[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]
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