99-15-03]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Stemme GmbH & Co. KG Model S10-VT 
    Sailplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment adopts a new airworthiness directive (AD) that 
    applies to certain Stemme GmbH & Co. KG (Stemme) Model S10-VT 
    sailplanes. This AD requires modifying the wastegate control in order 
    to eliminate heat damage. This AD is the result of mandatory continuing 
    airworthiness information (MCAI) issued by the airworthiness authority 
    for Germany. The actions specified by this AD are intended to prevent 
    the wastegate control from malfunctioning because of heat damage, which 
    could result in loss of automatic manifold pressure control and engine 
    damage.
    
    DATES: Effective August 31, 1999.
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of August 31, 1999.
    
    ADDRESSES: Service information that applies to this AD may be obtained 
    from Stemme GmbH & Co. KG, Gustav-Meyer-Allee 25, D-13355 Berlin, 
    Germany; telephone: 49.33.41.31.11.70; facsimile: 49.33.41.31.11.73. 
    This information may also be examined at the Federal Aviation 
    Administration (FAA), Central Region, Office of the Regional Counsel, 
    Attention: Rules Docket No. 99-CE-07-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: Mr. Mike Kiesov, Aerospace Engineer, 
    FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, 
    Missouri 64106; telephone: (816) 426-6934; facsimile: (816) 426-2169.
    
    
    [[Page 37842]]
    
    
    SUPPLEMENTARY INFORMATION:
    
    Events Leading to the Issuance of This AD
    
        A proposal to amend part 39 of the Federal Aviation Regulations (14 
    CFR part 39) to include an AD that would apply to certain Stemme Model 
    S10-VT sailplanes was published in the Federal Register as a notice of 
    proposed rulemaking (NPRM) on April 26, 1999 (64 FR 20229). The NPRM 
    proposed to require modifying the wastegate control in order to 
    eliminate heat damage. Accomplishment of the proposed action as 
    specified in the NPRM would be required in accordance with Stemme 
    Service Bulletin No. A31-10-034, Amendment 01.a, pages 3 and 4, dated 
    July 24, 1998.
        The NPRM was the result of mandatory continuing airworthiness 
    information (MCAI) issued by the airworthiness authority for Germany.
        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.
    
    The FAA's Determination
    
        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.
    
    Cost Impact
    
        The FAA estimates that 6 sailplanes in the U.S. registry will be 
    affected by this AD, that it will take approximately 4 workhours per 
    sailplane to accomplish this action, and that the average labor rate is 
    approximately $60 an hour. Parts cost approximately $150 per sailplane. 
    Based on these figures, the total cost impact of this AD on U.S. 
    operators is estimated to be $2,340, or $390 per sailplane.
    
    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 copy of the final 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.
    
    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:
    
    99-15-03  Stemme GMBH & Co. KG: Amendment 39-11222; Docket No. 99-
    CE-07-AD.
    
        Applicability: Model S10-VT sailplanes, serial numbers 11-004 
    through 11-006 and 11-008 through 11-013, certificated in any 
    category.
    
        Note 1: This AD applies to each sailplane 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 sailplanes 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 within the next 3 calendar months after the 
    effective date of this AD, unless already accomplished.
        To prevent the wastegate control from malfunctioning because of 
    heat damage, which could result in loss of automatic manifold 
    pressure control and engine damage, accomplish the following:
        (a) Modify the wastegate control in order to eliminate heat 
    damage, in accordance with the Instructions section of Stemme 
    Service Bulletin No. A31-10-034, Amendment 01.a, pages 3 and 4, 
    dated July 24, 1998.
        (b) 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 sailplane to a location where the 
    requirements of this AD can be accomplished.
        (c) An alternative method of compliance or adjustment of the 
    compliance time that provides an equivalent level of safety may be 
    approved by the Manager, Small Airplane Directorate, FAA, 1201 
    Walnut, suite 900, Kansas City, Missouri 64106. The request shall be 
    forwarded through an appropriate FAA Maintenance Inspector, who may 
    add comments and then send it to the Manager, Small Airplane 
    Directorate.
    
        Note 2: Information concerning the existence of approved 
    alternative methods of compliance with this AD, if any, may be 
    obtained from the Small Airplane Directorate.
    
        (d) Questions or technical information related to Stemme Service 
    Bulletin No. A31-10-034, Amendment 01.a, dated July 24, 1998, should 
    be directed to Stemme GmbH & Co. KG, Gustav-Meyer-Allee 25, D-13355 
    Berlin, Germany; telephone: 49.33.41.31.11.70; facsimile: 
    49.33.41.31.11.73. This service information may be examined at the 
    FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 
    E. 12th Street, Kansas City, Missouri 64106.
        (e) The modification required by this AD shall be done in 
    accordance with Stemme GmbH & Co. KG Service Bulletin No. A31-10-
    034, Amendment 01.a, pages 3 and 4, dated July 24, 1998. 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 Stemme GmbH & Co. KG, Gustav-Meyer-
    Allee 25, D-13355 Berlin, Germany. Copies may be inspected at the 
    FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 
    E. 12th Street, Kansas City, Missouri, 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 German AD 1998-
    400, dated October 22, 1998.
    
        (f) This amendment becomes effective on August 31, 1999.
    
        Issued in Kansas City, Missouri, on July 2, 1999.
    Marvin R. Nuss,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-17677 Filed 7-13-99; 8:45 am]
    BILLING CODE 4910-13-U
    
    
    

Document Information

Effective Date:
8/31/1999
Published:
07/14/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
99-17677
Dates:
Effective August 31, 1999.
Pages:
37841-37842 (2 pages)
Docket Numbers:
Docket No. 99-CE-07-AD, Amendment 39-11222, AD 99-15-03
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-17677.pdf
CFR: (1)
14 CFR 39.13