[Federal Register Volume 67, Number 152 (Wednesday, August 7, 2002)]
[Rules and Regulations]
[Pages 51069-51070]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-19880]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NM-233-AD; Amendment 39-12785; AD 2002-12-13]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 727 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document corrects an inadvertent error that appeared in
airworthiness directive (AD) 2002-12-13 that was published in the
Federal Register on June 26, 2002 (67 FR 42985). The inadvertent error
resulted in reference to an incorrect address for service information.
This AD is applicable to all Boeing Model 727 series airplanes. This AD
requires a review of maintenance records or a one-time test to
determine if elevator hinge support ribs on the trailing edge of the
horizontal stabilizer are made from a certain material, and follow-on
repetitive inspections for corrosion or cracking of the elevator hinge
support ribs, if necessary. For airplanes with the affected ribs
installed, this AD eventually requires replacement of all affected ribs
with new, improved ribs.
DATES: Effective July 31, 2002.
FOR FURTHER INFORMATION CONTACT: Technical Information: Duong Tran,
Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-
4056; telephone (425) 227-2773; fax (425) 227-1181.
Other Information: Judy Golder, Airworthiness Directive Technical
Editor/Writer; telephone (425) 687-4241, fax (425) 227-1232. Questions
or comments may also be sent via the Internet using the following
address: [email protected]. Questions or comments sent via the
Internet as attached electronic files must be formatted in Microsoft
Word 97 for Windows or ASCII text.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2002-12-13,
amendment 39-12785, applicable to all Boeing Model 727 series
airplanes, was published in the Federal Register on June 26, 2002 (67
FR 42985). That AD requires a review of maintenance records or a one-
time test to determine if elevator hinge support ribs on the trailing
edge of the horizontal stabilizer are made from a certain material, and
follow-on repetitive inspections for corrosion or cracking of the
elevator hinge support ribs, if necessary. For airplanes with the
affected ribs installed, this AD eventually requires replacement of all
affected ribs with new, improved ribs.
As published, paragraph (h) of that AD contained an incorrect
address for obtaining copies of service information. Paragraph (h) of
that AD identifies Airbus Industrie, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France, as the appropriate address for obtaining
copies of service information. However, the correct address is Boeing
[[Page 51070]]
Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124-
2207.
Since no other part of the regulatory information has been changed,
the final rule is not being republished in the Federal Register.
The effective date of this AD remains July 31, 2002.
Sec. 39.13 [Corrected]
On page 42989 of AD 2002-12-13, in the third column of paragraph
(h) on the fourth line following the table, correct the sentence,
``Copies may be obtained from Airbus Industrie, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France,'' to read ``Copies may be
obtained from Boeing Commercial Airplane Group, P.O. Box 3707, Seattle,
Washington 98124-2207.''
Issued in Renton, Washington, on July 29, 2002.
Vi L. Lipski,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 02-19880 Filed 8-6-02; 8:45 am]
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