99-8688. Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 Series Airplanes, and KC-10 (Military) Series Airplanes  

  • [Federal Register Volume 64, Number 67 (Thursday, April 8, 1999)]
    [Rules and Regulations]
    [Pages 17086-17087]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-8688]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-55-AD; Amendment 39-11072; AD 99-06-08]
    RIN 2120-AA64
    
    
    Airworthiness Directives; McDonnell Douglas Model DC-10 and MD-11 
    Series Airplanes, and KC-10 (Military) Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; correction.
    
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    SUMMARY: This document corrects erroneous references that appeared in 
    airworthiness directive (AD) 99-06-08 that was published in the Federal 
    Register on March 12, 1999 (64 FR 12249). That AD contained incorrect 
    references to certain paragraphs. This AD is applicable to certain 
    McDonnell Douglas Model DC-10 and MD-11 series airplanes, and KC-10 
    (military) series airplanes. This AD requires a one-time inspection for 
    blockage of the lubrication holes on the forward trunnion spacer 
    assembly, and a one-time inspection of the forward trunnion bolt on the 
    left and right main landing gear (MLG) to detect discrepancies; and 
    repair, if necessary.
    
    EFFECTIVE DATE: Effective April 16, 1999.
    
    FOR FURTHER INFORMATION CONTACT: Ron Atmur, Aerospace Engineer, 
    Airframe Branch, ANM-120L, FAA, Transport Airplane Directorate, Los 
    Angeles Aircraft Certification Office, 3960 Paramount Boulevard, 
    Lakewood, California 90712-4137; telephone (562) 627-5224; fax (562) 
    627-5210.
    
    SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 99-06-08, 
    amendment 39-11072, applicable to certain McDonnell Douglas Model DC-10 
    and MD-11 series airplanes, and KC-10 (military) series airplanes, was 
    published in the Federal Register on March 12, 1999 (64 FR 12249). That 
    AD requires a one-time inspection for blockage of the lubrication holes 
    on the forward trunnion spacer assembly, and a one-time inspection of 
    the forward trunnion bolt on the left and right main landing gear (MLG) 
    to detect discrepancies; and repair, if necessary.
        As published, that AD contained four erroneous references to 
    incorrect paragraphs. Paragraph (a) of the final rule states ``For 
    airplanes listed in McDonnell Douglas Service Bulletin MD11-32-074, 
    dated December 15, 1997: Except as provided by paragraphs (c) and (d) 
    of this AD * * *'' However, the exception referenced in that paragraph 
    should have been only to paragraph (c) because, unlike paragraphs (a) 
    and (c) of the final rule, paragraph (d) applies to certain McDonnell 
    Douglas Model DC-10-30, DC-10, -40, and KC-10(A) military series 
    airplanes, not to Model MD-11 series airplanes.
        Paragraph (b) of the final rule states ``For airplanes listed in 
    McDonnell Douglas Service Bulletin DC10-32-248, dated December 17, 
    1997: Except as provided by paragraph (e) of this AD * * *'' However, 
    the exception referenced in that paragraph also should have included 
    paragraph (d) because, like paragraph (b) of the final rule, paragraph 
    (d) applies to certain McDonnell Douglas Model DC-10-30, DC-10, -40, 
    and KC-10(A) military series airplanes.
        The last sentence in paragraphs (d) and (e) of the final rule 
    states ``* * * accomplish the requirements specified in paragraph (a) 
    of this AD.'' Paragraph (d) of the final rule applies to certain 
    McDonnell Douglas Model DC-10-30, DC-10-40, and KC-10A (military) 
    series airplanes, and paragraph (e) applies to certain McDonnell 
    Douglas Model DC-10-10 and DC-10-15 series airplanes. However, those 
    paragraphs require accomplishment of the requirements specified in 
    paragraph (a) of the final rule, which applies to certain McDonnell 
    Douglas Model MD-11 series airplanes. The correct reference should have 
    been to paragraph (b).
        Since no other part of the regulatory information has been changed, 
    the final rule is not being republished.
        The effective date of this AD remains April 16, 1999.
    
    
    Sec. 39.13  [Corrected]
    
        On page 12251, in the third column, paragraph (a) of AD 99-06-08 is 
    corrected to read as follows:
    * * * * *
    
    [[Page 17087]]
    
        (a) For airplanes listed in McDonnell Douglas Service Bulletin 
    MD11-32-074, dated December 15, 1997: Except as provided by paragraph 
    (c) of this AD, within 24 months after the effective date of this AD, 
    perform a one-time visual inspection of the lubrication holes on the 
    forward trunnion spacer assembly on the MLG for blockage by opposing 
    bushings, and perform a one-time visual inspection of the forward 
    trunnion bolt on the left and right MLG for chrome flaking, galling, 
    and corrosion in the grooves; in accordance with the service bulletin.
    * * * * *
        On page 12252, in the first column, paragraph (b) of AD 99-06-08 is 
    corrected to read as follows:
    * * * * *
        (b) For airplanes listed in McDonnell Douglas Service Bulletin 
    DC10-32-248, dated December 17, 1997: Except as provided by paragraphs 
    (d) and (e) of this AD, within 24 months after the effective date of 
    this AD, perform a one-time visual inspection of the lubrication holes 
    on the forward trunnion spacer assembly on the MLG for blockage by 
    opposing bushings, and perform a one-time visual inspection of the 
    forward trunnion bolt on the left and right MLG for chrome flaking, 
    galling, and corrosion in the grooves; in accordance with the service 
    bulletin.
    * * * * *
        On page 12252, in the second column, paragraph (d) of AD 99-06-08 
    is corrected to read as follows:
    * * * * *
        (d) For Model DC-10-30, DC-10-40, and KC-10A (military) series 
    airplanes on which the requirements specified in either paragraph 
    (c)(1)(i) or (c)(2)(ii) of AD 96-03-05, amendment 39-9502, have been 
    accomplished: Within 48 months after the effective date of this AD, 
    accomplish the requirements specified in paragraph (b) of this AD.
    * * * * *
        On page 12252, in the second column, paragraph (e) of AD 99-06-08 
    is corrected to read as follows:
    * * * * *
        (e) For Model DC-10-10 and DC-10-15 series airplanes, on which the 
    requirements specified in paragraph (a)(1)(i), (a)(2)(ii), (b)(2)(i), 
    or (b)(2)(ii) of AD 96-16-01, amendment 39-9701, have been 
    accomplished: Within 48 months after the effective date of this AD, 
    accomplish the requirements specified in paragraph (b) of this AD.
    * * * * *
        Issued in Renton, Washington, on April 1, 1999.
    Darrell M. Pederson,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-8688 Filed 4-7-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
4/16/1999
Published:
04/08/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
99-8688
Dates:
Effective April 16, 1999.
Pages:
17086-17087 (2 pages)
Docket Numbers:
Docket No. 98-NM-55-AD, Amendment 39-11072, AD 99-06-08
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-8688.pdf
CFR: (1)
14 CFR 39.13