99-45. Airworthiness Directives; Twin Commander Aircraft Corporation 500, 680, 690, and 695 Series Airplanes  

  • [Federal Register Volume 64, Number 2 (Tuesday, January 5, 1999)]
    [Rules and Regulations]
    [Page 395]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-45]
    
    
    =======================================================================
    -----------------------------------------------------------------------
    
    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 96-CE-54-AD; Amendment 39-10821; AD 98-08-25 R1]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Twin Commander Aircraft Corporation 
    500, 680, 690, and 695 Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Direct final rule; confirmation of effective date.
    
    -----------------------------------------------------------------------
    
    SUMMARY: This action confirms the effective date of Airworthiness 
    Directive (AD) 98-08-25 R1, which applies to certain Twin Commander 
    Aircraft Corporation (Twin Commander) 500, 680, 690, and 695 series 
    airplanes. AD 98-08-25 R1 requires replacing the nose landing gear 
    (NLG) drag link bolt with an approved heat-treated bolt that has the 
    manufacturer's serial number, manufacture date, and the last three 
    digits of the drawing number (055) on the bolt head; and changing the 
    bolt part number (P/N) to be installed on Models 690D and 695A from P/N 
    ED10055 to P/N 750076-1. This AD was the result of the FAA 
    inadvertently transposing the serial numbers of the 4 affected Model 
    695A airplanes. The actions specified in this AD are intended to 
    prevent the NLG from collapsing due to failure of a drag link bolt, 
    which could result in loss of control of the airplane during landing 
    operations.
    
    EFFECTIVE DATE: January 5, 1999.
    
    FOR FURTHER INFORMATION CONTACT: Jeffrey Morfitt, Aerospace Engineer, 
    FAA, Seattle Aircraft Certification Office, 1601 Lind Ave. S.W., 
    Renton, Washington, 98055-4056; telephone: (206) 227-2595; facsimile: 
    (206) 227-1181.
    
    SUPPLEMENTARY INFORMATION: The FAA published this direct final rule 
    with request for comments in the Federal Register on October 9, 1998 
    (63 FR 54347). The FAA uses the direct final rulemaking procedure for a 
    non-controversial rule where the FAA anticipates that there will be no 
    adverse public comment. This direct final rule advised the public that 
    no adverse comments were anticipated, and that unless a written adverse 
    comment, or a written notice of intent to submit such an adverse 
    comment, was received within the comment period, the regulation would 
    become effective on January 5, 1999. No adverse comments were received, 
    and thus this notice confirms that this final rule becomes effective on 
    that date.
    
        Issued in Kansas City, Missouri, on December 29, 1998.
    Marvin R. Nuss,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-45 Filed 1-4-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
1/5/1999
Published:
01/05/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Direct final rule; confirmation of effective date.
Document Number:
99-45
Dates:
January 5, 1999.
Pages:
395-395 (1 pages)
Docket Numbers:
Docket No. 96-CE-54-AD, Amendment 39-10821, AD 98-08-25 R1
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-45.pdf
CFR: (1)
14 CFR 39