Airworthiness Directives; Airbus Model A300-600 Series Airplanes; Correction

[Federal Register Volume 62, Number 164 (Monday, August 25, 1997)]
[Rules and Regulations]
[Page 44888]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-22488]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 95-NM-228-AD; Amendment 39-10097; AD 97-16-06]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A300-600 Series Airplanes; 
Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document corrects the compliance time information in 
airworthiness directive (AD) 97-16-06 that was published in the Federal 
Register on August 1, 1997 (62 FR 41257). A portion of the specified 
compliance times was inadvertently omitted in the AD. This AD is 
applicable to all Airbus Model A300-600 series airplanes, and requires 
an inspection to detect cracks of certain attachment holes; and 
installation of a new fastener and follow-on inspections or repair, if 
necessary.

DATES: Effective September 5, 1997.
    The incorporation by reference of certain publications listed in 
the regulations was previously approved by the Director of the Federal 
Register as of September 5, 1997 (62 FR 41257, August 1, 1997).

FOR FURTHER INFORMATION CONTACT: Tim Backman, Aerospace Engineer, 
Standardization Branch, ANM-113, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2797; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 97-16-06, 
amendment 39-10097, applicable to all Airbus Model A300-600 series 
airplanes, was published in the Federal Register on August 1, 1997 (62 
FR 41257). That AD requires an inspection to detect cracks of certain 
attachment holes; and installation of a new fastener and follow-on 
inspections or repair, if necessary.
    As published, the phrase ``whichever occurs later'' after the 
compliance times specified in paragraphs (a)(1) and (a)(2) of the AD 
was inadvertently omitted.
    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 September 5, 1997.
    In rule FR Doc. 97-20131 published on August 1, 1997 (62 FR 41257), 
make the following corrections:


Sec. 39.13  [Corrected]

    1. On page 41258, in the third column, paragraph (a)(1) of AD 97-
16-06 is corrected to read as follows:
* * * * *
    (a) * * *
    (1) For airplanes on which Airbus Modification 10454 (reference 
Airbus Service Bulletin A300-57-6050) has not been installed: Inspect 
prior to the accumulation of 13,800 total landings, or within 750 
landings after the effective date of this AD, whichever occurs later.
* * * * *
    2. On page 41258, in the third column, paragraph (a)(2) of AD 97-
16-06 is corrected to read as follows:
* * * * *
    (a) * * *
    (2) For airplanes on which Airbus Modification 10454 (reference 
Airbus Service Bulletin A300-57-6050) or Airbus Modification 10155 has 
been installed: Inspect prior to the accumulation of 18,700 total 
landings, or within 750 landings after the effective date of this AD, 
whichever occurs later.
* * * * *

    Issued in Renton, Washington, on August 19, 1997.
S. R. Miller,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 97-22488 Filed 8-22-97; 8:45 am]
BILLING CODE 4910-13-U

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