99-809. Airworthiness Directives; Israel Aircraft Industries (IAI), Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes  

  • [Federal Register Volume 64, Number 9 (Thursday, January 14, 1999)]
    [Rules and Regulations]
    [Pages 2428-2429]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 99-809]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 98-NM-108-AD; Amendment 39-10802; AD 98-20-35]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Israel Aircraft Industries (IAI), Ltd., 
    Model 1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; correction.
    
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    SUMMARY: This document corrects a typographical error that appeared in 
    airworthiness directive (AD) 98-20-35, that was published in the 
    Federal Register on September 29, 1998 (63 FR 51803). The typographical 
    error resulted in referencing a service bulletin that does not pertain 
    to this AD. This AD is applicable to all IAI, Ltd., Model 1121, 1121A, 
    1121B, 1123, 1124, and 1124A series airplanes. This AD requires 
    repetitive inspections of the trim actuator of the horizontal 
    stabilizer to verify jackscrew integrity and to detect excessive wear 
    of the tie rod, and replacement of the actuator or tie rod, if 
    necessary. This AD also requires accomplishment of the previously 
    optional terminating action.
    
    EFFECTIVE DATE: November 3, 1998.
    
    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: Airworthiness Directive (AD) 98-20-35, 
    amendment 39-10802, applicable to all IAI, Ltd., Model 1121, 1121A, 
    1121B, 1123, 1124, and 1124A series airplanes, was published in the 
    Federal Register on September 29, 1998 (63 FR 51803). That AD requires 
    repetitive inspections of the trim actuator of the horizontal 
    stabilizer to verify jackscrew integrity and to detect excessive wear 
    of the tie rod, and replacement of the actuator or tie rod, if 
    necessary. That AD also requires accomplishment of the previously 
    optional terminating action.
        As published, AD 98-20-35 contained an erroneous reference to a 
    service bulletin that was approved previously by the Director of the 
    Federal Register as of April 10, 1998 (63 FR 11106, March 6, 1998), for 
    incorporation by reference in AD 98-05-09, amendment 39-10370. 
    Paragraph (f) of AD 98-20-35 and paragraph (g) of AD 98-05-09 
    incorrectly reference Westwind Service Bulletin SB 1124-27-046, 
    Revision 1, dated May 28, 1997. The correct service bulletin is 
    Westwind Service Bulletin SB 1123-27-046, Revision 1, dated May 28, 
    1997.
        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 November 3, 1998.
    
    
    Sec. 39.13  [Corrected]
    
        On page 51804, in the third column, paragraph (f) of AD 98-20-35 is 
    corrected to read as follows:
    * * * * *
        (f) The actions shall be done in accordance with the following 
    Westwind and Commodore Jet service bulletins, as applicable, which 
    contain the specified effective pages:
    
    [[Page 2429]]
    
    
    
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                                                  Page number     Revision level
       Service bulletin referenced and date      shown on page     shown on page           Date shown on page
    ----------------------------------------------------------------------------------------------------------------
    Westwind SB 1124-27-133, August 14, 1996..  1-6...........  Original..........  August 14, 1996.
    Westwind SB 1124-27-133...................  1-4...........  1.................  May 28, 1997.
    Revision 1, May 28, 1997..................  5, 6..........  Original..........  August 14, 1996.
    Westwind SB 1123-27-046, August 14, 1996..  1-6...........  Original..........  August 14, 1996.
    Westwind SB 1123-27-046...................  1-4...........  1.................  May 28, 1997.
    Revision 1, May 28, 1997..................  5, 6..........  Original..........  August 14, 1996.
    Westwind SB 1124-27-136, September 1, 1997  1-3...........  Original..........  September 1, 1997.
    Westwind SB 1123-27-047, September 1, 1997  1-3...........  Original..........  September 1, 1997.
    Commodore Jet SB 1121-27-025, December 22,  1-3...........  Original..........  December 22, 1997.
     1997.
    Commodore Jet SB 1121-27-023, August 14,    1-6...........  Original..........  August 14, 1996.
     1996.
    Commodore Jet SB 1121-27-023..............  1-4...........  1.................  May 28, 1997.
    Revision 1, May 28, 1997..................  5, 6..........  Original..........  August 14, 1996.
    ----------------------------------------------------------------------------------------------------------------
    
        The incorporation by reference was approved previously by the 
    Director of the Federal Register as of April 10, 1998 (63 FR 11106, 
    March 6, 1998). Copies may be obtained from Galaxy Aerospace 
    Corporation, One Galaxy Way, Fort Worth Alliance Airport, Fort 
    Worth, Texas 76177. 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.
    * * * * *
        Issued in Renton, Washington, on January 7, 1999.
    John J. Hickey,
    Acting Manager, Transport Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 99-809 Filed 1-13-99; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
11/3/1998
Published:
01/14/1999
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
99-809
Dates:
November 3, 1998.
Pages:
2428-2429 (2 pages)
Docket Numbers:
Docket No. 98-NM-108-AD, Amendment 39-10802, AD 98-20-35
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
99-809.pdf
CFR: (1)
14 CFR 39.13