[Federal Register: January 3, 2005 (Volume 70, Number 1)]
[Rules and Regulations]
[Page 10-11]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr03ja05-4]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NM-409-AD; Amendment 39-13853; AD 2004-22-25]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 767-200, -300, and -300F
Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document corrects an error that appeared in airworthiness
directive (AD) 2004-22-25, which was published in the Federal Register
on November 9, 2004 (69 FR 64839). The error resulted in the incorrect
reference to cable spacers. This AD is applicable to certain Boeing
Model 767-200, -300, and -300F series airplanes. This AD requires a
one-time inspection for discrepancies of all wire bundles, including
certain power feeder cables, of the electrical system in the forward
cargo compartment ceiling at certain stations; and corrective actions
if necessary.
DATES: Effective December 14, 2004.
FOR FURTHER INFORMATION CONTACT: Elias Natsiopoulos, Aerospace
Engineer, Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-
4056; telephone (425) 917-6478; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2004-22-25,
amendment 39-13853, applicable to certain Boeing Model 767-200, -300,
and -300F series airplanes, was published in the Federal Register on
November 9, 2004 (69 FR 64839). That AD requires a one-time inspection
for discrepancies of all wire bundles, including certain power feeder
cables, of the electrical system in the forward cargo compartment
ceiling at certain stations; and corrective actions if necessary.
As published, the third cell of paragraph (a)(2)(ii) of Table 1 of
AD 2004-22-25 states, ``* * * install sleeving, lacing tape, cable
spacers, and straps,'' in accordance with Boeing Alert Service Bulletin
767-24A0128, Revision 3, dated June 24, 2004 (cited as the appropriate
service information for accomplishing the required actions). We
incorrectly specified ``cable spacers'' as part of the installation
requirements if the clearance between the power feeder cables and cargo
liner standoffs is less
[[Page 11]]
than 0.13 inch. The service bulletin does not describe procedures for
installation of cable spacers in that area. Therefore, we have
determined that ``cable spacers'' should be removed from the
requirements of paragraph (a)(2)(ii) of Table 1 of that AD.
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 December 14, 2004.
Sec. 39.13 [Corrected]
0
On page 64842, in Table 1, paragraph (a)(2)(ii) of AD 2004-22-25 is
corrected to read as follows:
* * * * *
Table 1.--Clearance Between Wire Bundles and Cargo Liner Standoffs
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If the clearance between the-- Is-- Then--
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(i) Wire bundles and cargo liner 0.25 inch or more.............................. No further action is
standoffs. required by this AD.
Between 0.13 and 0.25 inch..................... Install sleeving and
lacing tape.
Less than 0.13 inch............................ Install sleeving, lacing
tape, cable spacers, and
straps.
(ii) Power feeder cables and cargo 0.13 inch or more.............................. No further action is
liner standoffs. required by this AD.
less than 0.13 inch............................ Install sleeving, lacing
tape, and straps.
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* * * * *
Issued in Renton, Washington, on December 22, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-28666 Filed 12-30-04; 8:45 am]
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