98-22699. Airworthiness Directives; Sikorsky Aircraft Corporation Model S- 61A, D, E, L, N, NM, R, and V Helicopters; Correction  

  • [Federal Register Volume 63, Number 164 (Tuesday, August 25, 1998)]
    [Rules and Regulations]
    [Page 45170]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 98-22699]
    
    
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    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 97-SW-18-AD; Amendment 39-10126; AD 97-19-06]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Sikorsky Aircraft Corporation Model S-
    61A, D, E, L, N, NM, R, and V Helicopters; Correction
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule; correction.
    
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    SUMMARY: This document corrects the amendment number in airworthiness 
    directive (AD) 97-19-06 that was incorrectly published in the Federal 
    Register on September 19, 1997 (62 FR 49132). This AD is applicable to 
    Sikorsky Aircraft Corporation Model S-61A, D, E, L, N, NM, R, and V 
    helicopters and requires, before further flight, inspecting certain 
    main rotor blades to determine the anodizing date for certain pocket 
    assemblies installed on the blade, and if a blade has a pocket assembly 
    that was anodized by Poly-Metal Company during the period of October 1, 
    1996, through December 31, 1996, replacing it with an airworthy blade.
    
    DATES: Effective October 6, 1997.
        The incorporation by reference of certain publications listed in 
    the regulations was previously approved by the Director of the Federal 
    Register as of October 6, 1997 (62 FR 49132, September 19, 1997).
    
    FOR FURTHER INFORMATION CONTACT: Mr. Shep Blackman, Aerospace Engineer, 
    FAA, Rotorcraft Directorate, Rotorcraft Standards Staff, 2601 Meacham 
    Blvd., Fort Worth, Texas 76137, telephone (817) 222-5296, fax (817) 
    222-5961.
    
    SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 97-19-06, 
    amendment 39-10126, applicable to Sikorsky Aircraft Corporation Model 
    S-61A, D, E, L, N, NM, R, and V helicopters was published in the 
    Federal Register on September 19, 1997 (62 FR 49132). That AD requires, 
    before further flight, inspecting certain main rotor blades to 
    determine the anodizing date for certain pocket assemblies installed on 
    the blade, and if a blade has a pocket assembly that was anodized by 
    Poly-Metal Company during the period of October 1, 1996, through 
    December 31, 1996, replacing it with an airworthy blade.
        As published, the amendment number given throughout the AD is 
    incorrect.
        Since no other part of the regulatory information has been changed, 
    the final rule is not being republished.
        The effective date of the AD remains October 6, 1997.
        In rule FR Doc. 97-24075 published on September 19, 1997 (62 FR 
    49132), make the following corrections:
    
    
    Sec. 39.13  [Corrected]
    
        (1) On page 49132, in the first column, correct ``Amendment 39-
    10026'' to read ``Amendment 39-10126.''
        (2) On page 49133, in the first column, paragraph 2., correct the 
    two recitations of ``Amendment 39-10026'' to read ``Amendment 39-
    10126''.
    
        Issued in Fort Worth, Texas, on August 18, 1998.
    Henry A. Armstrong,
    Manager, Rotorcraft Directorate, Aircraft Certification Service.
    [FR Doc. 98-22699 Filed 8-24-98; 8:45 am]
    BILLING CODE 4910-13-P
    
    
    

Document Information

Effective Date:
10/6/1997
Published:
08/25/1998
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
98-22699
Dates:
Effective October 6, 1997.
Pages:
45170-45170 (1 pages)
Docket Numbers:
Docket No. 97-SW-18-AD, Amendment 39-10126, AD 97-19-06
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
98-22699.pdf
CFR: (1)
14 CFR 39.13